发明名称 Fuselage housed retractable aircraft undercarriage - has shock absorber to act as extension and retraction radius arm with linkage from jack to tilt wheel
摘要 <p>The retractable aircraft undercarriage comprises separate units for each side. Each unit has one or more wheels (2) on a transverse axle (1) mounted in fore and aft trunnions (4) in the main leg (5). The main leg is flexibly connected to a vertical pivot (6) housed in the fuselage. A shock absorber (8) and an operating jack (15), both with flexible end connections, are so arranged that the former acts as radius arm during extension and retraction. At the same time, the wheel is tilted transversely by means of a crossbar (23) from the jack cylinder to a lever (24).</p>
申请公布号 FR2383071(A2) 申请公布日期 1978.10.06
申请号 FR19770007393 申请日期 1977.03.11
申请人 MESSIER HISPANO 发明人
分类号 B64C25/10;(IPC1-7):64C25/10 主分类号 B64C25/10
代理机构 代理人
主权项
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