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Antiskid braking control system for airplane

A technology of anti-skid braking and control system, applied in the direction of aircraft braking arrangement, brake, control mechanism, etc., can solve the problems of complicated C/C manufacturing process, large workload of matching, and high cost, so as to reduce the working frequency and facilitate the operation. , to avoid the effect of peaking

Active Publication Date: 2013-01-09
CENT SOUTH UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the complex manufacturing process of C / C, the cycle is relatively long, the cost is relatively high, and the workload of other matching due to material changes is relatively large

Method used

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  • Antiskid braking control system for airplane
  • Antiskid braking control system for airplane
  • Antiskid braking control system for airplane

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Embodiment 1

[0037] In order to make the objectives, technical solutions, advantages, etc. of the embodiments of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention.

[0038] Such as figure 1 As shown, it is a system structure diagram of the present invention, and the system includes: the brake command sensor is connected with the brake pedal, installed in the aircraft cockpit, and is used to convert the pilot pedal brake displacement signal into an electrical signal; the cockpit operation information is mainly used It is used in the cockpit switch brake selection operation of the pilot to realize different types of brake operations such as landing gear retraction brake, no anti-skid brake, parking brake, and take-off brake; the wheel spe...

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PUM

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Abstract

The invention discloses an antiskid braking control system for an airplane. A left braking instruction sensor, a right braking instruction sensor, a left wheel speed sensor, a right wheel speed sensor, a cabin operation information port and a charcoal / charcoal (C / C) information storage unit are connected with an antiskid braking controller; and the antiskid braking controller controls a left mainmachine wheel and a right main machine wheel through a left electrohydraulic pressure servo valve and a right electrohydraulic pressure servo valve respectively. The antiskid braking control system for the airplane can effectively prevent the moment of a charcoal tray from reaching the peak, automatically regulates braking pressure, and powerfully ensures that the braking process is stable and safe.

Description

technical field [0001] The invention belongs to the field of aircraft anti-skid brake control and relates to an aircraft anti-skid brake control system. Background technique [0002] At present, carbon / carbon (C / C) composite materials have the characteristics of light material and high density, and have been widely used in aircraft braking systems. Since the dynamic friction torque of C / C friction materials has the characteristics of changing with different speeds, these characteristics determine The reason is that when the aircraft starts to brake during the landing process, the torque peak appears more obvious, resulting in overshooting of the slip rate, frequent anti-skid, brake vibration, and poor stability of the aircraft's braking. [0003] The current workaround is: [0004] 1. Change the technological level of C / C materials, improve the performance of C / C materials, and develop materials with high performance and low peak-to-valley ratio. However, due to the comple...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B60T8/171B60T8/172B64C25/44
Inventor 刘文胜吴华伟黄伟明胡春凯
Owner CENT SOUTH UNIV