发明名称 FORWARD SWEPT WINGLET
摘要 An aircraft may include a pair of wings. A forward swept winglet may be attached proximate to a wing tip of each wing. The forward swept winglet may include a leading edge and a trailing edge. The leading edge of each winglet may extend from the wing at a predetermined forward sweep angle relative to a line perpendicular to a chord of the wing tip in a direction corresponding to a forward portion of the aircraft.
申请公布号 CA2748875(A1) 申请公布日期 2012.04.15
申请号 CA20112748875 申请日期 2011.08.12
申请人 THE BOEING COMPANY 发明人 RAWDON, BLAINE K.;VASSBERG, JOHN C.
分类号 B64C23/06;B64C3/10;B64C5/08 主分类号 B64C23/06
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