发明名称 AIRFOIL WITH AN INTEGRALLY STIFFENED COMPOSITE COVER
摘要 An airfoil according to an exemplary aspect of the present disclosure includes, among other things, a main body extending between a leading edge and a trailing edge separated in a chordwise direction and extending between a tip and a root in a spanwise direction. The main body defines a suction side and a pressure side separated in a thickness direction and a plurality of channels extending inwardly from at least one of said suction and pressure sides. A composite cover is attached to the main body. The composite cover includes a plurality of stiffeners each received within one of the channels. A cover skin is adjacent the stiffeners, and an over-wrap surrounds the stiffeners and the cover skin.
申请公布号 WO2015034630(A1) 申请公布日期 2015.03.12
申请号 WO2014US50614 申请日期 2014.08.12
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FOSTER, LARRY
分类号 F01D5/14;F04D29/24;F04D29/38 主分类号 F01D5/14
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