发明授权
- 专利标题： Aircraft wing extension and nozzle system
- 专利标题（中）： 飞机机翼延伸和喷嘴系统
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申请号： EP11187906.0申请日： 2011-11-04
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公开(公告)号： EP2452873B1公开(公告)日： 2015-04-01
- 发明人: Robertson, Daniel B , Groninga, Kirk L
- 申请人： Bell Helicopter Textron Inc.
- 申请人地址： P.O. Box 482 Fort Worth, TX 76101 US
- 专利权人： Bell Helicopter Textron Inc.
- 当前专利权人： Bell Helicopter Textron Inc.
- 当前专利权人地址： P.O. Box 482 Fort Worth, TX 76101 US
- 代理机构： Lawrence, John
- 优先权： US201113224902 20110902; PCT/US2010/056571 20101112
- 主分类号： B64C3/54
- IPC分类号： B64C3/54 ; B64C15/02 ; B64C27/26 ; B64C27/82
摘要：
A system and method to control flight of an aircraft. The aircraft (101; 1001) having an engine (111; 1017) with a rotatably nozzle assembly (401) configured to create forward propulsion and yaw control of the aircraft (101; 1001). The engine exhaust (129c) passing through the nozzle (401) is redirected with a valve (419) disposed within the nozzle (401). Lift is created with a lift system (1009) carried by the wing (1007) of the aircraft (1001). Additional lift is created during flight with a retractable wing extension (1015) disposed within the wing (1007) of the aircraft (1001).
公开/授权文献
- EP2452873A3 Aircraft wing extension and nozzle system 公开/授权日：2014-01-01
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