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高温薄膜应变计应变传递过程的仿真研究

陈长源 周世威 周枳仲 蒋书文

航空科学技术2024,Vol.35Issue(11):76-83,8.
航空科学技术2024,Vol.35Issue(11):76-83,8.DOI:10.19452/j.issn1007-5453.2024.11.010

高温薄膜应变计应变传递过程的仿真研究

Simulation Study on the Strain Transfer Process of High Temperature Thin Film Strain Gauges

陈长源 1周世威 1周枳仲 1蒋书文1

作者信息

  • 1. 电子科技大学 电子薄膜与集成器件全国重点实验室,四川 成都 611731
  • 折叠

摘要

Abstract

The thin film strain gauge is a novel resistive strain gauge used for high-temperature strain measurements,it is an advanced technology for measuring stress/strain parameters and health monitoring of aeroengine turbine blades.In this paper,the strain transfer process of high temperature thin film strain gauges used in aeroengine were simulated and compared with the strain loss rate of adhesive strain gauges and spray strain gauges.The results show that,due to their small total thickness and high elastic modulus level,the thin film strain gauges exhibit the lowest strain loss rate and the highest accuracy in strain measurement.Meanwhile,the strain loss rate of the thin film strain gauges increases with the thickness of each film layer.

关键词

薄膜应变计/应变传递/应变测量/仿真/剪滞理论

Key words

thin film strain gauge/strain transfer/strain measurement/simulation/shear-lag theory

分类

航空航天

引用本文复制引用

陈长源,周世威,周枳仲,蒋书文..高温薄膜应变计应变传递过程的仿真研究[J].航空科学技术,2024,35(11):76-83,8.

基金项目

航空科学基金(20200046080001) Aeronautical Science Foundation of China(20200046080001) (20200046080001)

航空科学技术

1007-5453

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