IP Library Granted Patent US 12,344,183
Granted Patent B2
US 12,344,183 · App. 18/235,313 · Granted Jul 1, 2025

Systems and methods for improved airbag aspiration

Inventor: Jeffrey D. Williams (Roy, UT)
Assignee: Autoliv ASP, Inc.
B60R21/30B60R21/217B60R21/26
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Quick Facts
Patent No.
US 12,344,183
App. No.
18/235,313
Granted
Jul 1, 2025
Kind
B2
Abstract

Airbag cushion assemblies for aspirating ambient air and related assemblies. Some embodiments may comprise an aspirating airbag cushion assembly comprising an airbag cushion, which may be configured to deploy from a housing or the like. The assembly may further comprise one or more inflation conduits configured to deliver inflation gas into the airbag cushion through a plurality of inflation ports. An inflator module may be crimped onto an inflator hub, in some cases without the use of any fasteners and/or releasable coupling features.

Claims (23)

1. A method for assembly of an airbag cushion assembly, the method comprising the steps of:

inserting at least a portion of an inflator module into an inflator hub of an airbag cushion assembly, wherein the inflator module comprises:

an inflator; and

an inflator flange; and

crimping the inflator flange to the inflator hub.

2. The method of claim 1 , wherein the airbag cushion assembly comprises an aspirating airbag cushion assembly configured to aspirate ambient air into an airbag cushion using the inflator during inflation.

3. The method of claim 1 , further comprising coupling a metallic ring to the inflator hub.

4. The method of claim 3 , wherein the step of coupling the metallic ring to the inflator hub comprises inserting the metallic ring over an exterior surface of the inflator hub.

5. The method of claim 4 , wherein the step of coupling the metallic ring to the inflator hub further comprises overmolding the metallic ring to the inflator hub.

6. The method of claim 5 , wherein metallic ring comprises a protruding collar.

7. The method of claim 6 , wherein the step of crimping the inflator flange to the inflator hub comprises deforming the inflator flange to the protruding collar of the metallic ring.

8. The method of claim 1 , wherein the inflator flange comprises a cylindrical plate coupled with the inflator.

9. The method of claim 1 , wherein the inflator hub comprises a cylindrical recess, and wherein the step of inserting at least a portion of the inflator module into the inflator hub comprises:

extending the inflator into the cylindrical recess; and

extending the inflator flange about an exterior surface of the inflator hub.

10. The method of claim 9 , wherein the step of crimping the inflator flange onto the inflator hub comprises crimping a cylindrical plate about an entire perimeter of the cylindrical plate onto the exterior surface of the inflator hub.

11. The method of claim 1 , wherein the step of crimping the inflator flange onto the inflator hub comprises fixedly coupling the inflator module to the inflator hub without using any fasteners.

12. The method of claim 1 , further comprising coupling a crimping facilitator element to the inflator hub.

13. The method of claim 12 , wherein the step of crimping the inflator flange onto the inflator hub comprises crimping the inflator flange onto a portion of the crimping facilitator element.

14. The method of claim 13 , wherein the crimping facilitator element comprises a ring.

15. The method of claim 14 , wherein the ring comprises a metallic ring, and wherein the inflator flange comprises a metallic inflator flange.

16. The method of claim 15 , wherein the ring further comprises a plurality of holes, and further comprising overmolding a plastic material into at least a subset of the plurality of holes to fixedly couple the ring with the inflator hub.

17. The method of claim 1 , wherein the step of crimping the inflator flange to the inflator hub comprising crimping the inflator flange directly to the inflator hub.

Continuity (3)
Continuation In Part 18207123 · Jun 7, 2023
Continuation 17453178 · Nov 1, 2021
Related Publication 20230398957A1 · Dec 14, 2023
References Cited (38)
US 3801127A · Katter et al. · 1974 [cited by applicant]
US 3909037A · Stewart · 1975 [cited by examiner]
US 3910595A · Katter · 1975 [cited by examiner]
US 5201541A · Jones · 1993 [cited by examiner]
US 5275431A · Stephens · 1994 [cited by examiner]
US 5470105A · Rose · 1995 [cited by examiner]
US 5503426A · Lang · 1996 [cited by examiner]
US 5547213A · Lang · 1996 [cited by examiner]
US 5592812A · Hinshaw · 1997 [cited by examiner]
US 5605347A · Karlow · 1997 [cited by examiner]
US 5692768A · Mihm · 1997 [cited by examiner]
US 5967551A · Newkirk · 1999 [cited by examiner]
US 6364341B1 · Perkins · 2002 [cited by examiner]
US 9039038B2 · Breed et al. · 2015 [cited by applicant]
US 10124759B2 · Smith · 2018 [cited by examiner]
US 10913423B2 · Williams · 2021 [cited by examiner]
US 10988104B2 · Williams · 2021 [cited by examiner]
US 11155235B2 · Breed et al. · 2021 [cited by applicant]
US 11548466B2 · Disam · 2023 [cited by examiner]
US 11572030B1 · Parkinson · 2023 [cited by examiner]
US 20070284863A1 · Bostick · 2007 [cited by examiner]
US 20090250914A1 · Kemp · 2009 [cited by examiner]
US 20180079384A1 · Smith · 2018 [cited by examiner]
US 20190126887A1 · Williams · 2019 [cited by examiner]
US 20190359167A1 · Breed et al. · 2019 [cited by applicant]
US 20200101933A1 · Williams · 2020 [cited by examiner]
US 20220041126A1 · Breed · 2022 [cited by examiner]
DE 102019100262A1 · 2020 [cited by examiner]
EP 0046275A1 · 1982 [cited by applicant]
EP 0046275 · 1985 [cited by applicant]
EP 1911636A1 · 2008 [cited by examiner]
JP 4304849B2 · 2009 [cited by examiner]
WO 9640556 · 1996 [cited by applicant]
WO WO9742063A1 · 1997 [cited by examiner]
WO WO2016062378A1 · 2016 [cited by examiner]
Apr. 11, 2024 Non-Final Rejection, U.S. Appl. No. 18/207,123 (7 pgs). [cited by applicant]
Feb. 21, 2023 International Search Report—PCT/US22/048090 (4 pgs). [cited by applicant]
Feb. 21, 2023 Written Opinion—PCT/US22/048090 (9 pgs). [cited by applicant]