发明申请
- 专利标题: Rotor wing aircraft having an adjustable tail nozzle
- 专利标题(中): 转翼翼飞机具有可调式尾喷嘴
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申请号: US11265655申请日: 2005-11-02
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公开(公告)号: US20070095970A1公开(公告)日: 2007-05-03
- 发明人: Steven Richardson
- 申请人: Steven Richardson
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 主分类号: B64C27/24
- IPC分类号: B64C27/24 ; B64C15/12
摘要:
Aircraft including an airframe having a fuselage extending between a forward end and an aft end and a fixed wing extending laterally from the fuselage. The aircraft includes a power plant mounted on the airframe producing exhaust during operation. The aircraft includes a rotor/wing rotatably mounted on the airframe including a plurality of blades and an adjustable nozzle mounted on the airframe downstream from the power plant exhaust for selectively directing the power plant exhaust to exit the aircraft at a pre-selected angle with respect to the airframe within a range of angles extending from about horizontally rearward to about vertically downward.
公开/授权文献
- US07395988B2 Rotor wing aircraft having an adjustable tail nozzle 公开/授权日:2008-07-08
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