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Aircraft distribution line fault protection jump switch test system

A power distribution line and fault protection technology, which is applied in the field of the test system for the performance parameters of the aircraft power distribution line fault protection jumper switch, can solve the problems of low work efficiency, time-consuming labor, and damage to the aircraft.

Pending Publication Date: 2018-10-26
CIVIL AVIATION UNIV OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It avoids destroying the original circuit configuration of the aircraft during the maintenance process, and solves the problems of low work efficiency and time-consuming labor

Method used

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  • Aircraft distribution line fault protection jump switch test system
  • Aircraft distribution line fault protection jump switch test system
  • Aircraft distribution line fault protection jump switch test system

Examples

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Embodiment Construction

[0031] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0032] Such as figure 1 and figure 2As shown, the aircraft power distribution line fault protection jumper test system of the present invention includes: DC power supply voltmeter 1, AC three-phase integrated electricity meter 2, DC power supply ammeter 3, AC power supply switch 4, DC power supply switch 5, industrial control All-in-one machine control unit 6, electronic load unit 7, cooling fan 8, switching power supply 9, AC transformer 10, inverter power supply unit 11, data acquisition card 12, transformer rectifier 13, mouse and keyboard box 14, universal wheel 15, Function expansion plug 16, tested line output interface 17, insurance 18, aviation power socket 19. Wherein the AC power switch 4 and the DC power switch 5 are respectively connected with the aircraft AC power supply and the output port of the transformer rectifier 13, and th...

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PUM

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Abstract

The invention discloses an aircraft distribution line fault protection jump switch test system. The aircraft distribution line fault protection jump switch test system includes a test power supply device, a load control device, a to-be-tested object parameter acquiring device, and a parameter comparison and analysis device which are arranged in a test cabinet and are connected to an electric line.The beneficial effects of the invention are that: protective performance parameters of an aircraft jump switch is tested on a wing without breaking an original structure of an aircraft distribution line and without demounting parts of the aircraft during an aircraft distribution line fault isolation process or an aircraft line regular maintenance period, determination of an aircraft jump switch malfunction and a real line fault can be achieved quickly and accurately, the reliability of ground maintenance fault positioning of the aircraft distribution line is ensured, and the maintenance efficiency is greatly improved; the test system has sufficient test capacity, loading test of all the data can be successively completed by one-time wiring, and the human cost and time cost can be saved greatly; and the test system has a long service life and upgrading space, and a new module can be added into the test system to achieve a new test function as needed in the future.

Description

technical field [0001] The invention relates to the field of fault diagnosis of aircraft power distribution lines, in particular to a test system for the performance parameters of the fault protection trip switch of aircraft power distribution lines. Background technique [0002] The aircraft power distribution system is the part from the power bus bar to the input of the electrical equipment. The power distribution system of the aircraft is composed of the grid power distribution device and the grid protection device. Its function is to transmit and distribute the electrical energy generated by the power supply to the electrical equipment of the aircraft. With the continuous improvement of aircraft performance, there are more and more on-board electrical equipment, and on-board electrical equipment plays a key or important role in the safe flight of the aircraft and the successful execution of tasks, so the reliability of aircraft power distribution lines, Security requir...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/327G01R31/08G01R31/02
CPCG01R31/085G01R31/327G01R31/50
Inventor 杨娟李运富马垠飞张靖宇
Owner CIVIL AVIATION UNIV OF CHINA
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