发明名称 着陸装置
摘要 <p>Aircraft landing gear including an axle pivotally connected to a bogie beam and a locking device. The locking couples the axle to the bogie beam, and has a movable member and a follower. The movable member is movable between first and second configurations. Movement of the movable member towards the second configuration causes corresponding movement of the follower so as to transfer a steering force to the axle through the follower which causes the axle to rotate in a first direction. With the movable member in the first configuration, the follower is in a first configuration that inhibits the movable member being moved by an external force applied to the axle. With the movable member in the second configuration, the follower in a second configuration that permits the movable member to be moved by an external force applied to the axle.</p>
申请公布号 JP5656203(B2) 申请公布日期 2015.01.21
申请号 JP20120549420 申请日期 2011.01.19
申请人 发明人
分类号 B64C25/50;B64C25/34 主分类号 B64C25/50
代理机构 代理人
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