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.
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
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