发明名称 |
Nacelle/wing assembly with wake control device |
摘要 |
In a wing and nacelle combination, where the nacelle is positioned below and forwardly of the wing leading edge, a wake control device to control a turbulent wake which is formed at the upper forward lip portion of the nacelle. This wake control device comprises a forward vortex generating portion to create a vortex which travels over the leading edge of the wing, and also a fence located at the middle third of the nacelle to control boundary layer air and thus properly locate the wake control vortex.
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申请公布号 |
US4540143(A) |
申请公布日期 |
1985.09.10 |
申请号 |
US19830520826 |
申请日期 |
1983.08.04 |
申请人 |
THE BOEING COMPANY |
发明人 |
WANG, TIMOTHY;ZIERTEN, THOMAS A. |
分类号 |
B64C23/06;B64D29/02;(IPC1-7):B64C23/06 |
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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