三维编织复合材料圆柱销剪切试验与数值模拟

胡龙; 刘振国; 王一博; 林强; 亚纪轩

doi:10.13700/j.bh.1001-5965.2015.0105

三维编织复合材料圆柱销剪切试验与数值模拟

doi: 10.13700/j.bh.1001-5965.2015.0105

北京航空航天大学航空科学与工程学院, 北京 100083

详细信息

作者简介:
胡龙男,博士研究生。主要研究方向:复合材料结构力学仿真与试验、复合材料结构优化设计、三维编织复合材料力学性能数值分析等。Tel.:010-82314980 E-mail:hulong0754@buaa.edu.cn;刘振国男,博士,教授,博士生导师。主要研究方向:先进复合材料结构设计、复合材料力学性能数值仿真和试验研究、三维编织复合材料成型与制造工艺等。Tel.:010-82314980 E-mail:liuzg@buaa.edu.cn

通讯作者:
刘振国,Tel.:010-82314980 E-mail:liuzg@buaa.edu.cn

中图分类号: V257;O346.5
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- 被引次数: 0
出版历程
- 收稿日期: 2015-03-03
- 网络出版日期: 2016-02-20

Test and numerical simulation on shear property of 3D braided composite straight pin

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 复合材料紧固件连接技术是复合材料结构加工制造的关键技术之一,针对三维编织复合材料圆柱销紧固件的剪切性能进行了试验和有限元数值模拟分析。试件采用了三维全五向编织工艺进行制备。通过双剪性能测试得到了三维编织复合材料圆柱销的极限承载能力和破坏断裂形式,采用均匀化方法对圆柱销试件的宏观弹性常数进行了预测,采用改进后的Tsai-Hill准则并引入连续介质损伤力学建立了一套三维编织复合材料强度分析方法,并根据该方法对圆柱销试件在剪切载荷作用下的渐进失效破坏过程进行了有限元分析,计算结果与试验结果具有良好的一致性,表明提出的强度分析方法在预测三维编织复合材料结构件的宏观强度性能方面是有效可行的。
- 三维编织复合材料 /
- 圆柱销 /
- 剪切性能 /
- 渐进损伤 /
- 强度
Abstract: Joining technique using composite fasteners is one of the key technologies for the manufacturing of composite structures. Test and numerical research on the shear property of 3D braided composite straight pin fastener is presented. Three-dimensional full five-directional braided technology is used to fabricate the specimens. The shear tests of the specimens are preformed to study the ultimate bearing capacity and failure style of the 3D braided composite straight pin. A homogenization method is used to predict the elastic constants of the straight pin specimens. A strength analysis method is established to describe the strength characteristics of the 3D braided composite straight pin specimens. The modified Tsai-Hill failure criterion and continuum damage theory are introduced into the method. According to this method, a finite element model is developed to simulate the progressive damage process of the specimens. Good agreements are achieved in the load-deflection curves and damage distributions between test and numerical results under shear load, indicating that the proposed analysis method is effective and feasible in predicting the macroscopic strength of 3D braided composite structures.
- 3D braided composites /
- straight pin /
- shear property /
- progressive damage /
- strength

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参考文献(20)

[1]	YANG J M,MA C L,CHOU T W.Fiber inclination model of three-dimensional textile structural composites[J].Journal of Composite Materials,1986,20(5):472-484.
[2]	WANG Y Q,WANG A S D.Microstructure/property relationships in three-dimensionally braided fiber composites[J].Composites Science and Technology,1995,53(2):213-222.
[3]	SANKAR B V,MARREY R V.Analytical method for micromechanics of textile composites[J].Composites Science and Technology,1997,57(6):703-713.
[4]	SUN X,SUN C.Mechanical properties of three-dimensional braided composites[J].Composite Structures,2004,65(3):485-492.
[5]	SHOKRIEH M M,MAZLOOMI M S.A new analytical model for calculation of stiffness of three-dimensional four-directional braided composites[J].Composite Structures,2012,94(3):1005-1015.
[6]	ZENG T,WU L,GUO L.A damage model for 3D braided composites with transverse cracking[J].Composite Structures,2003,62(2):163-170.
[7]	ZENG T,WU L,GUO L.A finite element model for failure analysis of 3D braided composites[J].Materials Science and Engineering:A,2004,366(1):144-151.
[8]	FANG G D,LIANG J,WANG B L.Progressive damage and nonlinear analysis of 3D four-directional braided composites under unidirectional tension[J].Composite Structures,2009,89(1):126-133.
[9]	DONG J,FENG M.Asymptotic expansion homogenization for simulating progressive damage of 3D braided composites[J].Composite Structures,2010,92(4):873-882.
[10]	GUO Q,ZHANG G,LI J.Process parameters design of a three-dimensional and five-directional braided composite joint based on finite element analysis[J].Materials & Design,2013,46(4):291-300.
[11]	ZHOU L D,ZHUANG Z.Strength analysis of three-dimensional braided T-shaped composite structures[J].Composite Structures,2013,104:162-168.
[12]	WU L,GU B,SUN B.Finite element analyses of four-step 3D braided composite bending damage using repeating unit cell model[J].International Journal of Damage Mechanics,2015,24(1):59-75.
[13]	HAENSEL D,HALD H,RUEHLE F,et al.Development of a joining method for high temperature constructions[C]//European Conference on Spacecraft Structures,Materials and Mechanical Testing.Paris:European Space Agency,1999:333-338.
[14]	DOGIGLI M,HANDRICK K,BICKEL M,et al.CMC key technologies-background,status,present and future applications[C]//Hot Structures and Thermal Protection Systems for Space Vehicles.Paris:European Space Agency,2003:79.
[15]	李俊,矫桂琼,王刚,等.室温下C/SiC复合材料螺纹紧固件的拧紧特性[J].复合材料学报,2012,29(5):164-170. LI J,JIAO G Q,WANG G,et al.Tightening characteristic of C/SiC composite threaded fasteners at room temperature[J].Acta Materiae Compositae Sinica,2012,29(5):164-170(in Chinese).
[16]	MEI H,CHENG L,KE Q,et al.High-temperature tensile properties and oxidation behavior of carbon fiber reinforced silicon carbide bolts in a simulated re-entry environment[J].Carbon,2010,48(11):3007-3013.
[17]	王杰,李克智,郭领军,等.炭布叠层穿刺C/C复合材料螺栓连接件微观组织和力学性能[J].固体火箭技术,2012,35(2):248-252. WANG J,LI K Z,GUO L J,et al.Microstructure and mechanical properties of C/C composite bolts[J].Journal of Solid Rocket Technology,2012,35(2):248-252(in Chinese).
[18]	国防工业技术委员会.紧固件试验方法双剪:GJB715.26A-2008[S].北京:中国航空综合技术研究所,2008:1-6. The Commission of Science,Technology and Industry for National Defense of the PRC.Fastener test methods double shear test:GJB715.26A-2008[S].Beijing:AVIC China Aero-Polytechnology Establishment,2008:1-6.
[19]	黄雨霓.三维编织复合材料力学性能研究[D].北京:北京航空航天大学,2012:43-62. HUANG Y N.Research on the mechanical properties of three dimensional braided composites[D].Beijing:Beihang University,2012:43-62(in Chinese).
[20]	CORDEBOIS J P,SIDOROFF F.Damage induced elastic anisotropy[M]//Mechanical Behavior of Anisotropic Solids/Comportment Méchanique des Solides Anisotropes.Berlin:Springer Netherlands,1982:761-774.