发明名称 |
Leading and trailing edge device deflections during descent of an aircraft |
摘要 |
<p>A system (300) for increasing the descent rate of an aircraft may include a flight control computer(450), an edge control system (460), and a speedbrake control device (532). The flight control computer may be configured to compute a first setting for a leading edge device (150) and/or a trailing edge device (240) of an aircraft wing. The edge control system may be communicatively coupled to the flight control computer and may include an edge control device (453) having a plurality of control device positions (458) including a cruise position (462). The speedbrake control device may include a plurality of speedbrake detents (536) including a flight detent (542). The edge control system (460) may be configured to automatically command the leading edge device (150), the trailing edge device (240), or both, to a deflection angle corresponding to the first setting if the edge control device is in the cruise position and the speedbrake control device is in the flight detent.</p> |
申请公布号 |
EP2851289(A1) |
申请公布日期 |
2015.03.25 |
申请号 |
EP20140186027 |
申请日期 |
2014.09.23 |
申请人 |
THE BOEING COMPANY |
发明人 |
MOSER, MATTHEW A;LIU, BENJAMIN M;FINN, MICHAEL R |
分类号 |
B64C9/32;B64C13/16;B64C19/02;G05D1/00;G05D1/06 |
主分类号 |
B64C9/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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