发明名称 Wing/winglet configurations and methods for aircraft
摘要 A wing/winglet configuration, which basically comprises: (a) a wing having upper and lower wing surfaces, a wing leading edge, a wing trailing edge, and a wing tip; and (b) a winglet having upper and lower winglet surfaces, a winglet leading edge, a winglet trailing edge, and a winglet tip, where the winglet is mounted to the wing tip at a winglet/wing tip intersection and extends upwardly from the wing tip Aft portions of the upper wing surface and upper winglet surface are flattened near the winglet/wing tip intersection to substantially reduce flow separation near wing/winglet intersection.
申请公布号 US5275358(A) 申请公布日期 1994.01.04
申请号 US19910739615 申请日期 1991.08.02
申请人 THE BOEING COMPANY 发明人 GOLDHAMMER, MARK I.;SCHIPPERS, KAREL A.
分类号 B64C3/14;B64C23/06;(IPC1-7):B64C5/08 主分类号 B64C3/14
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