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Prediction of bearing failure inpin-loaded laminates

机译:插销式层压板的轴承失效预测

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摘要

This thesis presents the results of an investigation of bearing failure at a loaded hole in carbon fibre composite laminates. The investigation included finite element analysis and a program of experimental testing for quasi-isotropic laminates, uni-directional laminates and laminates with fibres steered along predefined trajectories. The investigation formed part of a research program in the Cooperative Research Centre for Advanced Composite Structures Ltd (CRC-ACS) support by the Office of Naval Research from the United States. Work in progress in the CRC includes research defined in this thesis including the addition of nano-particles to the resin to improve the bearing strength.The literature survey undertaken in this thesis identified that the micro-buckling theory proposed by Professor C.T. Sun from Purdue University, Indiana USA, is the best analysis procedure for initial bearing failure in pin-loaded laminates. This failure theory has therefore been implemented in a Fortran program using the results from a finite element analysis for the nonlinear contact problem of a pin bearing on a hole in a composite laminate. The finite element analysis is executed using the commercial finite element system MSC.MARC. The numerical predictions have been validated by a test of progressive failure with the aid of an acoustic emission monitoring system.The acoustic emission parametric and frequency analysis is performed using the acoustic emission software Vallen Systeme. Fast fourier transformation of the waveform have been achieved to distinguish and identify microfailure mode. Failure mechanisms have been verified by post-mortem microstructural examination.There are 3 failure mechanisms associated with bearing failure in carbon fibre reinforced epoxy composite, the first is fibre matrix interfacial failure, followed by fibre fracture, and subsequently matrix splitting. The application of AE technique has been applied successfully to characterise the development of failure.
机译:本文提出了碳纤维复合材料层压板加载孔处的轴承失效研究结果。该研究包括有限元分析和准各向同性层压板,单向层压板以及纤维沿预定轨迹转向的层压板的实验测试程序。该调查是美国海军研究办公室在高级复合结构合作研究中心(CRC-ACS)支持下的一项研究计划的一部分。 CRC的工作包括本论文中定义的研究,包括在树脂中添加纳米颗粒以提高轴承强度。本论文进行的文献调查确定了C.T教授提出的微屈曲理论。美国印第安纳州普渡大学的Sun是销钉层压板初始轴承失效的最佳分析程序。因此,该故障理论已在Fortran程序中实现,使用了有限元分析的结果来解决销钉在复合材料叠层中的孔上的非线性接触问题。使用商业有限元系统MSC.MARC执行有限元分析。借助于声发射监测系统,通过对渐进式故障进行测试,对数值预测进行了验证。声发射参数和频率分析是使用声发射软件Vallen Systeme进行的。已经实现了波形的快速傅立叶变换,以区分和识别微故障模式。失效机理已通过事后微观结构检验得到验证。碳纤维增强环氧复合材料中与轴承失效相关的失效机理有3种,首先是纤维基质界面失效,其次是纤维断裂,随后是基体分裂。 AE技术的应用已成功应用于表征故障的发展。

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