发明名称 |
Landing gear for aircraft |
摘要 |
The invention concerns a landing gear. The landing gear is characterized essentially by the fact that it comprises at least one shock absorber (15), this shock absorber being mounted in the leg (1) and casing (2) assembly by means of two convex surfaces (22, 31) made on the cylinder (16) of the shock absorber (15) and cooperating with two concave surfaces (25, 32) integral respectively with the leg (1) and the casing (2). This landing gear finds an application as a nose gear of the rocker-beam type.
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申请公布号 |
US4396170(A) |
申请公布日期 |
1983.08.02 |
申请号 |
US19810317729 |
申请日期 |
1981.11.03 |
申请人 |
MESSIER-HISPANO-BUGATTI |
发明人 |
TURIOT, ANDRE;DERRIEN, MICHEL |
分类号 |
B64C25/50;F16F9/54;(IPC1-7):B64C25/58 |
主分类号 |
B64C25/50 |
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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