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X-cor夹层结构压缩强度模型改进与实验验证
引用本文:党旭丹,肖军,谭永刚,李勇,原永虎.X-cor夹层结构压缩强度模型改进与实验验证[J].航空动力学报,2009,24(12):2802-2807.
作者姓名:党旭丹  肖军  谭永刚  李勇  原永虎
作者单位:南京航空航天大学材料科学与技术学院,南京,210016
摘    要:详细阐述了X-cor夹层结构固化工艺过程中残余应力的产生过程,分析结果为碳纤维Z-pin受残余拉应力,考虑工艺过程残余应力的影响,将Z-pin视为弹性基础上梁,提出一种X-cor夹层结构压缩强度改进计箅模型,并计算其压缩强度.制作了不同Z-pin密度、直径和角度的X-cor夹层结构实验件用于压缩强度实验.实验值和模型计算值的对比验证了该压缩强度计算模型的正确性,工艺过程中Z-pin所受残余拉应力随Z-pin直径、植入密度增加而增加,随Z-pin植入角度增加而减小.

关 键 词:X-cor夹层结构  压缩强度  残余应力  计算模型
收稿时间:12/4/2008 9:32:00 PM
修稿时间:1/8/2009 4:37:39 PM

Computational modified model and experimental verification of compressive strength of the X-cor sandwich
DANG Xu-dan,XIAO Jun,TAN Yong-gang,LI Yong and YUAN Yong-hu.Computational modified model and experimental verification of compressive strength of the X-cor sandwich[J].Journal of Aerospace Power,2009,24(12):2802-2807.
Authors:DANG Xu-dan  XIAO Jun  TAN Yong-gang  LI Yong and YUAN Yong-hu
Institution:College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The generation process of residual stress during the curing process of X-cor sandwich was described,and the analytical results indicate that carbon fiber Z-pins are subject to residual tensile stress.In consideration of the effects of residual stress,Z-pins were treated as beams upon an elastic foundation,then a sort of compressive strength computational modified model of X-cor sandwich was proposed and its compressive strength was computed.The X-cor sandwich samples of different density,diameter and angle of Z-pins were made for compressive strength experiments.Through contrast between experimental and computational results the computational model was verified.The residual stress increases as the Z-pin's diameter and density become bigger,or decreases as the Z-pin's angle increases.
Keywords:Z-pin  X-cor sandwich  compressive strength  Z-pin  residual stress  computational model
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