Tensile properties and damage evolution in a 3D C/SiC composite at cryogenic temperatures

Abstract Tensile test was used upon a 3D-C/SiC composite under air or nitrogen atmosphere to characterize its mechanical behaviors and associated damage evolutions from room to cryogenic temperatures. The tensile strength relatively weakened most at −40 °C, however, that is recovered as temperature decreasing to −100 °C. The mismatch of coefficient of thermal expansions between carbon fiber and SiC matrix plays a role in this mechanical response. An interfacial damage model based on microscopic observation is proposed. Finite element method is used to analysis C/SiC deformations. Some generalizations were provided under the cryogenic environment.

[1]  H. Kakisawa,et al.  Tensile damage evolution and notch sensitivity of Al2O3 fiber-ZrO2 matrix minicomposite-reinforced Al2O3 matrix composites , 2002 .

[2]  G. Requena,et al.  Thermal expansion behaviour of aluminum matrix composites with densely packed SiC particles , 2008 .

[3]  R. Shenoi,et al.  Measurement of braided preform permeability , 2006 .

[4]  Hejun Li,et al.  Study on the thermal expansion properties of C/C composites , 2007 .

[5]  G. Groboth,et al.  Thermal expansion behaviour of unidirectional carbon-fibre-reinforced copper-matrix composites , 1998 .

[6]  A. Derré,et al.  High temperature thermal and mechanical properties of high tensile carbon single filaments , 1996 .

[7]  Lai-fei Cheng,et al.  Comparison of oxidation behaviors of 3D C/PyC/SiC and SiC/PyC/SiC composites in an O2-Ar atmosphere , 2006 .

[8]  D. Glass Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles , 2008 .

[9]  Han. Dong,et al.  Tensile creep behavior of notched two-dimensional-C/SiC composite , 2006 .

[10]  Henk Nijmeijer,et al.  Stable mounting of beamsplitters for an interferometer , 2009 .

[11]  David E. Glass,et al.  Airframe Technology Development for Next Generation Launch Vehicles , 2003 .

[12]  Yongdong Xu,et al.  Tensile behavior and microstructural evolution of a carbon/silicon carbide composite in simulated re-entry environments , 2008 .

[13]  Lai-fei Cheng,et al.  Effects of temperature and stress on the oxidation behavior of a 3D C/SiC composite in a combustion wind tunnel , 2010 .

[14]  W. Krenkel,et al.  C/C–SiC composites for space applications and advanced friction systems , 2005 .

[15]  J.M.A. Longo,et al.  The Sharp Edge Flight Experiment SHEFEX II, a Mission Overview and Status , 2008 .

[16]  P. Bowen,et al.  Fatigue behaviour of cross-ply Nicalon/CAS-II glass–ceramic matrix composite at room and elevated temperatures , 2004 .