Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Model-based aircraft system fault positioning method

A fault location and aircraft system technology, applied in aircraft maintenance, special data processing applications, geometric CAD, etc., can solve problems such as difficult case revision consistency inspection, inability to interpret diagnosis results, and difficulty in obtaining case knowledge, so as to improve fault Diagnosis efficiency, saving manpower, avoiding the effect of model analysis process

Inactive Publication Date: 2021-04-02
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
View PDF1 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There is a knowledge acquisition bottleneck in the rule-based diagnosis method. The connection chain between the symptoms observed by the system and the corresponding faults is often strengthened with the increase of the complexity of the system. The rule of expert experience is often not unique, and quite difficult
Neural network-based diagnostic methods usually require more training examples for neural network learning in order to make the network converge and obtain stable diagnostic results, and cannot make a reasonable explanation for the diagnostic results
The case-based diagnosis method also has limitations. Usually, it is very time-consuming to retrieve cases from a large case base, and it is difficult to decide which symptoms and their weights should be selected. It is difficult to deal with the consistency test when the case is revised. The acquisition of case knowledge is still a difficult problem in the process of

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Model-based aircraft system fault positioning method
  • Model-based aircraft system fault positioning method
  • Model-based aircraft system fault positioning method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0028] This embodiment provides a model-based aircraft system fault location method, based on the SysML language (system modeling language) to construct a graphical model with LRU (field replaceable unit) as the basic unit as the aircraft system design knowledge base and fault diagnosis Its main function is to describe the simplified model of the system for the specific functions of the aircraft system, mainly including the LRU model and the connection relationship between LRUs. Using the fault model and event input, compare the difference between the expected behavior of the system under normal conditions and the actual output of the system, and judge the state of the fault event according to the established knowledge base and fault model, so as to gradually find the fault source event.

[0029] In this embodiment, the model-based aircraft system fault location method combines figure 1 , including the following steps:

[0030] Step 1: Based on the SysML language, establish a...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention belongs to the field of aircraft complex system fault diagnosis design, and particularly relates to a method for achieving LRU-level rapid fault positioning of an aircraft system. The aircraft system fault diagnosis method based on the model is provided and used for rapidly achieving LRU-level fault positioning after an outfield aircraft system breaks down, so the replacement of a fault unit is rapidly completed, and finally the integrity rate and the attendance rate of an aircraft are increased.

Description

technical field [0001] The invention belongs to the field of aircraft complex system fault diagnosis design, and in particular relates to a method for realizing LRU-level fast fault location for aircraft systems. Background technique [0002] At present, the existing aircraft system fault diagnosis methods mainly include: rule-based reasoning, artificial neural network-based and case-based methods, etc. There is a knowledge acquisition bottleneck in the rule-based diagnosis method. The connection chain between the symptoms observed by the system and the corresponding faults is often strengthened with the increase of the complexity of the system. The rule of expert experience is often not unique, and There is considerable difficulty. Neural network-based diagnostic methods usually require more training examples for neural network learning in order to make the network converge and obtain stable diagnostic results, and cannot make reasonable explanations for the diagnostic res...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/20B64F5/40
CPCG06F30/15G06F30/20B64F5/40
Inventor 尹行孙勇林健刘斌蔡炳忠
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products