Invention Grant
US09180962B2 Leading edge variable camber system and method 有权
前缘可变外倾系统及方法

Leading edge variable camber system and method
Abstract:
A system for varying a wing camber of an aircraft wing may include a leading edge device coupled to the wing. The leading edge device may be configured to be actuated in an upward direction and a downward direction relative to a retracted position of the leading edge device.
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