首页> 外国专利> apparatus for steering a nose landing gear into an aircraft, method for constructing a centering mechanism on an aircraft steering module, and method for centering a steering axis and retaining it in a centered position.

apparatus for steering a nose landing gear into an aircraft, method for constructing a centering mechanism on an aircraft steering module, and method for centering a steering axis and retaining it in a centered position.

机译:用于将前起落架转向飞机的装置,在飞机转向模块上构造对中机构的方法以及使转向轴对中并将其保持在对中位置的方法。

摘要

An apparatus for steering a nosewheel on an aircraft, or the like, while the aircraft is on the ground. The apparatus includes a steering shaft that engages a cluster of gears and transfers torque from a steering command to the gears. The steering shaft is rotatable from a centered position in response to steering torque. A centering mechanism imparts a counter-torque on the cluster of gears to restore the steering shaft to the centered position when steering torque is released. The gear cluster comprises two drive gears that accurately guide the steering shaft to the centered position under the influence of the centering mechanism. The gear cluster is configured to minimize and compensate for gear wear, permitting accurate and consistent centering of the main shaft each time a steering torque is released.
机译:一种用于在飞机处于地面上时操纵飞机等的前轮的装置。该设备包括转向轴,该转向轴接合齿轮组并将扭矩从转向命令传递到齿轮。转向轴可响应转向转矩从居中位置旋转。对中机构在齿轮组上施加反扭矩,以在释放转向扭矩时将转向轴恢复到对中位置。齿轮组包括两个驱动齿轮,这些驱动齿轮在对中机构的影响下将转向轴精确地引导到对中位置。齿轮组配置为最小化并补偿齿轮磨损,从而在每次释放转向扭矩时都能使主轴准确,一致地定心。

著录项

  • 公开/公告号BR0215880B1

    专利类型

  • 公开/公告日2012-02-07

    原文格式PDF

  • 申请/专利权人

    申请/专利号BR20020215880

  • 申请日2002-10-08

  • 分类号B64C25/50;B64C13/04;G05G1/08;G05G5/05;

  • 国家 BR

  • 入库时间 2022-08-21 17:25:32

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