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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:在主起落架地面接触后,直到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 method of controlling aircraft braking during landing on a runway as soon as the running gear of the main landing gear has made runway contact and prior to the nose gear making contact, comprises: determining the value of the nose-up angle DELTA of the aircraft as soon as it makes runway contact with its main landing gear providing a signal representative of the value of the nose-up angle and controlling braking of the aircraft by any appropriate braking apparatus as a function of a magnitude representative of the signal to ensure acceptable variation of said nose-up angle.
机译:一旦主起落架的起落架已经与跑道接触并且前起落架接触之前,控制飞机在跑道上着陆时的飞机制动的方法包括:确定飞机的机头上升角DELTA的值一旦它与主起落架接触跑道,便提供代表机头上升角值的信号,并通过任何适当的制动装置控制飞机的制动,并根据代表信号的幅度来控制飞机,以确保可接受的变化所说的隆起角度。

著录项

  • 公开/公告号ES8504593A1

    专利类型

  • 公开/公告日1985-04-16

    原文格式PDF

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

    申请/专利号ES19840530357

  • 发明设计人

    申请日1984-03-07

  • 分类号B64C25/42;G05B13/02;

  • 国家 ES

  • 入库时间 2022-08-22 08:06:06

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