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.
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
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