A ceramic–matrix composite, consisting of five-harness satin Hi-Nicalon fiber in silicon carbide matrix prepared by slurry melt infiltration method, was characterized for tension–tension fatigue and creep behaviors under the combustion and laboratory environments at 1205℃. There was about 100 times reduction in fatigue life under the combustion environment in comparison to the laboratory environment. There was about 50 times reduction in the creep life under the combustion environment in comparison to the laboratory environment. The combustion caused more embrittlement in the tested CMC than the laboratory environment, and it was more in fatigue than creep under the combustion environment only.
MallickPK. Composites engineering handbook, New York: Marcel Dekker, Inc., 1997.
2.
KimTTMallSZawadaLP. Fatigue characterization of a melt-infiltrated woven Hi-NiC-S/BN/SIC ceramic matrix composite using a unique combustion test facility. Ceram Trans2009; 179: 103–116.
3.
Nye AR. Ceramic matrix composite characterization under a combustion and loading environment. PhD Thesis, Air Force Institute of Technology, USA, 2009.
4.
KimTTMallSZawadaLP. Simultaneous fatigue and combustion exposure of a SiC/SiC ceramic matrix composite. J Compos Mater2011; 44: 2991–3016.
5.
KimTTMallSZawadaLP. Fatigue behavior of Hi-Nicalon Type-S™ /BN/SiC ceramic matrix composites in a combustion environment. Int J Appl Ceram Technol2011; 8: 261–272.
6.
MallSNyeARJeffersonG. Tension-tension fatigue behavior of Nextel™ 720/Alumina under combustion environment. Int J Appl Ceram Technol2012; 9: 159–171.
7.
MorscherGNOjardGMillerR. Tensile creep and fatigue of Sylramic-iBN melt-infiltrated SiC matrix composites: Retained properties, damage development, and failure mechanisms. Compos Sci Technol2008; 68: 3305–3313.
8.
NaslainRR. SiC-matrix composites: Nonbrittle ceramics for thermo-structural application. Int J Appl Ceram Technol2005; 2: 75–84.
9.
VenkateswaranVFlechetteFSrinivasanGV. Development of a high temperature SiC fiber for ceramic matrix composite. Ceram Eng Sci Proc1995; 16: 63–69.
10.
XuYChengLZhangL. Carbon/silicon carbide composites prepared by chemical vapor infiltration combined with silicon melt infiltration. Carbon1999; 37: 1179–1187.
11.
LuthraKSinghRBrunM. Toughened silcomp composites – process and preliminary properties. Am Ceram Soc Bull1993; 72: 79–84.
12.
Luthra K, Singh R and Brun M. High temperature ceramic composites. In: Naslain R, Lamon J and Doumeing D (eds) The 6th European conference on composite materials, Bordeaux, France, 1993. Cambridge: Woodhead Publishing Ltd.
13.
Corman G, Brun M, Meschter P, et al. Toughened silcomp ceramic composites for gas turbine engine applications. In: The 39th international SAMPE symposium, society for the advancement of materials and process engineering, Covina, CA, USA, 1994, pp. 2300–2313.
14.
Corman G, Heinen J and Goetze R. Ceramic composites for industrial gas turbine engine applications: DOE CFCC Phase 1 evaluations. In: The 40th ASME international gas turbine and aeroengine congress and exposition, ASME Paper 95-GT-387, Houston, TX, USA, 1995.
15.
Corman G, Brun M and Luthra K. SiC fiber reinforced SiC-Si matrix composites prepared by melt infiltration (MI) for gas turbine engine applications. In: The 44th ASME gas turbine and aeroengine technical congress, exposition and users symposium, ASME Paper 99-GT-234, Indianapolis, IN, USA, 1999.
16.
YangWArakiHKohyamaA. Fabrication in-situ SiC nanowires/SiC matrix composite by chemical vapour infiltration process. Mater Lett2004; 58: 3145–3148.
17.
NannettiCAOrtonaADe PintoDA. Manufacturing SiC-fiber-reinforced SiC matrix composites by improved CVI/slurry infiltration/polymer impregnation and pyrolysis. J Am Ceram Soc2004; 87: 1205–1209.
18.
BrennanJJ. Interfacial characterization of a slurry-cast melt-infiltrated SiC/SiC ceramic-matrix composite. Acta Mater2000; 48: 4619–4628.
19.
HilligWB. Melt infiltration approach to ceramic matrix composites. J Am Ceram Soc1988; 71: 96–99.
20.
TatsuyaHLara-CurzioESneadLL. Mechanical properties of high purity SiC fiber-reinforced CVI-SiC matrix composites. Fusion Sci Technol2003; 44: 211–218.
21.
CormanGDeanABrabetzS. Rig and engine testing of melt infiltrated ceramic composites for combustor and shroud applications. Trans ASME, J Eng Gas Turb Power2002; 124: 459–464.
22.
Dean A, Corman G, Bagepalli B, et al. Design and testing of CFCC shroud and combustor components. In: ASME 1999 International gas turbine and aeroengine congress and exhibition, Indianapolis, Indiana, USA, 7–10 June, 1999, paper no. 99-GT-235.
23.
FeitelbergAStarkeyMSchieferR. Performance of a reduced NOx diffusion flame combustor for the MS5002 gas turbine. Trans ASME, J Eng Gas Turb Power2000; 122: 301–306.
24.
FeitelbergATangiralaVElliottR. Reduced NOx diffusion flame combustors for industrial gas turbines. Trans ASME, J Eng Gas Turb Power2001; 123: 757–765.
