发明名称 HIGH-POSITIONED 3-POSITION VARIABLE CAMBER KRUEGER
摘要 <p>A system and method to enable natural laminar flow over a fluid-dynamic body using a variable camber Krueger flap (306) is disclosed. A sequence of flap positions is deployed where the variable camber Krueger flap (306) is below and aft of the wing leading edge (402, 540) before reaching a configured takeoff and landing position (554, 702). The variable camber Krueger flap (306) is positioned in a high position relative to a wing leading edge (402, 540) when the variable camber Krueger flap (306) is fully deployed.</p>
申请公布号 CA2795637(A1) 申请公布日期 2013.08.10
申请号 CA20122795637 申请日期 2012.11.14
申请人 THE BOEING COMPANY 发明人 SAKURAI, SEIYA;FOX, STEPHEN J.;REYES, VICTOR;CHARLES, KARA MARIE
分类号 B64C3/44;B64C3/50;B64C9/04;B64C13/24 主分类号 B64C3/44
代理机构 代理人
主权项
地址