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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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