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复合材料螺栓连接渐近失效分析 被引量:7

PROGRESSIVE DAMAGE ANALYSIS OF COMPOSITE BOLTED JOINTS
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摘要 为了研究预紧力和摩擦系数对复合材料螺栓连接强度的混合影响及其机理,使用ANSYS软件建立了复合材料层合板单钉连接的三维有限元模型。采用渗透接触法来模拟螺栓的预紧力,考虑各组件之间的接触摩擦和结构二次弯曲的影响,使用改进后的三维Hashin失效准则和Camanho退化模型,对复合材料单钉连接进行渐进失效分析。数值模拟结果与文献中的实验结果吻合良好。分析结果表明,增大接触面的摩擦系数和施加合适的预紧力均能提高接头强度。摩擦系数小时,通过增加预紧力来提高接头强度的效果不明显,反而使复合材料容易发生基体开裂。在施加预紧力的同时应综合考虑摩擦系数的大小。 In order to investigate the combined influence of friction coefficient and bolt-torque on the strength of single-bolted composite joints and their mechanism,a three-dimensional finite element model of laminate in singlebolted joints has been built in ANSYS software. The bolted-torque is applied by using penetrative contact method.The influence of friction in components and secondary bending of the plates has been considered. The progressive damage analysis of composite bolted joints is implemented by using improved Hashin failure criterion and Camanho degradation model. The model is validated through comparison with experimental data in literature. It is shown that the joint strength can be enhanced by increasing the friction coefficient and applying appropriate bolt-torque. Increment in the bolt-torque cannot improve the joint strength obviously and higher bolt-torque can make the matrix crushing when the friction coefficient is small. Thus friction coefficient should be considered when applying bolt-torque. The results are instructive for engineering application.
作者 梅俊杰 倪爱清 王继辉 MEI Jun-jie NI Ai-qing WANG Ji-hui(State Key Laboratory of Advanced Technology for Materials Synthesis and Processing, Wuhan University of Technology, Wuhan 430070, Chin)
出处 《玻璃钢/复合材料》 CSCD 北大核心 2017年第7期40-44,共5页 Fiber Reinforced Plastics/Composites
关键词 复合材料 螺栓连接 渐进失效 摩擦系数 预紧力 composites bolt joint progressive damage friction coefficient torque
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  • 1叶红,颜廷武,刘元胜.法兰连接中的螺栓预紧力[J].有色矿冶,2005,21(3):46-48. 被引量:29
  • 2姜云鹏,岳珠峰.复合材料层合板螺栓连接失效的数值模拟[J].复合材料学报,2005,22(4):177-182. 被引量:45
  • 3顾亦磊,赵美英.复合材料层合板螺栓连接失效分析[J].航空计算技术,2006,36(2):110-113. 被引量:10
  • 4刘风雷.用于复合材料干涉结构的多功能紧固系统[J].航空制造技术,2007,50(3):98-101. 被引量:5
  • 5董刚,李建功,潘凤章.机械设计[M].北京:机械工业出版社,1999.
  • 6Hinton M J, Soden P D. Predicting failure in composite laminates: the background to the exercise. Comp Sci & Tech,1998,58(7): 1001-1010.
  • 7Jenkins C F. Report on materials of construction used in aircraft and aircraft engines. Great Britain Aeronautical Research Committee, 1920.
  • 8Rowlands R E. Strength (Failure) theories and their experimental correlation. In: Sih G C, Skudra A M, eds. Failure Mechanics of Composites. North-Holland, Amsterdam: Elsevier Science Pub Co, 1985. 71-125.
  • 9Nahas M N. Survey of failure and post-failure theories of laminated fiber-reinforced composites. J Gomp Tech & Res,1986, 8(4): 138-153.
  • 10Labossiere P, Neal K W. Macroscopic failure criteria for fiber-reinforced composite materials. Solid Mech Arch,1987, 12:439-450.

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