发明名称 COMPOSITE SCISSORS FOR A SWASHPLATE
摘要 The composite scissor assembly utilizes one or more flexible composite straps (21) disposed either in a radial or non-radial relationship between a hub attached to a rotor shaft (24) and an inner or outer ring (26) of a helicopter swashplate (20). The composite material has sufficient edge-wise stiffness to allow effective torque transmission between the rotor shaft (24) and the swashplate (20) yet has sufficient flexibility to allow for a vertical and angular displacement of the swashplate (20) relative to the rotor shaft (24). Utilizing a flexible composite scissor assembly eliminates the need for mechanical linkages having pins and bearings which are a frequent source for wear, increasing the reliability of the rotor assembly, while reducing weight. <IMAGE>
申请公布号 EP0452248(A3) 申请公布日期 1992.08.12
申请号 EP19910630020 申请日期 1991.04.11
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HUNTER, DAVID H.;LAUCK, KENNETH L.;WHITE, KEVIN A.;MILNE, ROBERT J.;DOOLIN, LEONARD L.;POULIN, STEPHEN V.
分类号 B64C27/605;(IPC1-7):B64C27/605 主分类号 B64C27/605
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