发明名称 STRAIN ISOLATED TRIM TAB
摘要 A rotor blade assembly system includes a trim tab assembly which utilizes relatively thick resilient members bonded between a trim tab and the two trim tab doublers. Spanwise segmenting of the tab and the use of thick resilient member isolates the trim tab from normal strain. Because the trim tab is made of aluminum, the tab can be readily adjusted the field using a conventional tool.
申请公布号 WO2004111442(A2) 申请公布日期 2004.12.23
申请号 WO2004US18518 申请日期 2004.06.10
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 SCHMALING, DAVID, N.;CARLETON, JAMES, B.
分类号 F01D5/00;F01D5/14 主分类号 F01D5/00
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