发明名称 High-positioned 3-position variable camber Krueger flap
摘要 A system and method to enable natural laminar flow over a fluid-dynamic body using a variable camber Krueger flap (502) is disclosed. A sequence of flap positions is deployed where the variable camber Krueger flap (502) is below and aft of the wing leading edge before reaching a configured takeoff (556) and landing (554) position. The variable camber Krueger flap (502) is positioned in a high position relative to a wing leading edge (540) when the variable camber Krueger flap (502) is fully deployed.
申请公布号 EP2626295(A3) 申请公布日期 2014.09.10
申请号 EP20120193411 申请日期 2012.11.20
申请人 THE BOEING COMPANY 发明人 SAKURAI, SEIYA;FOX, STEPHEN J.;REYES, VICTOR;CHARLES, KARA MARIE
分类号 B64C9/22;B64C9/24 主分类号 B64C9/22
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