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Airborne device testing method and system and simulation control testing device

A technology of airborne equipment and control devices, applied in the field of testing, can solve the problems of complex management, prolonging the time of aircraft assembly, reducing the production efficiency of aircraft assembly, etc., achieving the effects of easy management, improving test efficiency, and shortening test time

Active Publication Date: 2017-01-11
BEIJING RUNKE GENERAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the defects of the first test method are: for modern increasingly complex aircraft systems, it is necessary to be equipped with a variety of special test equipment, the management is complicated, and the efficiency of manual testing by testers is difficult to achieve.
The defect of the second test method is that the test can only be carried out after the aircraft system is fully assembled and the aircraft system is powered on.
Once the test finds that there are problems with the airborne equipment, it is necessary to disassemble the aircraft after the final assembly, replace or repair the airborne equipment with problems, and then reassemble the aircraft, which prolongs the time of aircraft final assembly and reduces the production efficiency of aircraft final assembly

Method used

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Examples

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Embodiment 1

[0057] In this embodiment, a method for testing airborne equipment is provided, which is applied to a simulation test control device. See figure 1 , which shows a flow chart of the airborne equipment testing method provided by the present application, which may include the following steps:

[0058] Step S11: receiving the automated test program delivered by the test management device for the airborne equipment under test and the configuration table corresponding to the automated test program.

[0059] In this embodiment, the test management device manages the test task of the airborne equipment in the final assembly process. The automated test program is sent to the simulation test control device, and the configuration table corresponding to the automated test program is sent to the simulation test control device at the same time. Among them, the automated test program is used for functional testing of the airborne equipment under test. The configuration table corresponding t...

Embodiment 2

[0093] In this example, in figure 1 On the basis of the shown airborne equipment test method, another airborne equipment test method is extended, please refer to image 3 , can include the following steps:

[0094] Step S31: receiving the automated test program delivered by the test management device for the airborne equipment under test and the configuration table corresponding to the automated test program.

[0095] Step S32: Configure the driver program of the I / O simulation resource device according to the configuration table corresponding to the automated test program.

[0096] Step S33: After completing the configuration of the driver program of the I / O simulation resource device, control the I / O simulation resource device to output a test signal to the airborne device under test according to the automated test program.

[0097] Step S34: receiving the feedback data collected by the I / O simulation resource device from the airborne equipment under test.

[0098] The fe...

Embodiment 3

[0108] In this example, in figure 1 On the basis of the shown airborne equipment test method, another airborne equipment test method is extended, please refer to Figure 4 , can include the following steps:

[0109] Step S41: receiving the automated test program delivered by the test management device for the airborne equipment under test and the configuration table corresponding to the automated test program.

[0110] Step S42: Configure the driver program of the I / O simulation resource device according to the configuration table corresponding to the automated test program.

[0111] Step S43: After completing the configuration of the driver program of the I / O simulation resource device, control the I / O simulation resource device to output a test signal to the airborne device under test according to the automated test program.

[0112] Step S44: receiving the feedback data collected by the I / O simulation resource device from the airborne equipment under test.

[0113] The f...

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Abstract

The application provides an airborne device testing method and system and a simulation control testing device. The airborne device testing method comprises the following steps: according to a configuration table corresponding to an automation test program, a driving program of an I / O simulation resource apparatus is configured; according to the automation test program, the I / O simulation resource apparatus is controlled to output test signals to an airborne device being tested, feedback data collected by the I / O simulation resource apparatus from the airborne device being tested is received, and whether the feedback data is in a preset standard threshold value scope corresponding to the airborne device being tested is determined; if yes, that the airborne device being tested is up to usage standard is determined; if no, that the airborne device being tested is not up to usage standard is determined. According to the airborne device testing method and system and the simulation control testing device, testing time is reduced via the above mode, testing efficiency is improved, airplane assembling time can be reduced, and production efficiency of general assembly of airplanes can be improved.

Description

technical field [0001] The present application relates to the field of testing, in particular to an airborne equipment testing method, system and simulation control testing device. Background technique [0002] Before the aircraft is put into use, it is necessary to perform a functional test on the on-board equipment of the aircraft. At present, there are two commonly used test methods for airborne equipment, specifically: the first method, testers use the special test equipment for each airborne device to manually test it; the second method uses the aircraft itself Self-inspection system to detect airborne equipment. [0003] However, the defects of the first test method are: for modern increasingly complex aircraft systems, it is necessary to be equipped with a variety of special test equipment, the management is complicated, and the efficiency of manual testing by testers is difficult to achieve. . The defect of the second test method is that the test can only be carri...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/00G05B17/02
CPCG01R31/008G05B17/02
Inventor 吴海鸿
Owner BEIJING RUNKE GENERAL TECH
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