针对三维碳/碳复合材料板件开孔敏感性问题进行了试验与有限元分析。建立了三维碳/碳复合材料代表体积单元(RVE)和完好板件、开孔板件的有限元模型,给出了宏观应力到细观应力的转换方法,并基于此方法,实现了完好板件、开孔板件拉伸破坏过程的数值模拟。进行了三维碳/碳复合材料完好板件和开孔板件的单向拉伸试验,模拟计算结果与试验结果吻合良好。分析了不同宽径比(WTDR)对开孔板件拉伸强度的影响,其中当宽径比达到6时,开孔板拉伸极限强度相比完好板下降11.5%,可以认为如果宽径比不低于6,开孔对板件拉伸极限强度影响较小。该结论可以为碳/碳复合材料开孔板件设计提供指导。
Experiments and finite element analysis were carried out for the problem of open hole sensitivity of 3D carbon/carbon composite material plates.Finite element models of the representative volume element (RVE),the intact plate and open-hole plates of 3D carbon/carbon composite were established.Transition method between macro level stress and meso level stress was given and numerical simulation on the tensile failure of the intact plate and open-hole plates was implemented based on this method.By uniaxial tensile tests of 3D carbon/carbon composite intact plates and open-hole plates,good agreement between numerical results and experiments was observed.In addition,the influence of width to diameter ratio (WTDR)on the tensile strength was analyzed.The results show that the tensile strength of open-hole plate decreases by 1 1.5% comparing with that of intact plate when the WTDR reaches 6 .It can be considered that the open hole makes little influence on the tensile strength of plates if the WTDR is not less than 6.And the result of the investigation provides insight into the design of carbon/carbon composite open-hole plate.
参考文献
[1] | Chen, X.;Taylor, L.W.;Tsai, L.-J..An overview on fabrication of three-dimensional woven textile preforms for composites[J].Textile research journal,20119(9):932-944. |
[2] | KADIR BlLISIK.Multiaxis 3D Woven Preform and Properties of Multiaxis 3D Woven and 3D Orthogonal Woven Carbon/Epoxy Composites[J].Journal of Reinforced Plastics and Composites,20108(8):1173-1186. |
[3] | 余育苗;王肖钧;王志海;李永池.三维正交机织复合材料的力学性能研究[J].实验力学,2008(3):206-212. |
[4] | 许承海;孟松鹤;齐菲;胡江华;宋乐颖.三维机织碳/碳复合材料双轴压缩载荷下的力学行为[J].复合材料学报,2012(6):206-211. |
[5] | 郭兴峰.纬纱接结的三维正交机织物结构[J].纺织学报,2008(01):62-65. |
[6] | Koerber, H.;Xavier, J.;Camanho, P. P.;Essa, Y. E.;de la Escalera, F. Martin.High strain rate behaviour of 5-harness-satin weave fabric carbon-epoxy composite under compression and combined compression-shear loading[J].International Journal of Solids and Structures,2015:172-182. |
[7] | 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].哈尔滨工业大学,2010. |
[8] | Junwu Mu;Zhidong Guan;Tianya Bian.The Experiment and Numerical Simulation of Composite Countersunk-head Fasteners Pull-through Mechanical Behavior[J].Applied composite materials,20145(5):773-787. |
[9] | Guan, Zhidong;Mu, Junwu;Su, Fei;Bian, Tianya;Huang, Yongjie;Li, Zengshan.Pull-Through Mechanical Behavior of Composite Fastener Threads[J].Applied composite materials,20153(3):251-267. |
[10] | 董伟锋;肖军;李勇;吴海桥;张立泉.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(5):659-663. |
[11] | 郑君;温卫东;崔海涛;高建辉.2.5维机织结构复合材料的几何模型[J].复合材料学报,2008(2):143-148. |
[12] | 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(5):58-62,67. |
[13] | 边天涯;关志东;刘发齐;王仁宇;穆军武.含孔隙基体缎纹编织复合材料面内压缩弹性性能预报[J].北京航空航天大学学报,2016(5):1016-1024. |
[14] | 李星;关志东;刘璐;黎增山.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(2):190-195. |
- 下载量()
- 访问量()
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%