首页> 外国专利> Electromechanical linear actuator for linearly displacing e.g. nozzle flap, of aircraft's turbojet engine, has satellite rollers including helical teeth cooperating with bush's internal thread and external thread of rod's rear end part

Electromechanical linear actuator for linearly displacing e.g. nozzle flap, of aircraft's turbojet engine, has satellite rollers including helical teeth cooperating with bush's internal thread and external thread of rod's rear end part

机译:用于线性位移的机电线性致动器飞机的涡轮喷气发动机的喷嘴襟翼具有副滚轮,副滚轮包括与衬套的内螺纹和杆的后端部分的外螺纹配合的螺旋齿

摘要

The actuator (10) has electric motors (18), where each motor comprises a stator (56) fixedly mounted in a cylindrical body (12) around a cylindrical bush (20). The bush is being fixed in translation and axially moves a tubular movable rod (14) using a planetary or satellite roller crown wheel (22) mounted around the rod. The wheel is housed inside the bush. The wheel is carried by a rear end part of the rod and axially immobilized on the end part. Satellite rollers comprise helical teeth cooperating with an internal thread of the bush and an external thread of the rear end part of the rod.
机译:致动器(10)具有电动机(18),其中每个电动机包括定子(56),该定子固定地安装在围绕圆柱形衬套(20)的圆柱形主体(12)中。衬套被固定成平移,并使用绕着该杆安装的行星轮或卫星轮冠轮(22)轴向移动管状可移动杆(14)。车轮位于衬套内。轮由杆的后端部承载并且轴向固定在端部上。附属辊具有与衬套的内螺纹和杆的后端部的外螺纹配合的螺旋齿。

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