发明名称 Helicopter blade retention composite yoke
摘要 A rotary wing aircraft yoke (40) is provided including an arcuate medial portion (42). A pair of arms (44a, 44b) extends from the medial portion (42) and each terminates in a distal end (46a, 46b). The yoke (40) is made from multiple plies of glass and graphite fibers of varying orientations. The number of graphite plies increases along each arm from adjacent the medial portion (42) to the distal ends (46a, 46b).
申请公布号 EP2634091(A1) 申请公布日期 2013.09.04
申请号 EP20120199470 申请日期 2012.12.27
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 CABRERA, PEDRO L.;DEYO, KENNETH F.;TEMPLETON, DAVID;LAITENBERGER, KEVIN
分类号 B64C27/48 主分类号 B64C27/48
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