首页> 外国专利> SYSTEM FOR CONTROLLING A ROTORCRAFT ROTOR, A ROTORCRAFT FITTED WITH SUCH A SYSTEM, AND AN ASSOCIATED CONTROL METHOD

SYSTEM FOR CONTROLLING A ROTORCRAFT ROTOR, A ROTORCRAFT FITTED WITH SUCH A SYSTEM, AND AN ASSOCIATED CONTROL METHOD

机译:用于控制转桨转子的系统,一种配备有该系统的转桨以及相关的控制方法

摘要

A control system for controlling at least one rotor of a rotorcraft, the control system comprising at least one piloting member suitable for operating at least one control for controlling movements of the at least one rotor. Such a control system comprises: at least one memory enabling information representative of a predetermined control margin threshold to be stored; calculation means for calculating a current control margin, which margin is defined as being the difference between a current position and a limit of the control for controlling movements of the rotor(s); comparator means for comparing the current control margin with the predetermined control margin threshold; and a control unit for modifying an operating relationship of the control for controlling movements of the rotor(s) when the current control margin is less than or equal to the predetermined control margin.
机译:一种用于控制旋翼飞机的至少一个旋翼的控制系统,该控制系统包括至少一个引导构件,该引导构件适于操作用于控制至少一个旋翼的运动的至少一个控制器。这种控制系统包括:至少一个存储器,其使得能够存储代表预定控制裕量阈值的信息;计算装置,用于计算电流控制裕度,该裕度被定义为当前位置与用于控制转子运动的控制极限之间的差;比较器装置,用于将当前控制余量与预定控制余量阈值进行比较;当电流控制裕度小于或等于预定控制裕度时,控制单元用于修改用于控制转子运动的控制的操作关系。

著录项

  • 公开/公告号US2017113792A1

    专利类型

  • 公开/公告日2017-04-27

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201615298530

  • 发明设计人 JEAN-BAPTISTE VALLART;ROMEO BYZERY;

    申请日2016-10-20

  • 分类号B64C27/57;B64C11/34;B64C27/06;

  • 国家 US

  • 入库时间 2022-08-21 13:50:23

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