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Method of control of the impulse of a multi engine aircraft, the control device of the impulse of a multi engine aircraft, and aircraft.

机译:多引擎飞机的脉冲的控制方法,多引擎飞机的脉冲的控制装置以及飞机。

摘要

Method of control of the impulse of a multi engine aircraft, the control device of the impulse of a multi engine aircraft, and the aircraft.The device (1) comprises a means (3) to determine the current weight of the aircraft, a means (4) for calculating a value of the pulse reduced is proportional to the mentioned current weight, a means (5) for determining at least one order of command of the engines, so that they release a pulse equal to the Mentioned value of impulse reduced.And a means (7) to implement this order of command engines not in crash of the aircraft.
机译:控制多引擎飞机的脉冲的方法,多引擎飞机的脉冲的控制装置以及飞机。装置(1)包括确定飞机当前重量的装置(3),该装置(4)用于计算减小的脉冲的值与所提及的当前重量成正比的装置(5),用于确定发动机的至少一个指令级,以便它们释放等于所述减小的脉冲的所述值的脉冲。以及一种在飞机失事时不执行命令引擎顺序的装置(7)。

著录项

  • 公开/公告号BRPI0707011A2

    专利类型

  • 公开/公告日2011-04-12

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号BR2007PI07011

  • 发明设计人 GERARD MATHIEU;BENEIT LEMAIGNAN;

    申请日2007-03-08

  • 分类号B64D31/10;

  • 国家 BR

  • 入库时间 2022-08-21 18:07:09

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