Aircraft Occupant Protection System

• US 20110204181A1
• Filed: 07/27/2009
• Published: 08/25/2011
• Est. Priority Date: 10/22/2007
• Status: Active Grant

• Current Assignee: Textron Innovations Incorporated (Textron Inc)
• Original Assignee: Textron Innovations Incorporated (Textron Inc)
• Inventors: Tho, Cheng-Ho, Lu, Zi, Hill, Andrew T., Smith, Michael R.
• Granted Patent: US 8,474,753 B2
• Time in Patent Office: Days
• US Class Current: 244/100.A
• CPC Class Codes: B64C 27/04 Helicopters
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C

Abstract

A crash attenuation system for an aircraft includes an airbag carried by the aircraft that is inflatable generally adjacent an exterior of the aircraft. The airbag is in fluid communication with at least one vent passage for channeling gas from within the interior of the airbag to a region external to the airbag that allows the gas to escape without being obstructed by the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag. A vent valve is provided within the vent passage for controlling a flow of gas through the vent passage, thereby controlling deflation of the airbag. The vent valve is continuously adjustable to and between an open state, a closed state, and any number of partially open states.

Claims

1. A crash attenuation system for an aircraft, the system comprising:

an airbag assembly carried by the aircraft and inflatable generally adjacent an exterior of the aircraft, the airbag assembly comprising;

first and second inflatable airbags; and

a vent system, the vent system comprising first and second vent passages supported by the aircraft, the first and second vent passages each having a respective one of first and second continuously adjustable vent areas through which gas can escape from within the first airbag;

a gas source system in fluid communication with an interior of at least one of the first and second airbags for inflating at least one of the first and second airbags with gas provided by a gas source;

a sensor system for detecting selected crash conditions; and

a control system for controlling the first vent system and the second vent system independently of one another based on the detected crash conditions;

wherein the first vent passage extends between a first opening in the first vent passage and a second opening in the first vent passage; and

wherein the first opening is in fluid communication with the interior of the first airbag, and the second opening is positioned beyond an outermost extent of the first airbag when the first airbag is inflated.

2. The crash attenuation system according to claim 1, wherein the first vent system comprises an active vent valve for controlling at least a portion of the first adjustable vent area.

3. The crash attenuation system according to claim 2, wherein the active vent valve includes a vent plate that is continuously adjustable between a fully closed position and a fully open position.

4. The crash attenuation system according to claim 3, wherein the vent plate is hingedly connected to the vent passage.

5. The crash attenuation system according to claim 3, wherein the first vent passage includes a shoulder, and wherein the vent plate is in contact with the shoulder when the vent plate is in the fully closed position.

6. The crash attenuation system according to claim 5, further comprising a locking system for locking the vent plate in the fully closed position.

7. The crash attenuation system according to claim 1, wherein the first vent system comprises a pop-off pressure release mechanism.

8. The crash attenuation system according to claim 1, wherein the control system determines a first open vent area for the first adjustable vent area based on one or more of the detected crash conditions and wherein the control system determines a second open vent area for the second adjustable vent area based on one or more of the detected crash conditions.

9. The crash attenuation system according to claim 1, wherein at least one of the first and second vent passages extends below the aircraft.

10. The crash attenuation system according to claim 1, wherein at least one of the first and second vent passages extends through at least a portion of the aircraft.

11. A crash attenuation system for an aircraft, the system comprising:

an airbag assembly carried by the aircraft and inflatable generally adjacent an exterior of the aircraft, the airbag assembly comprising an airbag and a vent system,

wherein the vent system comprises a vent passage supported by the aircraft, the vent passage having a continuously adjustable vent area through which gas can escape from within the first airbag;

a gas source system in fluid communication with an interior of the airbag;

a sensor system for detecting selected crash conditions; and

a control system for controlling rate at which gas can escape from within the airbag through the vent passage based on the detected crash conditions;

wherein the vent passage extends between a first opening in the vent passage and a second opening in the vent passage; and

wherein the first opening is in fluid communication with the interior of the airbag, and the second opening is positioned beyond an outermost extent of the airbag when the airbag is inflated.

12. The crash attenuation system according to claim 11, wherein the vent system comprises an active vent valve for controlling at least a portion of the adjustable vent area.

13. The crash attenuation system according to claim 12, wherein the active vent valve includes a vent plate that is continuously adjustable between a fully closed position and a fully open position.

14. The crash attenuation system according to claim 13, wherein the vent plate is hingedly connected to the vent passage.

15. The crash attenuation system according to claim 13, wherein the vent passage includes a shoulder, and wherein the vent plate is in contact with the shoulder when the vent plate is in the fully closed position.

16. The crash attenuation system according to claim 15, further comprising a locking system for locking the vent plate in the fully closed position.

17. The crash attenuation system according to claim 11, wherein the vent system comprises a pop-off pressure release mechanism.

18. The crash attenuation system according to claim 17, wherein the control system determines an open vent area for the adjustable vent area based on one or more of the detected crash conditions.

19. The crash attenuation system according to claim 11, wherein at least one of the first and second vent passages extends below the aircraft.

20. The crash attenuation system according to claim 11, wherein at least one of the first and second vent passages extends through at least a portion of the aircraft.