Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; 2000
DOI: 10.1115/2000-gt-0638
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Rig and Engine Testing of Melt Infiltrated Ceramic Composites for Combustor and Shroud Applications

Abstract: GE has developed SiC fiber reinforced SiC-Si matrix composites produced by silicon melt infiltration (MI) for use in gas turbine engine applications. High temperature, high pressure combustion rig testing and engine testing has been performed on combustor liners and turbine shrouds made from such MI composites. Frame 5 sized combustor liners were rig tested under LHE diffusion flame conditions for 150 hours, including 20 thermal trip cycles, with no observed damage to the ceramic liners. Similarly, 46 cm diame… Show more

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Cited by 15 publications
(13 citation statements)
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“…Silicon carbide fiber‐reinforced silicon carbide (SiC/SiC) ceramic matrix composites (CMCs) possess excellent properties such as high strength and toughness, high thermal conductivity, excellent creep resistance, and good environmental stability (oxidation resistance). These materials could be applied at high temperature in aerospace applications such as aerojet engines, thermal protection, gas turbines, and hot control surfaces . The benefits of these materials are reduced cooling air requirements, lower weight, simpler component design, longer service life and high thrust .…”
Section: Introductionmentioning
confidence: 99%
“…Silicon carbide fiber‐reinforced silicon carbide (SiC/SiC) ceramic matrix composites (CMCs) possess excellent properties such as high strength and toughness, high thermal conductivity, excellent creep resistance, and good environmental stability (oxidation resistance). These materials could be applied at high temperature in aerospace applications such as aerojet engines, thermal protection, gas turbines, and hot control surfaces . The benefits of these materials are reduced cooling air requirements, lower weight, simpler component design, longer service life and high thrust .…”
Section: Introductionmentioning
confidence: 99%
“…SiC/SiC composites exhibit high thermal conductivity, excellent creep resistance, low density, good toughness, and good environmental stability (oxidation resistance). These properties make them suitable for hot‐section components of gas turbines, 2,3 aerojet engines, 4 thermal protection systems, 5 and hot‐control surfaces 6 . The advantages of using CMCs in these areas would be reduced cooling air requirements, lower weight, simpler component design, longer service life, and higher thrust 7 …”
Section: Introductionmentioning
confidence: 99%
“…The matrix was formed by melt infiltration (Heidenreich, 2008). The material was supplied to the authors on the condition that analytical techniques would not be used to determine its composition; however, the literature indicates that the fibers would be coated with a layer of boron nitride (BN) (Corman et al, 2002). For the tensile test, 3 cm × 4 mm strips were cut from the sheet with a diamond saw.…”
Section: Methodsmentioning
confidence: 99%