发明申请
- 专利标题: BODY TAB YAW DEFLECTOR
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申请号: US15479654申请日: 2017-04-05
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公开(公告)号: US20170341730A1公开(公告)日: 2017-11-30
- 发明人: Kenneth Merle Dorsett
- 申请人: Lockheed Martin Corporation
- 主分类号: B64C9/02
- IPC分类号: B64C9/02 ; B64C9/34 ; B64C3/10
摘要:
In one embodiment, an apparatus includes a first deflector configured to couple to a shaft of an aircraft. The first deflector may form part of a top surface of the aircraft when in a first closed position. The apparatus may further include a second deflector configured to couple to the shaft and form part of a bottom surface of the aircraft when in a second closed position. The first deflector and the second deflector may be configured to be positioned at a junction of a body of the aircraft and a wing of the aircraft. The first deflector and the second deflector may be configured to simultaneously pivot from the closed positions to respective first and second open positions upon actuation of the shaft.
公开/授权文献
- US10370085B2 Body tab yaw deflector 公开/授权日:2019-08-06
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