发明名称 |
Aircraft landing gear, in particular for helicopters |
摘要 |
The landing gear comprises: a rod including nested first and second tubes between which there slides a cylinder whose outer end supports a running gear; a strut surrounding the top of the rod and including a steering mechanism cooperating with a rotary tube disposed between the rod and the strut; and a fluid actuator constituted by at least one chamber between the strut and the rod and having a feed inlet only. The landing gear is particularly applicable to helicopters that are required to "kneel down" camel fashion, e.g., for storage in the hold of an aircraft carrier or a cargo plane.
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申请公布号 |
US4630788(A) |
申请公布日期 |
1986.12.23 |
申请号 |
US19840666170 |
申请日期 |
1984.10.29 |
申请人 |
MESSIER-HISPANO-BUGATTI (S.A.) |
发明人 |
VEAUX, JACQUES;DERRIEN, MICHEL |
分类号 |
B64C25/58;B64C25/00;B64C25/60;(IPC1-7):B64C25/60 |
主分类号 |
B64C25/58 |
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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