INORGANIC MATERIALS AND CERAMIC MATRIX COMPOSITES |
|
|
|
|
|
Effects of Needle Density on Mechanical Behavior of Carbon/Carbon Composite |
DONG Hongnian*, YANG Ming, LIN Tianyi, CHEN Peiran, WEI Tingting
|
Shanghai Space Propulsion Technology Research Institute, Shanghai 201108, China |
|
|
Abstract The optimal control of needle punching process parameters is very important to improve the mechanical properties of carbon/carbon compo-site. The development of “virtual reality test” method based on simulation technology can quickly and concurrently optimize the optimal combination of needle punching process parameters. In this work, the unit cell model of needle-punched C/C composites (NP C/C) with different needling densities (25 pin/cm2, 36 pin/cm2, 64 pin/cm2 and 100 pin/cm2) is established, and the maximum stress criterion and Hashin failure criterion are applied to the failure analysis of fiber web layer and weft-free layer, respectively, based on the periodic boundary condition. The mechanism of the influence of the needling density on the damage failure mode and mechanical behavior of NP C/C is analyzed. It is found that with the increase of loading, the cracks first appear at the circumferential boundary of the needle-punched fiber bundle in both the fiber web layer and the weft-free layer. Moreover, the cracks appear a “Cross” type which is nearly ±45° with the direction of loading. For C/C composite with higher needled density, the proportion of damage area caused byneedle-punched fiber bundles is higher, making it more prone to transverse cracks perpendicular to the loading direction, thereby weakening the material’s load-bearing capacity. Compared to 25 pin/cm2, the fracture strength of NP C/C with needle density of 36 pin/cm2, 64 pin/cm2, and 100 pin/cm2 decreases by 3%, 5%, and 19%, respectively. In addition, the results of secant stiffness degradation indicate that the mechanical behavior of NP C/C exhibits non-linearity before failure. This is mainly caused by progressive cracking damage during the tensile process. The model established in this paper can be used to guide the optimal design of the preform of NP C/C.
|
Published: 10 May 2025
Online: 2025-04-28
|
|
|
|
1 Liu Y F, Feng X, Wang J M, et al. Journal of Inorganic Materials, 2020, 35(10), 1105 (in Chinese). 刘宇峰, 俸翔, 王金明, 等. 无机材料学报, 2020, 35(10), 1105. 2 Wang H Y, Jia J G, Liu D Q, et al. Materials Reports, 2022, 36(13), 21040028 (in Chinese). 王晓昱, 贾建刚, 刘第强, 等. 材料导报, 2022, 36(13), 21040028. 3 Gou J X, Zhang C Y, Wu X J, et al. Materials Reports, 2013, 27(7), 74 (in Chinese). 缑建杰, 张程煜, 吴小军, 等. 材料导报, 2013, 27(7), 74. 4 Zou J J. Study on mechanical properties of carbon/carbon composite structure based on needled technology. Master’s Thesis, Nanjing University of Aeronautics and Astronautics, China, 2019 (in Chinese). 邹佳俊. 基于针刺工艺的碳/碳复合材料结构力学性能研究. 硕士学位论文, 南京航空航天大学, 2019. 5 Fan K. Structure and properties of three-dimensional needle-punched carbon felt reinforced resin-based carbon composites. Master’s Thesis, Jiangnan University, China, 2019 (in Chinese). 樊凯. 三维针刺碳毡增强树脂炭复合材料的结构及性能研究. 硕士学位论文, 江南大学, 2019. 6 Xu Y R, Yang M. Journal of Shanghai University, 2014. 20(4), 480 (in Chinese). 许玉荣, 杨敏. 上海大学学报, 2014. 20(4), 480. 7 Zhang H J. Study on meso-mechanics model and oxidation behavior of needled-punched carbon/carbon composites. Ph. D. Thesis, Nanjing University of Aeronautics and Astronautics, China, 2017 (in Chinese). 张海军. 针刺碳/碳复合材料细观力学建模及氧化行为研究. 博士学位论文, 南京航空航天大学, 2017. 8 Deng J H, Wang Y, Li H J, et al. Rare Metal Materials and Engineering, 2018. 47(11), 3420 (in Chinese). 郑金煌, 王毅, 李贺军, 等. 稀有金属材料与工程, 2018. 47(11), 3420. 9 Yu J, Zhou C W, Zhang H J. Composites Science and Technology, 2017. 153, 48 10 Li Y. Fabrication and ablation mechanism of non-woven cloth needled C/C throat composites. Ph. D. Thesis, Northwestern Polytechnical University, China, 2018 (in Chinese) 李艳. 无纬布针剌CC喉衬材料的制备及其烧蚀机制研究. 博士学位论文, 西北工业大学, 2018. 11 Chen T Y. Research on the throat thermal structure of C/C composite materials based on the Jones-Nelson constitutive model. Master’s thesis, Academy of Aerospace Solid Propulsion Technology, China, 2016 (in Chinese). 陈天宇. 基于Jones-Nelson本构模型的C/C复合材料喉衬热结构研究. 硕士学位论文, 航天动力技术研究院, 2016. 12 Li M X. Experimental study on ultra-high temperature tensile mechanical properties of needle-punched C/C composites. Master’s thesis, Harbin Institute of Technology, China, 2020 (in Chinese). 李明旭. 针刺碳/碳复合材料超高温拉伸力学性能试验研究. 硕士学位论文, 哈尔滨工业大学, 2020. 13 Tan Y Y, Yan Y, Li X, et al. Acta Aeronautica et Astronautica Sinica, 2016. 37(12), 3734 (in Chinese). 谭勇洋, 燕瑛, 李欣, 等. 航空学报, 2016. 37(12), 3734. 14 Hashin, Z. Journal of Applied Mechanics, 1980. 47(2), 329. 15 Xia Z H, Zhou C W, Yong Q L. International Journal of Solids ans Structures, 2006. 43(2), 266. 16 Pang S Y, Wang P Y, Hu C L, et al. Journal of Inorganic Materials, 2019. 34(12), 1272 (in Chinese). 庞生洋, 王佩瑶, 胡成龙, 等. 无机材料学报, 2019. 34(12), 1272. |
|
|
|