发明申请
- 专利标题: Crash Attenuation System for Aircraft
- 专利标题(中): 飞机衰减衰减系统
-
申请号: US12089884申请日: 2006-11-08
-
公开(公告)号: US20100044507A1公开(公告)日: 2010-02-25
- 发明人: Michael R. Smith , Somen Chowdhury , Cheng-Ho Tho
- 申请人: Michael R. Smith , Somen Chowdhury , Cheng-Ho Tho
- 国际申请: PCT/US2006/043706 WO 20061108
- 主分类号: B64C25/56
- IPC分类号: B64C25/56 ; B64D25/00
摘要:
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.
公开/授权文献
- US07954752B2 Crash attenuation system for aircraft 公开/授权日:2011-06-07
信息查询