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Patent 2460996 Summary

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(12) Patent Application: (11) CA 2460996
(54) English Title: PROCESS AND APPARATUS FOR SILICON BOAT, SILICON TUBING AND OTHER SILICON BASED MEMBER FABRICATION
(54) French Title: PROCEDE ET APPAREIL DE FABRICATION DE NACELLE EN SILICIUM, TUYAUX EN SILICIUM ET AUTRE ELEMENT AU SILICIUM
Status: Dead
Bibliographic Data
(51) International Patent Classification (IPC):
  • B29C 43/16 (2006.01)
  • B22F 3/17 (2006.01)
  • B22F 3/20 (2006.01)
  • B22F 3/22 (2006.01)
  • B29C 47/02 (2006.01)
  • C30B 11/00 (2006.01)
  • C30B 23/06 (2006.01)
  • C30B 25/08 (2006.01)
  • C30B 29/34 (2006.01)
  • C30B 35/00 (2006.01)
(72) Inventors :
  • PANDELISEV, KIRIL A. (United States of America)
(73) Owners :
  • PANDELISEV, KIRIL A. (Not Available)
(71) Applicants :
  • PHOENIX SCIENTIFIC CORPORATION (United States of America)
(74) Agent: R. WILLIAM WRAY & ASSOCIATES
(74) Associate agent:
(45) Issued:
(86) PCT Filing Date: 2002-09-19
(87) Open to Public Inspection: 2003-03-27
Availability of licence: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): Yes
(86) PCT Filing Number: PCT/US2002/029516
(87) International Publication Number: WO2003/024876
(85) National Entry: 2004-03-19

(30) Application Priority Data:
Application No. Country/Territory Date
60/323,098 United States of America 2001-09-19
60/336,712 United States of America 2001-12-07

Abstracts

English Abstract




Process, apparatus and application of silicon/silicon alloy/silicon compound
(10) comprising at least one silicon atom boat, silicon/silicon alloy/silicon
compound (10) comprising at least one silicon atom made epitaxial chamber and
various silicon/silicon alloy/silicon compound comprising at least one silicon
atom made tubing and liners is described here. Powder pressing (12-16), plasma
and non plasma powder deposition, slurry deposition and slurry casting,
silicon/silicon alloy casting and directional solidification are among few
methods described here. Silicon/silicon alloy (10) made articles and some of
their applications in the wafer processing industry is also described.


French Abstract

L'invention porte sur un procédé, sur un appareil et sur l'application d'un composite en silicium/alliage de silicium/silicium comprenant au moins une nacelle formée d'atomes de silicium, un composite en silicium/alliage de silicium/silicium comprenant au moins une chambre épitaxiale formée d'atomes de silicium et divers composites en silicium/alliage de silicium/silicium comprenant au moins un ensemble tubulaire et des revêtements formés d'atomes de silicium. L'invention porte également sur des procédés de compression des poudres, de dépôt des poudres par plasma et sans plasma, de dépôt et coulée de suspensions, de coulée de silicium/alliage de silicium et de solidification directionnelle, ainsi que sur des articles fabriqués en silicium/alliage de silicium et certaines de leurs applications dans l'industrie de transformation des plaquettes.

Claims

Note: Claims are shown in the official language in which they were submitted.



41

I claim:

1. Apparatus for forging a body comprising an
enclosure having a mold, forging material provided in the
mold, and a forged product formed from the forging material
in the mold at a predetermined temperature.

2. The apparatus of claim 1, wherein the enclosure is
a heated enclosure having a chamber for housing the mold, a
chamber heater, a ram heater and an anvil heater in the
enclosure, a multiport coupled to the chamber for supplying
material to the chamber, and a line coupled to the chamber
for removing exhaust gases.

3. The apparatus of claim 2, wherein the multiport is
an inlet/outlet multiport.

4. The apparatus of claim 2, wherein the line is a
vacuum/vent line.

5. The apparatus of claim 2, wherein the forged
product is a monocrystal, polycrystal or amorphous body.

6. The apparatus of claim 1, wherein the predetermined
temperature ranges between about 400°C and about a melting
point of the body.

7. The apparatus of claim 1, wherein the predetermined
temperature is not greater than about 400°C.

8. The apparatus of claim 1, wherein the predetermined
temperature is not greater than a melting point of a lowest
melting phase in the body.

9. The apparatus of claim 5, wherein the body is
forged at a temperature of about 400°C.

10. The apparatus of claim 5, wherein the body is
forged at a temperature of about 600°C.

11. The apparatus of claim 5, wherein the body is
forged at a temperature of about 800°C.

12. The apparatus of claim 5, wherein the body is of
polycrystalline material.

13. The apparatus of claim 1, wherein the body is of
amorphous material.



42

14. The apparatus of claim 5, wherein the body
comprises single crystalline, polycrystalline and amorphous
portions.

15. The apparatus of claim 2, wherein the product is
formed in an atmosphere having a predetermined pressure in
the chamber.

16. The apparatus of claim 15, wherein the atmosphere
is selected from a group consisting of vacuum, reduced
pressure, inert atmosphere, reactive atmosphere, and
combinations thereof.

17. The apparatus of claim 15, wherein the atmosphere
is reactive atmosphere

18. The apparatus of claim 17, wherein the reactive
atmosphere is selected from a group consisting of plasma,
reactive gases, solids, and combinations thereof.

19. The apparatus of claim 15, wherein the body is
formed by purification of the forging material.

20. The apparatus of claim 1, wherein the forging
material is a powder.

21. The apparatus of claim 20, wherein the powder
comprises constituents selected from a group consisting of
silicon, silicon compound comprising at least one atom of
silicon, silicon and germanium, Si x Ge1-x solid solution,
silicon and silicon carbide Si x(SiC)1-x, silicon and silicon
dioxide Si x(SiO2)1-x, silicon and ceramic, silicon and any
oxide Si x(Oxide)1-x, silicon and any metal Si x M1-x, silicon and
any alloy Si x A1-x, and combinations thereof.

22. The apparatus of claim 21, wherein the anvil has a
temperature during forging between at least about room
temperature and lower than a melting point of at least one of
the constituents forming the crystal R T <= T <= T M.

23. The apparatus of claim 22, wherein the temperature
is about 400°C <= T <= 800°C.

24. The apparatus of claim 22, wherein the temperature
is about 200°C <= T <= 1000°C.



43

25. The apparatus of claim 22, wherein the temperature
is about 200°C <= T <= 1200°C.

26. The apparatus of claim 22, wherein the temperature
is not greater than about 200°C.

27. The apparatus of claim 26, wherein the temperature
is not lesser than about 1200°C.

28. The apparatus of any of the preceding claims,
wherein the body is forged in vacuum, reduced pressure or
inert atmosphere having desired pressure.

29. The apparatus of any of the preceding claims,
wherein the body is forged in vacuum, reduced pressure or
reactive atmosphere having desired pressure.

30. The apparatus of claim 29, wherein the reactive
atmosphere is selected from a group consisting of plasma,
reactive gases, solids and combinations thereof and wherein a
process of purification is administered.

31. The apparatus of any of the preceding claims,
wherein the powder forged is silicon powder or shot having
various grain sizes from sub-micron to large shot sizes of
several millimeters or larger or the powder forged is silicon
compound comprising at least one atom of silicon.

32. The apparatus of claim 31, wherein the powder
forged is silicon powder and germanium powder or shot having
various grain sizes from sub-micron to rather large shot
sizes of several millimeters or larger.

33. The apparatus of claim 31, wherein the powder
forged is silicon powder and Si x Ge1-x (0 <= x <=1) powder or
shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.

34. The apparatus of claim 31, wherein the powder
forged is silicon powder and silicon carbide, Si x(SiC)1-x (0 <=
x <=1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.

35. The apparatus of claim 31, wherein the powder


44

forged is silicon powder and silicon dioxide, Si x(SiO2)1-x (0 <=
x <=1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.

36. The apparatus of claim 31, wherein the powder
forged is silicon powder and metal, Si x M1-x (0 <= x <=1) powder
or shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.

37. The apparatus of claim 31, wherein the powder
forged is silicon powder and Si x(Alloy)1-x (0 <= x <=1) powder
or shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.

38. The apparatus of claim 31, wherein the powder
forged is silicon powder and/or metal and/or ceramic and/or
alloy and/or oxide and/or any suitable additive powder or
shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.

39. The apparatus of claim 2, wherein the forging
apparatus comprises an anvil, a ram and a mold for forging
the crystal.

40. The apparatus of claim 39, wherein each part in the
enclosure is independently heated.

41. The apparatus of claim 39, wherein the enclosure is
heated from all sides.

42. The apparatus of claim 39, wherein the enclosure is
enclosed fully or partially in a vacuum, reduced pressure or
desired pressure chamber, and wherein the chamber is filled
with inert gas, reactive gas or plasma gas.

43. An extrusion apparatus for extruding a body,
wherein the body has a temperature between 400°C and near
melting point.

44. The apparatus of claim 43, wherein the temperature
is less than 400°C or from 400°C to a melting point of a
lowest melting phase in the body being extruded.

45. The apparats of claim 43, further comprising an


45
extrusion chamber for holding powder and forming an extruded
body, further comprising a refill hopper for delivering
material to be extruded from a material delivery assembly.
46. The apparatus of claim 45, further comprising a
piston and a tube shaper for forcing the extruded body
through the tube shaper.
47. The apparatus of claim 46, further comprising a
surrounding chamber having a cooled wall and an internal
heater, the chamber being coupled to a gas inlet/outlet
multiport and a vacuum/vent line.
48. The apparatus of any of the preceding claims 43 to
47, wherein the body is extruded at a temperature of about
400°C.
49. The apparatus of any of the preceding claims 43 to
48, wherein the body is extruded at a temperature of about
600°C.
50. The apparatus of any of the preceding claims 43 to
49, wherein the body is extruded at a temperature of about
800°C.
51. The apparatus of any of the preceding claims 43 to
50, wherein the extruded body is monocrystal or
polycrystalline material having at least one atom of silicon.
52. The apparatus of any of the preceding claims 43 to
51, wherein the extruded body is amorphous material having at
least one atom of silicon.
53. The apparatus of any of the preceding claims 43 to
52, wherein the extruded body comprises single crystalline
portion and polycrystalline portion and amorphous portion.
54. The apparatus of any of the preceding claims 43 to
53, wherein the extruding is in vacuum, reduced pressure or
inert atmosphere having desired pressure.
55. The apparatus of any of the preceding claims 43 to
54, wherein the extruding is in vacuum, reduced pressure or
reactive atmosphere having desired pressure.
56. The apparatus of any of the preceding claims 43 to


46
55, wherein the reactive atmosphere is plasma, reactive gases
or solid and a process of purification is administered.
57. The apparatus of any of the preceding claims 43 to
56, wherein the extruding powder is selected from a group
consisting of silicon, silicon compound comprising at least
one atom of silicon, silicon and germanium, Si x Ge1-x solid
solution, silicon and silicon carbide Si x(SiC)1-x, silicon and
silicon dioxide Si x(SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x(Oxide)1-x, silicon and any metal Si x M1-x,
silicon and any alloy Si x A1-x, any combination between
themselves at temperature equal or greater than room
temperature and lower than the melting point of one or more
constituents of the pressed body R T <= T <= T M.
58. The apparatus of any of the preceding claims 43 to
57, wherein the temperature is about 400°C <= T <=
800°C.
59. The apparatus of any of the preceding claims 43 to
58, wherein the temperature is about 200°C <= T <=
1000°C.
60. The apparatus of any of the preceding claims 43 to
59, wherein the temperature is about 200°C <= T <=
1200°C.
61. The apparatus of any of the preceding claims 43 to
60, wherein the temperature is smaller than 200°C or greater
than 1200°C.
62. The apparatus of any of the preceding claims 43 to
61, wherein the extruding is in vacuum, reduced pressure or
inert atmosphere having desired pressure.
63. The apparatus of any of the preceding claims 43 to
62, wherein the extruding is in vacuum, reduced pressure or
reactive atmosphere having desired pressure.
64. The apparatus of any of the preceding claims 43 to
63, wherein the reactive atmosphere is plasma, reactive gases
or solid and a process of purification is administered.
65. The apparatus of any of the preceding claims 43 to
64, wherein the powder is silicon powder or shot having
various grain sizes from sub-micron to rather large shot
sizes of several millimeters or larger or silicon compound


47
comprising at least one atom of silicon.
66. The apparatus of any of the preceding claims 43 to
65, wherein the powder is silicon powder and germanium powder
or shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.
67. The apparatus of any of the preceding claims 43 to
66, wherein the powder is silicon powder and Si x Ge1-x (0 <= x
<=1) powder or shot having various grain sizes from sub-micron
to rather large shot sizes of several millimeters or larger.
68. The apparatus of any of the preceding claims 43 to
67, wherein the powder is silicon powder and silicon carbide,
Si x (SiC)1-x (0 <= x <= 1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
69. The apparatus of any of the preceding claims 43 to
68, wherein the powder is silicon powder and silicon dioxide,
Si x (SiO2)1-x (0 <= x <= 1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
70. The apparatus of any of the preceding claims 43 to
69, wherein the powder is silicon powder and metal, Si x M1-x (0
<= x <= 1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
71. The apparatus of any of the preceding claims 43 to
70, wherein the powder is silicon powder and Si x (Alloy)1-x (0
<= x <= 1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
72. The apparatus of any of the preceding claims 43 to
71, wherein the powder is silicon powder and/or metal and/or
ceramic and/or alloy and or oxide and/or any suitable
additive powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.


48
73. The apparatus of any of the preceding claims 43 to
72, wherein the powder forged is silicon powder and/or metal
and/or ceramic and/or alloy and/or oxide and/or any suitable
additive powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
74. The apparatus of any of the preceding claims 43 to
73, wherein the forging apparatus comprises an anvil, a ram
and a mold for forging the crystal.
75. The apparatus of any of the preceding claims 43 to
74, wherein each part in the enclosure is independently
heated.
76. The apparatus of any of the preceding claims 43 to
75, wherein the enclosure is heated from all sides.
77. The apparatus of any of the preceding claims 43 to
76, wherein the enclosure is enclosed fully or partially in a
vacuum, reduced pressure or desired pressure chamber, and
wherein the chamber is filled with inert gas, reactive gas or
plasma gas.
78. Apparatus for plasma deposition comprising at least
one substrate, material for deposition on the substrate,
plasma generators or sources for the material, and a gas and
a powder input system, wherein the substrate is a hollow tube
or a solid body.
79. The apparatus of claim 78, wherein the substrate is
one or a plurality of substrates and wherein plasma heated
softened particles strike and stick to the substrate and form
layers as the one or the plurality of substrates are rotated
and/or translated.
80. The apparatus of claim 79, further comprising a
chamber surrounding the deposition, wherein the substrate
and/or the chamber are heated.
81. The apparatus of any of preceding claims 78 to 80,
further comprising gas inlet/outlet multiport and vacuum/vent
line coupled to the chamber.


49
82. The apparatus of any of preceding claims 78 to 81,
further comprising one or more plasma generators or plasma
sources, gas input system, powder input system, vacuum
chamber, with or without one or more chamber heating
elements, and the substrate with or without heating elements.
83. The apparatus of any of preceding claims 78 to 82,
further comprising one or more deposition ports in the
chamber.
84. The apparatus of any of preceding claims 78 to 83,
wherein substrate has rotation and/or translation mechanisms.
85. The apparatus of any of preceding claims 78 to 84,
wherein the chamber has rotation and/or translation
mechanisms.
86. The apparatus of any of preceding claims 78 to 85,
wherein the plasma assisted deposition of powder comprises
powder selected from a group consisting of silicon, silicon
compound comprising at least one atom of silicon, silicon and
germanium, Si x Ge1-x solid solution, silicon and Silicon
Carbide Si x(SiC)1-x, Silicon and silicon dioxide Si x(SiO2)1-x,
silicon and any ceramic, silicon and any oxide Si x(Oxide)1-x,
silicon and any metal Si x M1-x, Silicon and any alloy Si x A1-x,
any combination between themselves at temperature equal or
greater than room temperature and lower than the melting
point of one or more constituents of the deposited body R T <=
T <= T M.
87. The apparatus of any of preceding claims 78 to 86,
wherein~ the powder is deposited under vacuum, reduced
pressure, reactive atmosphere, inert gas, plasma, and any
combinations thereof.
88. The apparatus of any of preceding claims 78 to 87,
wherein the deposition is in inert atmosphere having desired
pressure.
89. The apparatus of any of preceding claims 78 to 88,
wherein the reactive atmosphere is plasma, reactive gases or
solid and a process of purification is administered.


50
90. The apparatus of any of preceding claims 78 to 89,
wherein a temperature in the chamber is between temperature
equal to or greater than room temperature and lower than the
melting point of one or more constituents of the deposited
body R T <= T <= T M.
91. The apparatus of any of preceding claims 78 to 90,
wherein the temperature in the chamber is about 400°C <= T
<=
800°C.
92. The apparatus of any of preceding claims 78 to 90,
wherein the temperature in the chamber is about 200°C <= T
<=
1000°C.
93. The apparatus of any of preceding claims 78 to 90,
wherein the temperature in the chamber is about 200°C <= T
<=
1200°C.
94. The apparatus of any of preceding claims 78 to 90,
wherein the temperature is smaller than 200°C or greater than
1200°C.
95. The apparatus of any of preceding claims 78 to 90,
wherein the temperature of the substrate is between
temperature equal to or greater than room temperature and
lower than the melting point of one or more constituents of
the deposited body R T <= T <= T M.
96. The apparatus of any of preceding claims 78 to 95,
wherein the temperature of the substrate is about 400°C <= T
<=
800°C.
97. The apparatus of any of preceding claims 78 to 95,
wherein the temperature of the substrate is about 200°C <= T
<=
1000°C.
98. The apparatus of any of preceding claims 78 to 95,
wherein the temperature of the substrate is about 200°C <= T
<=
1200°C.
99. The apparatus of any of preceding claims 78 to 95,
wherein the temperature is smaller than 200°C or greater than
1200°C.
100. Deposition apparatus for spraying of powder, powder


51
and organic and/or inorganic base material, powder and
gaseous material comprising a substrate, plurality of
sprayers positioned to spray at least one portion of one
side, and heating elements for heating the substrate at least
from one side.
101. The apparatus of claim 100, wherein the substrate
is rotated, and the substrate or slurry delivery tubes
translate the sprayer, and wherein spray heated powder is
heated and softened by heaters.
102. The apparatus of claim 101, wherein the powder is
selected from a group consisting of silicon, silicon compound
comprising at least one atom of silicon, silicon and
germanium, Si x Ge1-x solid solution, silicon and Silicon
Carbide Si x(SiC)1-x, silicon and silicon dioxide Si x(SiO2)1-x.
silicon and any ceramic, silicon and any oxide Si x(Oxide)1-x,
silicon and any metal Si x M1-x, silicon and any alloy Si x A1-x,
any combination between themselves at temperature equal to or
greater than room temperature and lower than the melting
point of one or more constituents of the deposited body R T <=
T <= T M.
103. The apparatus of any of preceding claims 100 to
102, wherein the substrate is tubular having any cross-
section, planar, flat, curved or have any desired shape or
form suitable for a particular application.
104. The apparatus of any of preceding claims 100 to
103, wherein the substrate comprises at least one element and
wherein the substrate is rotated and translated.
105. The apparatus of any of preceding claims 100 to
104, wherein the substrate is heated from inside and/or
outside, and wherein each substrate is independently heated.
106. The apparatus of any of preceding claims 100 to
105, wherein the sprayers are one or more sprayers and they
are oscillated, rotated and translated in relation to
themselves and to the substrate on which the deposition takes
place, and wherein each sprayer delivers same or different


52
compounds for spraying of a premixed compound or provides for
compound formation on a surface of the substrate.
107. The apparatus of any of preceding claims 100 to
106, wherein the apparatus is enclosed in vacuum, reduced
pressure or any process suitable chamber that has vacuum and
vent valves and gas delivery system.
108. The apparatus of any of preceding claims 100 to
107, wherein the deposition process is under vacuum, reduced
pressure, reactive gas, inert gas, plasma, and any
combinations thereof.
109. The apparatus of any of preceding claims 100 to
108, wherein the process is in inert atmosphere having
desired pressure.
110. The apparatus of any of preceding claims 100 to
109, wherein the reactive atmosphere is plasma, reactive
gases or solid, and wherein a process of purification is
administered.
111. The apparatus of any of preceding claims 100 to
110, wherein a temperature in the chamber and a substrate
temperature are between temperature equal to or greater than
room temperature and lower than the melting point of one or
more constituents of the deposited body R T <= T <= T M.
112. The apparatus of any of preceding claims 100 to
111, wherein the temperature in the chamber is about 400°C <=
T <= 800°C.
113. The apparatus of any of preceding claims 100 to
111, wherein temperature in the chamber is about 200°C <= T
<=
1000°C.
114. The apparatus of any of preceding claims 100 to
111, wherein temperature in the chamber is about 200°C <= T
<=
1200°C.
115. The apparatus of any of preceding claims 100 to
111, wherein temperature in the chamber is smaller than 200°C
or greater than 1200°C.
116. The apparatus of any of preceding claims 100 to


53
111, wherein temperature of the substrate is between
temperature equal to or greater than room temperature and
lower than the melting point of one or more constituents of
the deposited body R T <= T <= T M.
117. The apparatus of any of preceding claims 100 to
116, wherein temperature of the substrate is about 400°C <= T
<= 800°C.
118. The apparatus of any of preceding claims 100 to
116, wherein temperature of the substrate is about 200°C <= T
<= 1000°C.
119. The apparatus of any of preceding claims 100 to
116, wherein temperature of the substrate is about 200°C <= T
<= 1200°C.
120. The apparatus of any of preceding claims 100 to
116, wherein temperature of the substrate is smaller than
200°C or greater than 1200°C.
121. Apparatus for making tubular members having any
cross section, any length and any desired shape or form
comprising a body within or without a mold, a heater covering
part of the mold and a chamber fully or partially surrounding
at least one member and heating elements.
122. The apparatus of claim 121, wherein the chamber has
a gas inlet/outlet multiport and a vacuum/vent line.
123. The apparatus of claim 122, further comprising a
silicon or a silicon containing compound preform placed in
the heated chamber.
124. The apparatus of claim 123, wherein the preform is
rotated and a heated ring is translated along the preform for
sintering or melting the material and forming a solid
product.
125. The apparatus of any of preceding claims 121 to
124, wherein the chamber is a vacuum, low pressure or
pressure chamber.
126. The apparatus of any of preceding claims 121 to
125, wherein the chamber surrounding the member and the


54
heating elements is absent.
127. The apparatus of any of preceding claims 121 to
126, wherein the member is rotated and/or translated.
128. The apparatus of any of preceding claims 121 to
127, wherein the member is heated from inside and/or outside.
129. The apparatus of any of preceding claims 121 to
128, wherein the member is heated from outside by chamber
heaters and a gone heater for directional or non-directional
processing.
130. The apparatus of any of preceding claims 121 to
129, wherein the chamber has vacuum and/or vent valves.
131. The apparatus of any of preceding claims 121 to
130, wherein the chamber has a gas inlet/outlet multiport.
132. The apparatus of any of preceding claims 121 to
131, wherein the chamber has one or more plasma source
attached.
133. The apparatus of any of preceding claims 121 to
132, wherein the material processed is solid material,
powder, powder and organic or inorganic base material, powder
and gaseous material.
134. The apparatus of any of preceding claims 121 to
133, wherein the powder is selected from a group consisting
of silicon, silicon compound comprising at least one atom of
silicon, silicon and germanium, Si x Ge1-x solid solution,
silicon and Silicon Carbide Si x(SiC)1-x, Silicon and silicon
dioxide Si x(SiO2)1-x, silicon and any ceramic, silicon and any
oxide Si x(Oxide)1-x, silicon and any metal Si x M1-x, Silicon and
any alloy Si x A1-x, any combination between themselves at
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body R T <= T <= T M.
135. The apparatus of any of preceding claims 121 to
134, further comprising at least one substrate, plurality of
sprayers positioned to spray at least one portion of one
side, and heating elements for heating the substrate at least


55


from one side.
136. The apparatus of any of preceding claims 121 to
135, wherein the substrate is tubular having any cross-
section, planar or have any desired shape or form suitable
for a particular application.
137. The apparatus of any of preceding claims 121 to
136, wherein processing of the material is under vacuum,
reduced pressure, reactive gas, inert gas, plasma, and any
combinations thereof.
138. The apparatus of any of preceding claims 121 to
137, wherein processing of the material is in inert
atmosphere having desired pressure.
139. The apparatus of any of preceding claims 121 to
138, wherein the reactive atmosphere is plasma, reactive
gases or solid, and wherein a process of purification is
administered.
140. The apparatus of any of preceding claims 121 to
139, wherein the process temperature is between temperature
equal to or greater than room temperature and lower than a
melting point of one or more constituents of the deposited
body RT <= T <= TM .
141. The apparatus of any of preceding claims 121 to
140, wherein the process temperature is about 400°C <= T <=
800°C.
142. The apparatus of any of preceding claims 121 to
140, wherein the process temperature is about 200°C ltoreq. T ltoreq.
1000°C.
143. The apparatus of any of preceding claims 121 to
140, wherein the process temperature is about 200°C <= T <=
1200°C. The temperature is smaller than 200°C or greater than
1200°C.
144. The apparatus of any of preceding claims 121 to
143, wherein the temperature of the substrate is between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the




56


deposited body RT <= T <= TM.
145. The apparatus of any of preceding claims 121 to
144, wherein the temperature of the substrate is about 400°C
<= T <= 800°C.
146. The apparatus of any of preceding claims 121 to
144, wherein the temperature of the substrate is about 200°C
<= T <= 1000°C.
147. The apparatus of any of preceding claims 121 to
144, wherein the temperature of the substrate is about 200°C
<= T <= 1200°C.
148. The apparatus of any of preceding claims 121 to
144, wherein the temperature is smaller than 200°C or greater
than 1200°C.
149. The apparatus of any of preceding claims 121 to
148, wherein the member is tubular and has any cross section
such as round, elliptical, rectangular, polygonal or any
other shape.
150. The apparatus of any of preceding claims 121 to
149, wherein the member has uneven thickness pattern over its
entire surface.
151. The apparatus of any of preceding claims 121 to
150, wherein the member has different composition and density
over the entire body.
152. The apparatus of any of preceding claims 121 to
151, wherein the member has different composition and density
over its thickness.
153. The apparatus of any of preceding claims 121 to
152, wherein the composition and material properties is
layered over any dimension of the member such as length,
thickness, width, radius, etc.
154. A preform comprising a horizontal or vertical wafer
processing boat preform comprising a plurality of protrusions
for fabrication of slots for wafers and openings for gas flow
between the wafers to enable deposition of even thickness.
155. The preform of claim 154, wherein the wafer boat




57


preform is made of material selected from a group consisting
of silicon, silicon compound comprising at least one atom of
silicon, silicon and germanium, SixGe1-x solid solution,
silicon and silicon carbide Six(SiC)1-x Silicon and silicon
dioxide Six(SiO2)1-x, silicon and any ceramic, silicon and any
oxide Six(Oxide)1-x, silicon and any metal SixM1-x, Silicon and
any alloy SixA1-x, any combination between themselves, or made
from composite material, wherein 0 <= x <=1.
156. The preform of claim 154, wherein the wafer boat
preform is made by layering one or more of the following
materials: Si, silicon compound comprising at least one
silicon atom, SixGe1-x, SiC, Six (SiC)1-x, Six (SiO2)1-x.
Six (Oxide)1-x, SixM1-x, composite material, and any combination
or order between themselves, wherein 0 <= x <=1.
157. The preform of any of preceding claims 154 to 156,
wherein the wafer boat preform has closed ends at a base and
a top that are half or full discs and end discs having outer
diameters equal or greater than an outer diameter of the
wafer boat.
158. The preform of any of preceding claims 154 to 157,
wherein the end discs are solid discs.
159. The preform of any of preceding claims 154 to 158,
wherein the end discs have certain portions removed.
160. The preform of any of preceding claims 154 to 159,
wherein the wafer boat preform is fabricated from material
selected from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
SixGe1-x solid solution, silicon and Silicon Carbide Six (SiC) 1-
x, Silicon and silicon dioxide Six (SiO2)1-x, . silicon and any
ceramic, silicon and any oxide Six(Oxide)1-x, silicon and any
metal SiXM1-x, Silicon and any alloy SixA1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <=1.
161. The preform of any of preceding claims 154 to 160,
wherein the wafer boat preform is fabricated by heating and




58


melting or sintering a boat fabrication material using a mold
or prefabricated using a mold having desired shape and form,
or transferring it to the mold, solidifying it, cooling it
down at a desired cool-down regime, machining it to a desired
tolerance, and sintering it using process defined parameters.
162. The preform of any of preceding claims 154 to 161,
wherein the boat fabrication material is powder mixed with
organic and/or inorganic compounds for shaping purposes.
163. The preform of any of preceding claims 154 to 161,
wherein the boat fabrication material is solid material.
164. The preform of any of preceding claims 154 to 163,
wherein the melting or sintering is done in a vacuum chamber.
165. The preform of any of preceding claims 154 to 164,
wherein the melting or sintering is done under reduced or
high pressure of inert or reactive gas.
166. The preform of any of preceding claims 154 to 165,
wherein the reactive gas is mixture between atomic or charged
molecular state gas such as plasma gas and a neutral inert or
reactive gas.
167. The preform of any of preceding claims 154 to 167,
wherein the melting or sintering is preceded by one or more
steps of purging and purification.
168. Wafer boat preform comprising boat fabrication
material selected from a group consisting of silicon, silicon
compound comprising at least one silicon atom, silicon and
germanium, SixGe1-x solid solution, silicon and Silicon
Carbide Six (SiC) 1-X, Silicon and silicon dioxide SiX (SiO.,) 1-x.
silicon and any ceramic, silicon and any oxide Six(Oxide)1-x,
silicon and any metal SixM1-x, Silicon and any alloy SixA1-x,
any combination between themselves, or made from composite
material, wherein 0 <= x <=1.
169. The wafer boat preform of claim 168, wherein the
boat is made by pressing the boat fabrication material within
a die having desired shape and form, sintering, cooling it
down at a desired cool-down regime, and machining it to a




59


desired tolerance.
170. The wafer boat preform of claim 169, wherein the
boat fabrication material is powder mixed with organic and/or
inorganic compounds for shaping purposes.
171. The wafer boat preform of claim 169, wherein the
boat fabrication material is solid material.
172. The wafer boat preform of any of preceding claims
168 to 171, wherein the pressing is done in a vacuum chamber.
173. The wafer boat preform of any of preceding claims
168 to 171, wherein the pressing is done under reduced or
high pressure of inert or reactive gas.
174. The wafer boat preform of any of preceding claims
168 to 173, wherein the reactive gas is mixture between
atomic or charged molecular state gas such as plasma gas and
a neutral inert or reactive gas.
175. The wafer boat preform of any of preceding claims
168 to 174, wherein the melting or sintering is preceded by
one or more steps of purging and purification.
176. A process for fabrication of wafer boat preforms
consisting of providing a boat fabrication material selected
from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
SixGe1-x solid solution, silicon and silicon carbide Six(SiC)1-
x, Silicon and silicon dioxide Six(SiO2)1x, silicon and any
ceramic, silicon and any oxide Six(Oxide)1-x, silicon and any
metal SixM1-x, Silicon and any alloy SixA1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <=1.
177. The process of claim 176, further comprising
extruding the fabrication material within a die having
desired shape and form, sintering, cooling it down at a
desired cool-down regime, and machining it to a desired
tolerance.
178. The process of claim 177, wherein the boat
fabrication material is powder.




60


179. The process of claim 178, wherein the boat
fabrication material is powder mixed with organic or
inorganic materials.
180. The process of claim 178, wherein the boat
fabrication material is solid material.
181. The process of any of preceding claims 176 to 180,
wherein the pressing is done in a vacuum chamber.
182. The process of any of preceding claims 176 to 181,
wherein the pressing is done under reduced or high pressure
of inert or reactive gas.
183. The process of any of preceding claims 176 to 182,
wherein the reactive gas is a mixture between atomic or
charged molecular state gas such as plasma gas and a neutral
inert or reactive gas.
184. The process of any of preceding claims 176 to 183,
wherein the melting or sintering is preceded by one or more
steps of purging and purification.
185. Process for fabrication of a member having shape of
tube, plate, rod or any other shape or form consisting of
providing a material selected from a group consisting of
silicon, silicon compound comprising at least one silicon
atom, silicon and germanium, SixGe1-x solid solution, silicon
and silicon carbide Six(SiC)1-x, silicon and silicon dioxide
Six(SiO2)1-x, silicon and any ceramic, silicon and any oxide
SiX (oxide)1-x, silicon and any metal SixM1-x, Silicon and any
alloy SixA1-x, any combination between themselves, or made
from composite material, wherein 0 <= x <=1.
186. The process of claim 185, further comprising
heating and melting or sintering the material made with a
mold having desired shape and form, or transferring the
material to the mold, solidifying it, cooling it down at a
desired cool-down regime, removing the mold, machining it to
the desired tolerance, and sintering again.
187. The process of claim 186, wherein the material is
powder mixed with organic or inorganic materials.




61


188. The process of claim 186, wherein the material is
solid material.
189. The process of any of preceding claims 185 to 188,
wherein the melting is done in a vacuum chamber.
190. The process of any of preceding claims 185 to 188,
wherein the melting or sintering is done under reduced or
high pressure of inert or reactive gas.
191. The process of any of preceding claims 185 to 190,
wherein the reactive gas is a mixture between atomic or
charged molecular state gas such as plasma gas and a neutral
inert or reactive gas.
192. The process of any of preceding claims 185 to 191,
wherein the melting or sintering is preceded by one or more
steps of purging and purification.
193. The process of any of preceding claims 185 to 192,
further comprising fabricating wafer boat members having
shape of tube, plate, rod or any other shape.
194. The process of any of preceding claims 185 to 193,
further comprising cutting the member or solidified boat in
two along medial lines, forming openings in cylindrical
walls, coating and fusing depositing material on top of base
material.
195. The process of any of preceding claims 185 to 194,
further comprising forming two boats by melting or molding or
casting or hot pressing and sintering the powder material.
196. The process of any of preceding claims 185 to 195,
further comprising forming slots in inward and/or outward
ribs or extensions, forming ends of the boats having
complementary steps to connect the boats end-to-end in an
axial stack or row.
197. Fabrication process comprising the steps of
providing with a powder or solid, heating the powder or the
solid to a plastic slate and forming a tube, plate or rod.
198. The process of claim 197, further comprising
forming a chamber liner and applying to a process chamber,




62


forming a chemical vapor deposition (CVD) station, halving
formed tubes lengthwise, cutting windows, inward ribs or
extensions in the tubes, or the inner walls are slotted,
forming a vertical boat, and in parallel steps cutting
windows, plotting the boat and forming a horizontal boat.
199. The process of claim 198, wherein the powder is
mixed with organic or inorganic material.
200. The process of claim 198, wherein the powder is
selected from a group consisting of silicon, silicon compound
containing at least one atom of silicon, silicon and
germanium, SixGe1-x solid solution, silicon and Silicon
Carbide Six(SiC)1-x, Silicon and silicon dioxide Six(SiO2)1-x,
silicon and any ceramic, silicon and any oxide Six(Oxide)1-x,
silicon and any metal SixM1-x, Silicon and any alloy SixA1-x,
any combination between themselves, or made from composite
material, wherein 0 <= x <=1.
201. Wafer processing apparatus comprising a processing
chamber, wafer handling tools, wafer boat handling tools
consisting of one or more processing chambers, shields and
enclosures employing one or more members, and at least one
member made of material containing at least one atom of
silicon.
202. The apparatus of claim 201, wherein the at least
one member is of material selected from a group consisting of
silicon, silicon compound comprising at least one silicon
atom, silicon and germanium, SixGe1-x solid solution, silicon
and silicon carbide Six(SiC)1-x, silicon and silicon dioxide
Six(SiO2)1-x, silicon and any ceramic, silicon and any oxide
SiX (Oxide)1-x, silicon and any metal SixM1-x, Silicon and any
alloy SixA1-x, any combination between themselves, or made
from composite material, wherein 0 <= x <=1.
203. the apparatus of claim 202, wherein each chamber
comprises separate or a common gas delivery and venting
system, vacuum system, internal or external heating elements,
and cooled or not cooled vacuum shell.




63


204. The apparatus of claim 203, wherein the vacuum
shell is partially or fully lined with material selected from
a group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, SixGe1-x solid
solution, silicon and Silicon Carbide Six(SiC)1-x, Silicon and
silicon dioxide Six(SiO2)1-x, silicon and any ceramic, silicon
and any oxide Six (Oxide)1-x, silicon and any metal SixM1-x,
Silicon and any alloy SixA1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.
205. Wafer processing apparatus comprising plural
processing chambers, wherein at least one of the processing
chambers is a chemical vapor deposition (CVD) chamber
comprising one or more members consisting of material
selected from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
SixGe1-x solid solution, silicon and Silicon Carbide Six(SiC)1-
x, Silicon and silicon dioxide. Six(SiO2)1-x, silicon and any
ceramic, silicon and any oxide Six(Oxide)1-x, silicon and any
metal SixM1-x, Silicon and any alloy SixA1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <=1.
206. The apparatus of claim 205, wherein each CVD
chamber comprises separate or common gas delivery and venting
system, vacuum system, internal or external heating elements,
and cooled or not cooled vacuum shell.
207. The apparatus of claim 206, wherein the vacuum
shell is partially or fully lined with material selected from
a group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, SixGe1-x solid
solution, silicon and silicon carbide Six(SiC)1-x, silicon and
silicon dioxide Six(SiO2)1-x. silicon and any ceramic, silicon
and any oxide Six (Oxide)1-x, silicon and any metal SixM1-x,
Silicon and any alloy SixA1-x, any combination between
themselves, or made from composite material, wherein 0 <= x




64


<=1.
208. Wafer processing apparatus comprising plural
processing chambers, wherein at least one of the processing
chambers is an epitaxial chamber comprising one or more
members consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, SixGe1-x solid
solution, silicon and Silicon Carbide Six(SiC)1-x, Silicon and
silicon dioxide Six(S1O2)1-x, silicon and any ceramic, silicon
and any oxide Six (Oxide) 1-x, silicon and any metal SixM1-x,
Silicon and any alloy SixA1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.
209. The apparatus of claim 208, wherein each epitaxial
chamber comprises separate or common gas delivery and venting
system, vacuum system, internal or external heating elements,
and cooled or not cooled vacuum shell.
210. The apparatus of claim 209, wherein the vacuum
shell is partially or fully lined with material selected from
a group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, SixGe1-x solid
solution, silicon and Silicon Carbide Six(SiC)1-x, Silicon and
silicon dioxide Six(S1O2)1-x, silicon and any ceramic, silicon
and any oxide Six (Oxide) 1-x, silicon and any metal SixM1-x,
Silicon and any alloy SixA1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.
211. Wafer processing apparatus comprising plural
processing chambers, wherein at least one of the processing
chambers is a thin film deposition chamber comprising one or
more members made of material selected from a group
consisting of silicon, silicon compound comprising at least
one silicon atom, silicon and germanium, SixGe1-x solid
solution, silicon and Silicon Carbide Six(SiC)1-x, Silicon and
silicon dioxide Six(S1O2)1-x, silicon and any ceramic, silicon
and any oxide Six(Oxide)1-x silicon and any metal SixM1-x,


65


Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.

212. The apparatus of claim 211, wherein the thin film
deposition chamber comprises separate or common gas delivery
and venting system, vacuum. system, internal or external
heating elements, cooled or not cooled vacuum shell.

213. The apparatus of claim 212, wherein the vacuum
shell is partially or fully lined with material selected from
a group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and Silicon Carbide Si x (SiC)1-x, Silicon and
silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-x, silicon and any metal Si x M1-x,
Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein all
cases 0 <= x <=1.

214. Wafer processing apparatus comprising plural
processing chambers, wherein at least one of the processing
chambers is thin film removal chamber comprising one or more
members consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and Silicon Carbide Si x (SiC)1-x, Silicon
and silicon dioxide Si x (SiO2)1-x, silicon and any ceramic,
silicon and any oxide Si x (Oxide)1-x, silicon and any metal
Si x M1-x, Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein all
cases 0 <= x <=1.

215. The apparatus of claim 214, wherein the thin film
removal chamber comprises separate or common gas delivery and
venting system, vacuum system, internal or external heating
elements, cooled or not cooled vacuum shell partially or
fully lined with silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and Silicon Carbide Si x (SiC)1-x, Silicon and




66


silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-X, silicon and any metal Si x M1-x,
Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.

216. The apparatus of any of the preceding claims 201 to
215, wherein one of the chambers is a main chamber connected
with other chambers directly or via one or more gate valves.

217. The apparatus of any of the preceding claims 201 to
216, wherein one or more chambers is vacuum, low pressure or
desired pressure chamber.

218. The apparatus of any of the preceding claims 201 to
217, wherein one or more chambers has at least one internal
or external heater.

219. The apparatus of any of the preceding claims 201 to
218, wherein one or more chambers has at least one partial or
complete heat shield.

220. A chemical vapor deposition (CVD) system comprising
a vacuum vessel with cooled or not cooled chamber with single
or double wall, a robot handling arm having elements for
wafer or wafer boat delivery/removal that forms a vacuum
tight seal when the chamber is loaded, a wafer tray/boat
containing one or more wafers resting on the wafer boat
delivery/removal arm, a shield surrounding the wafer
tray/boat and an inside portion of the wafer handling arm,
process gas delivery system with all respective valves
attached to the chamber and having a delivery tube extending
into a wafer area, inert gas delivery system with all
respective valves attached to the chamber and having a
delivery tube with or without diffuser extending into the
wafer area, vacuum pumping system connected to the chamber,
and an inside or outside heater directing heat into the
process area.

221. The system of claim 220, wherein the process area
comprises one or more members of material selected from a




67



group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and Silicon Carbide Si x (SiC)1-x, Silicon and
silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-x, silicon and any metal Si x M1-x,
Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.

222. The system of claim 221, wherein the CVD system is
vertical, horizontal or of any suitable position from -90° to
+90°.

223. The system of any of the preceding claims 220 to
222, wherein the wafer boat is of solid connected members
made from material selected from a group consisting of
silicon, silicon compound comprising at least one silicon
atom, silicon and germanium, Si x Ge1-x solid solution, silicon
and Silicon Carbide Si x (SiC)1-x, Silicon and silicon dioxide
Si x (SiO2)1-x, silicon and any ceramic, silicon and any oxide
Si x (Oxide)1-x, silicon and any metal Si x M1-x, silicon and any
alloy Si x A1-x, any combination between themselves, or made
from composite material, wherein 0 <= x <=1.

224. The system of any of the preceding claims 220 to
222, wherein the wafer boat is of modular elements made from
material selected from a group consisting of silicon, silicon
compound comprising at least one silicon atom, silicon and
germanium, Si x Ge1-x solid solution, silicon and silicon
carbide Si x (SiC)1-x, Silicon and silicon dioxide Si x (SiO2)1-x,
silicon and any ceramic, silicon and any oxide Si x (Oxide)1-x,
silicon and any metal Si x M1-x, Silicon and any alloy Si x A1-x,
any combination between themselves, or made from composite
material, wherein 0 <= x <=1.

225. The system of any of the preceding claims 220 to
224, wherein the wafer boat comprises one or more slots for
supporting wafers spaced at appropriate distances.

226. The system of any of the preceding claims 220 to




68


225, wherein the wafers in the boat are positioned so there
is no other material between the wafers other than vacuum or
any gas present in a processing part of the chamber.

227. The system of any of the preceding claims 220 to
226, wherein the wafer boats comprise slots for wafer support
and susceptors between the wafers for improved temperature
distribution over wafer surfaces resulting in more uniform
deposited layer thickness and composition.

228. The system of any of the preceding claims 220 to
227, wherein the susceptor in the boat is part of the wafer
boat.

229. The system of any of the preceding claims 220 to
227, wherein the susceptor in the boat is inserted after or
prior to the boat being made, or together with the wafer
loading.

230. The system of any of the preceding claims 220 to
229, wherein the boat is modular.

231. The system of any of the preceding claims 220 to
230, wherein each module of the boat comprises support for
one or more wafers.

232. The system of any of the preceding claims 220 to
231, wherein each module comprises support for one or more
wafers separated by inserted or built in susceptors.

233. The system of any of the preceding claims 220 to
232, wherein the susceptors are full body or have cuts to
allow wafer only insertion/removal handling.

234. The system of any of the preceding claims 220 to
233, wherein the boat is made from modular parts connected
via chemical or mechanical bonding.

235. The system of any of the preceding claims 220 to
234, wherein the boat has round, elliptical, polygonal or any
other cross section.

236. The system of any of the preceding claims 220 to
235, wherein the boat has one or more elements at each end
for mechanical strength during handling.




69


237. The system of any of the preceding claims 220 to
236, wherein end parts of the boat are modules.

238. The system of any of the preceding claims 220 to
237, wherein all parts of the boat are made from same or
different materials.

239. A single wafer processing system for chemical vapor
deposition (CVD), epitaxial deposition, thin film
deposition/removal or any other wafer processing for chips
comprising a vacuum vessel with cooled or not cooled chamber
wall and with single or double wall, connected directly or
through at least one gate valve to a chamber with multistage
wafer handling mechanism for wafer delivery/removal, a shield
surrounding the wafer processing area, process and inert gas
delivery system with all respective valves attached to the
chamber, a delivery tube extending into a wafer area, vacuum
pumping system connected to the chamber, inside and/or
outside heater directing heat into the process area.

240. The system of claim 239, wherein the process area
comprises one or more members consisting of silicon, silicon
compound comprising at least one silicon atom, silicon and
germanium, Si x Ge1-x solid solution, silicon and silicon
carbide Si x (SiC)1-x, silicon and silicon dioxide Si x (SiO2)1-x,
silicon and any ceramic, silicon and any oxide Si x (Oxide)1-x,
silicon and any metal Si x M1-x, silicon and any alloy Si x A1-x,
any combination between themselves, or made from composite
material, wherein 0 <= x <= 1.

241. The system of claim 240, further comprising vacuum
pumping systems and gas delivery systems for both chambers.

242. The system of claim 241, further comprising heating
elements located around or in the chambers.

243. The system of claim 242, further comprising chamber
connection ports connecting a chamber to additional chambers
for transferring or removing the wafers.

244. The system of any of the preceding claims 239 to
243, wherein the process chamber is a CVD chamber.




70


245. The system of any of the preceding claims 239 to
243, wherein the process chamber is an epitaxial deposition
chamber.

246. The system of any of the preceding claims 239 to
243, wherein the process chamber is a thin film
deposition/removal chamber.

247. The system of any of the preceding claims 239 to
243, wherein the process chamber is a wafer process chamber.

248. The system of any of the preceding claims 239 to
247, wherein the process chamber has any cross section and
height.

249. The system of any of the preceding claims 239 to
248, wherein the system is vertical, horizontal or has any
suitable position from -90° to +90°.

250. The system of any of the preceding claims 239 to
249, wherein the members are made from material selected from
a group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and silicon carbide Si x (SiC)1-x, silicon and
silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-x, silicon and any metal Si x M1-x,
silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1.

251. The system of any of the preceding claims 239 to
250, wherein the members are solidly connected by chemical or
mechanical bonding.

252. The system of any of the preceding claims 239 to
251, wherein the members are made of material selected from a
group consisting of silicon, silicon compound comprising at
least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and silicon carbide Si x (SiC)1-x, silicon and
silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-x, silicon and any metal Si x M1-x,
silicon and any alloy Si x A1-x, any combination between


71


themselves, or made from composite material, wherein 0 <= x
<=1, and wherein the members are modular.

253. The system of any of the preceding claims 239 to
251, wherein the members are made of material selected from a
group consisting of silicon, silicon compound comprising at
a least one silicon atom, silicon and germanium, Si x Ge1-x solid
solution, silicon and Silicon Carbide Si x (SiC)1-x, Silicon and
silicon dioxide Si x (SiO2)1-x, silicon and any ceramic, silicon
and any oxide Si x (Oxide)1-x, .silicon and any metal Si x M1-x,
Silicon and any alloy Si x A1-x, any combination between
themselves, or made from composite material, wherein 0 <= x
<=1, and comprise one or more slots for wafers' support to
optimize the process.

254. The system of any of the preceding claims 239 to
253, wherein the wafer processing chamber has a susceptor
next to the wafer for improved temperature distribution over
the wafer surface that results in more uniform deposited
layer thickness and composition.

255. The system of any of the preceding claims 239 to
254, wherein the susceptor in the process chamber is part of
the chamber.

256. The system of any of the preceding claims 239 to
255, further comprising a wafer delivery arm, wherein the
wafer delivery arm is made in full or partially from material
selected from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
Si x Ge1-x solid solution, silicon and silicon carbide Si x (SiC)1-
x, silicon and silicon dioxide Si x (SiO2)1-x, silicon and any
ceramic, silicon and any oxide Si x (Oxide)1-x, silicon and any
metal Si x M1-x, Silicon and any alloy Si x A1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <=1.

257. The system of any of the preceding claims 239 to
256, wherein the susceptor is a full body or has certain cuts
to allow wafer only insertion/removal handling.





72



258. The system of any of the preceding claims 239 to
257, wherein all chamber parts are made in full or partially
from material selected from a group consisting of silicon,
silicon compound comprising at least one silicon atom,
silicon and germanium, Si x Ge1-x solid solution, silicon and
silicon carbide Si x (SiC)1-x, silicon and silicon dioxide
Si x (SiO2)1-x, silicon and any ceramic, silicon and any oxide
Si x (Oxide)1-x, silicon and any metal Si x M1-x, silicon and any
alloy Si x A1-x, any combination between themselves, or made
from composite material, wherein 0 <= x <=1, and are from
modular parts connected via chemical or mechanical bonding or
by assembling without bonding.

259. The system of any of the preceding claims 239 to
258, wherein the chamber has round, elliptical, polygonal or
any other applicable cross section.

260. The system of any of the preceding claims 239 to
259, further comprising end parts of the wafer processing
chamber, wherein the end parts are modules.

261. The system of any of the preceding claims 239 to
260, wherein all parts of the boat are made from the same or
different materials.

262. Epitaxial/CVD chamber body comprising epitaxial/CVD
chambers made in full or partially from material selected
from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
Six Ge1-x solid solution, silicon and silicon carbide Si x (SiC)1-
x, silicon and silicon dioxide Si x (SiO2)1-x, silicon and any
ceramic, silicon and any oxide Si x (Oxide)1-x, silicon and any
metal Si x M1-x, silicon and any alloy Si x A1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <= 1.

263. The chamber body of claim 262, further comprising
bodies, an optical window for wafer radiation and at least
one opening for wafer and gas delivery/removal.

264. The chamber body of claim 263, wherein the bodies




73


are bonded together along side edges forming the chamber, a
wafer heater accesses wafers in the chamber through the
window, and a wafer lifting and rotating mechanism port and
assembly supports wafers through an opposite window.

265. The chamber body of any of the preceding claims 262
to 264, wherein the chambers have suitable wall thicknesses
and at least one infrared window at each side, hollow
interior and at least one gate opening for connection to a
wafer supply and process gas supply chamber and a gas
exhaust.

266. The chamber body of any of the preceding claims 262
to 265, wherein the chamber is made from materials selected
from a group consisting of silicon, silicon compound
comprising at least one silicon atom, silicon and germanium,
Si x Ge1-x solid solution, silicon and silicon carbide Si x (SiC)1-
x, silicon and silicon dioxide Si x (SiO2)1-x, silicon and any
ceramic, silicon and any oxide Si x (Oxide)1-x, silicon and any
metal Si x M1-x, Silicon and any alloy Si x A1-x, any combination
between themselves, or made from composite material, wherein
0 <= x <=1.

267. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber body comprises a single
body made by pressing of material, machining it from inside
and out in its green state, purifying the said body at a
certain temperature by immersing it in a chemically reactive
gas, plasma or liquid for certain period of time, sintering
the said body at appropriate temperature determined by its
composition, final machining of the said body, if needed, to
meet the specifications of the epitaxial deposition process.

268. The chamber body of claim 267, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

269. The chamber body of any of the preceding claims 262




74


to 266, wherein the epitaxial chamber body comprises a single
body made by casting of the material, machining it from
inside and out in its green state, purifying said body at a
certain temperature by immersing it in a chemically reactive
gas, plasma or liquid for certain period of time, sintering
the said body at appropriate temperature determined by its
composition, final machining of the said body, if needed, to
meet the specifications of the epitaxial deposition process.

270. The chamber body of claim 269, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

271. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises upper and
lower parts made by casting to shape the material, machining
the parts, purifying the said body at a certain temperature
by immersing it in a chemically reactive gas, plasma or
liquid for certain period of time, sintering the said body at
appropriate temperature determined by its composition,
joining the parts by chemical and/or mechanical means, final
machining of the said body, if needed, to meet the
specifications of the epitaxial deposition process.

272. The chamber body of claim 271, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

273. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises single part
or upper and lower parts made by casting or cold or hot
pressing to shape to shape the material, machining the parts,
purifying the said body at a certain temperature by immersing
it in a chemically reactive gas, plasma or liquid for
certain period of time, sintering the said body at



75


appropriate temperature determined by its composition,
joining the parts by chemical and/or mechanical means, final
machining of the said body, if needed, to meet the
specifications of the epitaxial deposition process.

274. The chamber body of claim 273, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

275. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises one part or
upper and lower parts made by cold or hot pressing of a block
of the material, machining the chamber, purifying the said
body at a certain temperature by immersing it in a chemically
reactive gas, plasma or liquid for certain period of time,
sintering the said body at appropriate temperature determined
by its composition, joining the parts by chemical and/or
mechanical means, final machining of the said body, if
needed, to meet the specifications of the epitaxial
deposition process.

276. The chamber body of claim 275, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

277. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises one part or
upper and lower parts made by cold or hot extrusion of a
block or a desired shape of the material, machining the
chamber, purifying the said body at a certain temperature by
immersing it in a chemically reactive gas, plasma or liquid
for certain period of time, sintering the said body at
appropriate temperature determined by its composition,
joining the parts by chemical and/or mechanical means, final
machining of the said body, if needed, to meet the



76


specifications of the epitaxial deposition process.

278. The chamber body of claims 277, wherein the
finished body is subjected to thin film deposition such as
chemical vapor deposition, plasma enhanced deposition, or
other suitable deposition method for better finish on the
inside and outside.

279. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises one part or
upper and lower parts made by plasma spraying of the
material, and forming a chamber to a desired shape, machining
the chamber, purifying the said body at a certain temperature
by immersing it in a chemically reactive gas, plasma or
liquid for certain period of time, sintering the said body at
appropriate temperature determined by its composition,
joining the parts by chemical and/or mechanical means, final
machining of the said body, if needed, to meet the
specifications of the epitaxial deposition process.

280. The chamber body of claim 279, wherein the finished
body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

281. The chamber body of any of the preceding claims 262
to 266, wherein the epitaxial chamber comprises one part or
upper and lower parts made by spraying of organic or
inorganic based slurry of the material and forming a chamber
to a desired shape, machining the chamber, purifying the said
body at a certain temperature by immersing it in a chemically
reactive gas, plasma or liquid for certain period of time,
sintering the said body at appropriate temperature determined
by its composition, joining the parts by chemical and/or
mechanical means, final machining of the said body, if
needed, to meet the specifications of the epitaxial
deposition process.

282. The chamber body of claim 281, wherein the finished



77


body is subjected to thin film deposition such as chemical
vapor deposition, plasma enhanced deposition, or other
suitable deposition method for better finish on the inside
and outside.

283. The chamber body of any of the preceding claims 262
to 282, wherein the chamber comprises two separate halves
joined at one plane followed by final machining.

284. The chamber body of any of the preceding claims 262
to 282, wherein the chamber comprises a single body machined
from a solid block material.

285. The chamber body of any of the preceding claims 262
to 282, wherein the chamber comprises a single body made by
method of plasma spraying followed by final machining.

286. The chamber body of any of the preceding claims 262
to 282, wherein the chamber comprises a single body made by
method of slurry spraying.

287. The chamber body of any of the preceding claims 262
to 282, wherein the chamber comprises a single body machined
by method of casting, forging or extrusion followed by
sintering and final machining.

288. The chamber body of any of the preceding claims 262
to 287, wherein the chamber has a vacuum, reduced pressure or
desired pressure chamber.

289. The chamber body of any of the preceding claims 262
to 288, wherein the chamber has a liner for a vacuum, reduced
pressure or desired pressure chamber for wafer processing
applications.

290. The chamber body of any of the preceding claims 262
to 289, wherein the chamber is made of modular pieces stacked
on top of each other or bonded by mechanical or chemical
means.

291. The chamber body of any of the preceding claims 262
to 290, further comprising an optical window, wherein the
optical window is from same or suitable material stacked on
the chamber or bonded by mechanical or chemical means.




78


292. The chamber body of any of the preceding claims 262
to 291, wherein the chamber has one or more optical windows
depending on the process requirements.

293. The chamber body of any of the preceding claims 262
to 292, further comprising a gas delivery system for
delivering process and inert gases into the chamber attached
to the chamber or to the chamber wall.

294. The chamber body of any of the preceding claims 262
to 293, further comprising gas delivery members exposed to
the process atmosphere made from the chamber material or
chamber lining material.

295. The chamber body of any of the preceding claims 262
to 294, further comprising a wafer delivering/removing arm
to/from the chamber made from the chamber material or chamber
lining material.

296. The chamber body of any of the preceding claims 262
to 295, further comprising a susceptor and a member that
either holds the wafer or surrounds the wafer from the sides,
the top or the bottom, as required by the process made from
the chamber material or chamber lining material.

297. The chamber body of any of the preceding claims 262
to 296, further comprising a reduced pressure chamber
surrounding the epitaxial /CVD chamber made in full or
partially from material selected from a group consisting of
silicon, silicon compound comprising at least one silicon
atom, silicon and germanium, Si x Ge1-x solid solution, silicon
and silicon carbide Si x(SiC)1-x, silicon and silicon dioxide
Si X(SiO2)1-x, silicon and any ceramic, silicon and any oxide
Si x(Oxide)1-x, silicon and any metal Si X M1-x, silicon and any
alloy Si x A1-x, any combination between themselves, or made
from composite material, wherein 0 <= × <=1.

298. The chamber body of any of the preceding claims 262
to 297, further comprising a body, an optical window for
wafer radiation and at least one opening for wafer and gas
delivery/removal.


79


299. The chamber body of any of the preceding claims 262
to 298, further comprising an outer chamber of vacuum,
reduced pressure or desired pressure as required by the
process.

300. The chamber body of any of the preceding claims 262
to 299, wherein the chamber comprises one or more optical
windows depending on the process requirements.

301. The chamber body of any of the preceding claims 262
to 300, wherein the chamber has gas delivery system for
delivering process and inert gases into the chamber attached
to the chamber or to the chamber wall.

302. A single wafer processing system for CVD, epitaxial
deposition, thin film deposition/removal or any other wafer
processing for a chip comprising a vacuum vessel with cooled
or not cooled chamber wall with single or double wall,
connected directly or through at least one gate valve to a
chamber with multistage wafer handling mechanism for wafer
delivery/removal, a shield surrounding the wafer processing
area, process and inert gas delivery system with all
respective valves attached to the chamber and having a
delivery tube extending into a wafer area, vacuum pumping
system connected to the chamber, inside and/or outside heater
directing heat into the process area employing one or more
members made from material selected from a group consisting
of silicon, silicon compound comprising at least one silicon
atom, silicon and germanium, Si x Ge1-x solid solution, silicon
and silicon carbide Si x(SiC)1-x, silicon and silicon dioxide
Si X(SiO2)1-x, silicon and any ceramic, silicon and any oxide
Si X(Oxide)1-x, silicon and any metal Si x M1-x, Silicon and any
alloy Si X A1-x, any combination between themselves, or made
from composite material, wherein 0 <= × <=1, employing at
least
one epitaxial chamber.

303. Process for fabrication of silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom members comprising processing high purity quartz or



80

fused silica material and forming different structures for
processing wafers.

304. The process of claim 303, wherein the forming
further comprises making silicon boats having desired
mechanical properties.

305. The process of claim 304, wherein the processing
comprises forging, extrusion, plasma and hot substrate powder
deposition, slurry spray and slurry casting, silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom casting and directional solidification for the
fabrication of the members.

306. The process of any of the preceding claims 303 to
305, wherein the processing comprises silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom powder pressing and/or forging and extrusion.

307. The process of any of the preceding claims 303 to
306, wherein the forming comprises fabrication of epitaxial
reactors, chemical vapor deposition (CVD) chambers, CVD
chamber liners, tubing, and combinations thereof.

308. The process of any of the preceding claims 303 to
306, wherein the forming comprises fabrication of
silicon/silicon alloy/composite/silicon compound having at
least one silicon atom members selected from a group
consisting of wafer boats for horizontal and vertical wafer
processing furnaces and deposition chambers, epitaxial
reactors, lining for CVD chambers, epitaxial reactors and
other wafer processing tools, tubing having any form or cross
section shape, and combinations thereof.

309. The process of any of preceding claims 303 to 308,
wherein the processing comprises pressing silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom material at room temperature or at an elevated
temperature in vacuum or in a controlled atmosphere,
outgassing, removing oxygen, nitrogen, water vapor and other
undesired gases before/during/after pressing of the material.



81


310. The process of any of the preceding claims 303 to
309, wherein the pressing comprises pressing to a near shape
of a part being fabricated.

311. The process of any of the preceding claims 303 to
309, wherein the pressing comprises pressing into a raw
material for further processing into desired members.

312. The process of any of the preceding claims 303 to
311, wherein the material comprises a powder selected from a
group consisting of silicon, silicon compound having at least
one silicon atom, silicon and germanium, silicon and metal,
silicon and silicon carbide, silicon and ceramic, silicon and
a suitable element or compound and combinations thereof.

313. The process of any of the preceding claims 303 to
312, wherein processing the material comprises providing
silicon powder, silicon compounds having at least one atom of
silicon, silicon based alloys or composites having a desired
grain size in a pressing chamber.

314. The process of any of the preceding claims 303 to
313, wherein the processing further comprises treating with
gas treatment and/or vacuuming the residual gas and then
pressing the material.

315. The process of any of the preceding claims 303 to
314, wherein the processing comprises pressing at a
temperature as low as room temperature or as high as a
softening point of the lowest melting point constituent.

316. The process of any of the preceding claims 303 to
315, wherein the processing further comprises sintering the
pressed part in vacuum or in appropriate gaseous atmosphere
and fabricating very dense materials with predetermined
hardness.

317. The process of claim 316, further comprising
tailoring various parts for various applications by adjusting
a grain size of the material, wherein smaller grain sizes are
used for making parts with higher fracture strength and vice-
versa.



82


318. The process of any of the preceding claims 303 to
317, further comprising machining the parts made before the
sintering, sintering, and after the sintering allowing the
parts to yield near shape for using as sintered parts or for
subjecting sintered parts to a further final machining.

319. The process of any of the preceding claims 303 to
318, wherein the processing comprises processing at pressures
of up to 800,000 psi or higher.

320. The process of any of the preceding claims 303 to
319, wherein the processing comprises processing at
temperatures of suitable for the material during pressing and
sintering and varying the temperatures corresponding to a
composition of the material.

321. The process of any of the preceding claims 303 to
320, wherein the processing comprises processing at
temperatures between 300°C and 1350°C.

322. The process of any of the preceding claims 303 to
320, wherein the processing comprises processing at
temperatures up to about 300°C and greater than about 1350°C
corresponding to the material being processed and desired
properties of the members.

323. The process of any of the preceding claims 303 to
322, wherein the forming comprises press-shaping solid
silicon of single crystal or polycrystalline material into
various parts, heating the silicon to a desired temperature
and obtaining appropriate plastic properties.

324. The process of claim 323, wherein the press-shaping
comprises shaping by forging or extrusion of the
silicon/silicon alloy/composite/silicon compound having at
least one silicon atom material.

325. The process of claims 303 and 324, wherein the
pressing and shaping of the material is done before, during
or after sintering of the material.

326. The process of any of the preceding claims 303 to
325, further comprising selecting a desired material



83


corresponding to a plasticity of the material for determining
grain size and fracture strength.

327. The process of any of the preceding claims 303 to
326, wherein the pressing comprises several steps of hot
pressing the material.

328. The process of any of the preceding claims 303 to
327, wherein the processing comprises extrusion followed by
forging and/or high pressure annealing.

329. The process of any of the preceding claims 303 to
305, wherein the shaping of the material further comprises
imbedding stronger material in the part being made for
reinforcement purposes.

330. The process of claim 329, wherein the imbedding
comprises providing a strong layer within the part or forming
the stronger layer on an outer or inner surface of the part
and fabricating parts having desired strength pattern.

331. Member forming process comprising providing plasma
heated or not heated silicon powder material or non plasma
heated or non-heated silicon powder material, introducing the
material into a chamber, directing the material towards a
heated substrate and depositing on the substrate.

332. The process of claim 331, wherein the chamber is a
vacuum, low pressure, normal pressure or high-pressure
chamber.

333. The process of claim 332, wherein the powder
deposition comprises depositing silicon only, or silicon and
other material particles and reinforcing silicon structure
without changing chemical behavior or material particles that
change the properties of silicon and forming a silicon alloy
or solid solution.

334. The process of any of the preceding claims 331 to
333, wherein the material is selected from a group consisting
of Ge, Si x G1-x, SiC, silicon based materials, silicon compound
having at least one silicon atom, ceramics, suitable elements
or compounds and doping and/or reinforcing the material.



84


335. The process of any of the preceding claims 331 to
334, wherein the depositing comprises depositing layers
corresponding to a temperature of the substrate, wherein the
deposited layers have different densities and thicknesses,
sintering the layers and forming very dense material having
desired fracture strengths.

336. The process of any of the preceding claims 331 to
335, further comprising injecting the non-plasma heated
powder or not heated powder material in the chamber and
directing towards a hot substrate within a heated or non-
heated controlled atmosphere or vacuum chamber.

337. The process of any of the preceding claims 331 to
336, further comprising heating the powder material to a
desired temperature on its way to and from the substrate,
adhering grains of the material to the substrate and/or other
previously deposited grains on the substrate and forming a
deposited body.

338. The process of any of the preceding claims 331 to
337, wherein a density of the deposited body is proportional
to grain size, grain temperature at impact and substrate
temperature.

339. The process of any of the preceding claims 331 to
338, wherein the member is a silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom member having shapes selected from a group consisting of
rod, tube having any cross-section and shape, any chamber
looking type shape with one or more gates, and combinations
thereof.


340. The process of any of the preceding claims 331 to
339, wherein the substrate is heated up to a softening point
of silicon material.

341. The process of any of the preceding claims 331 to
340, wherein an optimal temperature is between about 800°C to
about 1350°C.

342. The process of any of the preceding claims 331 to


85

341, wherein the temperatures are less than about 800°C and
more than about 1350°C.

343. The process of any of the preceding claims 331 to
342, wherein the sintering of the silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom members is done in situ, or after machining, shaping or
joining of the members with other parts made by the same or
different process.

344. The process of any of the preceding claims 331 to
343, wherein the sintering temperature corresponds to
chemical composition of the parts and their applications.

345. Chemical vapor deposition (CVD) process comprising
deposition of silicon and/or silicon/composite and/or silicon
alloy and/or silicon compound having at least one silicon
atom materials on a substrate, reinforcing deposited layers
without changing the chemical behavior of a surface of
interest and forming members for various applications.

346. The process of claim 345, wherein the deposition of
the silicon/silicon alloy/composite/silicon compound having
at least one silicon atom material on the substrate comprises
providing a suitable substrate having a sticking coefficient
to deposited material.

347. The process of claim 46, wherein the material is
selected from a group consisting of silicon nitrides,
graphite, metal silicates, ceramics, silicon, silicon
compound having at least one silicon atom, and substances
suitable as substrate for particular applications, and
combinations thereof.

348. The process of any of the preceding claims 345 to
347, wherein the deposition comprises depositing the material
at variable temperatures of the substrate and variable
pressures during the deposition process.

349. The process of any of the preceding claims 345 to
348, wherein the deposited layers have initial thicknesses
that after sintering results in very dense material having


86

desired thickness for a particular application.

350. The process of any of the preceding claims 345 to
349, wherein the members are silicon/silicon
alloy/composite/silicon compound having at least one silicon
atom members having shapes selected from a group consisting
of rod, tube having desired cross-section, shape and size,
plate or any wafer processing chamber suitable type shape,
having one or more gates leading inside the chamber.

351. Fabrication process for forming members comprising
mixing a powder with a high purity liquid chemical compound
and forming a slurry, spraying or casting the slurry, and
forming a desired body.

352. The process of claim 351, wherein the spraying
comprises depositing the slurry on a substrate that rotates
and/or translates.

353. The process of claim 352, wherein the substrate
comprises any material that does not react with or
contaminate the slurry.

354. The process of claim 353, further comprising either
incorporating the material in the fabricated body or curing
and removing liquids and separating the material during or
after deposition of the slurry.

355. The process of any of the preceding claims 351 to
354, further comprising roughly machining the cured articles
before a bake-out process is implemented.

356. The process of any of the preceding claims 351 to
355, further comprising implementing a bake out process and
completely removing chemical substances such as binders and
sintering the silicon/silicon alloy/composite powder/silicon
compound having at least one silicon atom made member.

357. The process of any of the preceding claims 351 to
356, further comprising machining the members into desired
shapes following the bake-out process.

358. The process of any of the preceding claims 351 to
357, wherein the slurry deposition and/or casting is


87

conducted in vacuum or controlled gas atmosphere chamber
employing one or more heaters.

359. The process of any of the preceding claims 351 to
358, wherein the curing and sintering is conducted in the
same or in a different chamber.

360. The process of any of the preceding claims 351 to
359, wherein the silicon/silicon alloy/composite/silicon
compound having at least one silicon atom member have shapes
of rod, round tube, rectangular tube, plate or any wafer
processing chamber suitable type shape.

361. Fabrication process comprising casting to shape
silicon/silicon alloy/composite/silicon compound comprising
at least one silicon atom material or re-melting and casting
solid silicon and forming various made parts.

362. The process of claim 361, further comprising
providing a high purity mold made from easily removable
material that does not react with silicon/silicon
alloy/composite/silicon compound, filling the mold, with shot,
powder or small chunks of the material to be melted.

363. The process of claim 362, wherein the material for
casting is melted in a separate container and transferred
into the mold after melting.

364. The process of claim 363, further comprising
removing oxygen, nitrogen, water vapor, and other
contaminants before the melting process.

365. The process of claim 364, wherein the forming the
member comprises forming silicon/silicon
alloy/composite/silicon compound member having a shape
selected from a group consisting of rod, round tube, tube or
any other shape or form.

366. Fabrication process comprising gelcasting
silicon/silicon alloy/composite/silicon compound having at
least one silicon atom material and forming a body.

367. The process of claim 366, further comprising


88

converting the material in powder having desired grain size.

368. The process of claim 367, further comprising
suspending the powder in a monomer solution which is
polymerized in a mold to form a rigid polymer/solvent gel.

369. The process of any of the preceding claims 366 to
368, further comprising adding organic or inorganic
substances to the powder/polymer binder, triggering a
polymerization process.

370. The process of any of preceding claims 366 to 369,
wherein the polymerization process is triggered at desired
process conditions.

371. The process of any of the preceding claims 366 to
370, wherein the process comprises up to 10-20 weight %
polymer.

372. The process of any of the preceding claims 366 to
371, wherein the percentage is as low as few weight percent
and over 20 weight percent.

373. The process of any of the preceding claims 366 to
372, further comprising drying and removing a solvent portion
after removing the fabricated part from the mold.

374. The process of any of the preceding claims 366 to
372, further comprising wherein the solution is aqueous or
non-aqueous.

375. The process of claim 374, wherein the non-aqueous
solution comprises 50-55 volume o of powder with balance
being a dispersion solution.

376. The process of any of preceding claims 366 to 375,
wherein the solution comprises about 10% dispersant such as
Rohm & Haas Triton X-100, or N-100 Dupont dibasic ester (DBE)
or ICI Americas Solsperse 2000 in dibutil phtalate (DBP) and
90 % gelcasting premix, wherein the premix includes 10-30
volume % of monomers such as trifunctional trimethilpropane
triacrylate (TMPTA) and difunctional 1,6 hexanediol
diacrilate (HDODA) from Hoechst Celanese, 0.5 to 10 volume
of dybenzoil peroxide initiator with the rest being either


89

DBA, DBP or other suitable solvent.

377. The process of any of preceding claims 366 to 376,
further comprising hardening of the material mass in the
mold, spraying onto a substrate having desired process
temperature, and fabricating the member,

378. The process of any of preceding claims 366 to 377,
wherein the spraying comprises spraying in vacuum or desired
gaseous atmosphere.

379. The process of any of the preceding claims 366 to
378, wherein the spraying comprises spraying the slurry or
spraying various components onto the substrate, mixing,
reacting and hardening into the desired shape.

380. The process of any of preceding claims 366 to 379,
wherein the fabrication comprises continuous feeding onto a
beltline type apparatus.

381. The process of any of preceding claims 366 to 380,
further comprising hardening, drying and sintering as part of
the continuous process.

382. The process of any of the preceding claims 366 to
381, wherein the feed comprises already made mixture of the
material.

383. The process of any of the preceding claims 366 to
382, wherein the feed comprises mixing material at a feeding
point.

384. Fabrication process for fabricating large size
silicon/silicon alloys/composites/silicon compound having at
least one silicon atom material into a member by directional
solidification in an open or closed mold/container containing
the material to be solidified.

385. The process of claim 384, wherein the member
fabricated is a plate, rod, tube or any other shape.

386. The process of claim 385, wherein the process is
conducted in a vacuum or controlled atmosphere chamber.

387. The process of any of the preceding claims 384 to
386, further comprising removing oxygen, nitrogen, water


90

vapor, and other possible contaminants are taken before
melting the material.

388. The process of any of the preceding claims 384 to
387, wherein the member made may has shapes selected from a
group consisting of plate, rod, tube or any other shape or
form.

Description

Note: Descriptions are shown in the official language in which they were submitted.



CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
1
Process and Apparatus for Silicon Boat, Silicon Tubing
and Other Silicon Based Member Fabrication
BACKGROUND OF THE INVENTION
Wafer Boats and wafer holders made from high purity
quartz, fused silica or silicon carbide are being used in
silicon and other wafer processing. Some processing is done
in quartz-lined stainless steel chambers. As the device size
becomes smaller the mismatch between the thermal properties
of the silicon wafer, the wafer boat housing the wafer during
various chemical and thermal treatments and the chamber
housing the boat with the wafers becomes a problem.
Particulates are created and the stress imposed on the
wafer during various processing steps affects the yield of
the process. New approach to the process environment is
needed.
SUMMARY OF THE INVENTION
High purity quartz or fused silica is used as material
for various epitaxial reactors, CVD chambers, CVD chamber
liners and/or tubing for processing the wafers. Silicon
boats made from single crystalline silicon only will not have
the desired mechanical properties. Single crystal silicon
considerably softens at 400°C and makes it not suitable for
many high temperature applications. The present invention
provides a solution to those and other problems.
Process and apparatus for various approaches for making
various silicon/silicon alloy members is described below.
Forging, extrusion, plasma and hot substrate powder
deposition, slurry spray and slurry casting, silicon/silicon
alloy casting and directional solidification is described
here in more detail. Other methods modified for silicon
member fabrication may be used for fabrication of the same.
Silicon/Silicon Alloy Powder Pressina/Foraina and Extrusion


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Silicon/Silicon Alloy Powder Pressing/Forging and
Extrusion may be employed for fabrication of various
silicon/silicon alloy members that include, but is not
limited to, wafer boats for horizontal and vertical wafer
processing furnaces and deposition chambers, epitaxial
reactors, lining for CVD, epitaxial reactors and other wafer
processing tools, tubing having any form or cross section
shape.
Silicon/silicon alloy powder is pressed at room
temperature or at an elevated temperature in vacuum or in a
controlled atmosphere. Outgassing, removal of oxygen,
nitrogen, water vapor and removal of other undesired gases
may also be effected before the pressing of the powder. The
powder is pressed to a near shape of the part being
fabricated, or it may be pressed into a raw material for
further processing of the same. The powder consists of
silicon, silicon and germanium, silicon and any metal,
silicon and silicon carbide, silicon and any ceramic, or
silicon and any suitable element or compound.
Silicon powder, silicon based alloys or other suitable
silicon or nonsilicon based materials, and/or composites
having the desired grain size is placed in a pressing
chamber. The compound may or may not contain silicon alloy.-
After proper gas treatment and/or vacuuming the residual gas,
the powder is pressed. The pressing temperature may be as
low as room temperature or as high as the softening point of
the lowest melting point constituent. Such pressed part is
later on sintered in vacuum or appropriate gaseous
atmosphere. Very dense materials having predetermined
hardness results from this process. Knowing that the
fracture strength is inversely proportional to the grain size
(the smaller the grain size the higher the fracture strength)
one may tailor various parts for various applications.
Parts made by this process may be machined before the
sintering (green part machining). After the sintering


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process they are expected to yield near shape and they may be
used as they are or may be subjected to final machining.
Pressures of up to 800,000 psi or higher may be used for
this process. The temperature of the material during
pressing and sintering may vary depending on the composition.
Temperatures between 300°C and 1350°C may be used. Lower
than 300°C and higher than 1350°C may also be used depending
on the material processed and the properties desired.
If press-shaping solid silicon (single crystal or
polycrystalline material) into various parts the silicon is
heated to the desired temperature for the appropriate plastic
properties. The shaping may be done using forging or
extrusion of the silicon/silicon alloy or other alloy
material.
Pressing and shaping of the material may be done before,
during or after the sintering of the material. The
plasticity of the material may determine the grain size and
the fracture strength of the same. Several steps of hot
press process may be employed. For instance, extrusion may
be followed by forging and/or high pressure annealing.
The shaping of the material may be used for imbedding
stronger material in the part itself for reinforcement
purposes. The strong layer may be within the part or may
constitute the outer or inner surface of the part. Parts
having desired strength pattern may be made by this method.
Powder De~aosition
Plasma heated silicon grain is introduced in a chamber
that may be a vacuum, low pressure, normal pressure, medium
pressure, or high-pressure chamber. The so heated powder is
directed towards heated substrate and deposited. The powder
deposition may consist of silicon only, or silicon and other
material particles that might reinforce the silicon structure
without changing the chemical behavior or material particles
that change the properties of silicon and form a silicon


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alloy or solid solution that may or may not contain any
silicon. Ge, SiXGl_x, SiC, other silicon based materials or
ceramics or other suitable elements or compounds that contain
no silicon or silicon alloys may be used for doping,
reinforcement purposes or as main materials for the part
being made. Depending on the temperature of the substrate,
the deposited layers may have different densities and
thicknesses which after sintering results in very dense
material having desired fracture strengths.
Non-plasma heated powder or not heated powder may be
injected in the chamber and directed towards a hot substrate
within heated or non-heated controlled atmosphere or vacuum
chamber. The powder grain is heated to the desired
temperature on its way to the substrate and from the hot
substrate. Such heated grain adheres to the substrate and/or
other previously deposited grains. The density of the
deposited body depends greatly on the grain size, grain
temperature at impact and the substrate temperature.
The silicon/silicon alloy/composite member made may have
any shape: rod, tube having any cross-section and shape, or
any chamber looking type shape where there may be one or more
gates. The substrate may be heated up to the softening point
of silicon. Optimal temperature is expected to be, but not
limited to, between 800°C to 1350°C. Temperatures less than
800°C and more than 1350°C may also be applied.
The sintering of the silicon/silicon alloy/composite
members may be done in situ, or after they have been
machined, shaped or joined with other parts made by the same
or different process. The sintering temperature will greatly
depend on the chemical composition of the parts and their
applications.
rV=position
CVD deposition of any type may be used for deposition of
silicon and/or silicon and other materials that provides for


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reinforcement of the deposited layers without changing the
chemical behavior of the surface of interest. The
silicon/silicon alloy/composite layers may be on suitable
substrate that has sticking coefficient to the deposited
material. Silicon nitrides, graphite, metal silicates, some
ceramics such as SiC and other combinations may be suitable
as substrate for particular applications.
The temperature of the substrate as well as the pressure
of the deposition process may vary depending on the method
used. So deposited layers may have initial thickness that
after sintering results in very dense material having desired
thickness for a particular application. Silicon/silicon
alloy/composite members having shape of rod, tube having
desired cross-section shape and size, plate or any wafer
processing chamber suitable type shape may be made. There
might be one or more gates leading inside the chamber.
Slurry method and apparatus
Mixing the powder with a high purity liquid chemical
compound and forming a slurry for spraying or casting of
desired body may be also be employed. In case of spraying,
the slurry is deposited on a substrate that may rotate or
translate. The substrate may be any material that does not
react with or contaminate the slurry and that can either be
incorporated in the product made or it can be separated after
the removal of the liquid by curing during or after the
deposition of the slurry. Such cured articles can be roughly
machined before the bake-out process. A bake out process is
employed to completely remove the chemical substance (binder)
and to sinter the silicon/silicon alloy/composite powder made
member. Machining of these parts into desired shapes follows
the bake-out process.
The slurry deposition and/or casting may be conducted in
vacuum or controlled gas atmosphere chamber employing one or
more heaters. The curing and sintering may be conducted in


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the same or in a different chamber.
Silicon/silicon alloy members having shapes of rod,
round tube, rectangular tube, plate or any wafer processing
chamber suitable type shape may be made by this approach.
Cantina
Casting to shape of silicon/silicon alloy/composite
grain or re-melting and casting solid silicon may be used for
forming various alloy made parts. A high purity mold made
from easily removable material that does not react with
silicon/silicon alloy/composite is filled with shot, powder
or small chunks of the material to be processed. The
material used for casting may be melted in a separate
container and transferred into the mold after melting. All
appropriate steps for removal of the oxygen, nitrogen, water
vapor, and other possible contaminants are taken before the
processing takes place. The silicon/silicon alloy/ composite
member made may have any shape: rod, round tube, tube or any
other shape or form.
Gelcasting of silicon/silicon alloy/composite material
members
During gelcasting the Silicon/Silicon Alloy/Composite
Material the material is first converted in powder having
desired grain size. The powder is suspended in a monomer
solution which is polymerized in a mold to form a rigid
polymer/solvent gel. Organic or inorganic substances might
be added to the powder/polymer binder to trigger the
polymerization process at desired process conditions such as
temperature, viscosity, etc. The system may contain up to
10-20 weight o polymer. This percentage may be as low as few
weight percent and may be over 20 weight percent. The
solvent portion is removed by drying step after the part is
removed from the mold.
The solution may be aqueous or non-aqueous. Typical


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non-aqueous solution might contain 50-55 volume % of powder
with the balance being the dispersion solution. The solution
may have about 10o dispersant such as Rohm & Haas Triton
X-100, or N-100 Dupont dibasic ester (DBE) or ICI Americas
Solsperse 2000 in dibutil phtalate (DBP) and 90 o gelcasting
premix. The premix might include 10-30 volume o of monomers
such as trifunctional trimethilpropane triacrylate (TMPTA)
and difunctional 1,6 hexanediol diacrilate (HDODA) both from
Hoechst Celanese, 0.5 to 10 volume o of dybenzoil peroxide
initiator with the rest being either DBA, DBP or other
suitable solvent.
The member fabrication may be done by hardening of the
mass in a mold, by spraying onto a substrate having desired
process temperature. The spraying might be vacuum or desired
gaseous atmosphere. The spraying method may consist of
spraying the slurry or spraying the various components onto
the substrate where they mix, react and harden into the
desired shape.
The member fabrication may be by continuous feed onto a
beltline type apparatus. Hardening, drying and even
sintering may be part of the continuous process. The feed
may consist of already made mixture, or mixing it at the
feeding point.
Directional Solidification
Fabrication of large size silicon/silicon
alloys/composite in a plate, rod, tube or any other shape
might be made economical by the use of directional
solidification. The process may be carried out in an open or
closed mold/container containing the material to be
solidified. The process may be conducted in a vacuum or
controlled atmosphere chamber. All appropriate steps for
removal of oxygen, nitrogen, water vapor, and other possible
contaminants are taken before the processing takes place.
The member made may have any shape: plate, rod, tube or any


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other shape or form.
These and further and other objects and features of the
invention are apparent in the disclosure, which includes the
above and ongoing written specification, with the claims and
the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1. Reshaping/Forging silicon/silicon
alloy/composite material.
Figure 2. High temperature vacuum/special gas
atmosphere reshaping/forging silicon/silicon alloy/composite
material.
Figure 3. Extrusion Apparatus with refill hopper.
Figure 4. High temperature vacuum/special gas
atmosphere extrusion apparatus.
Figure 5. Material deposition via powder only and/or
plasma heated powder spray deposition of silicon/silicon
alloy/composite.
Figure 6. Silicon/silicon alloy/composite slurry
deposition
Figure 7. Directional solidification fabrication of
tubing used as a liner or for fabrication of wafer boat.
Figure 8. Solid and shaped tubing for fabrication of
wafer boat.
Figure 9. Semi fabricated silicon/silicon
alloy/composite wafer processing boat.
Figure 10. Semi fabricated wafer processing boat made
from structurally reinforced silicon/silicon alloy/composite
material.
Figure 11. Cross section of the base material for wafer
processing boat made from structurally reinforced
silicon/silicon alloy/composite material.
Figure 12. Schematic diagram for making tubing and
wafer processing fabricates thereof from casting


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silicon/silicon alloy/COmposite powder.
Figure 13. Schematic diagram for making tubing and
wafer processing fabricates thereof by Cold/hot pressing
silicon/silicon alloy/composite powder.
Figure 14. Schematic diagram for making tubing, plate
or rod and wafer processing fabricates thereof from pressing
silicon/silicon alloy/composite powder.
Figure 15. Vertical CVD chamber lined with employing
silicon/silicon alloy/composite material employing
silicon/silicon alloy/COmposite wafer boat.
Figure 16. Mufti-chamber wafer processing system
employing at least one silicon lined chamber and silicon
equipped chamber.
Figure 17. Top and side view of epitaxial/CVD chamber
fabrication process.
Figure 18. Top view of a mufti-chamber wafer processing
system employing at least one silicon made chamber and
silicon equipped chamber.
Figure 19. Side view of a mufti-chamber epitaxial wafer
prooessing system employing at least one silicon made chamber
and silicon equipped chamber.
Figure 20. Germanium - Silicon phase diagram.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring to Figures 1 and 2, powder is forged into body
with a ram 12, anvil 14 and mold 16. In Figure 2, heated
enclosure 20 has a heater 22, a ram heater 24 and an anvil
heater 26. A gas inlet/outlet multiport 27 supplies chamber
20. A vacuum/vent line 29 removes gases.
Forging the monocrystal body uses a temperature between
400°C and near melting point. The temperature may be less
than 400°C or several degrees less than the melting point of
the lowest melting phase in the crystal.
Forging the monocrystal body uses a temperature of


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400°C.
Forging the monocrystal body uses a temperature of
600°C.
Forging the monocrystal body uses a temperature of
800°C.
The forged body 10 is polycrystalline material.
The forged body is amorphous material.
The forged body may be composed of single crystalline
portion and polycrystalline portion and amorphous portion.
The forging is in vacuum, reduced pressure or inert
atmosphere having desired pressure.
The forging is in vacuum, reduced pressure or reactive
atmosphere having desired pressure.
The reactive atmosphere in chamber 20 may be plasma,
reactive gases or solid and process of purification is
administered.
Forging powder for body 10 consists of silicon, silicon
and germanium, SiXGel_X solid solution, silicon and Silicon
Carbide Six (SiC) 1_X, Silicon and silicon dioxide SiX (SiO~) 1_X,
silicon and any ceramic, silicon and any oxide SiX(Oxide)1_X,
silicon and any metal SixM1_X, Silicon and any alloy SixA1_x,
any combination between themselves at temperature equal or
greater than room temperature and lower than the melting
point of one or more constituents of the pressed body RT _< T
_< TM.
The temperature may be 400°C <_ T <_ 800°C.
The temperature may be 200°C _< T <_ 1000°C.
The temperature may be 200°C <_ T <_ 1200°C. The
temperature may be smaller than 200°C or greater than 1200°C.
The forging is in vacuum, reduced pressure or inert
atmosphere having desired pressure.
The forging is in vacuum, reduced pressure or reactive
atmosphere having desired pressure.
The reactive atmosphere may be plasma, reactive gases or
solid and process of purification is administered.


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The powder may be silicon powder or shot having various
grain sizes from sub-micron to rather large shot sizes of
several millimeters or larger.
The powder may be silicon powder and germanium powder or
shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.
The powder may be silicon powder and SiXGel_X (0 <_ x __<1)
powder or shot having various grain sizes from sub-micron to
rather large shot sizes of several millimeters or larger.
The powder may be silicon powder and silicon carbide,
SiX (SiC) 1_X (0 <_ x <_1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
The powder may be silicon powder and silicon dioxide,
SiX(Si02)1_X (0 <_ x <_1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
The powder may be silicon powder and metal, SixMl_.~ (0 <_
x <_1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
The powder may be silicon powder and SiX(Alloy)1_x (0 _< x
<_1) powder or shot having various grain sizes from sub-micron
to rather large shot sizes of several millimeters or larger.
The powder may be silicon powder and/or metal and/or
ceramic and/or alloy and/or oxide and/or any suitable
additive powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
The powder can be any material suitable for the member
fabrication.
The forging apparatus may consist of anvil, mold that
contains the forged body and ram.
Each part may be independently heated.
The forging apparatus may be heated from all sides.


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The forging apparatus may be enclosed fully or partially
in a vacuum, reduced pressure or desired pressure chamber
that may be filled with inert, reactive gas or plasma gas.
Figures 3 and 4 show extruding monocrystal tubular body
30 having a temperature between 400°C and near melting point.
The temperature might be less than 400°C or several degrees
less than the melting point of the lowest melting phase in
the crystal.
Extrusion chamber 32 holds silicon powder 33 which
becomes extruded material 34 delivered by refill hopper 36
from material delivery assembly 37. The extruded body 30 is
forced by piston 38 through a tube shaper 39. A surrounding
chamber 40 has a cooled wall 42 and an internal heater 44, a
gas inlet/outlet multiport 46 and a vacuum/vent line 48.
The material being extruded may be a single crystal,
polycrystalline chunks of material or powder consisting of
silicon/silicon alloy/composite material.
Extruding a monocrystal body uses a temperature of
400°C.
Extruding a monocrystal body uses a temperature of
600°C.
Extruding a monocrystal body uses a temperature of
800°C.
The extruded body is polycrystalline material.
The extruded body is amorphous material.
The extruded body may be composed of single crystalline
portion and polycrystalline portion and amorphous portion.
The extruding is in vacuum, reduced pressure or inert
atmosphere having desired pressure.
The extruding is in vacuum, reduced pressure or reactive
atmosphere having desired pressure.
The reactive atmosphere may be plasma, reactive gases or
solid and a process of purification is administered.
Extruding powder 33 consists of silicon, silicon and
germanium, SixGe1_X solid solution, silicon and Silicon


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Carbide SiX (SiC) 1_X, Silicon and silicon dioxide SiX (SiOZ) 1_~,
silicon and any ceramic, silicon and any oxide SiX(Oxide)1_x.
silicon and any metal Si;~MI_x, Silicon and any alloy SixAl_X,
any combination between themselves~at temperature equal or
greater than room temperature and lower than the melting
point of one or more constituents of the pressed body RT <_ T
<_ TM.
The temperature may be 400°C _< T _< 800°C.
The temperature may be 200°C <_ T _< 1000°C.
The temperature may be 200°C <_ T _< 1200°C. The
temperature may be smaller than 200°C or greater than 1200°C.
The extruding is in vacuum, reduced pressure or inert
atmosphere having desired pressure.
The extruding is in vacuum, reduced pressure or reactive
atmosphere having desired pressure.
The reactive atmosphere may be plasma, reactive gases or
solid and a process of purification is administered.
The powder may be silicon powder or shot having various
grain sizes from sub-micron to rather large shot sizes of
several millimeters or larger.
The powder may be silicon powder and germanium powder or
shot having various grain sizes from sub-micron to rather
large shot sizes of several millimeters or larger.
The powder may be silicon powder and SiXGel-X (0 <_ x <_1)
powder or shot having various grain sizes from sub-micron to
rather large shot sizes of several millimeters or larger.
The powder may be silicon powder and silicon carbide,
SiX(SiC)1-X (0 <_ x <_1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
The powder may be silicon powder and silicon dioxide,
Si,;(SiO~)1-~ (0 < x <_1) powder or shot having various grain
sizes from sub-micron to rather large shot sizes of several
millimeters or larger.
The powder may be silicon powder and metal, SiXMl_x (0 <_


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x __<1) powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
The powder may be silicon powder and Si~(Alloy)1_,; (0 <- x
<_1) powder or shot having various grain sizes from sub-micron
to rather large shot sizes of several millimeters or larger.
The powder may be silicon powder and/or metal and/or
ceramic and/or alloy and/or oxide and/or any suitable
additive powder or shot having various grain sizes from sub-
micron to rather large shot sizes of several millimeters or
larger.
The Extruding apparatus may consist of anvil, mold that
contains the forged body and a ram.
Each part may be independently heated.
The extruding apparatus may be heated from all sides.
The extruding apparatus may be enclosed fully or
partially in a vacuum, reduced pressure or desired pressure
chamber that may be filled with inert, reactive gas or plasma
gas.
Figure 5 shows material deposition on a substrate 50, in
this case a hollow tube from plasma generators or sources 51
supplied by a gas and powder input system 52. Plasma heated
softened particles 53 strike and stick to the substrate and
form layers as they are rotated 54 and translated 55. A
chamber 56 surrounding the deposition is heated 57. Gas
inlet/outlet multiport 58 and vacuum/vent line 59 are
connected to the chamber.
Plasma deposition apparatus 59 consists of one or more
plasma generators or plasma sources, gas input system, powder
input system, vacuum chamber, with or without one or more
chamber heating elements, substrate without heating
elements.
The chamber may have one or more deposition ports.
The substrate may have rotation and/or translation
mechanism.


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The chamber may have rotation and/or translation
mechanisms.
Plasma assisted deposition of powder consisting of
silicon, silicon and germanium, SiXGel_X solid solution,
silicon and Silicon Carbide Six(SiC)~_x, Silicon and silicon
dioxide SiX(SiOz)i-x, silicon and any ceramic, silicon and any
oxide Six (Oxide) 1_X, silicon and any metal SiXMl_X, Silicon and
any alloy SixAl_~, any combination between themselves at
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T <_ TM.
The deposition process occurs under vacuum, reduced
pressure, reactive atmosphere, inert gas, plasma, and any
combinations thereof.
The deposition process is in atmosphere having desired
pressure.
The reactive atmosphere may be plasma, reactive gases or
solid and a process of purification is administered.
The temperature in the chamber may be between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT _< T <_ TM.
The temperature in the chamber may be 400°C _< T <_ 800°C.
The temperature in the chamber may be 200°C _< T _<
1000°C.
The temperature in the chamber may be 200°C <_ T <_
1200°C. The temperature may be smaller than 200°C or greater
than 1200°C.
The temperature of the substrate may be between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T <_ TM.
The temperature of the substrate may be 400°C _< T <_
800°C.
The temperature of the substrate may be 200°C <_ T <_


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1000°C.
The temperature of the substrate may be 200°C _<_ T <
1200°C. The temperature may be smaller than 200°C or greater
than 1200°C.
In Figure 6, substrate 50 is rotated 54. The substrate
or slurry delivery tubes 60 translate 55 sprayer 61 spray
heated powder which is heated an softened by heaters 62.
Deposition apparatus for spraying of powder, powder and
organic or inorganic base material, powder and gaseous
material. The powder may consist of silicon, silicon and
germanium, SixGel_X solid solution, silicon and Silicon
Carbide Si;~(SiC)1_X, silicon carbide, silicon nitride, silicon
oxynitride, any silicon compound, Silicon and silicon dioxide
SiX(SiOz)1_~, silicon and any ceramic, silicon and any oxide
SiX (Oxide) 1_x, silicon and any metal SiXMl_X, Silicon and any
alloy SiXAI_X, any combination between themselves at
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T <_ TM, consisting of a substrate, '
plurality of sprayers positioned to spray at least one
portion of one side, heating elements capable to heat the
substrate at least from one side.
The substrate may be tubular having any cross-section,
planar or have any desired shape or form suitable for the
particular application.
The substrate may be rotated and translated.
The substrate may be heated from inside and/or outside.
The sprayers may be one or more and they may be
oscillated, rotated and translated in relations to themselves
and to the substrate the deposition takes place on.
The apparatus may be enclosed in vacuum, reduced
pressure or any process suitable chamber that may have vacuum
and vent valves and gas delivery system.
The deposition process may be under vacuum, reduced
pressure., reactive gas, inert gas, plasma, and any


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combinations thereof.
The process is in atmosphere having desired pressure.
The reactive atmosphere may be plasma, reactive gases or
solid, and a process of purification is administered.
The temperature in the chamber may be between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T <_ TM.
The temperature in the chamber may be 400°C _< T <_ 800°C.
The temperature in the chamber may be 200°C <_ T <-
1000°C.
The temperature in the chamber may be 200°C <_ T <_
1200°C. The temperature may be smaller than 200°C or greater
than 1200°C.
The temperature of the substrate may be between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T _< TM.
The temperature of the substrate may be 400°C <_ T <-
800°C.
The temperature of the substrate may be 200°C <_ T _<
1000°C.
The temperature of the substrate may be 200°C <_ T _<
1200°C. The temperature may be smaller than 200°C or greater
than 1200°C.
In Figures 7 and 8, a silicon preform 71 is placed in a
heated 72 chamber 73. The preform is rotated 74 and a heated
ring 75 is translation 76 along the preform for sintering
and/or melting the material and forming a solid product.
Apparatus 77 for making tubular members 71 has any cross
section and length and any other desired shape or form
consisting of mold 70 filled with desired material and heater
75 covering part of this mold and a chamber 73 fully or
partially surrounding the member 71 and the heating elements
72. The chamber has a gas inlet/outlet, multiport 78 and a


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vacuum/vent line 79.
The chamber is a vacuum, low pressure or pressure
chamber.
In one embodiment, there is no chamber surrounding the
member and the heating elements.
The member can be rotated and/or translated.
The member can be heated from the inside and/or outside.
The member can be heated from outside by chamber heaters
72 and a zone heater 75 for directional or non-directional
processing.
The chamber has vacuum and/or vent valves 79.
The chamber has a gas inlet/outlet multiport 78.
The chamber has one or more plasma source attached.
The material processed is solid material, powder, powder
and organic or inorganic base material, powder and gaseous
material. The powder may consist of silicon, silicon compound
comprising at least one atom of silicon, silicon and
germanium, SixGel_X solid solution, silicon and Silicon
Carbide Six (SiC) 1_x, Silicon and silicon dioxide Six (SiOz) 1_X,
silicon and any ceramic, silicon and any oxide Six(Oxide)1-x,
silicon and any metal SixMl_x, Silicon and any alloy SixAl_x.
any combination between themselves at temperature equal or
greater than room temperature and lower than the melting
point of one or more constituents of the deposited body RT <_
T <_ TM, consisting of a substrate, plurality of sprayers
positioned to spray at least one portion of one side, heating
elements capable to heat the substrate at least from one
side.
The substrate may be tubular having any cross-section,
planar or have any desired shape or form suitable for the
particular application.
The processing of the material may be under vacuum,
reduced pressure, reactive gas, inert gas, plasma, and any
Combinations thereof.
The processing of the material is in inert atmosphere


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having desired pressure.
The reactive atmosphere may be plasma, reactive gases or
solid, and a process of purification is administered.
The process temperature may be between temperature equal
or greater than room temperature and lower than the melting
point of one or more constituents of the deposited body RT _<
T _< TM.
The process temperature may be 400°C <_ T <_ 800°C.
The process temperature may be 200°C _< T <_ 1000°C.
The process temperature may be 200°C _< T s 1200°C. The
temperature may be smaller than 200°C or greater than 1200°C.
The temperature of the substrate may be between
temperature equal or greater than room temperature and lower
than the melting point of one or more constituents of the
deposited body RT <_ T <_ TM.
The temperature of the substrate may be 400°C <_ T <_
800°C.
The temperature of the substrate may be 200°C <_ T <_
1000°C.
The temperature of the substrate may be 200°C <_ T <_
1200°C. The temperature may be smaller than 200°C or greater
than 1200°C.
The member may be tubular and have any cross section
such as round, elliptical, rectangular, polygonal or any
other shape.
The member may have uneven thickness pattern over its
entire surface.
The member may have different composition and density
over the entire body.
The member may have different composition and density
over its thickness.
The composition and material properties may be layered
over any of the dimensions of the member such as length,
thickness, width, radius, etc.
In Figures 9, 10, 11, 12 and 13, a horizontal or


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vertical wafer processing boat preform 80 has a plurality of
protrusions 81 for fabrication of slots for wafers and
openings for gas flow between the wafers to enable even
thickness deposition.
The wafer boat preform 80 may be made from silicon,
silicon compound, silicon and germanium, SixGel_X solid
solution, silicon and Silicon Carbide Si;~ (SiC) 1_,;, Silicon and
silicon dioxide Six(SiO~)1_x, silicon and any ceramic, silicon
and any oxide SiX (Oxide) 1_x, silicon and any metal SiXM~_X,
Silicon and any alloy SixA1_x, any combination between
themselves, or made from composite material. In all cases 0
x 1.
The wafer boat preform may be made by layering one or
more of the following materials: Si, silicon compound, SixGel_
X, S1C, S1X (S1C) 1_X, SlX (512) 1-xi S1X (~Xlde) 1_X, SlxM1_X, CompOSlte
material, and any combination or order between themselves. In
all cases,0 x 1.
The wafer boat preform may have closed ends by a base
and a top that may be half or full discs having outer
diameters equal or greater than the outer diameter of the
wafer boat.
The end disk might be solid disk or may have certain
portions removed.
The process fabricates wafer boat preforms consisting of
silicon, silicon compound, silicon and germanium, Si;~Gei_X
solid solution, silicon and Silicon Carbide SiX(SiC)1_x,
Silicon and silicon dioxide SiX(Si02)1_X, silicon and any
ceramic, silicon and any oxide Six(Oxide)1-x, silicon and any
metal SiXMl_X, Silicon and any alloy SixAl_x, any combination
between themselves, or made from composite material (in all
Cases 0 <_ x <_1) by heating and melting the boat material
within a mold having desired shape and form, or transferring
it to the mold, solidifying it, cooling it down at a desired
cool-down regime, and machining it to the desired tolerance.
The boat fabrication material is powder.


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The boat fabrication material is solid material.
The melting is done in a vacuum chamber.
The melting is done under reduced or high pressure of
inert or reactive gas.
The reactive gas is mixture between atomic or Charged
molecular state gas such as plasma gas and a neutral inert or
reactive gas.
The sintering and/or melting is preceded by one or more
steps of purging and purification.
Wafer boat preforms consist of silicon, silicon
compound, silicon and germanium, SixGel_x solid solution,
silicon and Silicon Carbide SiX(SiC)1_X, Silicon and silicon
dioxide Six(Si02)1_~, silicon and any ceramic, silicon and any
oxide SiX (Oxide) 1_,;, silicon and any metal SiXMl_x, Silicon and
any alloy SiXAl_x, any combination between themselves, or made
from composite material (in -all cases 0 _< x _<1) by pressing
the boat material within a die having desired shape and form,
sintering, cooling it down at a desired cool-down regime, and
machining it to the desired tolerance. The boat fabrication
material is powder. The boat fabrication material is solid
material. The pressing is done in a vacuum chamber. The
pressing is done under reduced or high pressure of inert or
reactive gas. The reactive gas is mixture between atomic or
charged molecular state gas such as plasma gas and a neutral
inert or reactive gas.
The melting is preceded by one or more steps of purging
and purification.
The process fabricates wafer boat preforms consisting of
silicon, silicon compound, silicon and germanium, SiXGe1_X
solid solution, silicon and Silicon Carbide SiX(SiC)1_,~,
Silicon and silicon dioxide Si~ (SiO~) 1_X, silicon and any
ceramic, silicon and any oxide SiX(Oxide)1_X, silicon and any
metal SiXMl_x, Silicon and any alloy SiXA1_x, any combination
between themselves, or made from composite material (in all
cases 0 <_ x __<1) by extruding the boat material within a die


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having desired shape and form, sintering, Cooling it down at
a desired cool-down regime, and machining it to the desired
tolerance. The boat fabrication material is powder. The
boat fabrication material is powder mixed with organic or
inorganic material, or the boat fabrication material is solid
material. The pressing is done in a vacuum Chamber. The
pressing is done under reduced or high pressure of inert or
reactive gas. The reactive gas is mixture between atomic or
charged molecular state gas such as plasma gas and a neutral
inert or reactive gas. The melting is preceded by one or
more steps of purging and purification.
The invention provides processes for fabrication of
member having shape of tube, plate, rod or any other shape
Consisting of silicon, silicon compound including but not
limited to SiN, Si~N4, SiON, and/or the like, silicon and
germanium, SiXGel_X solid solution, silicon and Silicon
Carbide Six (Sic) 1_X, Silicon and silicon dioxide SiX (Si02) i-:~,
silicon and any Ceramic, silicon and any oxide SiX(Oxide)1-X.
silicon and any metal SixMl_X, Silicon and any alloy SixAl_X,
any combination between themselves, or made from composite
material (in all cases 0 <_ x <_1) by heating and melting the
member material within a mold having desired shape and form,
or transferring it to the mold, solidifying it, Cooling it
down at a desired cool-down regime, and machining it to the
desired tolerance. The member fabrication material is
powder, or the member fabrication material is solid material.
The process is done in a reduced pressure chamber.
The melting is done under reduced or high pressure of
inert or reactive gas. The reactive gas is mixture between
atomic or Charged molecular state gas such as plasma gas and
a neutral inert or reactive gas. The melting is preceded by
one or more steps of purging and purification.
The new process provides for fabrication of members
having shape of tube, plate, rod or any other shape
consisting of silicon, silicon and germanium, Sl~Ge1_x solid


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23
solution, silicon and Silicon Carbide SiX(SiC)1_x, Silicon and
silicon dioxide SiX(Si02)1_x, silicon and any ceramic, silicon
and any oxide Si,; (Oxide) 1_;i, silicon and any metal SixM1_x,
Silicon and any alloy SiXAl_X, any combination between
themselves, or made from composite material (in all cases 0 <_
x <_1) by pressing the member material within a die having
desired shape and form, sintering, cooling it down at a
desired cool-down regime, and machining it to the desired
tolerance. The member fabrication material is powder, or the
member fabrication material is solid material. The pressing
is done in a vacuum Chamber. The pressing is done under
reduced or high pressure of inert or reactive gas.
The reactive gas is mixture between atomic or charged
molecular state gas such as plasma gas and a neutral inert or
reactive gas. The melting is preceded by one or more steps
of purging and purification.
The new process provides for fabrication of member
having shape of tube, plate, rod or any other shape
consisting of silicon, silicon compound including but not
limited to SiN, Si3N9, SiON, and/or the like, silicon and
germanium, Si~Gel_X solid solution, silicon and Silicon
Carbide Si;~ (SiC) 1_X, Silicon and silicon dioxide Six (Si02) i-,;,
silicon and any ceramic, silicon and any oxide Six(Oxide)1_X,
silicon and any metal SixMl-X, Silicon and any alloy SixAl_X,
any combination between themselves, or made from Composite
material (in all cases 0 <_ x <_1) by extruding the member
material within a die having desired shape and form,
sintering, cooling it down at a desired cool-down regime, and
machining it to the desired tolerance.
The member fabrication material is powder.
The member fabrication material is powder mixed with
organic or inorganic material.
The member fabrication material is solid material.
The pressing is done in a vacuum chamber.
The pressing is done under reduced,or high pressure of


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24
inert and/or reactive gas.
The reactive gas is mixture between atomic or charged
molecular state gas such as plasma gas and a neutral inert or
reactive gas.
The sintering may be preceded by one or more steps of
purging and purification.
The melting is preceded by one or more steps of purging
and purification. -
The material may be made only by sintering and without
melting.
The process cuts the preform or solidified boat 80 in
two along medial lines 82. Openings 83 are formed in the
cylindrical walls 84. Deposited material 85 is coated and
fused on top of base material 86. Two boats 87 result. The
powder 85 is melted 88 or molded 89, or hot pressed 90 and
sintered 91. Finally slots 92 are formed in the inward ribs
or extensions 81. Ends 93 of boats 87 may have complementary
steps to connect boats end-to-end in an axial stack or row.
Figure 14 shows steps of beginning with a powder or
solid 101, heating 103 to a plastic slate and forming 105 a
tube, plate or rod. A chamber liner 107 is formed and
applied to a process chamber 109, forming a chemical vapor
deposition (CVD) station 111. Formed tubes 105 are halved
lengthwise. Windows are cut 113. Inward ribs or extensions
or the inner walls are slotted 115, forming a vertical boat
117. In parallel steps, windows are cut 113. The boat is
plotted 115 and a horizontal boat 119 is formed.
In Figure 15, wafer processing apparatus 120 consists of
a process chamber 121, wafer handling tools, wafer boat
handling tools 123, 124, consisting of one or more processing
Chambers 127, 128, shields 125 and enclosures 129 employing
one or more members consisting of silicon, silicon and
germanium, Si~Gel_X solid solution, silicon and Silicon
Carbide SiX (SiC) 1_X, Silicon and silicon dioxide Si,; (SiOa) 1_x,
silicon and any ceramic, silicon and any oxide SiX(Oxide)1-X,


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silicon and any metal SixM1_X, Silicon and any alloy SiXA1_X,
any combination between themselves, or made from composite
material (in all cases 0 _< x <_1). Each chamber may be
equipped with separate or common gas delivery and venting
system 130, vacuum system 131, internal or external heating
elements 133, cooled or not cooled vacuum shell 135,
partially or fully lined with silicon, silicon and germanium,
SixGel_h solid solution, silicon and Silicon Carbide SiX (SiC) 1_
X; Silicon and silicon dioxide Six(Si02)i-X, silicon and any
ceramic, silicon and any oxide SiX(Oxide)1_x, silicon and any
metal SiXMl_x, Silicon and any alloy SiXAl_X, any combination
between themselves, or made from composite material (in all
cases 0 <_ x <_1) .
At least one of the processing chambers may be a CVD
chamber employing one or more members consisting of silicon,
silicon and germanium, SiXGel_~ solid solution, silicon and
Silicon Carbide SiX(SiC)1_x, Silicon and silicon dioxide
SiX(Si02)1_x, silicon and any ceramic, silicon and any oxide
SiX (Oxide) 1_X, silicon and any metal SixM1_X, Silicon and any
alloy Si~A1_x, any combination between themselves, or made
from composite material (in all cases 0 <_ x <_1). The CVD
chamber may be equipped with separate or common gas delivery
and venting system, vacuum system, internal or external
heating elements, cooled or not cooled vacuum shell partially
or fully lined with silicon, silicon and germanium, SiXGel_X
solid solution, silicon and Silicon Carbide Six(SiC)1_,~,
Silicon and silicon dioxide SiX(Si02)1_X, silicon and any
ceramic, silicon and any oxide Six(Oxide)1_x, silicon and any
metal SixMl_x, Silicon and any alloy SiXAl_X, any combination
between themselves, or made from composite material (in all
cases 0 _<< x _<1).
At least one of the processing chambers may be an
epitaxial chamber employing one or more members consisting of
silicon, silicon and germanium, SixGel_X solid solution,
silicon and Silicon Carbide Si~(SiC)1_#, Silicon and silicon


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dioxide SiX(SiOz)1_X, silicon and any ceramic, silicon and any
oxide Six (Oxide) 1_X, silicon and any metal SixM1_X, Silicon and
any alloy SiXAl_x, any combination between themselves, or made
from composite material (in all cases 0 <_ x __<1). The
epitaxial chamber may be equipped with separate or common gas
delivery and venting system, vacuum system, internal or
external heating elements, cooled or not cooled vacuum shell
partially or fully lined with silicon, silicon and germanium,
SiXGel_X solid solution, silicon and Silicon Carbide SiX (SiC) 1_
X, Silicon and silicon dioxide SiX(Si02)1_x, silicon and any
ceramic, silicon and any oxide SiX(Oxide)1_X, silicon and any
metal SiXMl-X, Silicon and any alloy SiXA~_X, any combination
between themselves, or made from composite material (in all
cases 0 <_ x <_1) .
At least one of the processing chambers may be a thin
film deposition chamber employing one or more members
consisting of silicon, silicon and germanium, SihGel_x solid
solution, silicon and Silicon Carbide SiX(SiC)1_~, Silicon and
silicon dioxide Six(Si02)1_,~, silicon and any ceramic, silicon
and any oxide SiX (Oxide) 1_x, silicon and any metal SiXMl_R,
Silicon and any alloy Si~Al_;~, any combination between
themselves, or made from composite material (in all cases 0 <_
x <_1). The thin film deposition chamber may be equipped with
separate or common gas delivery and venting system,'vacuum
system, internal or external heating elements, cooled or not
cooled vacuum shell partially or fully lined with silicon,
silicon and germanium, SiXGel_;~ solid solution, silicon and
Silicon Carbide Six(SiC)1_X, Silicon and silicon dioxide
SiX(Si02)1-X. silicon and any ceramic, silicon and any oxide
SiX (Oxide) 1_x, silicon and any metal SixMl_X, Silicon and any
alloy SiXA1_X, any combination between themselves, or made
from composite material (in all oases 0 _< x <_1).
At least one of the processing chambers may thin film
removal chamber employing one or more members consisting of
silicon, silicon and germanium, SiXGe1-x solid solution,


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silicon and Silicon Carbide Six(SiC)1-x, Silicon and silicon
dioxide Six(Si02)1-x, silicon and any ceramic, silicon and
any oxide Six (Oxide) 1_x, silicon and any metal SiXMl_X, Silicon
and any alloy SixAl_x, any combination between themselves, or
made from composite material (in all cases 0 <_ x __<1). The
thin film removal chamber may be equipped with separate or
common gas delivery and venting system, vacuum system,
internal or external heating elements, cooled or not cooled
vacuum shell partially or fully lined with silicon, silicon
and germanium, SiXGel_X solid solution, silicon and Silicon
Carbide Six (SiC) 1_x, Silicon and silicon dioxide Six (Si02) i-X,
silicon and any ceramic, silicon and any oxide Six(Oxide)1-x.
silicon and any metal SixMl_x, Silicon and any alloy SixAl_x,
any combination between themselves, or made from composite
material (in all cases 0 _< x __<1).
One of the chambers may be a main chamber connected with
other chambers directly or via one or more gate valves.
One or more chambers may be vacuum, low pressure or
desired pressure chamber.
One or more chambers may have at least one internal or
external heater.
One or more chambers may have at least one partial or
complete heat shield.
Wafer processing apparatus employing at least one CVD
chamber employing one or more members consisting of silicon,
silicon and germanium, SixGe1_x solid solution, silicon and
Silicon Carbide Six(SiC)1_x, Silicon and silicon dioxide
Six(Si02)1_x, silicon and any ceramic, silicon and any oxide
Six (Oxide) 1_x, silicon and any metal SixM1_x, Silicon and any
alloy SixAl_{, any combination between themselves, or made
from composite material (in all cases 0 <_ x <_1). The CVD
chamber may be equipped with separate or common gas delivery
and venting system, vacuum system, internal or external
heating elements, cooled or not cooled vacuum shell partially
or fully lined with silicon, silicon and germanium, SixGel_x


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solid solution, silicon and Silicon Carbide Six(SiC)1_X.
Silicon and silicon dioxide SiX(SiO2y-X, silicon and any
ceramic, silicon and any oxide Six(Oxide)1_X, silicon and any
metal SiXM1_X, Silicon and any alloy SixAl_X, any combination
between themselves, or made from composite material (in all
cases 0 <_ x <_1).
At least one CVD chamber may be connected with other
chambers or with a main wafer distribution chamber directly
or via one or more gate valves.
At least one CVD chamber may be vacuum, low pressure or
desired pressure chamber.
At least one CVD chamber may have at least one internal
or external heater.
At least one CVD chamber may have at least one partial
or complete heat shield.
Wafer processing apparatus employing at least one
epitaxial chamber employing one or more members consisting of
silicon, silicon and germanium, SixGel_X solid solution,
silicon and Silicon Carbide Six(SiC)1_x, Silicon and silicon
dioxide Si~(SiO~)1_X, silicon and any ceramic, silicon and any
oxide SiX (Oxide) 1_x, silicon and any metal SixMl_x, Silicon and
any alloy SiXAl_,,, any combination between themselves, or made
from composite material (in all cases 0 <_ x __<1). The
epitaxial chamber may be equipped with separate or common gas
delivery and venting system, vacuum system, internal or
external heating elements, cooled or not cooled vacuum shell
partially or fully lined with silicon, silicon and germanium,
SiXGel_~ solid solution, silicon and Silicon Carbide SiX(SiC)1_
Silicon and silicon dioxide SiX(Si02)1_~, silicon and any
ceramic, silicon and any oxide Six(Oxide)1_X, silicon and any
metal Si~Ml_X, Silicon and any alloy SixAl_X, any combination
between themselves, or made from composite material (in all
cases 0 s x <_1.
At least one epitaxial chamber may be connected with
other chambers or with a main wafer distribution chamber


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29
directly or via one or more gate valves.
At least one epitaxial chamber may be vacuum, low
pressure or desired pressure chamber.
At least one epitaxial chamber may have at least one
internal or external heater.
At least one epitaxial chamber may have at least one
partial or complete heat shield.
Wafer processing apparatus employing at least one thin
film deposition chamber employing one or more members
consisting of silicon, silicon and germanium, SixGel_X solid
solution, silicon and Silicon Carbide SiX(SiC)1_X, Silicon and
silicon dioxide SiX(SiOz)1_X, silicon and any ceramic, silicon
and any oxide Six (Oxide) 1_x, -silicon and any metal SlxM1_x,
Silicon and any alloy SixAl_x, any combination between
themselves, or made from composite material (in all cases 0 _<
x __<1). The thin film deposition chamber may be equipped with
separate or common gas delivery and venting system, vacuum
system, internal or external heating elements, cooled or not
cooled vacuum shell partially or fully lined with silicon,
silicon and germanium, SixGe1_x solid solution, silicon and
Silicon Carbide Six(SiC)1_x, Silicon and silicon dioxide
Six(Si02)i-x. silicon and any ceramic, silicon and any oxide
Six (Oxide) 1_x, silicon and any metal SixMl_x, Silicon and any
alloy SixAl_x, any combination between themselves, or made
from composite material (in all cases 0 <_ x __<1).
At least one thin film deposition chamber may be
connected with other chambers or with a main wafer
distribution chamber directly or via one or more gate valves.
At least one thin film deposition chamber may be vacuum,
low pressure or desired pressure chamber.
At least one thin film deposition chamber may have at
least one internal or external heater.
At least one thin film deposition chamber may have at
least one partial or complete heat shield.
Wafer processing apparatus employing at least one thin


CA 02460996 2004-03-19
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film removal chamber employing one or more members consisting
of silicon, silicon and germanium, SixGel_~ solid solution,
silicon and Silicon Carbide SiX(SiC)1_x, Silicon and silicon
dioxide SiX(SiOz)i-x, silicon and any ceramic, silicon and any
oxide SiR (Oxide) 1_X, silicon and any metal SiXMl_X, Silicon and
any alloy SiXA1_X, any combination between themselves, or made
from composite material (in all cases 0 _< x <_1). The thin
film removal chamber may be equipped with separate or common
gas delivery and venting system, vacuum system, internal or
external heating elements, cooled or not cooled vacuum shell
partially or fully lined with silicon, silicon and germanium,
SixGe~_x solid solution, silicon and Silicon Carbide SiX (SiC) 1_
X, Silicon and silicon dioxide SiX(Si02)1_x, silicon and any
ceramic, silicon and any oxide SiX(Oxide)i_X, silicon and any
metal SiXM1_X, Silicon and any alloy SixAl_x, any combination
between themselves, or made from composite material (in all
oases 0 <_ x <_1).
At least one thin film removal chamber may be connected
with other chambers or with a main wafer distribution chamber
directly or via one or more gate valves.
At least one thin film removal chamber may be vacuum,
low pressure or desired pressure chamber.
At least one thin film removal chamber may have at least
one internal or external heater.
At least one thin film removal chamber may have at least
one partial or complete heat shield.
A chemical vapor deposition (CVD) system consisting of
a vacuum vessel with cooled or not cooled chamber with single
or double wall, a robot handling arm having appropriate
elements for wafer or wafer boat delivery/removal that forms
a vacuum tight seal when the chamber is loaded, a wafer
tray/boat containing one or more wafers resting on the wafer
boat delivery/removal arm, a shield surrounding the wafer
tray/boat and the inside portion of the wafer handling arm,
process gas delivery system with all appropriate valves


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attached to the chamber and having an delivery tube extending
into wafer area, inert gas delivery system with all
appropriate valves attached to the chamber and having an
delivery tube with or without diffuser extending into wafer
area, vacuum pumping system connected to the chamber, inside
or outside heater directing heat into the process area
employing one or more members consisting of silicon, silicon
and germanium, SiXGe1_:.s solid solution, silicon and Silicon
Carbide SiX (SiC) 1_X, Silicon and silicon dioxide SiX (Si02) i-X,
silicon and any ceramic, silicon and any oxide Si;~ (Oxide) 1_;~,
silicon and any metal SixMl_X, Silicon and any alloy SiXAl_X,
any combination between themselves, or made from composite
material (in all cases 0 _< x <_1.
The CVD system may be vertical, horizontal or have any
suitable position from -90 to +90.
The wafer boat may be solid connected members made from
silicon, silicon and germanium, SixGel_~ solid solution,
silicon and Silicon Carbide Six(SiC)1_X, Silicon and silicon
dioxide SiX(Si~2y-X. silicon and any ceramic, silicon and any
oxide Si;~ (Oxide) 1_x, silicon and any metal SiXMl_X, Silicon and
any alloy SiXAl_X, any combination between themselves, or made
from composite material (in all cases 0 <_ x <_1).
The wafer boat may be modular elements made from
silicon, silicon and germanium, SixGel_X solid solution,
silicon and Silicon Carbide Six(SiC)1_X, Silicon and silicon
dioxide SiX(SiOL)1_X, silicon and any ceramic, silicon and any
oxide Si,~ (Oxide) 1_X, silicon and any metal SiXM1_X, Silicon and
any alloy SiXAl_X, any combination between themselves, or made
from composite material (in all cases 0 s x <_1).
The wafer boat may contain one or more slots for wafers
support spaced at appropriate distance.
The wafers in the boat may be positioned so there is no
other material between the wafers other than vacuum or any
gas present in the processing part of the chamber.
The wafer boat may have slots for the wafer support and


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susceptors between the wafers for improved temperature
distribution over the wafer surface that results in more
uniform deposited layer thickness and composition.
The susceptor in boat may part of the wafer boat.
The susceptor in boat may be inserted after the boat has
been made or prior to or together with the wafer loading.
The boat may be modular.
Each module of the boat may contain support for one or
more wafers.
Each module may contain support for one or more wafers
separated by inserted or built in susceptors.
The susceptor may be full body or may have certain cuts
to allow wafer only insertion/removal handling.
The boat may be made from modular parts connected via
chemical or mechanical bonding.
The boat may have round, elliptical, polygonal or any
other applicable cross section.
The boat may have one or more elements at each end for
mechanical strength during handling.
The end parts of the boat may be modules.
All parts of the boat may be made from same or different
materials.
In Figure 16, a single wafer processing system 150 for
CVD, epitaxial deposition, thin film deposition/removal or
any other wafer processing the chip requires system consists
of a vacuum vessel 151 with cooled or not cooled chamber wall
153 with single or double wall 155, connected directly 157 or
through at least one gate valve 159 to a chamber 160 with
multistage wafer handling mechanism 161 for wafer
delivery/removal, a shield 163 surrounding the wafer
processing area, process and inert gas delivery system 165
with all appropriate valves 167 attached to the chamber 160
and having an delivery tube 169 extending into wafer area,
vacuum pumping system 170 connected to the chamber 160,
inside and/or outside heater directing heat into the process


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area employing one or more members consisting of silicon,
silicon and germanium, SiXGe1_X solid solution, silicon and
Silicon Carbide Six(SiC)1_X, Silicon and silicon dioxide
Six(Si02)i_,;, silicon and any ceramic, silicon and any oxide
SiX (Oxide) 1_X, silicon and any metal SiXMl_X, Silicon and any
alloy SiXAl_X, any combination between themselves, or made
from composite material (in all cases <_ x _< 1).
Similar vacuum pumping systems 170 and gas delivery
systems 167 may be used with both chambers. Heating elements
171 may be located around or in the chambers 151 and 160.
Chamber connection ports 173 are provided to connect chamber
160 to additional chambers for transferring or removing the
wafers .
The process chamber may be a CVD chamber.
The process chamber may be an epitaxial deposition
chamber.
The process chamber may be a thin film
deposition/removal chamber.
The process chamber may be any wafer process chamber.
The chamber may have any cross section and height and
the system may be vertical, horizontal or have any suitable
position from -90 to +90.
The members are made from silicon, silicon and
germanium, SiXGe1_X solid solution, silicon and Silicon
Carbide SiX (SiC) 1_x, Silicon and silicon dioxide SiX (SiO~) 1-x,
silicon and any ceramic, silicon and any oxide Six(Oxide)1_X,
silicon and any metal Si~M1_,~, Silicon and any alloy SiXAl_X,
any combination between themselves, or made from composite
material (in all cases 0 <_ x <_1) and may be solidly connected
by means of chemical or mechanical bonding.
The members are made from silicon, silicon and
germanium, SiXGel_X solid solution, silicon and Silicon
Carbide SiX (SiC) 1_X, Silicon and silicon dioxide Six.(Si02) 1-X,
silicon and any ceramic, silicon and any oxide Six(Oxide)1-X.
silicon and any metal SixMs_x, Silicon and any alloy SixAl_X,


CA 02460996 2004-03-19
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34
any combination between themselves, or made from composite
material (in all cases 0 <_ x <_1) and may be modular.
The members are made from silicon, silicon and
germanium, SiXGel_X solid solution, silicon and Silicon
Carbide Six (SiC) 1_x, Silicon and silicon dioxide Six (SiO~) 1_,,,
silicon -and any ceramic, silicon and any oxide Six(Oxide)1-x,
silicon and any metal SiXMl_X, Silicon and any alloy SiXA1_X,
any combination between themselves, or made from composite
material (in all cases 0 <_ x <_1) and may contain one or more
slots for wafers' support to optimize the process.
The wafer processing chamber may have a susceptor next
to the wafer for improved temperature distribution over the
wafer surface that results in more uniform deposited layer
thickness and composition.
The susceptor in the process chamber may be part of the
chamber.
The wafer delivery arm may be made in full or partially
from silicon, silicon and germanium, SixGel_X solid solution,
silicon and Silicon Carbide SiX(SiC)1_x, Silicon and silicon
dioxide Si~(Si02)1_X, silicon and any ceramic, silicon and any
oxide Six (Oxide) 1_x, silicon and any metal SiXMl_X, Silicon and
any alloy SixAl_x, any combination between themselves, or made
from composite material (in all cases 0 <_ x <_1)
The susceptor may be full body or may have certain cuts
to allow wafer only insertion/removal handling.
The chamber parts may be made in full or partially from
silicon, silicon and germanium, SixGel_x solid solution,
silicon and Silicon Carbide Six(SiC)1_x, Silicon and silicon
dioxide Six(SiQz)1_x, silicon and any ceramic, silicon and any
oxide Six (Oxide) 1_x, silicon and any metal SixMl_x, Silicon and
any alloy SixA1_x, any combination between themselves, or made
from composite material (in all cases 0 _< x <_1) and they may
be made from modular parts connected via chemical or
mechanical bonding or by assembling them without bonding.
The chamber may have round, elliptical, polygonal or any


CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
other applicable cross section.
The end parts of the wafer processing chamber may be
modules. All parts of the boat may be made from the same or
different materials.
Figure 17-19 show epitaxial/CVD chambers 175 made in
full or partially from silicon, silicon and germanium, SixGel_
X solid solution, silicon and Silicon Carbide SiX(SiC)1_x,
Silicon and silicon dioxide SiX (SiOz)~_x, silicon and any
ceramic, silicon and any oxide Si,;(Oxide)1_;~, silicon and any
metal SiXM1_x, Silicon and any alloy SiXAl_x, any combination
between themselves, or made from composite material (in all
cases 0 _< x <_1) having a body 177, 179, an optical window 180
for wafer radiation and at least one opening 181 for wafer
and gas delivery/removal. The bodies are bonded together
along side edges 183 forming the chamber 175. A wafer heater
185 accesses wafers in chamber 175 through one window 180. A
wafer lifting and rotating mechanism port a~'~.d assembly 187
supports wafers through the opposite window.
Epitaxial chambers have suitable wall thickness and at
least one infrared window at each side, hollow interior and
at least one gate opening for connection to a wafer supply
and process gas supply chamber and a gas exhaust is made from
silicon, silicon and germanium, SiXGel_X solid solution,
silicon and Silicon Carbide SiX(SiC)1_X, Silicon and silicon
dioxide SiX (Si02) 1-.::. silicon and any ceramic, silicon and any
oxide SiX (Oxide) 1_X, silicon and any metal Si~_Ml-x, Silicon and
any alloy Si,;AI_X, any combination between themselves, or made
from composite material (in all cases 0 <_ x <_1).
The epitaxial chamber body may comprise of a single body
made by pressing of material, machining it from inside and
out in its green state, purifying the said body at a certain
temperature by immersing it in a chemically reactive gas,
plasma or liquid for certain period of time, sintering the
said body at appropriate temperature determined by its
Composition, final machining of the said body, if needed, to


CA 02460996 2004-03-19
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36
meet the specifications of the epitaxial deposition process.
The finished body may be subjected to thin film deposition
such as chemical vapor deposition, plasma enhanced
deposition, or other suitable deposition method for better
finish on the inside and outside.
The epitaxial chamber body may comprise of a single body
made by casting of the material, machining it from inside and
out in its green state, purifying the said body at a certain
temperature by immersing it in a chemically reactive gas,
plasma or liquid for certain period of time, sintering the
said body at appropriate temperature determined by its
composition, final machining of the said body, if needed, to
meet the specifications of the epitaxial deposition process.
The finished body may be subjected to thin film deposition
such as chemical vapor deposition, plasma enhanced
deposition, or other suitable deposition method for better
finish on the inside and outside.
The epitaxial chamber may comprise of upper and lower
part made by casting to shape the material, machining the
parts, purifying the said body at a certain temperature by
immersing it in a chemically reactive gas, plasma or liquid
for certain period of time, sintering the said body at
appropriate temperature determined by its composition,
joining the parts by chemical and/or mechanical means, final
machining of the said body, if needed, to meet the
specifications of the epitaxial deposition process. The
finished body may be subjected to thin film deposition such
as chemical vapor deposition, plasma enhanced deposition, or
other suitable deposition method for better finish on the
inside and outside.
The epitaxial chamber may comprise of upper and lower
part made by cold or hot pressing to shape to shape the
material, machining the parts, purifying the said body at a
certain temperature by immersing it in a chemically reactive
gas, plasma or liquid for certain period of time, sintering


CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
37
the said body at appropriate temperature determined by its
composition, joining the parts by chemical and/or mechanical
means, final machining of the said body, if needed, to meet
the specifications of the epitaxial deposition process. The
finished body may be subjected to thin film deposition such
as Chemical vapor deposition, plasma enhanced deposition, or
other suitable deposition method for better finish on the
inside and outside.
The epitaxial Chamber may Comprise of upper and lower
part made by cold or hot pressing of a block of the material,
machining the chamber, purifying the said body at a certain
temperature by immersing it in a chemically reactive gas,
plasma or liquid for Certain period of time, sintering the
said body at appropriate temperature determined by its
composition, joining the parts by chemical and/or mechanical
means, final machining of the said body, if needed, to meet
the specifications of the epitaxial deposition process. The
finished body may be subjected to thin film deposition such
as Chemical vapor deposition, plasma enhanced deposition, or
other suitable deposition method for better finish on the
inside and outside.
The epitaxial chamber may comprise of upper and lower
part made by cold or hot extrusion of a block or a desired
shape of the material, machining the chamber, purifying the
said body at a certain temperature by immersing it in a
chemically reactive gas, plasma or liquid for certain period
of time, sintering the said body at appropriate temperature
determined by its composition, joining the parts by chemical
and/or mechanical means, final machining of the said body, if
needed, to meet the specifications of the epitaxial
deposition process. The finished body may be subjected to
thin film deposition such as chemical vapor deposition,
plasma enhanced deposition, or other suitable deposition
method for better finish on the inside and outside.
The epitaxial Chamber may comprise of upper and lower


CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
38
part made by plasma spraying of the material, and forming a
chamber to a desired shape, machining the chamber, purifying
the said body at a certain temperature by immersing it in a
chemically reactive gas, plasma or liquid for certain period
of time, sintering the said body at appropriate temperature
determined by its composition, joining the parts by chemical
and/or mechanical means, final machining of the said body, if
needed, to meet the specifications of the epitaxial
deposition process. The finished body may be subjected to
thin film deposition such as chemical vapor deposition,
plasma enhanced deposition, or other suitable deposition
method for better finish on the inside and outside.
The epitaxial chamber may comprise of upper and lower
part made by spraying of organic or inorganic based slurry of
the material and forming a chamber to a desired shape,
machining the chamber, purifying the said body at a certain
temperature by immersing it in a chemically reactive gas,
plasma or liquid for certain period of time, sintering the
said body at appropriate temperature determined by its
composition, joining the parts by chemical and/or mechanical
means, final machining of the said body, if needed, to meet
the specifications of the epitaxial deposition process. The.
ffinished body may be subjected to thin film deposition such
as chemical vapor deposition, plasma enhanced deposition, or
other suitable deposition method for better finish on the
inside and outside.
The chamber comprises two separate halves joined at one
plane followed by final machining.
The chamber comprises a single body machined from a
solid block material.
The chamber comprises a single body made by method of
plasma spraying followed by final machining.
The chamber comprises a single body made by method of
slurry spraying
The chamber comprises a single body machined by method


CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
39
of casting, forging or extrusion followed by final machining.
The chamber may be a vacuum, reduced pressure or desired
pressure chamber.
The chamber may have a liner for a vacuum, reduced
pressure or desired pressure chamber for wafer processing
applications.
The chamber may be modular pieces stacked on top of each
other or bonded by mechanical or chemical means.
The optical window may be from same or suitable material
stacked on the chamber or bonded by mechanical or chemical
means.
The chamber may have one or more optical windows
depending on the process requirements.
Gas delivery system 167 for delivering process and inert
gases into the chamber may attached to the chamber or to the
chamber wall.
The gas delivery members exposed to the process
atmosphere may be made from the chamber material or chamber
lining material.
The wafer delivering/removing arm to/from the chamber
may be made from the chamber material or chamber lining
material.
The susceptor and any other member that either holds the
wafer, surround the wafer from the sides, the top or the
bottom, as required by the process may be made from the
chamber material or chamber lining material.
Reduced pressure chamber surrounds epitaxial /CVD
chamber made in full or partially from silicon, silicon and
germanium, SiXGe1_~ solid solution, silicon and Silicon
Carbide SiX (SiC) 1_,;, Silicon and silicon dioxide SiX (Si02) 1_X,
silicon and any ceramic, silicon and any oxide Six(Oxide)1_X,
silicon and any metal SiXMl_X, Silicon and any alloy SixAl_x.
any combination between themselves, or made from composite
material (in all cases 0 <_ x <_1) having a body, an optical
window for wafer radiation and at least one opening for wafer


CA 02460996 2004-03-19
WO 03/024876 PCT/US02/29516
and gas delivery/removal.
The outer chamber may be vacuum, reduced pressure or
desired pressure as required by the process.
The chamber may have one or more optical windows
depending on the process requirements.
The chamber may have gas delivery system for delivering
process and inert gases into the chamber may attached to the
chamber or to the chamber wall.
A single wafer processing system for CVD, epitaxial
deposition, thin film deposition/removal or any other wafer
processing the chip requires system consists of a vacuum
vessel with cooled or not cooled chamber wall with single or
double wall, connected directly or through at least one gate
valve to a chamber with multistage wafer handling mechanism
for wafer delivery/removal, a shield surrounding the wafer
processing area, process and inert gas delivery system with
all appropriate valves attached to the chamber and having an
delivery tube extending into wafer area, vacuum pumping
system connected to the chamber, inside and/or outside heater
directing heat into the process area employing one or more
members consisting of silicon, silicon and germanium, SixGel_x
solid solution, silicon and Silicon Carbide Si;~ (SiC) 1-x,
Silicon and silicon dioxide Six(Si02)i-x. silicon and any
ceramic, silicon and any oxide Sih(Oxide)1_X, silicon and any
metal Si~Ml_~, Silicon and any alloy SiXAl_x, any combination
between themselves, or made from composite material (in all
cases 0 <_ x <_1), employing at least one epitaxial chamber
made by the method described herein.
While the invention has been described with reference to
specific embodiments, modifications and variations of the
invention may be constructed without departing from the scope
of the invention, which is defined in the following claims.

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Administrative Status , Maintenance Fee  and Payment History  should be consulted.

Administrative Status

Title Date
Forecasted Issue Date Unavailable
(86) PCT Filing Date 2002-09-19
(87) PCT Publication Date 2003-03-27
(85) National Entry 2004-03-19
Dead Application 2005-09-19

Abandonment History

Abandonment Date Reason Reinstatement Date
2004-09-20 FAILURE TO PAY APPLICATION MAINTENANCE FEE
2005-06-22 FAILURE TO RESPOND TO OFFICE LETTER

Payment History

Fee Type Anniversary Year Due Date Amount Paid Paid Date
Application Fee $200.00 2004-03-19
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
PANDELISEV, KIRIL A.
Past Owners on Record
None
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Claims 2004-03-19 50 2,514
Abstract 2004-03-19 2 69
Drawings 2004-03-19 20 357
Description 2004-03-19 40 2,062
Representative Drawing 2004-03-19 1 15
Cover Page 2004-05-18 2 51
PCT 2004-03-19 3 91
Assignment 2004-03-19 5 121
Correspondence 2004-05-14 1 28