发明名称 Structural attach method for thin fairings
摘要 A method, system, and apparatus for attaching a fairing to a body or aircraft wing are disclosed. A plurality of attach anchors is disposed on the body or aircraft wing to which the fairing is to be attached. Disposed in the fairing is a plurality of core pockets that are alignable with the plurality of attach anchors, and each of the core pockets defines a channel. The fairing is placed over the body or the aircraft wing such that the heads of the attach anchors are received in the core pockets. The fairing is then slid across the body or the aircraft wing with the channels sliding along the heads of the attach anchors such that the fairing is prevented from being lifted away from the body or aircraft wing.
申请公布号 US2004124311(A1) 申请公布日期 2004.07.01
申请号 US20020334452 申请日期 2002.12.31
申请人 KORDEL JAN A.;TANNER RICHARD B. 发明人 KORDEL JAN A.;TANNER RICHARD B.
分类号 B64C3/26;B64F5/00;(IPC1-7):B64C1/06 主分类号 B64C3/26
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