发明名称 Rapid extension shock absorber, in particular for carrier-based aircraft
摘要 A shock absorber comprising a strut (1), a sliding rod (3) mounted to slide inside the strut, at least one gas chamber (13, 17) under pressure, an oil chamber (6) associated with the gas chamber, and an expansion chamber (5) connected to the oil chamber via expansion throttling valve (8), the volume of the expansion chamber (5) varying as a function of the extent to which the sliding rod is received in the strut. The shock absorber also includes an expansion short circuit passage (18) between the oil chamber (6) and the expansion chamber (5), the expansion short circuit passage having a cross-section which is greater than the flow section of throttling valve (8), and the shock absorber includes controlled closure partition (32) for closing expansion short circuit passage (18).
申请公布号 US4886248(A) 申请公布日期 1989.12.12
申请号 US19880285425 申请日期 1988.12.16
申请人 MESSIER-HISPANO-BUGATTI 发明人 DELHAYE, MAURICE;DERRIEN, MICHEL;ENGERAND, JEAN-LUC
分类号 B64C25/02;B64C25/60;F16F9/06;F16F9/48 主分类号 B64C25/02
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