Active Vent and Re-Inflation System for a Crash Attenuation Airbag

• US 20130032665A1
• Filed: 12/29/2010
• Published: 02/07/2013
• Est. Priority Date: 12/29/2010
• Status: Active Grant

• Current Assignee: Textron Innovations Incorporated (Textron Inc)
• Original Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Inventors: Lu, Zi, Tho, Cheng-Ho, Smith, Michael R.
• Granted Patent: US 8,870,115 B2
• Time in Patent Office: Days
• US Class Current: 244/100.A
• CPC Class Codes: B64C 2025/325 specially adapted for helicopters
• CPC Class Codes: B64C 25/52 Skis or runners
• CPC Class Codes: B64C 25/56 inflatable
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use

Abstract

A crash attenuation system has an airbag inflatable generally adjacent to an exterior of the aircraft. The system includes a gas generator in fluid communication with an interior of the airbag. The system also includes a vent system having a vent passage supported by the aircraft, the vent passage being configured to allow gas to escape from within the airbag during an impact. The vent system also includes an actuator door for sealing the vent passage, thereby preventing gas from leaving the airbag. The actuator door is actuated by an actuator, the actuator being in fluid communication with the gas generator through an actuator duct. The system operates such that deployment of gas from the gas generator causes the actuator to inflate, thereby causing the actuator door to seal the vent passage. The gas generator is configured to re-inflate the airbag after the actuator door seals the vent passage.

Claims

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

an airbag inflatable generally adjacent to an exterior of the aircraft;

a first gas generator in fluid communication with an interior of the airbag for inflating the airbag with gas; and

a vent system, the vent system comprising;

a vent passage being configured to allow gas to escape from within the airbag during an impact;

an actuator door configured to selectively seal the vent passage, thereby preventing gas from leaving the airbag;

an actuator located proximate to the actuator door; and

an actuator duct that provides fluid communication between a second gas generator and the actuator;

wherein deployment of gas from the second gas generator causes the actuator to inflate, thereby causing the actuator door to seal the vent passage.

2. The crash attenuation system according to claim 1, wherein the actuator is an airbag actuator.

3. The crash attenuation system according to claim 1, wherein the actuator is a pneumatic actuator.

4. The crash attenuation system according to claim 1, the vent system further comprising:

a latch configured to lock the actuator door in the closed position.

5. The crash attenuation system according to claim 1, the vent system further comprising:

a one-way valve located in the actuator duct to prevent gas from moving away from the actuator.

6. The crash attenuation system according to claim 1, the vent system further comprising:

a pressure release valve configured to allow gas from the second gas generator to re-inflate the airbag after the actuator door has created a seal in the vent passage.

7. The crash attenuation system according to claim 6, wherein the pressure release valve is a blow-away door.

8. The crash attenuation system according to claim 1, further comprising:

a sensor system configured to detect a type of crash impact surface; and

a control system configured to selectively re-inflate the airbag based on the detected type of crash impact surface.

9. The crash attenuation system according to claim 1, wherein the actuator door is hingedly connected to the vent passage.

10. The crash attenuation system according to claim 1, further comprising:

a stop located in the vent passage, the stop being configured so that the actuator door is closed against the stop.

11. The crash attenuation system according to claim 10, further comprising:

a seal between the stop and the actuator door.

12. The crash attenuation system according to claim 1, further comprising:

a grate located in the vent passage, the grate being configured to provide positive pressure against the actuator when the actuator is deployed.

13. The crash attenuation system according to claim 1, further comprising:

a shear pin configured to selectively keep the actuator door in an open position.

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

an airbag inflatable generally adjacent to an exterior of the aircraft;

a gas generator having at least a first port and a second port, the first port being in fluid communication with an interior of the airbag; and

a vent system, the vent system comprising;

a vent passage being configured to allow gas to escape from within the airbag during an impact;

an actuator door configured to selectively seal the vent passage, thereby preventing gas from leaving the airbag;

an actuator located proximate to the actuator door; and

an actuator duct that provides fluid communication between the second port and the actuator;

wherein deployment of gas from the second gas generator causes the actuator to inflate, thereby causing the actuator door to close, thereby sealing the vent passage.

15. The crash attenuation system according to claim 14, the vent system further comprising:

a blow-away door configured to selectively allow gas from the second gas generator to re-inflate the airbag after the actuator door has created a seal in the vent passage.

16. The crash attenuation system according to claim 14, further comprising:

a frame located in the vent passage, the frame being configured to create a seal between the actuator door and the vent passage.

17. The crash attenuation system according to claim 14, further comprising:

a sensor system configured to detect a type of crash surface; and

a control system configured to selectively re-inflate the airbag based on the detected type of crash surface.

18. A method of operating a crash attenuation airbag on an aircraft, the method comprising:

detecting a crash condition of the aircraft, the crash condition indicating that subsequent flotation of the aircraft is desirable;

inflating the crash attenuation airbag prior to impact, the inflating occurring with a gas generator;

venting the crash attenuation airbag during impact, the venting occurring by allowing gas to exit the airbag through a vent passage;

sealing the vent passage in order to cease venting of the airbag, the sealing of the vent passage occurring by closing an actuator door by communicating pressurized gas to an actuator, the pressurized gas sourcing from the gas generator, the actuator expanding from the pressurized gas so as to forcibly close the actuator door; and

re-inflating the airbag with the gas generator so that the airbag aids in flotation of the aircraft.

19. The method according to claim 18, wherein the step of re-inflating the airbag occurs when a blow-away door allows air to enter the airbag.

20. The method according to claim 18, wherein the step of sealing the vent passage closes the actuator door against a stop, the stop being located in the vent passage.

21. The method according to claim 18, wherein the step of sealing the vent passage shears a shear pin so as to allow the actuator door to release.

22. The method according to claim 18, wherein the gas generator has a plurality of ports, each port being independently capable of providing pressurized gas, each port also being controlled by a gas controller.