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.
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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 |
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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