| Citation: | BIAN Tianya, GUAN Zhidong, LIU Faqiet al. Tensile test and numerical simulation for satin weave composite fastener[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2): 311-318. doi: 10.13700/j.bh.1001-5965.2016.0137(in Chinese)
|
Detailed sizes of threads in the satin weave composite fastener have reached the meso scale. It is not accurate to simulate the real failure mode if the uniform material is applied to the thread in the process of numerical simulation. For this problem, the finite element model of the fastener thread is established by stacking several layers of simplified satin weave composite meso-structure representative volume elements, which results in that the model includes essential fiber region and matrix region. Numerical simulation for the tensile test of thread model is carried out. Based on the failure criterion of each component material, prediction on the damage force of fastener is achieved. Tensile test for the satin weave carbon/carbon composite single thread fastener are accomplished. Good agreement between simulated failure mode and real damage mode is observed and the error of damage forces between the both methods is 5.17%, which verifies the rationality of the finite element model.
| [1] |
魏高峰,孙晓强,刘国永,等.三维编织复合材料几何建模及数值分析[J].固体力学学报,2011,32(增刊):65-69. http://www.cnki.com.cn/Article/CJFDTOTAL-GTLX2011S1013.htm
WEI G F,SUN X Q,LIU G Y,et al.Geometric model for three-dimensional braided composites and its numerical analysis[J].Chinese Journal of Solid Mechanics,2011,32(Suppl.):65-69(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-GTLX2011S1013.htm
|
| [2] |
董伟锋,肖军,李勇,等.2.5维编织复合材料弹性性能的理论研究[J].南京航空航天大学学报,2005,37(5):659-663. http://www.cnki.com.cn/Article/CJFDTOTAL-NJHK200505024.htm
DONG W F,XIAO J,LI Y,et al.Theoretical study on elastic properties of 2.5D braided composites[J].Journal of Nanjing University of Aeronautics and Astronautics,2005,37(5):659-663(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-NJHK200505024.htm
|
| [3] |
郑君,温卫东,崔海涛,等.2.5维机织结构复合材料的几何模型[J].复合材料学报,2008,25(2):143-148. http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE200802023.htm
ZHENG J,WEN W D,CUI H T,et al.Geometric model of 2.5 dimensional woven structures[J].Acta Materiae Compositae Sinica,2008,25(2):143-148(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE200802023.htm
|
| [4] |
曹海建,钱坤,盛东晓.2.5维机织复合材料的几何结构模型与验证[J].纺织学报,2009,30(5):58-62. http://www.cnki.com.cn/Article/CJFDTOTAL-FZXB200905015.htm
CAO H J,QIAN K,SHENG D X.Geometry model and experimental verification of 2.5-D woven composites[J].Journal of Textile Research,2009,30(5):58-62(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FZXB200905015.htm
|
| [5] |
杨振宇,俸翔,苏洲,等.2.5D编织复合材料细观结构及弹性性能[J].宇航材料工艺,2010(2):67-71. http://www.cnki.com.cn/Article/CJFDTOTAL-YHCG201002019.htm
YANG Z Y,FENG X,SU Z,et al.Meso-structure and elastic properties of 2.5D braided composites[J].Aerospace Materials and Technology,2010(2):67-71(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-YHCG201002019.htm
|
| [6] |
卢子兴,冯志海,寇长河,等.编织复合材料拉伸力学性能的研究[J].复合材料学报,1999,16(3):129-134. http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE903.023.htm
LU Z X,FENG Z H,KOU C H,et al.Studies on tensile properties of braided structural composite materials[J].Acta Materiae Compositae Sinica,1999,16(3):129-134(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE903.023.htm
|
| [7] |
COX B N,DADKHAH M S,MORRIS W L.On the tensile failure of 3D woven composites[J].Composites Part A:Applied Science and Manufacturing,1996,27(4):47-58. http://cn.bing.com/academic/profile?id=e991613b42b1a9f1c12168e2edb9de91&encoded=0&v=paper_preview&mkt=zh-cn
|
| [8] |
CALLUS P J,MOURITZ A P,BANNISTER M K,et al.Tensile properties and failure mechanisms of 3D woven GRP composites[J].Composites Part A:Applied Science and Manufacturing,1999,30(12):77-87. http://cn.bing.com/academic/profile?id=474eb87e92eaa10459686a5452cf5a8d&encoded=0&v=paper_preview&mkt=zh-cn
|
| [9] |
BIGAUD D,HAMELIN P.Mechanical properties prediction of textile reinforced composite materials using a multiscale energetic approach[J].Composite Structures,1997,38(1-4):361-371. doi: 10.1016/S0263-8223(97)00071-8
|
| [10] |
卢子兴,刘振国,麦汉超,等.三维编织复合材料强度的数值预报[J].北京航空航天大学学报,2002,28(5):563-565. http://bhxb.buaa.edu.cn/CN/abstract/abstract10779.shtml
LU Z X,LIU Z G,MAI H C,et al.Numerical prediction of strength for 3D braided composites[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(5):563-565(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract10779.shtml
|
| [11] |
ZENG T,WU L Z,GUO L C.A finite element model for failure analysis of 3D braided composites[J].Materials Science and Engineering:A,2004,366(1):144-151. doi: 10.1016/j.msea.2003.09.054
|
| [12] |
WAN Y M,WANG Y J,GU B H.Finite element prediction of the impact compressive properties of three-dimensional braided composites using multi-scale model[J].Composite Structures,2015,128:381-394. doi: 10.1016/j.compstruct.2015.03.066
|
| [13] |
LU Z X,ZHOU Y,YANG Z Y,et al.Multi-scale finite element analysis of 2.5D woven fabric composites under on-axis and off-axis tension[J].Computational Materials Science,2013,79:485-494. doi: 10.1016/j.commatsci.2013.07.003
|
| [14] |
YU X G,CUI J Z.The prediction on mechanical properties of 4-step braided composites via two-scale method[J].Composites Science and Technology,2007,67(3-4):471-480. doi: 10.1016/j.compscitech.2006.08.028
|
| [15] |
袁辉.碳/碳复合材料刚度与强度预测模型研究[D].南京:南京航空航天大学,2009:23-50,113.
YUAN H.Research on prediction models for stiffness and strength of C/C composites[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009:23-50,113(in Chinese).
|
| [16] |
阚晋.碳/碳复合材料微细观结构的表征及对有效性能的影响研究[D].哈尔滨:哈尔滨工业大学,2010:39,91-95.
KAN J.Investigation on characterization of micro and meso structures and their influence on effective properties of carbon/carbon composites[D].Harbin:Harbin Institute of Technology,2010:39,91-95(in Chinese).
|
| [17] |
MU J W,GUAN Z D,BIAN T Y,et al.The experiment and numerical simulation of composite countersunk-head fasteners pull-through mechanical behavior[J].Applied Composite Materials,2014,21(5):773-787. doi: 10.1007/s10443-013-9379-7
|
| [18] |
GUAN Z D,MU J W,SU F,et al.Pull-through mechanical behavior of composite fastener threads[J].Applied Composite Materials,2015,22(3):251-267. doi: 10.1007/s10443-014-9404-5
|
| [19] |
卢子兴,廖强,杨振宇,等.C/SiC复合材料螺栓螺牙承载能力[J].复合材料学报,2015,32(1):182-187. http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE201501024.htm
LU Z X,LIAO Q,YANG Z Y,et al.Load bearing capability pf thread teeth of C/SiC composite bolts[J].Acta Materiae Compositae Sinica,2015,32(1):182-187(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FUHE201501024.htm
|
| [20] |
SODEN P D,HINTON M J,KADDOUR A S.Lamina properties,lay-up configurations and loading conditions for a range of fiber-reinforced composite laminates[J].Composites Science and Technology,1998,58(7):1011-1022. doi: 10.1016/S0266-3538(98)00078-5
|
| [21] |
American Society for Testing and Materials International.Standard test method for measuring the fastener pull-through resistance of a fiber-reinforced polymer matrix composite:ASTM D7332/D7332-15a[S].West Conshohocken,PA:American Society for Testing and Materials International,2007.
|
| [22] |
BIAN T Y,GUAN Z D,MU J W,et al.An analytical model for predicting the tension modulus and Poisson's ratio of satin weave composites[C/OL]//Proceedings of 20th International Conference on Composite Materials(ICCM).[S.l.]:International Committee on Composite Materials,2015[2015-05-18] http://www.iccm-central.org/Proceedings/ICCM20proceedings/papers/paper-P105-4.pdf.
|
| [23] |
李星,关志东,刘璐,等.基于应变不变量失效理论的复合材料损伤模拟[J].北京航空航天大学学报,2013,39(2):190-195. http://bhxb.buaa.edu.cn/CN/abstract/abstract12528.shtml
LI X,GUAN Z D,LIU L,et al.Damage simulation of composite materials based on strain invariant failure theory[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(2):190-195(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract12528.shtml
|
Figures(12) / Tables(8)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
