Language selection

Search

Patent 2441668 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 2441668
(54) English Title: METHOD FOR WEAVING AN AIRBAG
(54) French Title: PROCEDE DE TISSAGE D'UN SAC GONFLABLE
Status: Expired and beyond the Period of Reversal
Bibliographic Data
(51) International Patent Classification (IPC):
  • D3D 1/02 (2006.01)
  • B60R 21/16 (2006.01)
(72) Inventors :
  • ESCHBACH, THOMAS (Germany)
  • BECKER, MICHAEL (Germany)
(73) Owners :
  • GLOBAL SAFETY TEXTILES GMBH
(71) Applicants :
  • GLOBAL SAFETY TEXTILES GMBH (Germany)
(74) Agent: MCCARTHY TETRAULT LLP
(74) Associate agent:
(45) Issued: 2008-06-17
(86) PCT Filing Date: 2002-04-02
(87) Open to Public Inspection: 2002-11-07
Examination requested: 2004-09-08
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): Yes
(86) PCT Filing Number: PCT/EP2002/003629
(87) International Publication Number: EP2002003629
(85) National Entry: 2003-09-24

(30) Application Priority Data:
Application No. Country/Territory Date
101 15 890.4 (Germany) 2001-03-30

Abstracts

English Abstract


Disclosed is a method for weaving a single-pieced airbag (2) or air tube
consisting of at least two layers on a mechanical loom, characterized in that
weft yarns of different strengths are woven in at least one layer.


French Abstract

L'invention concerne un procédé de tissage d'un sac gonflable (2) ou d'une chambre à air bicouche d'une seule pièce sur un métier à tissier, ledit procédé étant caractérisé en ce que, dans une couche au moins, des fils de trame de grosseurs différentes sont tissés.

Claims

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


8
Claims
1. A method for machine weaving an at least two-ply, one-piece
airbag or air tube comprising weft threads of differing
dtex woven in at least one ply, wherein at least a portion
of said weft threads are picked only in defined warp thread
length regions.
2. The method as set forth in claim 1, wherein the weft
threads picked only in defined warp thread length regions
have a defined dtex selected from among the weft threads of
differing dtex.
3. The method as set forth in claim 2, wherein said weft
threads comprise standard weft threads having a first dtex
and reinforcement weft threads having the defined dtex
picked only in the defined warp thread length.
4. The method as set forth in claim 3, wherein the defined
dtex is at least 25% higher than the first dtex.
5. The method as set forth in any one of claim 3 or 4, wherein
said reinforcement weft threads having the defined dtex are
picked with no change in weft set.
6. The method as set forth in any of the claims 3 to 5,
wherein part of said reinforcement weft threads are
interwoven only in defined width regions of the air bag.
7. The method as set forth in claim 6, wherein non-interwoven
regions of said reinforcement weft threads are parted from
the airbag or air tube as just woven in the machine.
8. The method as set forth in any one of claims 3 to 7,
wherein monofil threads are employed as reinforcement weft
threads.
9. A method for machine weaving an at least two-ply, one-piece
airbag or air tube comprising:

9
weaving weft threads of differing dtex in at least one ply,
picking said weft threads only in predetermined warp thread
length regions, and
interweaving part of said weft threads only in
predetermined and non-overlapping width regions of the
airbag.
10. The method as set forth in claim 9, further comprising
parting non-interwoven regions of said weft threads from
the airbag or air tube as just woven in the weaving
machine.
11. The method as set forth in claim 9, further comprising
picking standard weft threads of a first dtex and
reinforcement weft threads having a second dtex that is at
least 25% higher than the first dtex.
12. The method as set forth in claim 11, further comprising
picking said weft threads having the second, higher dtex
with no change in weft set.
13. The method as set forth in claim 9, further comprising
employing monofil threads as said weft threads.
14. A method for manufacturing an inflatable safety device, the
method comprising:
(a) weaving threads of a lower dtex value in a first area;
(b) weaving threads of a higher dtex value in a second
area; and
(c) weaving threads of the higher dtex value in a third
area,
wherein the first area is located between the second and
third areas, the second and third areas not overlapping
each other.
15. A method for manufacturing an airbag or passenger restraint
air tube, the method comprising:
(a) weaving a first reinforced area at a first gas
inflation location;
(b) weaving a second reinforced area at a second gas
inflation location, the first and second locations being in
fluid communication with each other, and
(c) weaving a non-reinforced area between the inflation
locations.
16. An inflatable safety device comprising:
(a) threads of a lower dtex value in a first area;

10
(b) threads of a higher dtex value in a second area; and
(c) threads of the higher dtex value in a third area;
wherein the first area is located between the second and
third areas, the second and third areas not overlapping
each other,
wherein the material is more easily folded in the first
area as compared to the second and third areas.

Description

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


CA 02441668 2003-09-24
Method for weaving an airbag
The invention relates to a method for broad loom machine
weaving an at least two-ply, one-piece airbag.
One-piece woven (OPW) airbags are known which find application
in the fabrication of vehicular airbag systems. For inflation
of such one-piece woven airbags a gas lance is inserted
thereinto. Experience has shown tears materializing in the
regions of the airbag in which gas is jetted into the airbag
from the gas lance. Gas lances often feature a train of slots,
so-called gills, oriented roughly transversely to the gas flow,
through which the gas is jetted into the airbag at several
locations. The aforementioned tears in the airbag may
materialize e.g. because of differences in the design of the
inflator, causing it to be more or less aggressive, termed
dispersion within and between inflator jets. Tears in the
airbag may also be influenced by the positioning of the jet
gills relative to the airbag chamber. In addition, airbag tears
more frequently occur in borderline situations as regards
inflator aggressiveness as well as the ambient temperature at
which the airbag is put to use.
21192222.1

CA 02441668 2008-01-23
2
The object of the invention is to propose a method for weaving
an at least two-ply, one-piece airbag in which the drawbacks as
known from prior art, particularly the incidence of tears in the
fabric occurring in the region impacted by the gas flow jetted
into the airbag, may be eliminated, alleviated or at least
reduced.
According to a first broad aspect of the present invention,
there is provided a method for machine weaving an at least two-
ply, one-piece airbag or air tube comprising weft threads of
differing dtex woven in at least one ply, wherein at least a
portion of the weft threads are picked only in defined warp
thread length regions.
According to a second broad aspect of the present invention,
there is provided a method for machine weaving an at least two-
ply, one-piece airbag or air tube comprising: weaving weft
threads of differing dtex in at least one ply, picking said weft
threads only in predetermined warp thread length regions, and
interweaving part of said weft threads only in predetermined and
non-overlapping width regions of the airbag.
According to a third broad aspect of the present invention,
there is provided a method for manufacturing an inflatable
safety device, the method comprising: (a) weaving threads of a
lower dtex value in a first area; (b) weaving threads of a
higher dtex value in a second area; and (c) weaving threads of
the higher dtex value in a third area, wherein the first area is
located between the second and third areas, the second and third
areas not overlapping each other.
According to a fourth broad aspect of the present invention,
there is provided a method for manufacturing an airbag or
passenger restraint air tube, the method comprising: (a) weaving
a first reinforced area at a first gas inflation location; (b)
weaving a second reinforced area at a second gas inflation
location, the first and second locations being in fluid
communication with each other, and (c) weaving a non-reinforced
area between the inflation locations.
According to a fifth broad aspect of the present invention,
there is provided an inflatable safety device comprising: (a)
threads of a lower dtex value in a first area; (b) threads of a
higher dtex value in a second area; and (c) threads of the
higher dtex value in a third area; wherein the first area is

CA 02441668 2008-01-23
2a
located between the second and third areas, the second and third
areas not overlapping each other, wherein the material is more
easily folded in the first area as compared to the second and
third areas.
The available fabric mass in the one-piece woven airbag as
tailorized by the method, now makes it possible to reinforce the
airbag fabric individually oriented. Thus, at a high stress
location formerly exhibiting airbag tears, a fabric quality is
now available of enhanced resistance, achieved among other

CA 02441668 2003-09-24
3
things by an increase in the thermal capacity in the neuralgic
locations of the airbag where namely the jet lances feature
their so-called jet gill zone. Now, by increasing the fabric
mass to advantage in desired airbag positions in the fabric, a
higher strength both mechanically and also thermally is
available in preventing tears in the airbag.
In one aspect of the invention a weft yarn is employed in the
desired region which as compared to standard yarn has an at
least 25% higher dtex. The invention will now be detailled with
reference to the drawing for a better understanding, in which:
Fig. 1 is a greatly diagrammatic illustration of an
airbag which in this case is a vehicular side
airbag extending over the side windows of the
right-hand front and rear seat of the vehicle.
Fig. la is a diagrammatic arrangement of a vehicular
airbag.
Fig. 2 is again a greatly diagrammatic illustration of
part of a fabric in which two airbags are
evident one alongside the other fully woven on
the machine.
Fig. 3 is a greatly diagrammatic illustration of a
cross-section through one ply of an airbag in
which weft threads of differing dtex are woven.
Referring now to Fig. 1 there is illustrated diagrammatically,
by way of example, an airbag 2 shown from the side. The
location of this airbag 2 in a motor vehicle may be imagined
for the right-hand side windows of a vehicle shown on the move
in the upper part (Fig. la) of the drawing. The airbag 2 is
framed by a single-ply woven edge 4 shown shaded in the
drawing. In accordance with its location in the vehicle, tabs 6
arranged "front" and "rear" serve to secure the airbag 2 in
place (not shown). The position of the airbag 2 in a vehicle 3
is indicated diagrammatically in Fig. la. The airbag 2 is
divided into various regions, namely a front seat region 8 and
a rear seat region 9 in which, in case of a collision, the head
of a vehicle occupant could impact the side window of the
21192184.1

CA 02441668 2003-09-24
4
vehicle. This is why the airbag 2 needs to be inflated at the
earliest in the cited regions 8 and 9. For inflating the airbag
a gas lance 12 is inserted into the interior 7 of the airbag 2,
the gas lance 12 comprising jet orifices 14 in the regions 8
and 9. The gas is jetted into the cited regions roughly in the
direction of an arrow GSR and is then distributed in the
airbag. The shaded edge 4 of the airbag 2 is, as just said,
woven single-ply whilst the interior 7 framed by the edge 4 is
woven two-ply in this example. Some regions within the airbag 2
serving particularly to shape the airbag 2 or orient the flow
of gas into the airbag 2 are included in the weave single-ply
woven as connecting regions in the form of surface areas 16a or
webs 16b. Thus, for example, in the vicinity of the so-called
A-pillar (not shown) and B-pillar (likewise not shown) of the
vehicle a region 16a and a webbed region 16b respectively are
woven single-ply. In these regions 16a, 16b upper and lower
fabric plies are joined to each other.
The fabric as is usually configured rather fine for an airbag
is subjected to exceptionally heavy stress in the region of the
jet orifices 14 of the gas lance 12 unlike other regions of the
airbag 2. The shock of the hot gas jet stresses the surface or
fabric of the airbag exceptionally in the corresponding
regions.
Referring now to Fig. 2 there is illustrated part of a fabric
20 in which two inwoven airbags I and II are evident. In this
case the airbags I and II are shown not yet parted from the
fabric 20. Indicated in airbag I is an inserted jet lance 12'
depicted by the dotted line which analog to the jet lance 12 as
shown in Fig. 1 comprises jet orifices arranged in the regions
8 and 9. The fabric 20 in the example as shown in this case is
basically woven single-ply in the non-shaded region located
outside of the airbags I and II. The requirement in this case
is substantially a woven structure and thus there is no need to
go into detail as regards the connections. What is particularly
of interest in the fabric 20 as shown in Fig. 2 is the special
use made of weft threads differing in dtex. A weft thread in
the direction of the arrow S transversely to the warps running
in the direction of the arrow K is picked, for example, over
the full width of the fabric 20 as shown here merely
sectionwise. To attain higher strength in the wall of the
airbag 2 in the regions 8 and 9 as cited above, regions of the
airbag offering greater resistance are created in accordance
with the invention (Fig. 2) in the regions 28 and 29 by
21192184.1

CA 02441668 2003-09-24
employing a yarn VS in the cited regions in the weft direction
S and which as compared to weft threads used in other regions
of the fabric 20 has a 25% higher dtex, for instance. This so-
called reinforcement weft yarn VS is picked, for example. with
no change in the weft set, into the fabric 20 so that in the
regions 28 and 29 a corresponding increase in the fabric mass
and thus the desired fabric strength is achieved. This
inventive approach attains, on the one hand, the desired
reinforcement where it is wanted within a ply of the airbag,
but, on the other hand, the reinforcement effect is also
achieved elsewhere in the airbag where not required. This may
result in the stiffness of the airbag as well as the pack
volume of airbag being unfavorable in some assembly conditions.
This situation can be improved by selecting in the
reinforcement regions 28 and 29 a weft sequence in which
reinforcement weft yarns VS differing in dtex, for example by
alternating 470 with 350 dtex reinforcement weft threads in a
predefined sequence. This permits reducing the stiffness and
thus also the pack volume of the airbag as compared to that of
an airbag woven with just one reinforcement weft thread dtex.
On top of this, any surfeit in the regions of the fabric (i.e.
the fabric may form advance cloth, indeed even folds, in
approaching the absolute limit to the fabric density that can
be accommodated, when only a single reinforcement weft thread
dtex with no change in the weft set is employed) is reduced.
In optimizing the procedure as just described in which the
reinforcement weft yarn VS reinforcing the full width of the
fabric in the regions 28 and 29 is picked, the reinforcement
weft yarn VS is picked only in defined regions transversely in
the fabric. To prevent the reinforcement regions from extending
over the full width of the fabric, i.e. over the full "height"
of the airbag, the reinforcement wefts VS are activated only in
defined regions (identified by the reference numeral 38 in Fig.
2) in which the inflow of gas is actually anticipated through
the jet orifices 14 of the gas lance 12 on inflation of the
airbag.
Referring now to Fig. 3 there is illustrated how, in this
procedure a reinforcement weft thread VS (depicted merely
diagrammatically) is picked in the fabric only in the region 38
whilst outside thereof it is present as a floating
reinforcement weft also outside of the fabric. Analogous to the
location of the reinforcement weft VS a basic weft thread BS
21192184.1

CA 02441668 2003-09-24
6
runs in the region 38 floating outside of the fabric 20, whilst
in the remaining regions of the fabric it is interwoven into
the plies of the fabric conventionally.
Evident likewise from Fig. 3, shown in section, are the warp
threads KF which together with the basic weft thread BS and
reinforcement weft thread VS form a ply of the airbag 2. It
will be understood that the illustration as shown in Fig. 3 is
merely diagrammatic and not at all true to scale. The person
skilled in the art will recognize from the diagrammatic
illustration the various principles and weaves of different
weft and warp threads involved. In the regions 40 the
reinforcement thread VS is located floating, whilst in the
region 38 the basic weft thread is located floating outside of
the fabric. To advantage the reinforcement weft threads VS may
furthermore be parted on the machine in the floating regions so
that they actually remain only in the desired regions 38 of the
fabric 20. This procedure has many advantages. The fabric is
reinforced only in the regions in which stress is anticipated
whilst the pack volume is reduced practically to that of the
standard fabric. Likewise, the stiffness of the airbag is
minimized.
The method in accordance with the invention also covers, of
course, a method for weaving an air tube for a so-called
airbelt, in other words an inflatable seat belt. It is of
advantage with such air tubes when particularly elastic weft
threads, e.g. monofil threads, are picked in regions of the
fabric desired to be particularly elastic. Thus, regions in the
fabric required to have "only" an airbag function in the
finished airbelt, may be woven with very fine, soft weft
threads whilst other regions having "also" an airbelt function
are woven at least in part with monofil threads in thus making
for enhanced cost effectiveness and more function-specific
airbelt fabrication.
It will be understood that the above description gives no
details as to how the remaining regions of the airbag (single-
ply region, two-ply region, etc) are woven in kind, since these
basics are known to the person skilled in the art. Also,
implementing the method in accordance with the invention by
ways and means as described above is intended merely to be
appreciated as an example. Employing a Jacquard weaving machine
permits discrete localized interweaving of reinforcement weft
threads in making use of the "picked weft technology" as just
21192184.1

CA 02441668 2003-09-24
7
described with all of its advantages as likewise described.
Just as possible too, is the arrangement of further juxtaposed
airbags in a fabric web.
21192184.1

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 2017-04-03
Letter Sent 2016-04-04
Letter Sent 2010-08-31
Letter Sent 2008-10-23
Grant by Issuance 2008-06-17
Inactive: Cover page published 2008-06-16
Letter Sent 2008-02-26
Amendment After Allowance Requirements Determined Compliant 2008-02-26
Amendment After Allowance (AAA) Received 2008-01-23
Pre-grant 2008-01-23
Inactive: Amendment after Allowance Fee Processed 2008-01-23
Inactive: Final fee received 2008-01-23
Notice of Allowance is Issued 2007-07-23
Letter Sent 2007-07-23
4 2007-07-23
Notice of Allowance is Issued 2007-07-23
Inactive: Approved for allowance (AFA) 2007-03-20
Amendment Received - Voluntary Amendment 2006-09-08
Inactive: S.30(2) Rules - Examiner requisition 2006-03-08
Inactive: Correspondence - Formalities 2006-03-03
Letter Sent 2005-11-21
Letter Sent 2004-11-10
Appointment of Agent Requirements Determined Compliant 2004-09-29
Inactive: Office letter 2004-09-29
Inactive: Office letter 2004-09-29
Revocation of Agent Requirements Determined Compliant 2004-09-29
Revocation of Agent Request 2004-09-08
Request for Examination Requirements Determined Compliant 2004-09-08
All Requirements for Examination Determined Compliant 2004-09-08
Request for Examination Received 2004-09-08
Appointment of Agent Request 2004-09-08
Inactive: IPRP received 2004-03-10
Letter Sent 2003-12-12
Inactive: Courtesy letter - Evidence 2003-12-02
Inactive: Cover page published 2003-11-30
Inactive: Notice - National entry - No RFE 2003-11-26
Inactive: Single transfer 2003-11-18
Inactive: IPRP received 2003-10-20
Application Received - PCT 2003-10-15
National Entry Requirements Determined Compliant 2003-09-24
Application Published (Open to Public Inspection) 2002-11-07

Abandonment History

There is no abandonment history.

Maintenance Fee

The last payment was received on 2008-03-25

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.

Patent fees are adjusted on the 1st of January every year. The amounts above are the current amounts if received by December 31 of the current year.
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
GLOBAL SAFETY TEXTILES GMBH
Past Owners on Record
MICHAEL BECKER
THOMAS ESCHBACH
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 (Temporarily unavailable). 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 2003-09-23 1 8
Description 2003-08-04 7 348
Drawings 2003-08-04 1 39
Claims 2003-08-04 1 33
Abstract 2003-08-04 2 68
Cover Page 2003-11-27 1 33
Description 2003-09-23 7 284
Claims 2003-09-23 1 34
Description 2006-09-07 7 291
Claims 2006-09-07 3 90
Drawings 2006-09-07 1 35
Description 2008-01-22 8 340
Representative drawing 2008-05-20 1 10
Cover Page 2008-05-20 1 35
Notice of National Entry 2003-11-25 1 204
Courtesy - Certificate of registration (related document(s)) 2003-12-11 1 125
Acknowledgement of Request for Examination 2004-11-09 1 177
Commissioner's Notice - Application Found Allowable 2007-07-22 1 164
Courtesy - Certificate of registration (related document(s)) 2008-10-22 1 122
Maintenance Fee Notice 2016-05-15 1 170
PCT 2003-09-23 5 122
PCT 2003-09-24 8 396
Correspondence 2003-11-25 1 26
PCT 2003-09-24 5 219
Correspondence 2004-09-07 2 45
Correspondence 2004-09-28 1 18
Correspondence 2004-09-28 1 18
Fees 2005-03-30 1 23
Fees 2006-03-02 1 24
Correspondence 2006-03-02 1 24
Fees 2007-03-27 1 26
Correspondence 2008-01-22 1 30
Fees 2008-03-24 1 26