2005
DOI: 10.1016/j.jpcs.2004.06.030
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Fabrication of SiC fiber reinforced SiC composite by chemical vapor infiltration for excellent mechanical properties

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Cited by 50 publications
(26 citation statements)
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“…As thermal protection concepts for superalloy components used in the most advanced gas turbine engines reach their high-temperature limits, interest has grown in the development of components made from ceramic materials with much higher maximum use temperatures [1][2][3][4][5]. The focus has concentrated upon damage-tolerant fiber-reinforced ceramic matrix composites (CMCs) with weak fiber/matrix interfaces.…”
Section: Introductionmentioning
confidence: 99%
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“…As thermal protection concepts for superalloy components used in the most advanced gas turbine engines reach their high-temperature limits, interest has grown in the development of components made from ceramic materials with much higher maximum use temperatures [1][2][3][4][5]. The focus has concentrated upon damage-tolerant fiber-reinforced ceramic matrix composites (CMCs) with weak fiber/matrix interfaces.…”
Section: Introductionmentioning
confidence: 99%
“…Unfortunately, these normally protective SiO 2 scales react with water vapor at high temperatures and pressures typical of the gas turbine combustion environment, to form gaseous silicon hydroxide (Si(OH) 4 ) resulting in recession of the SiC [10][11][12][13][14][15]. The rate of SiC volatilization by these mechanisms depends upon the temperature, the incident water vapor flux (pressure), and the effectiveness with which the silicon hydroxide reaction products can be removed.…”
Section: Introductionmentioning
confidence: 99%
“…1). State of the art in SiC/SiC composites has solved most of the potential issues of near-net shaping and machining, joining technology and evaluation technology [68][69][70][71][72][73][74][75][76][77][78][79][80][81][82][83][84][85][86]. There are no doubts that SiC/SiC composites are at the forefront of advanced materials technology and prime candidates for structural material in severe environments.…”
Section: Introductionmentioning
confidence: 99%
“…Several processes are still under consideration to deposit the SiC matrix within the woven fibrous preform (Naslain, 2004) and improve the thermo-mechanical behavior of the composite. Yet, the Chemical Vapor Infiltration (CVI) is promising since it produces a highly pure and near-stoichiometric b-SiC matrix (Deck et al, 2012;Igawa et al, 2005), which is required to limit degradation under radiation. Nevertheless, this process does not allow a perfect infiltration of the composite and leads to an inter-and intra-tow residual porosity.…”
Section: Introductionmentioning
confidence: 99%