发明名称 LEADING EDGE FLAP METHOD
摘要 A method of reducing drag of a leading edge device having first and second flow surfaces includes coupling the first flow surface to an airfoil and coupling the second flow surface to the first flow surface. The leading edge device may be moved between a retracted position and an extended position. The second flow surface may be positioned generally behind the first flow surface during at least a portion of the movement of the leading edge device between the retracted and extended positions
申请公布号 US2011024575(A1) 申请公布日期 2011.02.03
申请号 US20100897646 申请日期 2010.10.04
申请人 THE BOEING COMPANY 发明人 WHEATON JAMES M.;AMOROSI STEPHEN R.
分类号 B64C3/50 主分类号 B64C3/50
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