Aircraft air pads having restricted deployment volumes

Patent metadata

Field	Value
Publication number	US-10696406-B2
Application number	US-201815980227-A
Country	US
Kind code	B2
Filing date	May 15, 2018
Priority date	May 15, 2018
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

Systems and methods are provided for inflatable air pads for aircraft. One embodiment is an apparatus that includes an air pad affixed to a mount within an interior of an aircraft. The air pad includes a front face, a bladder that is inflatable within the air pad, and sides that constrain the front face of the air pad to extend a uniform distance outward from the mount when the bladder is inflated. The apparatus also includes an inflator that is coupled with the air pad and is configured to inflate the bladder from an undeployed volume to a deployed volume.

First claim

What is claimed is:

1. An apparatus comprising:
an air pad affixed to a mount within an interior of an aircraft, wherein the air pad includes a gap at a location of a component installed in a seat back of the aircraft, the air pad comprising:
a front face;
a bladder that is inflatable and constrained to extend a uniform distance outward from the mount when the bladder is inflated; and

an inflator that is coupled with the air pad and is configured to inflate the bladder from an undeployed volume to a deployed volume.

2. The apparatus of claim 1 wherein:
a maximum amount of the uniform distance during inflation of the bladder is between one and four inches.

3. The apparatus of claim 1 wherein:
the air pad is shaped in a form of the seat back of the aircraft.

4. The apparatus of claim 1 wherein:
the air pad is mounted to a seat back of the aircraft.

5. The apparatus of claim 1 wherein:
the air pad further comprises an additional bladder at an edge of the gap which is inflated by the inflator and expands into the gap during deployment.

6. The apparatus of claim 5 further comprising:
a gap at a location of a display installed in the seat back, wherein the air pad further comprises an additional bladder that covers the display during deployment of the air pad.

7. The apparatus of claim 1 wherein:
the bladder covers a portion of the seat back during deployment that is exposed prior to deployment.

8. The apparatus of claim 1 wherein:
the bladder inflates around corners of a display.

9. A system comprising:
an air pad affixed to a mount within an interior of an aircraft, wherein the air pad includes a gap at a location of a component installed in a seat back of the aircraft, the air pad comprising:
a front face;
a bladder that is constrained to to extend a uniform distance outward from the mount when the bladder is inflated;

an inflator that is coupled with the air pad and is configured to inflate the bladder from an undeployed volume to a deployed volume;
a sensor that determines a deceleration of the aircraft; and
a controller that receives input from the sensor indicating the deceleration of the aircraft, determines that the deceleration of the aircraft has exceeded a threshold value for longer than a period of time, and triggers the inflator for the air pad to deploy the air pad.

10. The system of claim 9 wherein:
a maximum amount of the uniform distance during inflation of the bladder is between one and four inches.

11. The system of claim 9 wherein:
the air pad is shaped in a form of the seat back of the aircraft.

12. The system of claim 9 wherein:
the air pad is mounted to a seat back of an aircraft.

13. The system of claim 9 wherein:
the air pad further comprises an additional bladder at an edge of the gap which is inflated by the inflator and that covers the gap during deployment.

14. The system of claim 13 further comprising:
a gap at a location of a display installed in the seat back, wherein the air pad further comprises an additional bladder that covers the display during deployment of the air pad.

15. The system of claim 9 wherein:
the bladder covers a portion of the seat back during deployment that is exposed prior to deployment.

16. The system of claim 9 wherein:
the bladder inflates around corners of a display.

17. A method comprising:
receiving input from a sensor indicating a deceleration of an aircraft;
determining that the deceleration of the aircraft has exceeded a threshold value for longer than a period of time;
triggering an inflator for an air pad that is mounted within an interior of the aircraft and includes a bladder that is constrained to extend a uniform distance outward when the bladder is inflated, wherein the air pad includes a gap at a location of a component installed in a seat back of the aircraft; and
deploying the bladder by inflating the bladder.

18. The method of claim 17 wherein:
the threshold value is sixteen Gravities (G's), and the period of time is two milliseconds.

19. The method of claim 17 wherein:
the bladder covers a portion of the seat back during deployment that is exposed prior to deployment.

20. The method of claim 17 wherein:
the bladder inflates around corners of a display during deployment.

Assignees

• Boeing Co

Inventors

• Kabir Mohammed H
• Byar Alan D
• Leon Jan M
• Depauw Todd C

Classifications

• B64D11/0621 Primary

  Airbag initiation or activation means · CPC title

• B64D25/00

  Emergency apparatus or devices, not otherwise provided for · CPC title

• B60R2021/0093

  Aircraft · CPC title

• B64D11/06205 Primary

  Arrangements of airbags · CPC title

• B64D2201/00

  Airbags mounted in aircraft for any use · CPC title