Chinan LIU , Yuan LI , Yi CHENG , An'an ZHAO , Kunpeng DU , Yue SHI , Ximing LI , Hui CHENG
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Then, stress distribution predicted by the above analytical method is compared with that provided by FE considering composite damage. Finally, a forced installation experiment is carried out to analyze the damage distribution of the joint. Results show that a central-symmetrically distributed stress is introduced by the hole-location error. With an increment of the error, strength of composite decreases due to extrusion damage. Therefore, stress presents a concave distribution on the hole. As the hole-location error exceeding 3%, stress decreases gradually due to failure of composite. Damage of holes does not exhibit a centrosymmetric distribution. Serious damage is mainly distributed on the entrance of the hole at the lower sheet.</p></div>","PeriodicalId":55631,"journal":{"name":"Chinese Journal of Aeronautics","volume":"37 1","pages":"Pages 201-217"},"PeriodicalIF":5.3000,"publicationDate":"2024-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S1000936123002741/pdfft?md5=ff82a5f741108fb3ae4548c9bcdfba72&pid=1-s2.0-S1000936123002741-main.pdf","citationCount":"0","resultStr":"{\"title\":\"Investigation of stress distribution and damage behavior caused by forced installation of a composite bolted joint with a hole-location error\",\"authors\":\"Chinan LIU , Yuan LI , Yi CHENG , An'an ZHAO , Kunpeng DU , Yue SHI , Ximing LI , Hui CHENG\",\"doi\":\"10.1016/j.cja.2023.07.038\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>In this paper, the influence of forced installation caused by a hole-location error on the 3D stress distribution and damage of a composite bolted joint is investigated. An analytical model of stress distributed on composite holes is promoted, in view of non-uniform extrusion caused by forced installation. At first, non-uniform extrusion of the hole edge caused by forced installation is analyzed. According to the contact state, expression of hole deformation is given. Then, based on Hertz theory, the maximum extrusion load is obtained with help of deformation expression. By constructing an elastic foundation beam model, 3D stress distributed on a hole could be analyzed according to the extrusion load. Then, stress distribution predicted by the above analytical method is compared with that provided by FE considering composite damage. Finally, a forced installation experiment is carried out to analyze the damage distribution of the joint. Results show that a central-symmetrically distributed stress is introduced by the hole-location error. With an increment of the error, strength of composite decreases due to extrusion damage. Therefore, stress presents a concave distribution on the hole. As the hole-location error exceeding 3%, stress decreases gradually due to failure of composite. Damage of holes does not exhibit a centrosymmetric distribution. 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引用次数: 0
摘要
本文研究了孔位置误差导致的强制安装对复合材料螺栓连接的三维应力分布和损坏的影响。针对强制安装造成的不均匀挤压,提出了复合材料孔上应力分布的分析模型。首先,分析了强制安装造成的孔边缘非均匀挤压。根据接触状态,给出了孔变形的表达式。然后,根据赫兹理论,借助变形表达式求出最大挤压荷载。通过构建弹性地基梁模型,可根据挤压荷载分析孔上的三维应力分布。然后,将上述分析方法预测的应力分布与考虑到复合材料损伤的 FE 所提供的应力分布进行比较。最后,通过强制安装实验来分析连接处的损伤分布。结果表明,孔位置误差引入了中心对称分布的应力。随着误差的增大,复合材料的强度会因挤压损伤而降低。因此,应力在孔上呈凹形分布。当孔定位误差超过 3% 时,应力会因复合材料的破坏而逐渐减小。孔的损伤不呈中心对称分布。严重的损坏主要分布在孔的入口处,即下层板上。
Investigation of stress distribution and damage behavior caused by forced installation of a composite bolted joint with a hole-location error
In this paper, the influence of forced installation caused by a hole-location error on the 3D stress distribution and damage of a composite bolted joint is investigated. An analytical model of stress distributed on composite holes is promoted, in view of non-uniform extrusion caused by forced installation. At first, non-uniform extrusion of the hole edge caused by forced installation is analyzed. According to the contact state, expression of hole deformation is given. Then, based on Hertz theory, the maximum extrusion load is obtained with help of deformation expression. By constructing an elastic foundation beam model, 3D stress distributed on a hole could be analyzed according to the extrusion load. Then, stress distribution predicted by the above analytical method is compared with that provided by FE considering composite damage. Finally, a forced installation experiment is carried out to analyze the damage distribution of the joint. Results show that a central-symmetrically distributed stress is introduced by the hole-location error. With an increment of the error, strength of composite decreases due to extrusion damage. Therefore, stress presents a concave distribution on the hole. As the hole-location error exceeding 3%, stress decreases gradually due to failure of composite. Damage of holes does not exhibit a centrosymmetric distribution. Serious damage is mainly distributed on the entrance of the hole at the lower sheet.
期刊介绍:
Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.