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Testing device for aircraft brake controller

A technology for testing equipment and aircraft, applied in general control systems, electrical testing/monitoring, control/regulation systems, etc., can solve problems such as troublesome testing, and achieve the effect of improving portability

Inactive Publication Date: 2017-07-07
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the research on controller testing is still in a lagging state, and the controller is still manually tested with instruments such as signal generators, oscilloscopes, and multimeters, which is quite troublesome to test.

Method used

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  • Testing device for aircraft brake controller
  • Testing device for aircraft brake controller

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Embodiment Construction

[0020] A test device for an aircraft brake controller according to an embodiment of the present invention will be described below with reference to the accompanying drawings.

[0021] figure 1 and 2 A test device for an aircraft brake controller according to an embodiment of the present invention is shown. like figure 1 As shown, the test device includes a power supply module for supplying power to the entire test device; a plurality of tested unit module brackets for detachably installing a plurality of tested unit modules; a collection control module for collecting and controlling the Signals of the plurality of unit modules under test and sensors on the aircraft; a conditioning module for switching and conditioning signals transmitted between the collection control module and the plurality of unit modules under test and the sensors; wherein , the power supply module and multiple tested unit module brackets are installed in the first box, the conditioning module and the a...

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Abstract

The present invention provides a testing device for an aircraft brake controller. The testing device comprises a power supply module for supplying power to the testing device, multiple tested unit module brackets used for removably installing multiple tested unit modules, an acquisition control module used for collecting and controlling signals from the multiple tested unit modules and a sensor in an aircraft, and a conditioning module used for switching and conditioning signals transmitted between the acquisition control module and the multiple tested unit modules and the sensor, wherein the power supply module and the multiple tested unit module brackets are installed in a first box, the conditioning module and the acquisition control module are installed in a second box body, the first box body and the second box body are stacked in use, and the modules installed in the first box body and the second box body are connected through a connection device.

Description

technical field [0001] The invention relates to automatic testing and rapid troubleshooting of aircraft brake controllers, more particularly to a testing device for aircraft brake controllers. Background technique [0002] The aircraft braking system is an important system to ensure the safety of the aircraft. It is mainly used to dissipate the kinetic energy of the aircraft when it rolls on the ground, to ensure that the aircraft brakes to stop, to shorten the distance of the aircraft to run, to prevent excessive wear of the wheels, and to cooperate with other airborne systems. Realizing the turning and parking functions of the aircraft is an important system to ensure the safe take-off and landing of the aircraft. Therefore, whether the aircraft brake system can operate normally and reliably is very important. The main control device in the braking process is the brake controller. The performance of the brake controller directly affects the braking performance of the airc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0221
Inventor 焦宗夏尚耀星董韶鹏李晓斌李锁兰
Owner BEIHANG UNIV
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