Invention Grant
- Patent Title: Crash attenuation system for aircraft
- Patent Title (中): 飞机衰减衰减系统
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Application No.: US12089884Application Date: 2006-11-08
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Publication No.: US07954752B2Publication Date: 2011-06-07
- Inventor: Michael R. Smith , Somen Chowdhury , Cheng-Ho Tho
- Applicant: Michael R. Smith , Somen Chowdhury , Cheng-Ho Tho
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Agent James E. Walton
- International Application: PCT/US2006/043706 WO 20061108
- International Announcement: WO2008/054401 WO 20080508
- Main IPC: B64C25/56
- IPC: B64C25/56 ; B64D25/18

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 first gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first 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. A second gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.
Public/Granted literature
- US20100044507A1 Crash Attenuation System for Aircraft Public/Granted day:2010-02-25
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