首页> 外国专利> Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored

Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored

机译:大型飞机的飞机转向系统和方法,其在前滑架被脚轮打滑时在低滑行速度下具有主起落架转向

摘要

A steering method and system for large aircraft wherein during low speed taxi the main landing gear wheels are steered and the nose gear is free to castor. During high speed taxi such as during take off and landing, the main gear steering is locked out while the nose gear is steered.
机译:一种用于大型飞机的转向方法和系统,其中在低速滑行期间,主起落架轮被转向并且前起落架对脚轮自由。在高速滑行期间,例如在起飞和着陆期间,前起落架转向时主齿轮转向被锁定。

著录项

  • 公开/公告号US5513821A

    专利类型

  • 公开/公告日1996-05-07

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19940219329

  • 发明设计人 HARRY C. RALPH;

    申请日1994-03-29

  • 分类号B64C25/50;B64C25/42;

  • 国家 US

  • 入库时间 2022-08-22 03:38:40

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