发明申请
- 专利标题: YAW CONTROL IN AN AIRCRAFT
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申请号: US15166369申请日: 2016-05-27
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公开(公告)号: US20170341731A1公开(公告)日: 2017-11-30
- 发明人: Kenneth Merle Dorsett , Robert Carl Storrie
- 申请人: Lockheed Martin Corporation
- 主分类号: B64C9/34
- IPC分类号: B64C9/34 ; B64C13/28 ; B64C9/02
摘要:
In one embodiment, an apparatus includes a first deflector configured to couple to a shaft of a wing of an aircraft and form part of a top surface of the wing when in a first closed position, and a second deflector configured to couple to the shaft and form part of a bottom surface of the wing when in a second closed position. The first deflector and the second deflector may be configured to be positioned proximate to the tip of the wing. 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.