Finite element simulation of stress transfer through the multilayer interphase in ceramic matrix composites

被引:0
|
作者
Fang G. [1 ]
Gao X. [2 ,3 ]
Song Y. [2 ,3 ]
机构
[1] School of Mechanical Engineering, Anhui University of Technology, Ma'anshan
[2] Key Laboratory of Aero-engine Thermal Environment and Structure, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
[3] Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
来源
Fang, Guangwu (fgw89424@ahut.edu.cn) | 2018年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 35期
关键词
Ceramic-matrix composites; Finite element method; Micromechanics; Multilayer interphase; Stress analysis;
D O I
10.13801/j.cnki.fhclxb.20180322.001
中图分类号
学科分类号
摘要
The stress transfer through the multilayer interphase in ceramic matrix composites was simulated by finite element method. The microstructure of ceramic matrix composites(CMCs) was modeled by a cylinder unit-cell, the sub-layers of interphase were created according to their real thickness within the model. The interfaces between interphase sub-layers, interphase and fibers, interphase and matrix were all assumed to be bonded perfectly. Different material properties were defined for interphase sub-layers, and the axis-symmetry finite element method was applied to analysis the stress. After all, a simulation method for stress transfer through the multilayer interphase was developed. The simulation results for stress transfer within pyolytic carbon(PyC) interphase of different thickness, interphase of different constituents (PyC and SiC), and interphase of different structure ((PyC/SiC) and (SiC/PyC)) were compared. It can be seen from the distribution of stress along fiber and radial direction that the stress transfer and failure mode of interphase in CMCs can be controlled and optimized by rational allocation of the structure, constituent and thickness of multilayer interphase. © 2018, Editorial Office of Acta Materiae Compositae Sinica. All right reserved.
引用
收藏
页码:3415 / 3422
页数:7
相关论文
共 23 条
  • [1] Zhang L., Cheng L., Discussion on strategies of sustainable development on continuous fiber reinforced ceramic matrix composites, Acta Materiae Compositae Sinica, 24, 2, pp. 1-6, (2007)
  • [2] Hutchinson J.W., Jensen H.M., Models of fiber debonding and pullout in brittle composites with friction, Mechanics of Materials, 9, 2, pp. 139-163, (1990)
  • [3] Meyer P., Waas A.M., Mesh-objective two-scale finite element analysis of damage and failure in ceramic matrix composites, Integrating Materials & Manufacturing Innovation, 4, 1, pp. 1-18, (2015)
  • [4] Fang G., Song Y., Gao X., Model and test validation of stress-strain for needled C/SiC compo-sites, Acta Materiae Compositae Sinica, 33, 4, pp. 827-832, (2016)
  • [5] Braginsky M., Przybyla C.P., Simulation of crack propagation/deflection in ceramic matrix continuous fiber reinforced composites with weak interphase via the extended finite element method, Composite Structures, 136, pp. 538-545, (2016)
  • [6] Kabel J., Yang Y., Balooch M., Et al., Micro-mechanical evaluation of SiC-SiC composite interphase properties and debond mechanisms, Composites Part B: Engineering, 131, 12, pp. 173-183, (2017)
  • [7] Yang F., Sun Z., Li L., Et al., Influence of interface debonding on matrix cracking of cross-ply SiC/CAS composites, Acta Materiae Compositae Sinica, 29, 4, pp. 231-238, (2012)
  • [8] Yang C., Jiao G., Effects of interface on tensile properties of fiber reinforced ceramic matrix compo-sites, Acta Materiae Compositae Sinica, 27, 3, pp. 116-121, (2010)
  • [9] Yu H., Fabrication and characterizations of multilayer interfaces and their effects on bulk properties of SiC/SiC composites, (2011)
  • [10] Naslain R.R., The design of the fibre-matrix interfacial zone in ceramic matrix composites, Composites Part A: Applied Science & Manufacturing, 29, 9-10, pp. 1145-1155, (1998)