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System, method and apparatus for ground-based manipulation and control of aerial vehicle during non-flying operations

机译:在非飞行操作期间用于飞行器的地面操纵和控制的系统,方法和设备

摘要

A device for controlling an aircraft during non-flying operations has a retractable tiller that extends with the nose landing gear of the aircraft. Ground crew use the control device to maneuver the aircraft for various ground-based operations. The tiller provides left and right directional input to the steering of the nose wheel. The tiller also provides throttle and brake controls, such as a twist-grip handle on the tiller. The throttle and brake controls are spring-loaded to an engine idle and braked position. Separate brakes also may be provided for additional braking control. The control device also includes various auxiliary controls for additional operations such as wing fold, tail hook extension and retraction, launch bar extension and retraction, etc. Other functions including engine start, engine shutdown, a vehicle system built in test and other functions and tests also may be provided on the control device.
机译:用于在非飞行操作期间控制飞机的装置具有随飞机的前起落架延伸的可伸缩的舵柄。地勤人员使用控制设备来操纵飞机进行各种地面操作。分er为前轮的转向提供左右方向输入。操纵杆还提供节气门和刹车控制,例如操纵杆上的扭握手柄。节气门和制动控制器弹簧加载到发动机怠速和制动位置。也可以提供单独的制动器,以进行额外的制动控制。该控制设备还包括用于辅助操作的各种辅助控件,例如机翼折叠,尾钩伸展和缩回,发射杆伸展和缩回等。其他功能包括发动机启动,发动机停机,内置于测试的车辆系统以及其他功能和测试也可以在控制装置上设置。

著录项

  • 公开/公告号US8079545B2

    专利类型

  • 公开/公告日2011-12-20

    原文格式PDF

  • 申请/专利权人 KEVIN J. RENSHAW;

    申请/专利号US20080006995

  • 发明设计人 KEVIN J. RENSHAW;

    申请日2008-01-08

  • 分类号B64C25/50;

  • 国家 US

  • 入库时间 2022-08-21 17:26:53

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