工程与试验2024,Vol.64Issue(1) :79-81,96.DOI:10.3969/j.issn.1674-3407.2024.01.020

典型钛合金蒙皮加支撑结构高温环境下振动疲劳寿命试验研究

Experimental Research on Vibration Fatigue Life of Typical Titanium Alloy Skin and Support Structure in High Temperature Environment

何石
工程与试验2024,Vol.64Issue(1) :79-81,96.DOI:10.3969/j.issn.1674-3407.2024.01.020

典型钛合金蒙皮加支撑结构高温环境下振动疲劳寿命试验研究

Experimental Research on Vibration Fatigue Life of Typical Titanium Alloy Skin and Support Structure in High Temperature Environment

何石1
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作者信息

  • 1. 中国飞机强度研究所,强度与结构完整性全国重点实验室,陕西 西安 710065
  • 折叠

摘要

针对典型钛合金蒙皮加支撑结构,搭建了一套热振联合试验系统,并开展高温环境下结构振动疲劳寿命对比试验研究,对比了 3种不同构型支撑结构以及2种连接形式对钛合金蒙皮加支撑结构振动疲劳寿命的影响.试验结果表明:不同支撑构型的典型结构,其在高温环境下的振动疲劳破坏模式与寿命均不相同;相同支撑构型的典型结构,其在高温环境下因不同连接形式造成抗振动疲劳性能也不相同.对比试验结果可为钛合金蒙皮加支撑结构设计提供参考.

Abstract

A thermal-vibration combined test system is established for typical titanium alloy skin and support structures,and comparative test of structural vibration fatigue life is carried out in high temperature environment.The effects of three different configurations of support structures and two different connection forms on the vibration fatigue life of titanium alloy skin and support structures are compared.The test results show that the typical structures with different support configurations have different vibration fatigue failure modes and life in high temperature environment.The typical structures with the same support configuration has different vibration fatigue performance in high temperature environment due to the different connection forms.The comparative test results can provide reference for the design of titanium alloy skin and support structures.

关键词

振动疲劳/典型连接结构/热振耦合/钛合金

Key words

vibration fatigue/typical connection structure/thermal-vibration coupling/titanium alloy

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出版年

2024
工程与试验
长春试验机研究所有限公司 中国仪器仪表学会试验机分会

工程与试验

影响因子:0.198
ISSN:1674-3407
参考文献量10
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