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Aircraft fault positioning method based on HMC code correlation analysis

A technology of correlation analysis and fault location, applied in the direction of instruments, electrical testing/monitoring, control/regulation systems, etc., can solve the problems of shortening the continuous dispatch time of aircraft, cumbersome manual troubleshooting process, and reducing the reading volume of HMC, etc., to achieve The effect of shortening the continuous dispatch time, shortening the maintenance time, and reducing the amount of reading

Active Publication Date: 2021-04-02
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Aiming at the cumbersome and inefficient manual troubleshooting process in the existing flight support process, the present invention proposes an aircraft fault location method based on HMC code correlation analysis. By analyzing a large amount of flight data and combining existing design experience, the The fault phenomenon and the fault cause establish a correlation HMC chain to form a HMC code correlation database. The airborne software directly outputs the fault source HMC code by searching the correlation database, and shields other fault HMC codes caused by the source fault. , the shielded HMC code will not be displayed, thereby greatly reducing the HMC reading volume of ground maintenance personnel, eliminating the interference of non-source fault HMC codes, directly indicating the source fault equipment, realizing fault location, and giving questions to ground maintenance personnel at the same time The solution greatly shortens the maintenance time, simplifies the troubleshooting process, and shortens the continuous dispatch time of the aircraft

Method used

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  • Aircraft fault positioning method based on HMC code correlation analysis
  • Aircraft fault positioning method based on HMC code correlation analysis

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Experimental program
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Effect test

Embodiment

[0036] For a certain type of aircraft fault prediction and health management system architecture, the method of aircraft fault location based on HMC code correlation analysis is adopted, and the solution steps are as follows:

[0037] (1) Summarize all fault codes (HMC codes) of the whole machine and classify them according to the system components;

[0038] A typical fault code database is shown in the following table:

[0039] Corresponding HMC code Fault description Monitor source components Disposal opinion 1001 Power frequency monitoring and reporting PIU_L Replace the power board 2004 pitch failure CC_1 / 2014 pitch failure CC_2 / 2024 pitch failure CC_3 / 2034 pitch failure CC_4 / 3001 temperature fault ATC / 4001 pressure failure APCs / … … …

[0040] (2) According to the aircraft failure mode, effect and hazard analysis (FMECA), conduct HMC code correlation analysis according to...

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PUM

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Abstract

The invention relates to an aircraft fault positioning method based on HMC code correlation analysis. Based on aircraft airborne fault prediction and health management system architecture operation, HMC codes are aircraft fault codes, an association relation HMC chain is established for fault phenomena and fault reasons by analyzing a large amount of flight data and combining with existing designspecifications, an HMC code association relationship database is formed, and airborne software searches the association relationship database, directly outputs a fault source HMC code by searching theincidence relation database, shields other fault HMC codes caused by a source fault, and does not display the shielded HMC code after a flight mission is finished, so that the interference of a non-source fault HMC code is eliminated, source fault equipment is directly indicated, and fault positioning is realized.

Description

technical field [0001] The invention belongs to aircraft fault location technology, in particular to the fault location technology based on aircraft fault code (HMC). Background technique [0002] In order to locate and record the faults that occur during the flight of the aircraft, the existing advanced aircraft adopts the PHM system architecture. After the aircraft lands, the ground maintenance personnel can check all the fault information and fault information that occurred during the flight by extracting the fault list. Including fault code (HMC), fault occurrence time, fault site parameter values, fault reporting equipment, etc. After checking the faults, ground maintenance personnel often need to check more detailed data to judge whether the fault reporting logic is correct and whether it is a false alarm, and based on maintenance experience, sort out the relationship between many fault codes (HMC) and locate the real fault. faulty equipment or components, thereby rep...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0262G05B2219/24065Y02P90/30
Inventor 梁兆鑫杨朝旭陈银超王涛叶子唐勇
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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