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Z-pin增强树脂基复合材料单搭接连接性能
引用本文:董晓阳,李勇,张向阳,肖军,李吻.Z-pin增强树脂基复合材料单搭接连接性能[J].航空学报,2014,35(5):1302-1310.
作者姓名:董晓阳  李勇  张向阳  肖军  李吻
作者单位:南京航空航天大学 材料科学与技术学院, 江苏 南京 210016
基金项目:军品配套项目(JPPT-1146)~~
摘    要:为提高复合材料单搭接头的连接性能,制备了不同参数的Z-pin增强单搭接头,通过拉伸试验,研究了Z-pin体积分数、直径以及植入角度对单搭接头连接性能的影响规律,分析了Z-pin对单搭接头性能的增强机理。结果表明Z-pin能明显提高复合材料单搭接头的连接性能:植入角度为90°、Z-pin直径为0.5 mm时,在0%~3.0%体积分数范围内,单搭接头强度随着Z-pin体积分数的增加呈线性增加,含3.0% Z-pin的接头剪切强度为16.76 MPa,比无Z-pin的接头强度提高了33.2%;Z-pin体积分数为1.5%、植入角度为90°时,Z-pin直径变化对单搭接头强度影响不大;含Z-pin体积分数为1.5%、直径为0.5 mm时,随着Z-pin植入角度(背离搭接末端)的增加,单搭接头强度先增加后下降,失效模式从Z-pin拔出失效转变为Z-pin剪断失效;在植入角度为40°时,剪切强度最大(21.04 MPa),比无Z-pin的接头剪切强度提高了67.1%。Z-pin植入角度(倾向于搭接末端)对单搭接头强度无影响。

关 键 词:树脂基复合材料  单搭接头  Z-pin增强  连接性能  拉伸试验  
收稿时间:2013-07-23
修稿时间:2013-09-20

Performance of Polymer Composite Single Lap Joints Reinforced by Z-pin
DONG Xiaoyang,LI Yong,ZHANG Xiangyang,XIAO Jun,LI Wen.Performance of Polymer Composite Single Lap Joints Reinforced by Z-pin[J].Acta Aeronautica et Astronautica Sinica,2014,35(5):1302-1310.
Authors:DONG Xiaoyang  LI Yong  ZHANG Xiangyang  XIAO Jun  LI Wen
Institution:College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:To enhance the performance of polymer composite single lap joints, the joints reinforced with different configurations of Z-pins are manufactured and tested. The effects of the volume fraction, diameter and implant angles of the Z-pins on the strength of single lap joints are investigated and their reinforcing mechanism is also analyzed. The study finds that the Z-pin can improve the performance of single lap joints significantly: When the Z-pin's diameter is 0.5 mm and the implant angle is 90°, the joint's strength increases linearly with the Z-pin volume fraction from 0% to 3.0%. The maximum strength is 16.76 MPa with a 3.0% Z-pin fraction, which is 33.2% higher than that without Z-pin. It also reveals that the Z-pin's diameter has little influence on the strength of polymer composite single lap joints while the Z-pin fraction is 1.5% and the angle is 90°. The strength and failure model is strongly dominated by the implant angles of the Z-pin (against the joint edge) for a Z-pin fraction of 1.5% with a diameter of 0.5 mm. With the increase of the implant angles, the failure mode of the joint is transformed from Z-pin pulling out to Z-pin shearing. The strength reaches its peak value of 21.04 MPa at 40°, which is 67.1% higher than that without Z-pin. The implant angles of the Z-pin (along the joint edge) have no influence on its strength and failure mode.
Keywords:polymer composite  single lap joint  Z-pin reinforcing  joint performance  tensile testing  
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