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

Aeroengine pipeline vibration testing device and method

An aero-engine and vibration testing technology, which is applied in the direction of engine testing, vibration testing, measuring devices, etc., can solve problems such as uncontrollable excitation sources and single test working conditions, and achieve test cost savings, reliability assurance, and optimized management. The effect of road assembly quality

Active Publication Date: 2017-03-08
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
View PDF6 Cites 17 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Many scientific research institutes at home and abroad have carried out relevant research on the vibration test of aero-engine pipelines, but most of them are related tests after the pipeline assembly conditions have solidified. In the past, such tests had uncontrollable excitation sources and test conditions. Single and other limitations

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
  • Aeroengine pipeline vibration testing device and method
  • Aeroengine pipeline vibration testing device and method
  • Aeroengine pipeline vibration testing device and method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0049] The specific implementation manners of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0050] This embodiment provides an aero-engine pipeline vibration testing device, such as figure 1 shown, including:

[0051] Vibration excitation device for vibration excitation of aero-engine piping;

[0052] A pipeline clamping device for clamping the pipeline of an aero-engine and connecting it with a vibration excitation device;

[0053] A vibration test and analysis device for detecting and analyzing vibration signals of aero-engine pipelines during the vibration test;

[0054] Assembly position measurement device for measuring the position of aeroengine piping constraints.

[0055] Such as figure 2 As shown, the vibration excitation device includes: a signal generator, a power amplification unit, an excitation control unit, and a vibration table; the output end of the signal generator is connected to the input end of...

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 an aeroengine pipeline vibration testing device and an aeroengine pipeline vibration testing method. The aeroengine pipeline vibration testing device comprises a vibration excitation device, a pipeline clamping device and a vibration test analysis device, wherein the vibration excitation device is used for conducting vibrating excitation on an aeroengine pipeline; the pipeline clamping device is used for clamping the aeroengine pipeline and is connected with the vibration excitation device; and the vibration test analysis device is used for performing vibration signal detection analysis on the aeroengine pipeline during the vibration testing process. The aeroengine pipeline vibration testing device and the aeroengine pipeline vibration testing method realize the effect of simulating actual assembly condition of the engine pipeline, realizes the inherent frequency and dynamic stress tests of the pipeline under multi-order resonance excitation, and realize vibration stress monitoring and test analysis of key points of the pipeline under different assembly structures. The aeroengine pipeline vibration testing device and the aeroengine pipeline vibration testing method realize the multi-order resonance excitation of the engine pipeline in an integral assembly state by utilizing the vibration excitation device and the pipeline clamping device, realizes vibration response test and analysis of the aeroengine pipeline vibration under an adjustable assembly structure by utilizing the vibration test analysis device and an assembly position measuring device, and provide data support for optimizing pipeline assembly quality and verifying reasonability of piping assembly.

Description

technical field [0001] The invention relates to the technical field of vibration testing of aero-engine structural parts, in particular to an aero-engine pipeline vibration testing device and method. Background technique [0002] With the mass production of aero-engines, the assembly quality of aero-engines is more and more considered to be the most important indicator to determine the final qualification and reliability of the engine. The overall assembly quality and rationality of the external pipeline of the engine are also an important factor in determining whether the aero-engine can operate effectively for a long time. Many scientific research institutes at home and abroad have carried out relevant research on the vibration test of aero-engine pipelines, but most of them are related tests after the pipeline assembly conditions have solidified. In the past, such tests had uncontrollable excitation sources and test conditions. Single and other limitations. [0003] The...

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): G01M15/00G01M7/02
CPCG01M7/025G01M15/00
Inventor 王国鹏张荫鳌姜凤赵宇谭亮
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com