发明授权
US5513821A Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored 失效
用于大型飞机的飞行器转向系统和方法,在起落架起落时,在低出租车速度下具有主起落架转向

  • 专利标题: Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored
  • 专利标题(中): 用于大型飞机的飞行器转向系统和方法,在起落架起落时,在低出租车速度下具有主起落架转向
  • 申请号: US219329
    申请日: 1994-03-29
  • 公开(公告)号: US5513821A
    公开(公告)日: 1996-05-07
  • 发明人: Harry C. Ralph
  • 申请人: Harry C. Ralph
  • 申请人地址: WA Seattle
  • 专利权人: The Boeing Company
  • 当前专利权人: The Boeing Company
  • 当前专利权人地址: WA Seattle
  • 主分类号: B64C25/50
  • IPC分类号: B64C25/50 B64C25/42
Aircraft steering system and method for large aircraft having main
landing gear steering during low taxi speed while nose gear is castored
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.
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