Language selection

Search

Patent 2350840 Summary

Third-party information liability

Some of the information on this Web page has been provided by external sources. The Government of Canada is not responsible for the accuracy, reliability or currency of the information supplied by external sources. Users wishing to rely upon this information should consult directly with the source of the information. Content provided by external sources is not subject to official languages, privacy and accessibility requirements.

Claims and Abstract availability

Any discrepancies in the text and image of the Claims and Abstract are due to differing posting times. Text of the Claims and Abstract are posted:

  • At the time the application is open to public inspection;
  • At the time of issue of the patent (grant).
(12) Patent: (11) CA 2350840
(54) English Title: GASKET TAB RETAINER
(54) French Title: DISPOSITIF DE RETENUE D'ATTACHE DE JOINT D'ETANCHEITE
Status: Expired and beyond the Period of Reversal
Bibliographic Data
(51) International Patent Classification (IPC):
  • F02F 11/00 (2006.01)
  • F16J 15/08 (2006.01)
(72) Inventors :
  • BELTER, JEROME G. (United States of America)
(73) Owners :
  • DANA AUTOMOTIVE SYSTEMS GROUP, LLC
(71) Applicants :
  • DANA CORPORATION (United States of America)
(74) Agent: SMART & BIGGAR LP
(74) Associate agent:
(45) Issued: 2009-09-22
(22) Filed Date: 2001-06-15
(41) Open to Public Inspection: 2001-12-19
Examination requested: 2006-06-01
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): No

(30) Application Priority Data:
Application No. Country/Territory Date
09/827,797 (United States of America) 2001-04-06
60/212,453 (United States of America) 2000-06-19

Abstracts

English Abstract


A gasket for sealing between a flange and a mating surface includes a metal
layer having at least two integral tabs formed as a continuation of said metal
layer.
The flange includes at least two apertures that are correspondingly sized and
positioned to receive the tabs. In a first embodiment, each tab is formed on
the outer
periphery of the metal layer and comprises two contoured, resilient legs
separated to
form a vertical slot between the legs, and a contoured tip located at a distal
end of
each tab leg. In a second embodiment, each tab includes a serrated resilient
edge that
promotes tab insertion, but digs into an inner periphery of the aperture upon
attempted
tab removal. In a third embodiment, each tab is formed on an inner periphery
of two
mounting apertures formed in the metal layer.


Claims

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


CLAIMS
What is claimed is:
1. An exhaust manifold gasket for sealing between an exhaust header and a
mating flange, said gasket comprising:
at least two metal layers having a length and a width defining at least two
mounting apertures, said length greater than said width, said layers
constituting at
least a part of the gasket and including at least one hole formed therein
corresponding
to a hole in the mating flange; and
at least two integral tabs formed on at least one of said layers, each of said
tabs
formed as a continuation of said layer on an inner periphery of each of said
mounting
apertures, said tabs bent generally perpendicular to said layer, each of said
tabs
received in an aperture formed on the mating flange.
2. An exhaust manifold gasket as recited in claim 1, wherein said tabs are
positioned generally vertical to said width of the gasket.
3. An exhaust manifold gasket as recited in claim 1, wherein said tabs are
formed
from two contoured tab legs that are separated to form a slot therebetween.
4. An exhaust manifold gasket as recited in claim 3, wherein each tab leg
further
includes a contoured tip located at a distal end thereof.
5. An exhaust manifold gasket as recited in claim 4, wherein said contoured
tip
of each said tab leg includes a laterally outwardly sloped portion along an
outside
edge of said tab leg.
6. An exhaust manifold gasket as recited in claim 5, wherein each said sloped
portion terminates in a contoured, laterally outwardly extending protrusion.
-10-

7. An exhaust manifold gasket as recited in claim 1, wherein an outermost
periphery of said tabs in an uncompressed state is greater in dimension than a
corresponding inner periphery of said apertures such that an interference fit
is created
by said tabs and said apertures.
8. An exhaust manifold gasket as recited in claim 7, wherein said outermost
periphery of said tabs includes a serrated edge, said edge oriented to promote
tab
insertion, but digging into said inner periphery upon attempted tab removal.
9. An exhaust manifold gasket as recited in claim 1, wherein the metal layers
are
stainless steel.
10. A sealing assembly, comprising:
a flange to be sealingly engaged against a mating surface, said flange and
said
mating surface including at least one first hole formed therein to be sealed,
said flange
further defining at least two apertures formed on said flange;
a metal layer constituting at least part of a gasket, said metal layer having
a
length and a width such that said length is greater than said width and
defining at least
two mounting apertures, said layer including at least one second hole
corresponding
to said first hole; and
at least two integral tabs, each of said tabs formed as a continuation of said
layer on an inner periphery of each of said mounting apertures, said tabs bent
generally perpendicularly to said layer and received in said apertures.
11. A sealing assembly as recited in claim 10, wherein an outermost periphery
of
said tabs in an uncompressed state is greater in dimension than a
corresponding inner
periphery of said apertures such that an interference fit is created by said
tabs and said
apertures.
12. A sealing assembly as recited in claim 11, wherein said outermost
periphery of
said tabs includes a serrated edge, said edge oriented to promote tab
insertion, but
digging into said inner periphery of said apertures upon attempted tab
removal.
-11-

13. A sealing assembly as recited in claim 10, wherein each of said tabs is
formed
from two contoured tab legs that are separated to form a slot therebetween.
14. A sealing assembly as recited in claim 13, wherein each tab leg further
includes a contoured tip located at a distal end of each tab leg.
15. A sealing assembly as recited in claim 14, wherein said contoured tip of
each
said tab leg includes an outwardly sloped portion.
16. A sealing assembly as recited in claim 15, wherein each of said sloped
portions terminates in a contoured, outwardly extending protrusion.
17. A sealing assembly as recited in claim 10, wherein the metal layers are
stainless steel.
-12-

Description

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


CA 02350840 2008-10-01
60680-1475 (5459-1 VIC) PATENT
GASKET TAB RETAINER
FIELD OF THE INVENTION
lo [0002] The present invention relates to a gasket tab retainer. More
particularly,
the present invention relates to a multiple layer steel laminate gasket
including at least
two integral tabs formed in a metal layer of the gasket to locate and retain
the gasket
on a mating flange.
BACKGROUND OF THE INVENTION
[0003] Gaskets are often used as seal between mating metal surfaces. One
common application involves the placement of a gasket between a head and an
exhaust manifold of an internal combustion engine. Another application
involves
gasket placement between the exhaust manifold and an exhaust pipe flange.
Gaskets
for either application can be considered high temperature gaskets and more
particularly exhaust manifold gaskets since they provide an exhaust seal which
prevents the byproducts of combustion exiting the engine from escaping into
the
engine compartment of a vehicle.
[00041 Exhaust manifold gaskets are typically installed by placing the gasket
between an exhaust manifold and its mating component and aligning bolt holes
or
apertures formed in the gasket with corresponding holes formed in the manifold
and
mating component. Typically, a threaded fastener passes through the manifold
and
gasket and engages a corresponding threaded aperture formed in the mating
component. Some maneuvering of the manifold and gasket relative to the mating
component may be required to align the holes therein with the corresponding
threaded
aperhtres of the mating component before the fasteners can be inserted.
However,
during the assembly process, the gasket may slip from its desired position or
drop off
-1-
- ~._., r_t..Ii,Tõ 1CT 7Q t an')'7ARTTC

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PATENT
the end of the inserted fastener before it can be fixed in place between the
exhaust
manifold and its mating component.
[0005] Attempts have been made to retain a gasket against a mating component
prior to and during assembly by providing separate clips for attaching the
gasket to a
gasket attaching portion of an engine part. Using such clips, a gasket is
placed
adjacent the mating component, and the separate clip is attached to the mating
component such that the gasket is secured in place between the clip and the
mating
component. The separate clips typically include one end for contacting the
gasket
about an outer periphery thereof while a second end is attached to an outer
periphery
1o of a mating component or to an outer periphery of a connecting portion
between
mating components. Use of such separate clips does not eliminate the problems
involved in the assembly process whereby a gasket may slip from its desired
position.
The clip attached to an outer periphery of the mating component may be jostled
or
become otherwise dislodged by contacting adjacent parts. Further, separate
clips may
become dislodged during sub-assembly handling and shipping of mating
components,
allowing the gasket to slip or drop. As a result, the gasket sealing portion
may become
offset or misaligned from the holes to be sealed before assembly, again
requiring
some maneuvering of the manifold and gasket relative to the mating component
during assembly in order to achieve a tight seal. Assembly of a gasket to a
mating
flange using separate clips is also a complex operation, requiring multiple
parts and
means to hold the gasket adjacent the mating flange while the clips are
attached.
Finally, because such clips are designed to interact with an outer periphery
of a
gasket, the gasket itself must cover the full radial extent of a mating
surface.
SUMMARY OF THE INVENTION
[0006] An exhaust manifold gasket for sealing between an exhaust header and a
mating flange is provided that includes integral tabs formed on an outer
periphery of
the gasket to locate and retain the gasket on the mating flange. In accordance
with the
present invention, at least two tabs are integrally formed on an outer
periphery of a
metal layer of a multiple layer steel laminate gasket for attaching the gasket
to a first
mating flange. After the gasket is attached, the first mating flange to which
the gasket
-2-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-I475 (5459-1 VIC) PATENT
is attached by the tabs is easily fixed to a second mating flange without
supporting the
gasket between the flanges.
[0007] The gasket of the present invention includes a metal layer having a
length
and a width, wherein the length is greater than the width. The metal layer
constitutes
at least a part of the gasket, and includes at least one hole formed therein
corresponding to an exhaust gas flow hole in the first mating flange. A first
outer
periphery is defined by a radially outer edge of the first mating flange,
while the
gasket length and width defines a second outer periphery. The second outer
periphery
fits entirely within the first outer periphery. At least two tabs are
integrally formed
along the width of the layer, and are bent generally perpendicular relative to
the rest
of the gasket. The two tabs prevent the gasket from rotating relative to the
mating
flange after the gasket has been installed. The first mating flange fitrther
includes at
least two apertures located within the first outer periphery that are sized
and
positioned to receive the tabs.
[0008] In one preferred embodiment, each tab comprises two contoured,
resilient
legs separated to form a vertical slot between the legs. Each tab leg further
includes a
contoured tip located at a distal end of each tab leg. The contoured tip
includes a
sloped portion that slopes laterally outwardly from the distal end of each tab
leg along
an outside edge of each tab leg. The sloped portion terminates in a laterally
outwardly
2o extending protnision that creates an interference fit when inserted into
the aperture.
The vertical slot between the legs allows each leg to deform to adjust for
aperture size
tolerance.
[0009] Because the apertures are formed inside the configuration of the mating
component, i.e. within the first outer periphery, a gasket formed according to
the
present invention uses less material, thereby reducing cost. The resilient tab
legs
deform when inserted into the corresponding apertures, such that insertion of
the legs
into corresponding aperh.ires positively locates the gasket in place against
the mating
flange. Thus, the configuration of the resilient legs produces a tight
interference fit
within the apertures. The gasket is therefore held tightly in place by the tab
legs. The
tab legs are also positioned vertical to the width of the gasket, allowing for
adjustment
of the gasket relative to the mating flange to account for linear tolerances
of the
apertures and for gasket tolerances. Finally, the tabs are integral to a metal
layer that
-3-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PA TENT
comprises at least a portion of a gasket, so that manufacture is easily
accomplished.
Moreover, no separate clips are needed to positively locate the gasket
adjacent a
mating flange.
[0010] In a second preferred embodiment, each tab comprises a serrated side
edge. The edge is oriented such that the tab may be easily inserted into a
mating
aperture. However, the edge digs into the inner periphery of the mating
aperture upon
attempted removal of the tab.
[0011] In accordance with a third embodiment, a two layer laminate gasket is
disclosed having at least two mounting apertures. The gasket includes at least
two
lo tabs; each tab being integrally formed on an inner periphery of an
aperture. The
geometry and function of the tabs are substantially similar to those disclosed
in the
first two embodiments.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] The features and inventive aspects of the present invention will become
more apparent upon reading the following detailed description, claims, and
drawings,
of which the following is a brief description:
[0013] FIG. 1 is a top view showing a component such as an engine manifold
with a flange according to the present invention.
[0014] FIG. 2 is a top view showing a gasket according to the present
invention
placed adjacent the mating flange of the component illustrated in FIG. 1.
[0015] FIG. 3 is a side view of a tab retainer as it is inserted into an
aperh.tre
according to lines 3-3 of FIG. 2.
[0016] FIG. 4 is a side view of a second embodiment of a tab retainer.
[0017] FIG. 5 is a bottom view of a third embodiment of a gasket according to
the
present invention.
[0018] FIG. 6 is a side view of a tab retainer as it is inserted into an
aperture
according to lines 6-6 of FIG. 5.
[0019] FIG. 7 is a side view of the gasket according to lines 7-7 of FIG. 5.
-4-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PATENT
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0020] In FIG. 2, a gasket 20 is shown installed adjacent a first mating
flange 22
on an exhaust manifold 23, the manifold being illustrated in FIG. 1. The
gasket 20
includes a plurality of bolt holes 24 and exhaust gas flow holes 26 that
correspond to
similar holes in the first mating flange 22. The mating flange 22 defines a
first outer
periphery 28, and the gasket 20 defines a second outer periphery 30. As can be
seen
in FIG. 2, the first outer periphery 28 fiilly encloses the second outer
periphery 30.
As a result, the gasket 20 covers less than the full extent of the mating
flange 22.
Because of the arrangement of the flow holes 26, the length L of the gasket 20
is
1 o greater than the width W of the gasket.
[00211 Because seals on the exhaust manifold must withstand high temperatures,
the gasket 20 is typically fonned from metal, and usually includes multiple
metal
layers. Typically, the metal layers are made from resilient steel, and all
layers of the
gasket 20 are sized and shaped to fit and seal a corresponding mating surface.
The
outermost (i.e. top and bottom) layers (not shown) of the gasket 20 may
further
include embossments, folds or any other surface feature designed to improve
fit, wear
and sealing ability of the gasket.
[0022] According to the present invention, at least one layer of the gasket 20
includes at least two integral tabs 32 formed along the second outer periphery
30. The
two tabs 32 are spaced from each other to prevent rotation of the gasket
relative to the
first mating flange 22 once the gasket 20 is installed. The first mating
flange 22
includes at least two apertures 341ocated within the first outer periphery
that are sized
and positioned to receive the tabs 32. Preferably, the tabs 32 are formed
along the
outer periphery of the gasket 20 parallel to the width W of the gasket 20,
thereby
allowing the tabs 32 to flex within the apertures 34 and account for linear
tolerances
of the apertures and for gasket tolerances. Moreover, because the apertures 34
are
located within the first outer periphery of the first mating flange 22, the
gasket itself
does not cover the entire surface of the first mating flange 22. Instead, the
gasket 20
is smaller than the first mating flange 22, thereby requiring less material
for
fabrication.
[0023] Prior to assembly of the gasket 20 against the first mating flange 22,
the
tabs 32 are bent generally perpendicular relative to the gasket 20. The gasket
20 is
-5-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PA TENT
then placed adjacent the first mating flange 22 so that the tabs 32 align with
and are
inserted into the apertures 34. The tabs 32 are sized to frictionally engage
the inner
surface 36 of the apertures 34 and to thereby retain the gasket 20 in place
against the
first mating flange 22. Thus, an outermost periphery of tabs 32 in an
uncompressed
state is greater in dimension than a corresponding inner surface of the
apertures 34.
[0024] The tabs 32 may be formed into any geometric shape that is convenient
to
manufacture and that achieves a tight interference fit within appropriately
sized
apertures 34. Most preferably, as seen in FIG.3, the tabs 32 are formed from
two
contoured legs 38 that are separated to form a slot 40 between the tab legs
38. Each
1o tab leg 38 further includes a contoured tip 42 located at a distal end 44
of each tab leg
38.
[0025] The contoured tip 42 of each tab leg is preferably formed into a sloped
portion 46 that slopes laterally outwardly from the distal end 44 along an
outside edge
48 of each tab leg 38. Each sloped portion 46 terminates in a contoured,
laterally
outwardly extending protrusion 50. Thus, a protnision 50 is located at either
side of
the tab 32. As the tab 32 is inserted into the aperture 34, a portion the
sloped portion
46 contacts the inner surface 36 of the aperture 34, forcing the tab leg 38 to
gradually
compress laterally inwardly as it is inserted. Thus, the sloped portion 46
aids in pre-
loading the tab legs 38 while making insertion into aperh.ire 34 easier. The
protrusion
50 is sized to create an interference fit when placed in contact with the
inner surface
36 of the aperture 34, but is small enough to be easily inserted within the
aperture 34.
[0026] As noted above, the tab legs 38 are separated to form a slot 40 between
the
tab legs. Formation of the slot 40 allows the slight inward deformation of
each
resilient tab leg 38 as it is inserted into the aperture 34. The slot 40 also
allows each
tab leg 38 to deform independently of the other tab leg, so that the tab legs
38 in
combination are able to self adjust to the actual diameter of the aperture 34.
The size
of the slot 40 also allows the tab legs 38 to adjust for minor variations in
the location
of the apertures, thus providing a suitable tolerance.
[0027] In assembling a gasket 20 to a first mating flange 22, the tabs 32 are
bent
generally perpendicular relative to the gasket 20, so that the tabs 32 are
positioned
generally vertical to the width of the gasket. As applied to the preferred
embodiment,
the tab legs 38 are thus positioned vertical to the width of the gasket. The
gasket 20 is
-6-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PATENT
then placed adjacent the first mating flange 22 so that the tabs 32, including
the tab
legs 38, align with and are inserted into the apertures 34. As the tabs 32 are
inserted
into the apertures 34, the sloped portion 46 first contacts the inner surface
36 of
aperture 34. As the tabs 32 are further inserted into the apei-ture 34, the
tab legs 38
are independently forced to deform slightly inwardly. When the tab legs 38
have
been fully inserted into the aperture 34, only the protrusions 50 contact the
inner
surface 36 of the aperture 34. The resilient tabs maintain a slightly
laterally inwardly
deformed position, thereby applying a force laterally outwardly against the
inner
surface 36 of the aperture 34. The outward force applied through the
protrusions 46 is
1o sufficient to cause a tight interference fit of the tabs 32 within the
aperture 34 such
that the entire gasket 20 is maintained in position adjacent the first mating
flange 22.
The first mating flange 22 may then await assembly or shipment to a location
for
assembly at a later time without the gasket 20 becoming dislodged from it.
[0028] Because the apertures 34 are formed inside the configuration of the
mating
component, i.e. within the first outer periphery, a gasket 20 formed according
to the
present invention uses less material, thereby reducing cost. The resilient tab
legs 38
deform independently when inserted into the corresponding apertures 34 such
that
insertion of the legs 38 into corresponding apertures 34 positively locates
the gasket
in place against the mating flange 22. The combination of the tab legs 38, the
slot
20 40 and the protrusions tabs 32, when placed into frictional engagement with
the inner
surface 36 of the apertures 34, effectively retains the gasket 20 in place
against the
first mating flange 22. Thus, the configuration of the resilient legs 38
produces a tight
interference fit within the apertures 34. The gasket 20 is therefore held
tightly in
place by the tab legs 38. Because the tab legs 38 are also positioned vertical
to the
width of the gasket, the tab legs 38 may deform to allow for adjustment of the
gasket
relative to the mating flange, thereby accounting for linear tolerances of the
apertures
and for overall gasket tolerances. And finally, because the tabs 32 are formed
as part
of a metal layer of the gasket 20, both manufacture and assembly are
simplified
because no separate clips are required to attach the gasket 20 to the first
mating flange
3o 22.
[00291 A second preferred embodiment of a tab 32' is illustrated in FIG. 4.
Tab
32' comprises a serrated side edge 52 terminating at a plurality of resilient
points 54.
-7-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 Y70 PATENT
Each point 54 extends upwardly and is angled with respect to an adjacent
valley 56
such that tab 32 may be easily inserted into mating aperture 34 as the points
54 bend
inwardly. However, each point 54 digs into the inner periphery 36 of the
mating
aperture 34 upon attempted removal of tab 32'.
[0030] A third alternative embodiment of the invention is disclosed in FIGS.
5, 6
and 7, showing a two-layer exhaust manifold gasket 120. While a two-layer
design is
illustrated, a three or more layer design is also within the scope of the
invention.
Gasket 120 includes a plurality of bolt holes 124 and gas flow holes 126 that
correspond to similar holes in a mating component. Like the first two
embodiments,
the layers of gasket 120 may further include embossments, folds or other
sealing
features. Because seals on the gasket must withstand high temperature and
resist
chemical attack, gasket 120 is preferably formed of a metal, and more
preferably
stainless steel. When formed from stainless steel, however, modifications to
the
production tooling may be required in view of the material characteristics.
[0031] According to the third embodiment, at least one metal layer of the
gasket
120 includes at least two integral tabs 132. Each tab 132 is formed as a
continuation
of the metal layer along an inner periphery 130 of a mounting aperture 131.
Permitting the tab to be formed as a continuation of a metal layer allows the
shape of
the tab to be formed in the same manufacturing operation. For example,
mounting
apertures 131, tabs 132, bolt holes 124 and gas flow holes 126 may be formed
in the
same stamping operation. As with the embodiments discussed above, tabs 132 are
bent generally perpendicular relative to gasket 120 so that tabs 132 are
positioned
generally vertical to the width of gasket 120. Additionally, tabs 132 are
spaced apart
to prevent rotation of gasket 120 once it is installed. The geometric shape of
tabs 132
is preferably substantially similar to tabs 32 in the first embodiment or,
alternatively,
may be formed substantially similar to tabs 32' in the second embodiment.
However,
it is within the scope of this embodiment that tabs 132 may be formed into any
geometric shape that is convenient to manufacture and that achieves a tight
interference fit within a mating aperture 134. The assembly of gasket 120 on a
mating
flange is substantially similar to the first embodiment as described above.
Moreover,
as with the earlier embodiments, tab legs 138 may deform to allow for
adjustment of
the gasket relative to the mating flange.
-8-
Express Mail Label No. EL781402788US

CA 02350840 2001-06-15
60680-1475 (5459-1 VIC) PA TENT
[0032] Accordingly, the present invention provides a gasket design that
incorporates integral tabs formed as a continuation of a gasket layer to
locate and
retain the gasket on an engine component. The use of integral tabs eliminates
the
need to use clips to attach the gasket to the gasket-attaching portion of the
component.
While the use of integral tabs has been described in relation to an exhaust
gasket, it is
recognized that the present invention may be incorporated into other engine
gaskets,
such as a head gasket, to retain the gasket in place prior to assembly of the
mating
component.
[0033] Although certain preferred embodiments of the present invention have
lo been described, the invention is not limited to the illustrations described
and shown
herein, which are deemed to be merely illustrative of the best modes of
carrying out
the invention. A person of ordinary skill in the art will realize that certain
modifications and variations will come within the teachings of this invention
and that
such variations and modifications are within its spirit and the scope as
defined by the
claims.
-9-
Express Mail Label No. EL781402788US

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

2024-08-01:As part of the Next Generation Patents (NGP) transition, the Canadian Patents Database (CPD) now contains a more detailed Event History, which replicates the Event Log of our new back-office solution.

Please note that "Inactive:" events refers to events no longer in use in our new back-office solution.

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 , Event History , Maintenance Fee  and Payment History  should be consulted.

Event History

Description Date
Time Limit for Reversal Expired 2011-06-15
Letter Sent 2010-06-15
Grant by Issuance 2009-09-22
Inactive: Cover page published 2009-09-21
Inactive: Final fee received 2009-07-02
Pre-grant 2009-07-02
Notice of Allowance is Issued 2009-03-23
Letter Sent 2009-03-23
Notice of Allowance is Issued 2009-03-23
Letter Sent 2009-03-18
Inactive: Approved for allowance (AFA) 2009-02-26
Letter Sent 2008-11-07
Reinstatement Requirements Deemed Compliant for All Abandonment Reasons 2008-10-20
Amendment Received - Voluntary Amendment 2008-10-01
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2008-06-16
Inactive: S.30(2) Rules - Examiner requisition 2008-04-11
Amendment Received - Voluntary Amendment 2006-07-12
Letter Sent 2006-06-29
Request for Examination Received 2006-06-01
Request for Examination Requirements Determined Compliant 2006-06-01
All Requirements for Examination Determined Compliant 2006-06-01
Inactive: IPC from MCD 2006-03-12
Application Published (Open to Public Inspection) 2001-12-19
Inactive: Cover page published 2001-12-18
Inactive: First IPC assigned 2001-08-16
Inactive: Filing certificate - No RFE (English) 2001-07-17
Filing Requirements Determined Compliant 2001-07-17
Letter Sent 2001-07-17
Application Received - Regular National 2001-07-17

Abandonment History

Abandonment Date Reason Reinstatement Date
2008-06-16

Maintenance Fee

The last payment was received on 2009-05-21

Note : If the full payment has not been received on or before the date indicated, a further fee may be required which may be one of the following

  • the reinstatement fee;
  • the late payment fee; or
  • additional fee to reverse deemed expiry.

Please refer to the CIPO Patent Fees web page to see all current fee amounts.

Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
DANA AUTOMOTIVE SYSTEMS GROUP, LLC
Past Owners on Record
JEROME G. BELTER
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

To view selected files, please enter reCAPTCHA code :



To view images, click a link in the Document Description column. To download the documents, select one or more checkboxes in the first column and then click the "Download Selected in PDF format (Zip Archive)" or the "Download Selected as Single PDF" button.

List of published and non-published patent-specific documents on the CPD .

If you have any difficulty accessing content, you can call the Client Service Centre at 1-866-997-1936 or send them an e-mail at CIPO Client Service Centre.


Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Representative drawing 2001-11-21 1 8
Description 2001-06-15 9 510
Drawings 2001-06-15 3 55
Abstract 2001-06-15 1 24
Claims 2001-06-15 3 109
Cover Page 2001-12-14 1 38
Description 2008-10-01 9 502
Representative drawing 2009-08-27 1 8
Cover Page 2009-08-27 1 40
Courtesy - Certificate of registration (related document(s)) 2001-07-17 1 112
Filing Certificate (English) 2001-07-17 1 163
Reminder of maintenance fee due 2003-02-18 1 106
Reminder - Request for Examination 2006-02-16 1 117
Acknowledgement of Request for Examination 2006-06-29 1 176
Courtesy - Abandonment Letter (Maintenance Fee) 2008-08-11 1 173
Notice of Reinstatement 2008-11-07 1 164
Commissioner's Notice - Application Found Allowable 2009-03-23 1 163
Maintenance Fee Notice 2010-07-27 1 170
Fees 2003-05-21 1 29
Fees 2004-05-19 1 31
Fees 2005-05-18 1 28
Fees 2006-05-19 1 27
Fees 2007-05-25 1 28
Fees 2008-10-20 1 34
Correspondence 2009-07-02 1 34
Fees 2009-05-21 1 44