发明名称 Dual chamber shock absorbers for aircrafts and the like
摘要 The shock absorber is characterized by the fact that it comprises a rod (1) sliding in a cylinder (2) through a piston (3) to determine at least two variable-volume chambers (4,6), ports (40,41) for placing the two chambers in communication, one of the two chambers (4) comprising first elastic fluid (44) at a first given pressure, the other chamber (6) comprising second elastic fluid (10) at a second given pressure, controllable according to at least one parameter, corresponding to a force to be absorbed.
申请公布号 US4506869(A) 申请公布日期 1985.03.26
申请号 US19830542094 申请日期 1983.10.17
申请人 MESSIER-HISPANO-BUGATTI 发明人 MASCLET, JEAN;VEAUX, JACQUES
分类号 F16F9/06;B60G17/015;B64C25/60;F16F9/50;(IPC1-7):B60G17/04;F16F9/43 主分类号 F16F9/06
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