Supercharge Your Innovation With Domain-Expert AI Agents!

System for testing thermal deformation performance of aviation temperature sensitive element

A technology of sensitive components and test systems, applied in the direction of strength characteristics, the use of stable tension/pressure to test the strength of materials, measurement devices, etc., can solve the problems of low degree of automation, low measurement efficiency, difficulty, etc. Wide, easy to promote and apply, high degree of automation effect

Pending Publication Date: 2022-03-11
BEIJING HANGKE ENGINE CONTROL SYST SCI & TECH
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Measuring thermal deformation of devices is a complex and difficult process
Due to the temperature rise, the measurement device itself, such as the error caused by the temperature change of the electronic components, the error caused by the mechanical fixture, the thermal shock deformation error, the thermal deformation of the box, etc., all of which increase the difficulty of measurement.
[0005] For the thermal deformation test of mechanical devices or components with strong temperature sensitivity, the traditional temperature-sensitive component thermal deformation test system has a series of problems such as large error, low measurement accuracy, low degree of automation, and low measurement efficiency, which need to be improved urgently

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
  • System for testing thermal deformation performance of aviation temperature sensitive element
  • System for testing thermal deformation performance of aviation temperature sensitive element
  • System for testing thermal deformation performance of aviation temperature sensitive element

Examples

Experimental program
Comparison scheme
Effect test

Embodiment approach

[0045] In other embodiments of the present application, a method for implementing thermal deformation performance testing of aviation temperature sensitive elements is provided, including the following steps:

[0046] S1. Test element preparation. Prepare the test elements according to the specifications and dimensions of the test elements.

[0047] S2. Standard test element clamping and temperature and force adjustment. Place the standard test element on the working surface of the fixture tooling in the temperature control box device, and use the computer control device to control and adjust the temperature and force load of the test element.

[0048] S3. Standard test element calibration of the test system. The computer control device is used to raise the temperature of the test components in the incubator device, and the temperature and deformation data of the standard test components are obtained through the deformation and force loading device, and compared with the dat...

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 provides a thermal deformation performance test system for an aviation temperature sensitive element. The thermal deformation performance test system comprises a base; the temperature control box is arranged on the base; the deformation and stress load testing device is arranged in the temperature control box and is used for testing elements; the power device is connected with the deformation and stress load testing device and used for providing acting force for the deformation and stress load testing device; the protection device is arranged above the temperature control box; wherein the power device is arranged in the protection device; the protection device is connected with the base through a stand column. The aviation temperature sensitive element thermal deformation performance test system provided by the invention is wide in applicable temperature range, small in error, high in precision, stable in operation, high in automation degree, simple and convenient to operate and easy to popularize and apply.

Description

technical field [0001] The application belongs to the technical field of mechanical performance testing, and in particular relates to a thermal deformation performance testing system of an aviation temperature sensitive element. Background technique [0002] The development of the aviation industry is closely related to engineering applications, but more importantly, the tremendous progress that mankind has made in this industry sector has had a significant and far-reaching impact on many sectors of the national economy and many aspects of social life, driving and changing face of the world. Various materials used in aircraft and its power plants, accessories, and instruments are one of the decisive factors in the development of aerospace engineering technology. The emergence of various new materials and new technologies also provides new and greater possibilities for the development of aircraft, which greatly promotes the development of aerospace technology. Because aviat...

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): G01N25/00G01N3/08
CPCG01N25/00G01N3/08G01N2203/0003G01N2203/0075G01N2203/0676G01N2203/0682
Inventor 郭硕杜鑫纪艳丽武忠华盛世伟
Owner BEIJING HANGKE ENGINE CONTROL SYST SCI & TECH
Features
  • R&D
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More