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 |
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代理人 |
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主权项 |
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地址 |
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