Crash attenuation system for aircraft

• US 8,418,957 B2
• Filed: 05/18/2011
• Issued: 04/16/2013
• Est. Priority Date: 11/09/2005
• Status: Active Grant

• Current Assignee: Textron Innovations Incorporated (Textron Inc)
• Original Assignee: Textron Innovations Incorporated (Textron Inc)
• Inventors: Smith, Michael R., Tho, Cheng-Ho, Chowdhury, Somen
• Primary Examiner(s): Timothy, Collins
• Assistant Examiner(s): Badawi, Medhat
• Application Number:
  US13/110,607
• Publication Number:
  US 20110226898A1
• Time in Patent Office: 699 Days
• Field of Search: None
• 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, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. The gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.

Claims

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

an airbag carried by the aircraft and inflatable generally adjacent to a position exterior of the aircraft, the airbag having at least one vent for releasing gas from the interior of the airbag for crash attenuation;

a gas source in fluid communication with the interior of the airbag for inflating the airbag to the position exterior of the aircraft with gas provided by the gas source;

a vent valve for controlling a flow of gas through each of the at least one vent, each vent valve being selectively configurable to adjust between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag;

a control system configured to activate and adjust the vent valve prior to and after impact; and

wherein the gas source is in fluid communication with the interior of the airbag for at least partially re-inflating the airbag with gas provided by the gas source after venting of gas through the at least one vent.

2. The crash attenuation system according to claim 1, wherein the gas source is a gas generator.

3. The crash attenuation system according to claim 1, wherein the gas source is a compressed gas tank.

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

a water-detection system for detecting the presence of water.

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

a water-detection system for detecting the presence of water;

wherein when the water-detection system detects water, each vent valve is switched to the closed state, and the gas source is used to at least partially re-inflate the airbag.

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

an airbag carried by the aircraft and inflatable generally adjacent to a position exterior of the aircraft, the airbag having a vent configured to release gas from the interior of the airbag for crash attenuation;

a gas source in fluid communication with the interior of the airbag, the gas source configured to inflate the airbag to the position exterior of the aircraft with gas provided by the gas source;

a vent valve configured to control a flow of gas through the vent, the vent valve being selectively configurable to adjust between an open state, in which gas can pass through the vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag;

a control system configured to activate and adjust the vent valve prior to and after impact;

a water-detection system for detecting the presence of water; and

wherein the gas source is in fluid communication with the interior of the airbag for at least partially re-inflating the airbag with gas provided by the gas source.

7. The crash attenuation system according to claim 6, wherein the gas source is a gas generator.

8. The crash attenuation system according to claim 6, wherein the gas source comprises compressed gas.

9. The crash attenuation system according to claim 6, further comprising:

wherein the water-detection system is configured to switch the vent valve to the closed state upon detection of water.

10. The crash attenuation system according to claim 6, wherein the water-detection system is configured to direct the gas source to at least partially re-inflate the airbag upon detection of water.