首页> 外国专利> NOSE LANDING GEAR WITH ACTUATING DEVICE FOR GEAR RETRACTION AS WELL AS FOR THE STEERING

NOSE LANDING GEAR WITH ACTUATING DEVICE FOR GEAR RETRACTION AS WELL AS FOR THE STEERING

机译:带有起落架以及转向装置的前起落架

摘要

A landing gear of an aircraft, including a strut including two arms forming a rotational axis for retracting the gear, a rotating tube mounted in a mobile manner such that it rotates inside the strut about a pivoting axis, a sliding rod that is mobile in a translatory manner in the rotating tube along the pivoting axis, and carries wheels of the gear at one of its ends, and at least one bearing point that is located on one of the elements of the gear at a distance from the retraction axis and can bear necessary efforts for the retraction, the bearing point being located on the rotating tube.
机译:飞机的起落架,包括:具有两个臂的支柱,该两个臂形成用于使齿轮缩回的旋转轴;以可移动的方式安装的旋转管,使得其在支柱内绕枢轴旋转;以及可滑动的滑杆。在旋转管中沿枢转轴平移,并在其一端之一处支撑齿轮的轮,并在距收缩轴一定距离处位于齿轮元件之一上的至少一个轴承点缩回所需的努力,支承点位于旋转管上。

著录项

  • 公开/公告号EP2454152B1

    专利类型

  • 公开/公告日2016-04-20

    原文格式PDF

  • 申请/专利权人 MESSIER-BUGATTI-DOWTY;

    申请/专利号EP20100726089

  • 发明设计人 MOINE DANIEL;

    申请日2010-06-23

  • 分类号B64C25/18;B64C25/50;

  • 国家 EP

  • 入库时间 2022-08-21 14:52:30

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