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Braking system and method for a landing airplane in the phase after ground contact of the main landing gear until touch down of the nose wheel

机译:在主起落架与地面接触后直至前轮着陆之前的阶段中,用于着陆飞机的制动系统和方法

摘要

The present invention relates to a method and brake control device.; The method for controlling the braking of an aircraft (1) during its atterrisage on a track (3) as soon as it has contacted the ground (2) by rolling means (6) of the main undercarriages (7) and previously before the working means (8) of the front landing gear (9) itself has contacted the ground comprises: - determining the value of the pitch angle Δ of the aircraft as soon as it contacts the track (2) by bearing means (6) of the main undercarriages (7) - developing a signal representative of the value of the pitch angle, - controlling the braking by any means of said aircraft as a function of a value representative of the signal to thereby obtain a variation of the angle of nose acceptable. Application to frainage aircraft.
机译:本发明涉及一种方法和制动控制装置。一旦飞机(1)通过主起落架(7)的滚动装置(6)接触地面(2),并在工作之前控制飞机(1)在轨道(3)上停飞时的制动方法前起落架(9)本身的装置(8)已与地面接触,包括: -一旦飞机通过轴承装置接触到轨道(2),便确定飞机的俯仰角Δ的值(6)主要起落架(7) -产生代表俯仰角值的信号, -通过所述飞机的任何方式控制制动表示信号的值,从而获得可接受的鼻角的变化。应用于排水飞机。

著录项

  • 公开/公告号EP0122162A1

    专利类型

  • 公开/公告日1984-10-17

    原文格式PDF

  • 申请/专利权人 MESSIER-HISPANO-BUGATTI (S.A);

    申请/专利号EP19840400302

  • 发明设计人 GUICHARD JEAN;

    申请日1984-02-15

  • 分类号B64C25/42;

  • 国家 EP

  • 入库时间 2022-08-22 08:57:00

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