发明名称 |
Vibration isolating engine mount. |
摘要 |
<p>A strut for mounting an engine and isolating the vibration of the engine from the framework of an aircraft to which it is attached. An engine mounting strut (32) includes a forward spar (40), which extends outwardly from a rib (34) of an aircraft (20). An aft spar (62) similarly extends outward from a rib (38) and is pivotally connected to a box beam (42) in a vibration isolation mount (78). The pivotal axis of mount (78) is generally aligned with the longitudinal axis of the box beam. A vibration isolation arm (44) extends from a pivotal connection (82) having an axis generally orthogonal to the longitudinal axis of the box beam and is connected to the forward spar at two spaced-apart vibration isolation mounts (46 and 84). The spars are enclosed with an aerodynamic skin (56) forming a torque box 48, to which are attached forward and aft fairings (58).</p> |
申请公布号 |
EP0311155(A2) |
申请公布日期 |
1989.04.12 |
申请号 |
EP19880200976 |
申请日期 |
1988.05.16 |
申请人 |
THE BOEING COMPANY |
发明人 |
CLAUSEN, CHARLES C.;JOHNSON, RONALD C.;CHEE, WAN T.;SCHMIDT, WARREN E. |
分类号 |
B64D27/20;B64D27/26 |
主分类号 |
B64D27/20 |
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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