发明名称 Composite flexural yoke for helicopters
摘要 A yoke for coupling helicopter blades to a mast is provided. The yoke comprises a long oval loop of glass fibers embedded in a cured adhesive to form a solid strap. The side portions of the loop are reinforced with layers of bias ply glass fibers arranged in parallel planes. Structure is provided to couple to the side portions of the loop for attachment to the mast.
申请公布号 US4227857(A) 申请公布日期 1980.10.14
申请号 US19770826111 申请日期 1977.08.19
申请人 TEXTRON, INC. 发明人 REYES, PETER A.
分类号 B64C27/43;(IPC1-7):B64C27/36 主分类号 B64C27/43
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