ACTIVE POSITIONING AIRBAG ASSEMBLY AND ASSOCIATED SYSTEMS AND METHODS

• US 20160096627A1
• Filed: 10/02/2014
• Published: 04/07/2016
• Est. Priority Date: 10/02/2014
• Status: Active Grant

• Current Assignee: AmSafe, Inc. (Transdigm Group Incorporated)
• Original Assignee: AmSafe, Inc. (Transdigm Group Incorporated)
• Inventors: Gehret, William J., Foubert, Daniel Nick
• Granted Patent: US 9,352,839 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B60R 2021/0093 Aircraft
• CPC Class Codes: B60R 2021/2074 in head rests
• CPC Class Codes: B60R 2021/23153 specially adapted for rear seat passengers
• CPC Class Codes: B60R 21/207 in vehicle seats
• CPC Class Codes: B64D 11/06205 Arrangements of airbags
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

Airbag assemblies and associated systems and methods for use in aircraft and other vehicles are described herein that can provide crash protection for occupants seated in an upright position while not injuring or striking occupants in the brace position. An airbag system configured in accordance with an embodiment of the present technology can include an airbag configured to deploy through an opening of a housing during a crash event. The housing can be affixed to a seat or other interior portion (e.g., a fixed portion) of an aircraft forward of a passenger seat. The airbag can initially deploy in a direction away from an occupant in the seat and then move into position between a potential strike hazard and the occupant such that the airbag system can be used to protect occupants seated in an upright position while not injuring occupants in the brace position.

Claims

1. An airbag system for use with an aircraft seat, the airbag system comprising:

an airbag stowed in a housing positioned forward of the aircraft seat and above a strike area associated with the aircraft seat, wherein the airbag includes an upper portion and a lower portion, wherein, in response to a crash event, the upper portion is configured to inflate proximate the housing and deploy in a generally upward direction away from the strike area, the lower portion is configured to inflate from the upper portion and deploy in a generally horizontal direction to an upper position above the strike area, and after the lower portion has inflated and deployed to the upper position, the lower portion is configured to move downwardly from the upper position to a lower position between the strike area and an occupant seated in a generally upright position in the aircraft seat.

23. The airbag system of claim 1 wherein the lower portion moves from a generally horizontal orientation in the upper position to a generally vertical orientation in the lower position.

24. The airbag system of claim 1 wherein the upper portion is configured to extend in a generally horizontal direction and the lower portion is configured to extend in a generally vertical direction when the airbag is fully deployed.

25. The airbag system of claim 1 wherein the aircraft seat is a first forward-facing seat, and wherein the airbag housing is mounted to an upper portion of a second forward-facing seat positioned forward of the first seat.

26. The airbag system of claim 1 wherein the aircraft seat is a forward-facing seat, and wherein the airbag housing is mounted to a fixed structure positioned forward of the aircraft seat in an interior of the aircraft.

2-3. -3. (canceled)

4. An airbag system for use with an aircraft seat, the airbag system comprising:

and airbag stowed in a position forward of the aircraft seat and above a strike area associated, with the aircraft seat, wherein the airbag is configured to inflate and deploy in a generally upward direction away from the strike area, and then downwardly to a position between the strike area and an occupant seated in a generally upright position in the aircraft seat, in response to a crash event.

5. The airbag system of claim 4 wherein the airbag is configured to deploy downwardly to a position adjacent to a back portion of an occupant seated in a brace position in the aircraft seat.

6. The airbag system of claim 4 wherein the aircraft seat is a forward-facing seat relative to a longitudinal axis of the aircraft.

7. The airbag system of claim 4 wherein the aircraft seat is a first forward-facing seat, and wherein the airbag is mounted to an upper portion of a second forward-facing seat positioned forward of the first seat.

8. The airbag system of claim 4 wherein the aircraft seat is a forward-facing seat, and wherein the airbag is mounted to a fixed structure positioned forward of the aircraft seat in an interior of the aircraft.

9. The airbag system of claim 4 wherein the airbag is configured to deploy in a generally horizontal direction after deploying in the generally upward direction and before deploying in the second generally downward direction.

10. The airbag system of claim 4 wherein the airbag is configured to deploy in a generally horizontal direction toward the aircraft seat after deploying in the generally upward direction and before deploying in the generally downward direction.

11. The airbag system of claim 4 wherein the airbag has a generally inverted L-shaped cross-sectional shape.

12. The airbag system of claim 4 wherein the airbag includes a first portion and a second portion, wherein the first portion is configured to extend generally perpendicular to the second portion when the airbag is fully deployed.

13. The airbag system of claim 4 wherein the airbag includes a first portion and a second portion, wherein the first portion is configured to extend in a generally horizontal direction, and the second portion is configured to extend downwardly in a generally vertical direction, when the airbag is fully deployed.

14. The airbag system of claim 4, further comprising a housing having an opening positioned forward of the aircraft seat, wherein the airbag is stowed in the housing and configured to deploy through the opening in response to the crash event.

15. The airbag system of claim 14, further comprising an inflator positioned within the housing in fluid communication with the airbag to provide gas for inflating the airbag in response to the crash event.

16. The airbag system of claim 14, further comprising an inflator remotely located from the housing in fluid communication with the airbag to provide gas for inflating the airbag in response to the crash event.

17. An airbag system for use with an aircraft seat, the airbag system comprising:

an airbag stowed above a strike hazard forward of the aircraft seat; and

means for deploying the airbag in a generally upward direction away from the strike hazard, and then downwardly to a position between the strike hazard and an occupant seated in the aircraft seat to protect the occupant during a crash event, wherein deploying the airbag protects the occupant from striking the hazard forward of the aircraft seat when the occupant is seated in an upright orientation during the crash event, and wherein deploying the airbag avoids inflating the airbag against the occupant when the occupant is seated in an out-of-position orientation during the crash event.

18. The airbag system of claim 17 wherein the out-of-position orientation is a brace position.

19. A method of deploying an airbag between a strike hazard positioned forward of an aircraft seat and an occupant seated in the aircraft seat, the method comprising:

detecting a deceleration event above a preset magnitude;

inflating the airbag from a housing positioned above the strike hazard in response to detecting the deceleration event, wherein inflating the airbag includes initially deploying the airbag from the housing in a first direction away from the strike hazard, and then deploying the airbag in a second direction toward the strike hazard to position the airbag between the strike hazard and the occupant seated in the aircraft seat.

20. The method of claim 19 wherein deploying the airbag in the first direction includes deploying the airbag in an upwardly direction, and wherein deploying the airbag in the second direction includes deploying the airbag in a downwardly direction.

21. The method of claim 20, wherein inflating the airbag further comprises deploying the airbag in a generally horizontal rearward direction toward the aircraft seat after deploying the airbag in the upwardly direction and before deploying the airbag in the downwardly direction.

22. The method of claim 19 wherein inflating the airbag further comprises inflating the airbag above the occupant if the occupant is seated in a brace position.