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腐蚀环境下复合材料修补件力学特性研究
引用本文:王浩伟,刘元海,刘成臣. 腐蚀环境下复合材料修补件力学特性研究[J]. 力学与实践, 2012, 34(1): 75-79,74. DOI: 10.6052/1000-0879-20120114
作者姓名:王浩伟  刘元海  刘成臣
作者单位:1. 北京航空航天大学航空科学与工程学院, 北京 100191;2. 中航工业特种飞行器研究所腐蚀防护与控制研究中心, 湖北荆门 448035
基金项目:"十一五"国防科技预研重点资助项目
摘    要:采用复合材料补片胶接修补含裂纹LY12CZ铝合金板,开展了试验室大气环境和加速预腐蚀环境下复合材料修补件静强度拉伸和疲劳裂纹扩展对比试验研究.结果表明,复合材料补片均能显著提高损伤结构的拉伸强度和疲劳寿命,且短周期的预腐蚀环境对修补件两种力学特性的影响可以忽略不计.同时,基于Paris公式和Rose分析模型,建立了常规环境和预腐蚀环境下疲劳裂纹扩展寿命预测模型,通过与试验结果的对比证明了该模型的工程有效性.

关 键 词:复合材料  胶接修补  静强度  疲劳  裂纹扩展  
收稿时间:2011-07-01;

MECHANICAL BEHAVIOR OF COMPOSITE REPAIRED COMPONENTS UNDER CORROSION ENVIRONMENT
WANG Haowei,+ LIU Yuanhai,LIU Chengchen. MECHANICAL BEHAVIOR OF COMPOSITE REPAIRED COMPONENTS UNDER CORROSION ENVIRONMENT[J]. Mechanics and Engineering, 2012, 34(1): 75-79,74. DOI: 10.6052/1000-0879-20120114
Authors:WANG Haowei  + LIU Yuanhai  LIU Chengchen
Affiliation:1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China;2. Corrosion Prevention and Control Research Center, AVIC Special Vehicle Research Institute, Hubei Jingmen 448035, China
Abstract:The center cracked LY12CZ aluminum alloy plates were adhesively bonded with composite patches, and the tensile strength,the fatigue life and the crack growth during fatigue under air environment and accelerated pre-corrosion environment were investigated experimentally.The experimental results show that both the static strength and the fatigue life of the repaired aluminum substrates are significantly increased for the bonded composite patches,and the short-term pre-corrosion environment does not have a notable effect on the mechanical performance of composite repaired components.Also,a simple fatigue crack growth life prediction model,based on Paris formula and Rose’s analytical solution,is proposed to predict the fatigue behavior of the repaired plates under air and pre-corrosion environments.The result shows a good quantitative agreement with experimental data.
Keywords:composite  bonded repair  static strength  fatigue  crack progress
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