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Sommaire du brevet 2248622 

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Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Demande de brevet: (11) CA 2248622
(54) Titre français: APPAREIL DE BIOLISTIQUE SERVANT A INJECTER DES SUBSTANCES DANS DES CELLULES OU DES TISSUS
(54) Titre anglais: BIOLISTIC APPARATUS FOR DELIVERING SUBSTANCES INTO CELLS AND TISSUES
Statut: Réputée abandonnée et au-delà du délai pour le rétablissement - en attente de la réponse à l’avis de communication rejetée
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • C12M 1/00 (2006.01)
  • A61M 37/00 (2006.01)
  • C12M 3/00 (2006.01)
  • C12N 15/87 (2006.01)
  • F16K 21/00 (2006.01)
(72) Inventeurs :
  • SANFORD, JOHN (Etats-Unis d'Amérique)
  • CELESTE, JOE (Etats-Unis d'Amérique)
  • LOOMIS, DALE (Etats-Unis d'Amérique)
(73) Titulaires :
  • JOHN SANFORD
  • JOE CELESTE
  • DALE LOOMIS
(71) Demandeurs :
  • JOHN SANFORD (Etats-Unis d'Amérique)
  • JOE CELESTE (Etats-Unis d'Amérique)
  • DALE LOOMIS (Etats-Unis d'Amérique)
(74) Agent: MOFFAT & CO.
(74) Co-agent:
(45) Délivré:
(22) Date de dépôt: 1998-09-23
(41) Mise à la disponibilité du public: 1999-03-23
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
60/059,771 (Etats-Unis d'Amérique) 1997-09-23

Abrégés

Abrégé français

Appareil de biolistique comportant un boîtier doté d'une membrane porteuse située dans une chambre de manière à se déplacer par rapport à une plaque de sortie comprenant plusieurs orifices. La membrane porte plusieurs micro-particules adhérant à sa surface à proximité des orifices pour être diffusées dans des cellules ou des tissus. Plusieurs membranes rupturables espacées sont fixées à la membrane porteuse. Dans un premier temps, un vide est créé à l'intérieur de l'ensemble, y compris dans l'orifice de sortie, pour faire évacuer tout gaz indésirable de l'appareil. De l'hélium sous haute pression est ensuite envoyé sur les membranes rupturables et, lorsque la pression atteint un niveau prédéterminé, les membranes se rompent, ce qui fait en sorte qu'un front de choc généré par l'hélium sous haute pression est forcé contre la membrane porteuse : les particules sont ainsi éjectées par les orifices de sortie.


Abrégé anglais


A biolistic apparatus is provided with a housing having
a carrier membrane disposed in a chamber for movement relative
to an outlet plate having a plurality of apertures therein.
The carrier membrane has a plurality of micro-particles
adhered thereto on the surface of the membrane adjacent the
apertures for delivery into cells or tissue. A plurality of
rupturable membranes are mounted in spaced relation to the
carrier membrane. Initially, a vacuum is provided within the
assembly including the outlet opening to purge the apparatus
of any undesirable gasses. High pressure helium is then
delivered to the rupturable membranes and upon reaching a
predetermined pressure, will cause the membranes to rupture
allowing a shock front of high pressure helium to strike the
carrier membrane and impel the articles through the outlet
openings.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


16
WHAT IS CLAIMED IS:
1. An apparatus for delivering micro-projectiles into
cells or tissue comprising:
a hollow cylindrical housing,
a nozzle assembly secured to one end of said housing and
including a plate having a plurality of through passages,
an annular ring slidably mounted in said nozzle,
a carrier membrane for carrying micro-projectiles
disposed between said annular ring and said plate,
a piston coaxially disposed in said housing in radial
spaced relation thereto and having a central bore extending
coaxially through said piston,
one end of said piston having a pressure chamber therein
and a flange disposed about said chamber,
support means mounting said piston for axial sliding
movement relative to said housing,
a plurality of burst membranes disposed between said
flange and said annular ring,
an opposite end of said piston having a radially
extending flange,
pressure means for applying pressure to said flange for
moving said piston to clamp said burst membranes against said
ring and for applying pressure to said burst membranes whereby
upon rupture of said burst membranes a surge of high pressure
will engage said carrier membrane to impel said micro-projectiles

17
outwardly of said nozzle assembly through said
passage in said plate.
2. An apparatus as set forth in claim 1, wherein said
carrier membrane is mounted for movement relative to said
plate, said plate having a peripheral flange with a plurality
of radially extending grooves whereby upon application of
pressure to said carrier membrane said carrier membrane will
be moved into engagement with said flange to close said
grooves.
3. An apparatus as set forth in claim 2, further
comprising a plurality of axially extending passages in said
annular ring disposed in communication with said grooves in
said plate in the absence of pressure being applied to said
carrier membrane and disposed in communication with an annular
space between said housing and said piston and means for
connecting said annular space to a vacuum source to provide a
vacuum in said passages of said plate when said nozzle
assembly is disposed in contact with tissue.
4. An apparatus as set forth in claim 3, further
comprising an end cap secured to an opposite end of said
housing and having vacuum and pressure connecting means
therein.
5. An apparatus as set forth in claim 1, wherein said
pressure chamber in said one end of said piston has a length
to width ratio of approximately 1:1 and is provided with a
substantially hemispherical configuration.

18
6. A biolistic device which effectively but gently
accelerates micro-projectiles into intact cells or tissues
such as skin comprising:
a gas shock generator,
a fixed, malleable membrane between the gas shock and the
target,
a shaped stopping surfaced for controlled de-acceleration
of the distending membrane, immediately separating the fixed
membrane and the target, and
apertures in the stopping surface which allow transport
of high speed micro-projectiles from the surface of the fixed
membrane into the target.
7. A high pressure fast valve, which effectively
contains high pressure until desired and which then opens
essentially instantaneously or sufficiently rapidly as to
crease an explosive gas shock, comprising:
either a permanent or electro-magnet with a smooth, flat,
magnetically active surface and a smooth, flat, magnetically
responsive surface which surfaces, when coupled, effectively
seal a valve,
a valve assembly which directs the force of the above
stated magnetic coupling in direct opposition to either high
pressure gas or liquid, and
explosive release of the gas or liquid is achieved either

19
when the pressure of the gas or liquid exceeds the strength of
the magnetic closure force or when the magnetic filed is
disrupted.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


CA 02248622 1998-09-23
1 PATE ~ 7UPP~ICA~IO~
8TIC APP~UURT~ FOR DB~IV~ING 8~nT2~N~
I2rrO CE~L~ 7~nD TI8B~E8
RP~T.~Il'~n aPPT.TCP.TION
Applicant~ claim priority bQnefits of provisional
S applicat~on 60/059771 filed September 23, 1997 under 35 USC
ll9(e)
BACKGRO~NP OF T~ L~ ON
The present invention i~ directed to a biolistic device
for accelerating mî~ro-projectiles into intact cellsi or
tissue6. More specifîcally, the pre~ent invention is airected
to a biolistic devîce having a ga~ shock gen~rator ~or
applying a gas 6hoc~ to a ~ixed carrier mRmbrane to di~end
the membrane and separate micro-projectile~ from the sur~ce
of the membrane at high ~ipeeds into th~ target cell~ or
tissue~: ~
For medical application~, a biolistic ~evice muGt hAve
~everal characteristics including sa~ety, r~producibility,
ease of use, n~n-trauma for the pat~ent and -;ni ~1 injury to
the bombarded tissue. At the same time, maximum partiale
dispersion, maximum particle velocity ~nd ~ 1 skin
pene~ration are nee~ed. Existing bioli~ic devices need
1s lmprovement in ter~ of aelivery~ Rfficacy, reproducibility,
gentleness and ease o~ u~e. Many o~ the prior art de~ice~
make a loud nois~ which can be frightening and impact ~he s~n
; ' ' , . ~ ,,.' . . . _
~; . : i!'-,"
.
. ~ . . , ! ' . ',i ' ' . ~ ..

CA 02248622 1998-09-23
2 P~TENT ~ P~ICATIO~
With a violerlt ~;hock wave o~ helium ga~;. Prior art
configuration~; utilizinS~ a "flying disk" has ~:hot to ~;hot
variation and ~ubj ect~ the ~kin to a viol~nt ghock wave and
~oes not achieve as much dispersal or penetration as might be
de~ired.
~UMM~RY OF T~E T~V~N~ION
The present inv~ntion provid~s a new and impr~ed
biolistic ~pparatus for injecting particles into cell~ and
ti~sue~ whi~h i~ extrQmely ~afe, ea~y to use, highly
reproducible, makes es~entially no noise, i~ painle~ and
cause~ minimal trauma to the bombarded ~kin~
~he device according to the present i~vention ha6 ~een
shown to re~ult in better particle di~pe~al, deeper ~kin
penetration and h~gher sub~equent biolog~cal activitie~.
The pre~ent invention provide~ a new and improved
bioli~tic device which effectively but gently accelerates
micro-pro~ectiles into intact cell~ or ti~ues ~uch a~ ~kin
compris~ng a gas shock generator, a fixed malleable membrane
between the gas shock and the targ~t, a ~hap~d ~topping
BUrface dispo~ed betw~3en thQ fix~3d m-3mbran~ and the target for
controlled decslQrzltion of the di~tending membrane ana
aper~ures in the ~topping ~urface which allow the tran~port of
high 6peed micro-pro~ectile~ from the surface of the fi~ed
membrane into the target.
The presen~ in~ention provides a new and improvea
bioli~tic device ~or acceleratlng micro-projectiles into

CA 02248622 1998-09-23
3 PA~E ~ APP~I ~ TION
intact cell8 or ti~ue~ wh~ch utilize~ a gas shock generator
comprised o~ a plurality of bur~t membrane~ which are clampea
together upon ini~ial ~pplication of p~es~ure and w$11
~ubstantially, simultan~o~sly burst when the pre66ure appl~ed
thereto reach~s a predetermined value ~hereby relea6ing the
ga~ under pressure ~ub~antially instantaneously to create a
~hock wavQ for contacting a carrier membrane and impaling the
mic~o-particles thereon into a target~
The pre~ent invention pro~ides ~ new ana improved
bioli~tic device for accelerating micro-pro~ectiles into
i~tact cells or ti~sue~ compri~ing a ga~ ~hock generator
including a ~agnetically controlled valve which i6 held ~:hut
by magnetic force until pres~ure being applied thereto i~
~uf~icient to ~reak the magnetic ~eal at which point the
magnetic seal suddenly collapse~ and the ~alve open~ whereby
a ~hock wave is projected again~t a de~ormable carrier
membrane to impel th~ micro-par~icle~ thereon into the cell~
or ti6~ue~.
The above and other object~, ~eatur~s and advantages of
the pre~ent invention will be more apparent and more readily
appreclated ~rom the following detailed de~cription o~
pre~erred ex~mplary embodiment o~ th~ pre~ent invention, taken
in connection with t~e accompanying drawingG.
~IEF DE8CRIPTTON ~F ~B DRAUING~
;. :.'. ;; .' :. .
: ' i ' , . ' . : ~' . ...
.,: - . . , ' ~, ~ .
: ..... . .
. .
, . . .

CA 02248622 1998-09-23
~ PA~ ~ A~PLIC~TIO~
Fig. 1 is a 3ide el~3vation view of a bioliE;tic devic~3,
partly in section and partly brokQn away, for accelerating
m~cro-projectiles into intact cells or tis~ues.
Fig. 2 i~ a sectional vlew of thQ houqing of the device
S 6hown in ~ig. 1.
Fig. 3 i~ a sectiona~ vie.w of the piston assembly which
exterld~: through said housing in concentric relation thereto.
Fig. 4 is a sectional vi~w o~ the nozzle body as s~own in
Fig~ 1.
Fig~ 5 is a sectional vi~w of the coupler ~hown in Fig.
1 between the bursti~le membranes and the carrier membrane
with ga~ flow pa~ages shown in phantom llne~.
Fig. 6 i~; a rear end view of the coupler ~hown in Fig. 5.
Fig. 7 i~ a front end vlew of the coupler shown in Fig.
5.
Fig. 8 is a sectional ViQW of a supporting ring ~or the
coupler a~ ~hown in Pig. 1.
Fig. 9 i~ a front end view of the support ring as ~ho~m
in Fig. 8.
Fig. 10 is an ena view o~ a ~upport ring for ~upporting
the forward end of the piston as~embly.
Fig. ~1 is a side elevation vi~w of the 6upport ring
shown in Fig. 10.
Fig. 12 i~ a 6ectional view o~ the nozzle outlet plate as
shown in Fig. 1.
Fig. 13 i~ a rear elevational view the~eof.
!'., . : . ,

-
CA 02248622 1998-09-23
PATEN~ APPLICATION
E'~g. 14 i8 a :~ront elsvational view thereof~. --
Fig. 15 i~ a sectional view of the retaining ring ~ecursd
in the opposite end o~ the hou~ing ~rom the nozzle body
Fig. 16 is a rear elevational view thereof.
Fig. 17 i~ a ~ront elevational view ther~of.
~ig. 18 is a sec~ional view of the pres~ure ch. ~r
securea to the retainer rlng at the rear end of the housing.
Fig. 19 ~ a rear elQvational view ther~of.
Fig. 20 is a front elevational view th~reof.
Fig~ 21 is a s~ctional view of the end cap ~ecured to the
pres~ure cham~er member.
~ig. 22 iG a rear elevational view ther~of.
~ig. 23 i~ a front ele~ational ~iew th~r~of.
Fig. 24 i~ a ~ectional view of a magn~tica;ly con~olled
ga~ pre~sure valvQ according to a ~econd embodiment of the
invention.
DET~TT.~D D~CR~PTIQN OF TEE l~v~lON
The app~ratus of the pre~ent invention i~ shown in
a~6embled form in Figure 1 and i~; compriged o~ a hollow,
cylindr~cal housing 20 having internal threads 22 and 24 at
opposite ends thereof. An ~longated plE:ton as~embly Z6 is
mounted ln ~he hollow, cylindrical housing 20 concentrically
thereo~. The piston assembly 26 i8 ~upport~d at it~ forw~rd
end ~ mean~ o~ an annular member 28 (Fig. 10~ di~po~d 1n
threaded engagement ~ith the thread~ 24 of the hou6ing. The
annular ~e~ber ~8 is provided with a plurality o~ radially,

CA 02248622 1998-09-23
6 PA~E ~ ~ ~lCA~ION
inwardly directed projection~ 30 having ~nner end~ 32 di~po~ed
on a circle having a diameter equal to the diameter of the
p~e~ure chamber 34 at the forward end o~ the pi~ton a~embly.
A plurality of cut out portion~ 36 are located between each
S pro;ection 30 to provide communication between the ahnular
chamber 38 located between the pi~ton a~sembly 26 and thQ
hou~ing ~0 and the interior o~ the nozzle a~sembly 40.
The nozzle as~embly 40 (~ig~. 4-9 and 14) i~ comprised of
a nozzle ~ody 42 having an externally threaded hub portion 44
di~po~ed in threaded engagement with the thread6 24 ~t the
forward end o~ the housing 20. The oppo~te end of the nozzle
body 42 is provided with a circular opening 46 which rec~ives
a nozzls outlet plate 48. ~he nozzle outlet plate 48 i8
pro~ided with a larger diameter flange portion 50 adapted to
engag~ the internal ~urface of an annular ~lang~ 52 formed on
the nozzlQ body 4z. A smaller diameter central portion 54
having a plurality of through passages 56 is located within
the opening 46 in the end of th~ nozzle body 42. An O ri~g 58
18 disposed in a groove on the internal fac~ of the flange ~2
to eeal the nozzle outle~ plate to the nozzle body 4Z. The
internal ~:urface of the nozzle outle~ plate 48 i8 prov~ded
with a recess 60 and the flange 50 i~ provided with four
groo~e~ 62 equally ~paced apart.
An annular coupler 64 i~ mounted in the no~zle body
ad~acent the nozzle o~let plate 48 by mean~ of an annular
ring 66 c~f delrin material. The ~orward end of the ~;u~port
, ~: , . ~ ' - ,
' .. r ~ ' .
.

CA 02248622 1998-09-23
7 ~T~ ~ ~iePLICATION
ring 66 is provid~d with ~our axially extending flange
portion~ 68 ~guall~ spac~d about the circumference of the ring
to de~ine gap~ 70 therebetween. The forward end of the
coupler 64 is provided with a recQ~ 72 ha~ing a trape~oidal
cros~ ~ection with the ~maller base ~f the trapezoid ha~ing a
diameter equal to the diameter of the axially extending
central passage 76 of the coupler 64. A plurality of axially
ext~ndi~g bores 74 are equally ~paced about the central
pasgage 76 to provide communication between the rece~s 72 and
the rearward ~urface of the eoupler.
The rearward ~urface 78 of the coupler is provided wi~h
an enlarged rec~3~3s 80 which i5 concentric with the axial bore
76 ~xtending through the coupler. The pres~ure chamber 34 of
the plston assembly 26 i~ provided wi~h a forwardly ext~n~ng
flange 82 with an annular crown 84 on the fo~ward end thereof.
The flange 82 is dimens~oned to clo~ely ~it within the reces~
80 in the coupler membe~. The pressure chamber portion 34 is
provided with a ~ub~antially hemispherical pre sure chamber
86 which merge~ into a cyl~ndrical pasgage 88 extending
through the flange 82 and having a diameter idQntical to the
diameter of th~ bore 76 extending through the coupler 64. A
plurality o~ kapton membranes 90 having an ex~ernal diameter
~ub~tantially ~ual to the diameter o~ the recess 80 in the
coupler, are disposed in the recess 80 for engagement by ~he
Z5 crown 84 on thQ forward end o~ the flange S2 on the pre~sure
ch~ ~cr member 34. ~he n~mber o~ membrane~ 90 may vary

CA 02248622 1998-09-23
~ ~aT~NT ~PPLICATIO~
depending upon thQ d~sired strength sinc~ the plurality of
mem}~ran~s ar~ ad~pted to bur~;t ~rhen the desired pre~;sure i6
rsachea in the pres6ure chamber 86. A sinyle ~tronger carrier
membrane 92 having a diamet~r e~ual to the diam~t~r of the
nozzle outlet plate flange S0 is disposed between the ~lange
~ 50 and the coupler with ~ufficient play ~o allow co~munication
between the through pas~agQs ~6~ ths rece-~sed portion 60, the
rRcessea portion 7~ and the annular chamber 38 in the ab~ence
of pre~surQ being applie~ to the membrane 92 in the forward
direct1on.
Th~ piston assembly ~6 ha~ an axially extending bore 96
e~tending the ~ull length of the piston as~embly i~
communication with the pres~;ure ~h~ h~t~ 86 and a cylindrical
reces~ 98 at ~he oppo~ite end thereof. ~he piston assembly 26
i~ provided with a cylindrical hub portion 100 ha~ing ~ larger
diameter than the elongated body 102 o~ the pis~on assQmbly.
At the end of the pi~ton assembly, an enlarged flange l04 i~
provided adjac~nt the hub portion 100.
Adjacent the rRarward end of the housing 20, a retaining
ring 106 having es~ternal thread6 108 thereon, i8 threaded into
- Qngagement w~ th the int~rnal thread~ 22 of the housing 20.
The retaining ring 106 is provided with an axially extending
rece~;E: 110 at thl3 forwar~ ena thereof having a plurallty c~f
rad~ally directed passages 112 extending ou~war~ly to the
threads }08. The retaining ring 106 is al30 pro~ided with a
reduced diametPr bore 114 in which the hub portion 100 of the
: !
. . . . ~ . , .

CA 02248622 1998-09-23
9 PATE ~ ~ PLICATION
piston as3embly 26 i~ ~lidably mounted. A pre~ure chamber
memb~r 120 is provided with a forwardly ex~n~ing recess 122
having an int:-3rnally threaded portion 124 which i6 threaded
onto the external thread~ o~ the retaining ring 106. The
enlarged diame~er end portion 104 of the pi~ton asse~bly 26 i~
disposed in a reces~ 123 in the rearward portion of th~
retaining ring 1-6 and is ~xposed to pr~urQ in the reces~
122 o~ the pressure chamb~r m~mber. Th~ preggure chamber
m~mber 120 is al~o provided with a plurality o~ ~hrough bor~
126 disposed adjacent the periphery o~ the pres~re member
lZ0. A central ~ore 128 is prov~de~ for ln~r~duclng pres~ure
into the pre~ure chamber and a plurality of threaded pa~ages
130 are provided about the central bore ~28 for the reception
of connecting member~.
An end cap 140 is ~cur~d to the rQarward end of ~he
pres~ure chamber member 120 by mean~ o~ cap scrQws (not shown)
extending through three bore~ 142 wh~ch are in alignment with
the threade~ pa~gages 130 in the prsssure chamber member. The
rear end of the end cap i~ pro~ided with an ~xt~rnally
threaaed nozzle 144 which is adapted to be connected to a
~uitable vacuum gource and a high prQ~Ure helium ~ource (not
shown) The end cap i~ provid~d with a rece~s 146 ~n the
forward end thereof ha~ing ~ tr~pezoidal cro~ section with
the rece~ in ~v lnication with the inlet passage 148
ext~n~ng through the nozzle 144.
':" ' , ' ' ' . ~' ', ' . '

CA 02248622 1998-09-23
10 PATENrr ~ PLIC~IO~
In the operation o~ the app~rat~ according to the
present inv~ntion, th~i forward end o~ ~he nozzle body 40 i~
pres~ed again~t the ti~su~ to be inoculated with particleis
6uch as genetic material~ Since th~ foxward ~urface of ~he
r~ozzle outlet plate 54 i8 recesssd rQl~tiv~ to thR nozzle body
as be~t ~een in FigurQ 1, a thin chamber is formed in
communication with the pa~age~ 56 through which th~ particles
are ejected. A vacuum i~ applied to th~ ~ntir~ assQmbly by
connecting t~e nozzle 144 to a ~uitabl~ vacuu~ ~ource through
valve m~ans ~not ~hown). 'rhe vacuum i8 applied through the
axial pa!3sagQ 148 of the nozzle 144, the rec~ 8 146 in the ~sind
cap and the annular cbamber 38 by means o~ the connecting
pa~sage~ 126. Th~ vacuum i~ al~o applied ~o the passag~s ~6
in the outlet pl~te 54 as well a~ the outèr surSac~ of the
outlet plate 54 through the reces~ 60 in the outlet plate 4~,
the pa~sage~ 74 ext~nding through the coupler 64 to the
annular chamber 38 through the opsnings 36 in the annular
support membQr 28, 5ince the carrier membranQ 92 is mounted
' ~th ~uf~icient play, it is po~ible for the vacuum to be
applied around the periphery of the carrier membran~ through
the grooves 62 in the flange of th~ ou~let plate. By applying
the vacuum to the system, the atmospheric ~a~ses, as ~ell a~
any residual heli~m ~e~ ~rom a pr~vioug usage, a~e removed
fxom the vacuum body a~ well as remo~ing any stray gas from
the high ~res~ure chamber and the line~ ~upplying the
accelerator. Thus, dur~ng a ~ubsequent Q~ ~ction opeiration,
''" '~1''' ' ~
..... j. . , ~ .
. S, . . i ~ , s, j~ ", , . ~ = =

CA 02248622 1998-09-23
11 ~A~E ~ ~ PLIC~TIO~
only helium ga~ will be in the high pre~sure Gha~ber 86 rather
than the u6ual mix of a~r and helium gas.
A~t~3r sufJ~icient vac~um ~ introduced, a vac~ ;en60r
(not 6ho~n) will initiate the introduction o~ prQs~urized
hellum ga~ through the nozzle 144~ The pre~surized heli~m ga~
will act on the enlarged end portion 104 of the pi~ton
assembly 26 to ~hift the pi~ton a~embly 26 axially to brlng
the crown 84 on the flange 82 of the pi~ton ~6emb1y 26 in~o
clamping engagement with ~he bur~t membrane~ go by clamping
the burst membranes 90 a~ain~t the bottom of the enlarged
r~cess 80 in t~e rear ~ur$ace o~ the ~ouple~. The pressurized
h~lium gas will also enter through the rece~6 98 in the
rearward end of the pi6ton a6~e~bly ana the elongated through
p~ssage 26 to the pre~6ure chamber 86. The pre~ure will ramp
up in t~s high pressure chamber 86 un~11 it reache~ the yield
pre~sure o~ the burst membrane~ 90. The membrane system can
consist of ~ny d~ired number of membranes~ For example, the
mem~rane ~ystem may con~ist of ~.0~2" (2 mil) kapton membran
~r di6k~. Each disk would have a bur~t pre~sure of
approximately 400 psi. ~s the pre~ure reache~ the yield
point of the kapton group, one of the membranes will bur~t,
rapidly followed by the ~:econd, third and fourth. ~heln the
~ourth membrane y~eld~, t~e pressure against it i~ ~our times
itQ burst point.
The ga~ chamb~r or high pre~u~e chamber 86 is designed
l:o allow an energy ef~icient gas front to reach the captivated
, ' ~ ;' ! , . ~; '
,'i, !,
!, . ~ ,

CA 02248622 1998-09-23
12 ~ATE~r lLPP~IC~hTIO~
membr~ne. The gas chamber i~ de~igned with a l~ngth to width
(aspect ratio) of approximately 1:1. The spherical rear ~hape
of the high pre~ure chamber recover~ some of the energy lo~t
when the membranes initially yield. The length o~ the chamber
is optimized to create the most efficiQnt pressure front with
the leas~ amount o~ exces~ ga~. ~hi~ allows a smaller vacuum
body to be de~igned, a6 le~ total volume ~f helium gas has to
be controlled. A~ the pre~ure front advance~, it accelerates
th~ captive carrier membrane which i~ al~o made of kapton
material. The carrisr membr~ne 1~ hal~ed abruptly as it ~tops
again~t the flange o~ the outlet plate an~ clo~e~ tho grooves
62. The p~rticle~ adhered to th~ ~ur~ac~ o~ the carrier
membranes, ~uch as generlc material, leave thQ carri~r
membrane a~ it ~uddenly de~orms into the rece~ 60 and fly
through the hole~ in the ~topping plate to enter the target
t:i~8u~. ~he rece~;f3 60 in the nozzlQ outlet plate 48 allow~
the carrîer membrane to deform outwardly without ruptur~ng.
However, under c:~rtain circum~tances, it may be desirable to
have the carrier membrane also rupture.
By contai~ing the carrier membranQ in tact, the ~orce of
the ga~: bla~ will not reach the tis~3uQ, thQreby eliminati~g
pre~3sure tr~uma to the t~su~. Force o~ the high pr~3s!3ure
helium can be dissipated rearwardly through the pa~sages 74 in
the coupler into the large annular chamber 38, which i~ ~till
und~r vacuum.
. . . ,; ! .~ ; .
.

CA 02248622 l998-09-23
13 ~AT~ ~ APPLICA~IO~
T~e actual ~light di~tance of the carrier menibrane i~
reduced fro~n many centimeter~ in prior art ~;tructure~: to far
lesG than one centinleter and the target i~: di~po~;ed in
substantially inti~ate contact with the ~topping plate. The
carrier m~mbrane so act~ a~ a one way valve ina~much a~
previou~ly allowed a vacuum to be introduc~d to the target but
which is ~eale~ aga~n~t the outlet plate to prevent the gas
front from getting ~n front of the carrier membrane and
di~rupting the fligh~ characteri~tice of the genetic materia~.
Accor~ing to a second embodiment of the pre~ent
invention, a magnetically controlled v~lve may ~e u~ili2ed ln
lieu of the rupturablQ membrane~ of the f ir~ embodiment
whereby repeatabi~ity can be enhanced without the need ~or
replacing the ruptured me~brane~. The valve, as shown in Pig.
24, would ~till b~ used with the carrier membrane as ~hown in
the previous embo~i ~nt.
A housing lS0 is provided with a rece~s having a valve
body 152 secured therein by mea~s of a threaded connection
154. Th~ valve body 152 i~ provid~d with a valve opening 156
having an annular valve ~eat 158 extending outwardly from a
valve chamber 160 def~ned between the housing and the valve
bc ~ly . A neodymium magnet 162 is moun~ed in a rece~ in the
hous~ng 150 with a ma~or ~urface th~reo~ expo~ed to the
interior o~ the valve chamber 160. An iron or ~teel plunger
164 is mounted in ~he val~e chamber 160 and is provided with
a E;tem 168 which extends through the valve opening lS6 and is

CA 02248622 1998-09-23
1~ PATE~rr ~ PLIC~ O~
provided with an enlarged head 166~ An O rlng 170 having a
diamet~r equal to the diameter of the valve seat 158 is
mounted in a groove 172 having a trapezoidal cro~6 section to
as~i~t in ret~ining the 0 ring within the groove under
E:tre~6~ul condition6.
In operation, the plunger i6 dratm int:o engagement:~rith
the magnet, whereby the o ring will be moved into ~ealing
engaqement with the valve ~eat. High pre~ure ga~ i~
introduced into the valve c~amber through a g~G line 17Z. The
high pressure ga~ ~ill~ the valv~ chamber 160 in contact with
opposite ~urface~ of the main body of the plunger and upon
reaching a pred~termined pre~ure, wit~ cause ~e p~unqeL t~
separat~ from the magnet. Once the plunger leave~ contact
with the magnet, the holding force will be substantially
reduced and the plunger will move do~nwardly a~ viewed in Fig.
Z4 to relea~e the gas within th~ ch~ ~r with an explosive
force creating a 8hock wave which will strike the carr~er
membrane to inject the particles adherin~ to the opposite
~urface of the membrane into cell~ or ti~sue. once the
pressure drops within the val~e chamber 160, the force of the
magnet will retract the plunger into contact with the magnet
and seal the valve opening by mean~ of the 0 ring 170.
Suitable bumper~ 176 are pro~ided on opposite sides of the
' ''' ''.''"'''~ ,
. .
. . !
,

CA 02248622 1998-09-23
15 PAT~r ~iPPLICATION
plung~r plate to cu~;h~on the impact of ~ e plunger plate
~gainst the housing and the valve boay.
The entire di6clo~ure o~ the provisional applicatlon upon
which pr~ority is claimed, i~ hereby incorpor~ted into the
present appl~ation by reference.
. While the invent~on ha~ been particularly ~hown and
described with reference to preferred embodi.ments thereof, it
will be und~rstood by those in ~he art that the foregoing ~nd
other chang~s in form and aetails may be ma~e therein without
departing from the ~pirit and scope of the invention~
, ' ' ., ! ~ . ,
. ,'. ' ,., ', ",'.'"' "' '-' ',. ' . , .
. . ' ,; . .;, it " , '
" ',r~ ',' ~' . :

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Le délai pour l'annulation est expiré 2004-09-23
Demande non rétablie avant l'échéance 2004-09-23
Inactive : Abandon.-RE+surtaxe impayées-Corr envoyée 2003-09-23
Réputée abandonnée - omission de répondre à un avis sur les taxes pour le maintien en état 2003-09-23
Inactive : Grandeur de l'entité changée 2002-09-17
Demande publiée (accessible au public) 1999-03-23
Inactive : CIB attribuée 1998-12-10
Inactive : CIB attribuée 1998-12-07
Inactive : CIB attribuée 1998-12-04
Inactive : CIB en 1re position 1998-12-04
Symbole de classement modifié 1998-12-04
Inactive : CIB attribuée 1998-12-04
Inactive : CIB attribuée 1998-12-04
Inactive : Certificat de dépôt - Sans RE (Anglais) 1998-11-10
Exigences de dépôt - jugé conforme 1998-11-10
Demande reçue - nationale ordinaire 1998-11-06

Historique d'abandonnement

Date d'abandonnement Raison Date de rétablissement
2003-09-23

Taxes périodiques

Le dernier paiement a été reçu le 2002-09-03

Avis : Si le paiement en totalité n'a pas été reçu au plus tard à la date indiquée, une taxe supplémentaire peut être imposée, soit une des taxes suivantes :

  • taxe de rétablissement ;
  • taxe pour paiement en souffrance ; ou
  • taxe additionnelle pour le renversement d'une péremption réputée.

Veuillez vous référer à la page web des taxes sur les brevets de l'OPIC pour voir tous les montants actuels des taxes.

Historique des taxes

Type de taxes Anniversaire Échéance Date payée
Taxe pour le dépôt - petite 1998-09-23
TM (demande, 2e anniv.) - petite 02 2000-09-25 2000-09-15
TM (demande, 3e anniv.) - petite 03 2001-09-24 2001-09-05
TM (demande, 4e anniv.) - générale 04 2002-09-23 2002-09-03
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
JOHN SANFORD
JOE CELESTE
DALE LOOMIS
Titulaires antérieures au dossier
S.O.
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
Documents

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Liste des documents de brevet publiés et non publiés sur la BDBC .

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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Dessin représentatif 1999-04-19 1 16
Abrégé 1998-09-23 1 28
Description 1998-09-23 15 620
Revendications 1998-09-23 4 125
Dessins 1998-09-23 7 165
Page couverture 1999-04-19 1 66
Certificat de dépôt (anglais) 1998-11-10 1 163
Rappel de taxe de maintien due 2000-05-24 1 111
Rappel - requête d'examen 2003-05-26 1 113
Courtoisie - Lettre d'abandon (taxe de maintien en état) 2003-11-18 1 176
Courtoisie - Lettre d'abandon (requête d'examen) 2003-12-02 1 167
Taxes 2001-09-05 1 37
Taxes 2000-09-15 1 36
Taxes 2002-09-03 1 41