发明申请
US20050051671A1 Non-jamming, fail safe flight control system with non-symmetric load alleviation capability
失效
具有非对称负载减轻能力的非干扰,故障安全飞行控制系统
- 专利标题: Non-jamming, fail safe flight control system with non-symmetric load alleviation capability
- 专利标题(中): 具有非对称负载减轻能力的非干扰,故障安全飞行控制系统
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申请号: US10657410申请日: 2003-09-08
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公开(公告)号: US20050051671A1公开(公告)日: 2005-03-10
- 发明人: Mihailo Djuric
- 申请人: Mihailo Djuric
- 主分类号: B64C13/14
- IPC分类号: B64C13/14 ; B64C13/30
摘要:
A non-jamming, fail safe flight control system with non-symmetric load alleviation capability includes a dual cable control system one for each side of control surface, like an elevator or an aileron, controlled by a pilot but driven by a driving system which allows control surfaces to even out the load from one side to the other without affecting pilots control while—if one side becomes jammed—enabling the pilot, with no extra action, to continue flying the aircraft utilizing the other side. In another embodiment an automatic lock feature ensures that a pilot is able to continue to complete the flight in case of severance of a control cable due to a discrete damage without interruption attributable to the control system. Yet another embodiment utilizing either the same or a separate locking feature enables the pilot to lock the surfaces upon parking the aircraft.
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