IP Library › Granted Patent US 12,269,415
Granted Patent B2
US 12,269,415 · App. 18/253,943 · Granted Apr 8, 2025

Airbag fabric

Inventor: Anton Fischer (Schechingen-Leinweiler, DE)
Assignee: ZF AUTOMOTIVE GERMANY GMBH
B60R21/235D03D1/02D03D13/008B60R2021/23509B60R2021/23542B60R2021/23547D10B2505/124
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Quick Facts
Patent No.
US 12,269,415
App. No.
18/253,943
Granted
Apr 8, 2025
Kind
B2
Abstract

An airbag fabric for an airbag comprises a mounting area ( 22 ) for mounting the airbag. The mounting area ( 22 ) includes a mounting hole ( 24 ), a load portion ( 26 ) which is adjacent to the mounting hole ( 24 ) in a load direction (B), and a transition portion ( 28 ) which is adjacent to the mounting hole ( 24 ) against the load direction (B). Furthermore, the load portion ( 26 ) and the transition portion ( 28 ) include different weaves. The fabric in the load portion ( 26 ) exhibits lower resistance to displacement than in the transition portion ( 28 ) so that a fiber bead forms of the fabric fibers of the load portion ( 26 ), which fiber bead is adjacent to the mounting hole ( 24 ) in the load direction (B), if bearing stress acts upon the mounting hole ( 24 ) in the load direction (B).

Claims (33)

1. An airbag fabric for an airbag comprising a mounting area for mounting the airbag,

wherein the mounting area includes a mounting hole, a load portion which is adjacent to the mounting hole in a load direction, and a transition portion with is adjacent to the mounting hole against the load direction,

wherein the load portion and the transition portion include different weaves and the fabric in the load portion exhibits lower resistance to displacement than in the transition portion so that a fiber bead forms of the fabric fibers of the load portion, the fiber bead being adjacent to the mounting hole in the load direction, if bearing stress acts upon the mounting hole in the load direction, wherein the airbag fabric is a one-piece-woven fabric in which the threads of opposite walls of an inflatable chamber at the edge merge into a joint weave.

2. The airbag fabric according to claim 1 , wherein the weave of the load portion has a first knot density and the transition portion includes a weave having a second knot density, the first knot density being lower than the second knot density.

3. The airbag fabric according to claim 2 , wherein the first knot density amounts to not more than 50% of the second knot density.

4. The airbag fabric according to claim 1 , wherein the fabric of the load portion has a tear propagation resistance which amounts to at least 150% of the tear propagation resistance of the transition portion.

5. The airbag fabric according to claim 1 , wherein the warp threads of the weave of the load portion extend perpendicularly or in parallel to the load direction.

6. The airbag fabric according to claim 1 , wherein the weave of the load portion is a Panama weave.

7. The airbag fabric according to claim 1 , wherein the transition portion merges into an airbag chamber portion which forms a wall of an inflatable chamber.

8. The airbag fabric according to claim 1 , wherein the load portion is multi-layered, with the threads of the layers merging integrally into the weave of the transition portion.

9. The airbag fabric according to claim 1 , wherein an edge portion is adjacent to the outside of the load portion, wherein the edge portion along with the transition portion frame-like surrounds the load portion, and wherein the edge portion and the transition portion include the same weave, and, if the load portion is multi-layered, the threads of the layers merge integrally into the weave of the transition portion and merge integrally into the single-layer weave of the edge portion.

10. The airbag fabric according to claim 1 , wherein the load portion is multi-layered, wherein the threads of the layers merge integrally into the weave of the transition portion and, if an edge portion surrounds the load portion, merge integrally into the single-layer weave of the edge portion.

11. The airbag fabric according to claim 1 , wherein the load portion has a base which tapers in the load direction.

12. The airbag fabric according to claim 1 , wherein the load portion defines the edge of the mounting hole over a peripheral angle of at least 60°.

13. The airbag fabric for an airbag comprising a mounting area for mounting the airbag,

wherein the mounting area includes a mounting hole which is disposed in a load portion, and a transition portion which is adjacent to the load portion toward an edge of the airbag,

wherein the load portion and the transition portion include different weaves and the fabric in the load portion exhibits lower resistance to displacement than in the transition portion so that a fiber bead forms of the fabric fibers of the area of the load portion, which fiber bead is adjacent to the mounting hole in a load direction, if bearing stress acts upon the mounting hole in the load direction, wherein the airbag fabric is a one-piece-woven fabric in which the threads of opposite walls of an inflatable chamber at the edge merge into a joint weave.

14. The airbag fabric according to claim 13 , wherein the weave of the load portion has a first knot density and the transition portion includes a weave having a second knot density, the first knot density being lower than the second knot density.

15. The airbag fabric according to claim 14 , wherein the first knot density amounts to not more than 50% of the second knot density.

16. The airbag fabric according to claim 13 , wherein the fabric of the load portion has a tear propagation resistance which amounts to at least 150% of the tear propagation resistance of the transition portion.

17. The airbag fabric according to claim 13 , wherein the warp threads of the weave of the load portion extend perpendicularly or in parallel to the load direction.

18. The airbag fabric according to claim 13 , wherein the weave of the load portion is a Panama weave.

19. The airbag fabric according to claim 13 , wherein the transition portion merges into an airbag chamber portion which forms a wall of an inflatable chamber.

20. The airbag fabric according to claim 13 , wherein the load portion is multi-layered, with the threads of the layers merging integrally into the weave of the transition portion.

21. The airbag fabric according to claim 13 , wherein a cushioning portion is adjacent to the load portion.

22. The airbag fabric according to claim 21 , wherein the cushioning portion is adjacent to the load portion at least in the load direction.

23. The airbag fabric according to claim 21 , wherein a tolerance portion or the transition portion is adjacent to the cushioning portion, or in that the cushioning portion forms at least partially the transition portion and is adjacent to the walls of the airbag.

24. The airbag fabric according to claim 2 , wherein the first knot density amounts to not more than 34% of the second knot density.

25. The airbag fabric according to claim 1 , wherein the fabric of the load portion has a tear propagation resistance which amounts to at least 200% of the tear propagation resistance of the transition portion.

26. The airbag fabric according to claim 11 , wherein the base of the load portion is in the form of a trapezoid, triangle, or circular segment.

27. The airbag fabric for an airbag comprising a mounting area for mounting the airbag,

wherein the mounting area includes a mounting hole which is disposed in a load portion, and a transition portion which is adjacent to the load portion toward an edge of the airbag,

wherein the load portion and the transition portion include different weaves and the fabric in the load portion exhibits lower resistance to displacement than in the transition portion so that a fiber bead forms of the fabric fibers of the area of the load portion, which fiber bead is adjacent to the mounting hole in a load direction, if bearing stress acts upon the mounting hole in the load direction, wherein a cushioning portion is adjacent to the load portion.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 26, 2023
From: FISCHER, ANTON
To: ZF AUTOMOTIVE GERMANY GMBH
Reel/Frame 064052/0395 →
Priority Claims (2)
DE 10 2020 131 168.0 · Nov 25, 2020 · national
DE 10 2021 118 314.6 · Jul 15, 2021 · national
Continuity (1)
Related Publication 20240092306A1 · Mar 21, 2024
References Cited (37)
US 5131434A · Krummheuer · 1992 [cited by examiner]
US 5336538A · Kitamura · 1994 [cited by examiner]
US 5707711A · Kitamura · 1998 [cited by examiner]
US 9475255B2 · Lowe · 2016 [cited by examiner]
US 11052863B2 · Gould · 2021 [cited by examiner]
US 11293122B2 · Mori · 2022 [cited by examiner]
US 11618982B2 · Albiez · 2023 [cited by examiner]
US 20010048219A1 · Heigl · 2001 [cited by applicant]
US 20080079243A1 · Kino et al. · 2008 [cited by applicant]
US 20140183848A1 · Aranzulla et al. · 2014 [cited by applicant]
US 20150266264A1 · Lowe · 2015 [cited by examiner]
US 20190322238A1 · Gould · 2019 [cited by examiner]
US 20190345650A1 · Mori · 2019 [cited by examiner]
US 20210140074A1 · Yoshida · 2021 [cited by examiner]
US 20210301430A1 · Albiez · 2021 [cited by examiner]
US 20220001830A1 · Fischer · 2022 [cited by examiner]
US 20230067893A1 · Stegmeier · 2023 [cited by examiner]
US 20240042958A1 · Ressencourt · 2024 [cited by examiner]
CA 2064693A1 · 1991 [cited by examiner]
CN 107829199A · 2018 [cited by examiner]
DE 112004000482T5 · 2006 [cited by applicant]
GB 2251410A · 1992 [cited by examiner]
GB 2386870A · 2003 [cited by examiner]
JP 07205736A · 1995 [cited by examiner]
JP 09175301A · 1997 [cited by examiner]
JP 2666580B2 · 1997 [cited by examiner]
JP 2007045418A · 2007 [cited by applicant]
JP 3941514B2 · 2007 [cited by examiner]
JP 2010030342A · 2010 [cited by examiner]
WO WO9009295A2 · 1990 [cited by examiner]
WO 2003078711A1 · 2003 [cited by applicant]
WO 2005075258A1 · 2005 [cited by applicant]
WO 2008105693A1 · 2008 [cited by applicant]
WO 2013013767A1 · 2013 [cited by applicant]
WO WO2019215092A1 · 2019 [cited by examiner]
JP2003205817A machine translation from espacenet.com (Year: 2024). [cited by examiner]
PCT Search REport for corresponding International Application Serial No. PCT/EP2021/082185, mailed Mar. 4, 2022, pp. 1-5. [cited by applicant]