南京航空航天大学学报2024,Vol.56Issue(3) :494-503.DOI:10.16356/j.1005-2615.2024.03.013

P型橡胶卡箍的拉压疲劳性能测试和寿命预测

Tension-Compression Fatigue Performance Testing and Fatigue Life Prediction of P-Type Rubber Clamp

沈兴铿 徐鹤鸣 刘伟 张屹尚 戴瑛 陈新民 周洪民
南京航空航天大学学报2024,Vol.56Issue(3) :494-503.DOI:10.16356/j.1005-2615.2024.03.013

P型橡胶卡箍的拉压疲劳性能测试和寿命预测

Tension-Compression Fatigue Performance Testing and Fatigue Life Prediction of P-Type Rubber Clamp

沈兴铿 1徐鹤鸣 2刘伟 3张屹尚 2戴瑛 4陈新民 5周洪民4
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作者信息

  • 1. 同济大学航空航天与力学学院,上海 200092;中国科学院宁波材料技术与工程研究所特种飞行器系统工程研究中心,宁波 315336
  • 2. 中国航发商用航空发动机有限责任公司研发中心,上海 200241
  • 3. 西北工业大学力学与土木建筑学院,西安 710072
  • 4. 同济大学航空航天与力学学院,上海 200092
  • 5. 中国科学院宁波材料技术与工程研究所特种飞行器系统工程研究中心,宁波 315336
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摘要

P型橡胶卡箍是航空发动机外部管路系统中连接管路与支架、机匣之间的重要连接件,其主要的失效形式为机体振动和管内高压液体脉动共同作用下的疲劳断裂.卡箍的疲劳性能极大地制约了管路系统的性能,因此对于卡箍的疲劳性能研究具有重要意义.本文首先设计并进行了卡箍的拉压疲劳试验,得到了不同加载位移下的疲劳寿命.后续的断口分析表明卡箍疲劳破坏呈现出两种不同的形式:一是卡箍的金属箍带发生由外侧向内侧扩展的疲劳断裂,二是卡箍的橡胶垫圈严重的磨损现象.其次,结合卡箍疲劳试验的加载过程,建立了对应的有限元模型,并通过与贴片位置的应变对比验证了构建模型的预测精度.针对卡箍箍带疲劳断裂的失效形式,通过卡箍箍带所采用的不锈钢材料的疲劳试验结果,建立了卡箍的 SWT(Smith-Watson-Topper)、FS(Fatemi-Socie)以及WB(Wang-Brown)临界平面疲劳寿命模型.最后,结合有限元分析得到的最大应力应变以及卡箍拉压疲劳试验得到的疲劳寿命结果,验证了提出的寿命模型均处于3倍分散带内,对于卡箍的疲劳寿命具有良好的估计精度.

Abstract

.The P-type rubber clamp is an important connector to connect pipelines,supports,and gearboxes in the external piping system of an aircraft engine.The main failure form of the clamp is fatigue fracture under the combined action of external vibration and high-pressure liquid pulsation inside the pipelines.The fatigue failure of clamps greatly restricts the performance of piping systems.Thus it is of great significance to study the fatigue performance of clamps.Firstly,tension-compression fatigue tests of the clamps are designed and conducted and the corresponding fatigue lives under different loading displacements are obtained.Subsequent fracture analysis shows that the fatigue failure of the clamp exhibits two different forms:The one is the fatigue fracture of metal band on the clamp extending from the outside to the inside and the other is the severe wear of rubber washer on the clamp.Secondly,based on the loading process of the tests,the corresponding finite element model is established and the predicted accuracy of the constructed model is further verified by comparing the strain at the strain gauge location.Then,based on the fatigue test results of the stainless steel used in the clamp band,the SWT(Smith-Watson-Topper),FS(Fatemi-Socie),and WB(Wang-Brown)critical plane fatigue life models of the clamp are established for the fatigue fracture the clamp band.Finally,by combining with the maximum stress and strain which are obtained from finite element analysis and the fatigue life results obtained from the tension-compression fatigue test of the clamps,it is verified that the proposed life models are all within the triple dispersion band and have good estimation accuracy for the fatigue life of the clamp.

关键词

P型橡胶卡箍/拉压疲劳/断口分析/临界平面模型/疲劳寿命预测

Key words

P-type rubber clamp/tension-compression fatigue/fracture analysis/critical plane model/fatigue life prediction

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基金项目

上海市商用航空发动机领域联合创新计划()

出版年

2024
南京航空航天大学学报
南京航空航天大学

南京航空航天大学学报

CSTPCDCSCD北大核心
影响因子:0.734
ISSN:1005-2615
参考文献量38
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