发明名称 ASSEMBLY FOR PROVIDING FLEXURE TO BLADE SYSTEM
摘要 An assembly for providing flexure to a blade of a rotary blade system includes an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween. At least one of the upper and lower yoke surfaces has a layer of cushioning material positioned thereon and secured thereto. An alternate embodiment includes an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween and directly contacting the support plates wherein one of the curved surfaces is a non-circular arc that does not form part of the circumference of a circle. Another alternate embodiment includes a similar assembly having a twist-shank type of yoke for providing rotation of attached blades about their respective pitch axes.
申请公布号 CA2592644(C) 申请公布日期 2011.10.11
申请号 CA20062592644 申请日期 2006.01.24
申请人 BELL HELICOPTER TEXTRON INC. 发明人 STAMPS, FRANK B.;TISDALE, PATRICK R.;SHERRILL, PAUL;RAUBER, RICHARD;CAMPBELL, THOMAS C.;BRASWELL, JAMES LEE JR.;MEASOM, RON;HIROS, TRICIA;POPELKA, DAVID A.;SOUTHERLAND, MICHAEL J.;STANNEY, KEITH;WASIKOWSKI, MARK;LEDBETTER, TIM
分类号 B64C27/473;B64C27/46 主分类号 B64C27/473
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