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

Method for Testing Aircraft Antiskid Brake Control Box Failures Under Temperature Cycling Conditions

A technology of anti-skid braking and temperature cycling, applied in the direction of electrical testing/monitoring, etc., can solve the problems of other faults, incomplete screening of defects, broken solder joints, etc.

Inactive Publication Date: 2016-11-23
XIAN AVIATION BRAKE TECH
View PDF8 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although this method has an obvious effect on screening defects such as welding of electronic products, some solder joints still break during use, or other failures occur, and the screening of defects is not thorough;
[0009] 2) According to the rapid temperature cycle method in GMW8287 "Highly Accelerated Life / Highly Accelerated Stress Screening and Sampling Inspection" written by General Motors Corporation of the United States, the heating and cooling rate is 45 ° C ~ 60 ° C / min, and the power is turned on during the test. Although it has a significant effect on screening welding defects of electronic products, because the influence of working current on welding and other defects is ignored, the excitation effect of welding and other defects under the conditions of temperature cycle and working current is not very ideal;
[0024] Therefore, the existing temperature cycle test technology has incomplete screening of faults

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
  • Method for Testing Aircraft Antiskid Brake Control Box Failures Under Temperature Cycling Conditions
  • Method for Testing Aircraft Antiskid Brake Control Box Failures Under Temperature Cycling Conditions
  • Method for Testing Aircraft Antiskid Brake Control Box Failures Under Temperature Cycling Conditions

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0086] This embodiment is a performance test of an anti-skid brake control box of a transporter under temperature cycle conditions.

[0087] Implementation steps:

[0088] Step 1. Determine the high temperature value of the antiskid brake control box temperature cycle

[0089] The high-temperature working limit of the anti-skid brake control box was tested by using the method of applying high-temperature step stress to the anti-skid brake control box disclosed in the invention of Patent No. 201110310885.1. The antiskid brake control box described in this embodiment is improved to achieve a high temperature working limit of 100°C;

[0090] Determine the high temperature value of the temperature change in the reliability strengthening test chamber. The high temperature value of the temperature cycle is 5°C lower than the high temperature working limit. The high temperature value in this embodiment is 95°C, and 95°C is used as the high temperature value for formulating the tempe...

Embodiment 2

[0128] Both embodiment 2 and embodiment 3 include determining the high temperature value of the antiskid brake control box temperature cycle, determining the low temperature value of the antiskid brake control box temperature cycle, determining the rising rate and falling rate of the temperature in the test chamber, and determining the output of the antiskid brake control box. working current, determine the output duration of the working current of the anti-skid brake control box, determine the duration after the anti-skid brake control box reaches the highest temperature and the lowest temperature, determine the number of temperature cycles, and carry out the test steps according to the requirements of the temperature cycle test. The specific process is the same as The process of Example 1 is the same.

[0129] The difference between Example 1 and Example 2 and Example 3 lies in that the test data in Example 2 and Example 3 are different from the test data in Example 1, as sho...

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

A method for testing the failure of an aircraft anti-skid brake control box under temperature cycle conditions. During the temperature cycle test process of the aircraft anti-skid brake control box, an anti-skid brake operating current is applied simultaneously. The high temperature value of the temperature cycle is determined according to the high temperature working limit of the antiskid brake control box, and the low temperature of the temperature cycle is determined according to the low temperature working limit of the antiskid brake control box. The determined temperature cycle profile is suitable for testing that the antiskid brake control box is sensitive to steady changes Manufacturing defects can stimulate the hidden danger of anti-skid brake control box failure in the working state, so as to effectively verify whether there are development defects in the anti-skid brake control box, and put forward improvement suggestions based on the test results.

Description

technical field [0001] The invention relates to the field of electrical products of an aircraft landing gear control system, in particular to a method for testing the failure of an aircraft anti-skid brake control box during a temperature cycle. Background technique [0002] The method of initiating failure of electronic products under temperature cycling conditions is an experimental technique in the development process. [0003] The anti-skid brake control box is an electronic product in the aircraft landing gear control system. It is designed to control the brake function of the take-off line, the anti-skid function during the landing brake process, the grounding protection function during landing, and the wheel of the left and right landing gear wheels during the landing process. There are multiple functions such as space protection, and any function that does not meet the design requirements is a failure. When the components in the anti-skid brake control box break dow...

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 Patents(China)
IPC IPC(8): G05B23/02
Inventor 乔建军陈永强刘刚周世民彭娟张宏艳
Owner XIAN AVIATION BRAKE TECH
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