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为了分析含钉群复合材料结构的钉载分配及承载能力问题,首先对Globle Bolted Joint Model (GBJM)方法进行了改进,然后采用改进的方法对复合材料多钉连接结构的钉载分配和承载能力进行了预测,并与试验结果进行了比较.结果表明:当孔边复合材料未出现损伤时,该方法对多钉载荷分配的预测和试验结果比较接近;而对结构承载能力的预测,该方法偏于保守,比试验结果约低15%.同时该方法具有两个显著优点:一是计算结构钉载分配时效率高,和三维有限元模型相比提高约75%;二是能够对含钉群复合材料结构的失效载荷进行有效的预测.

参考文献

[1] 中国航空研究院.复合材料结构设计手册[M].北京:航空工业出版社,2001:157-163.
[2] 赵美英 .复合材料机械连接失效分析及强度影响因素研究[D].西北工业大学,2006.
[3] Irisarri F X;Laurin F;Carrere N.Progressive damage and failure of mechanically fastened joints in CFRP laminatesPart Ⅱ:Failure prediction of an industrial junction[J].Computers & Structures,201294(08):2278-2284.
[4] 钱一彬;钟小丹;陈普会;刘利阳;王进.复合材料机身壁板的纵向连接设计与失效分析[J].航空学报,2012(8):1427-1433.
[5] G. N. LABEAS;S. D. BELESIS;I. DIAMANTAKOS;K. I. TSERPES.Adaptative Progressive Damage Modeling for Large-scale Composite Structures[J].International Journal of Damage Mechanics,20123(3):441-462.
[6] P. J. Gray;C. T. McCarthy.A global bolted joint model for finite element analysis of load distributions in multi-bolt composite joints[J].Composites, Part B. Engineering,20104(4):p.317.
[7] Gray P J;McCarthy C T.Finite element modelling of load distributions in multi-bolt composite joints:A global bolted joint model[A].Porto,Portugal,2009
[8] Gray P J;McCarthy C T;McCarthy M A.A global bolted joint model for finite element simulations of large-scale composite structures[A].Athens,Greece,2008
[9] Friberg M .Fastener load distribution and interlaminar stresses in composite laminates[D].Stockholm:Royal Institute of Technology,2000.
[10] McCarthy M A.BOJCAS:bolted joints in composite aircraft structures[J].Air and Space Europe,20013(3-4):139-142.
[11] SIMULIA.ABAQUS/standard version 6.10 user's manual[M].Rhode Island:Hibbit,Karlsson and Sorensen Incorporated,2010:24:1-24:6.
[12] Hashin Z.Failure criteria for unidirectional fiber composites[J].Journal of Applied Mechanics,198047(02):329-335.
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