发明名称 WING TIP DEVICE FOR AN AIRCRAFT WING
摘要 A wing tip device for an aircraft wing may include an upper winglet and a lower element. The upper winglet may extend upwardly from an aircraft wing. The lower element may extend downwardly from the upper winglet and may form a closed loop below the wing. The closed loop may have a hollow interior.
申请公布号 CA2879294(A1) 申请公布日期 2015.10.12
申请号 CA20152879294 申请日期 2015.01.21
申请人 THE BOEING COMPANY 发明人 ZAMAN, ABUMUHAMMED A.
分类号 B64C5/08;B64C3/52;B64C3/58 主分类号 B64C5/08
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