发明名称 |
RETRACTABLE ALIGHTING GEAR FOR A VEHICLE |
摘要 |
An aircraft landing gear including a leg member supporting at least one wheel, the leg having a first point of attachment around a first axis of rotation about a first point on the aircraft, a strut including a rod and a lever pivotally mounted on one another around a third axis, the rod having a second axis of rotation on a second point of attachment to the aircraft and the lever being pivoted about a fourth axis on the leg, and an operating jack applying at least one rotational torque to the strut and the leg wherein one end of the jack is connected to a third point on the leg and the other end of the jack is connected to a fourth point on the strut, the third and fourth points being located substantially near the first and second points of attachment. |
申请公布号 |
DE3064045(D1) |
申请公布日期 |
1983.08.11 |
申请号 |
DE19803064045 |
申请日期 |
1980.09.08 |
申请人 |
MESSIER-HISPANO-BUGATTI (S.A) |
发明人 |
MASCLET, JEAN;TURIOT, ANDRE |
分类号 |
B64C25/14;(IPC1-7):B64C25/14 |
主分类号 |
B64C25/14 |
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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