首页> 外国专利> SECURED LOCKING CORSET FOR SHUTTER CONTROLLED BY ACTUATOR, IN PARTICULAR ACTUATOR CORSET FOR AIRCRAFT DOOR AND LOCKING METHOD

SECURED LOCKING CORSET FOR SHUTTER CONTROLLED BY ACTUATOR, IN PARTICULAR ACTUATOR CORSET FOR AIRCRAFT DOOR AND LOCKING METHOD

机译:执行器控制的快门安全锁紧件,飞机门的特殊执行器锁紧件及锁紧方法

摘要

A secure corset is applied in particular to the immobilization in the maximum opening position of an aircraft landing gear cage hatch. The corset has two half-shells that are able to enclose the piston of the actuator having an axis coincident with the common longitudinal axis of the half-shells once they are closed around the piston. Locking pins are able to hold the half-shells around the actuator. The corset also has a casing secured to at least one of the half-shells and equipped with a hooking unit that is able to be coupled to a fixed point on the structure. A structure for varying the distance between the casing and the hooking unit are able to move the hooking unit away from or towards the corset along the common longitudinal axis of the half-shells.
机译:安全的紧身胸衣尤其用于固定在飞机起落架笼舱口的最大打开位置。紧身胸衣具有两个半壳体,一旦它们围绕活塞闭合,该半壳体能够封闭致动器的活塞,该致动器的轴线与半壳体的公共纵轴线重合。锁定销能够将半壳固定在执行器周围。紧身胸衣还具有壳体,该壳体固定至至少一个半壳,并配备有能够连接至结构上的固定点的挂钩单元。用于改变壳体和钩挂单元之间的距离的结构能够使钩挂单元沿着半壳体的共同的纵向轴线远离或朝向紧身胸衣移动。

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