CMC integration and demonstration for gas turbine engines (CINDERS)

Applied Thermal Engineering

Volumn 24, Issue 11-12, 2004, Pages 1755-1764

  Barnard, P ^a   Henderson, M B ^a   Rhodes, N ^a  

^a Alstom UK   (United Kingdom)

Author keywords

Ceramic matrix composites; Coatings; Combustors; Thermal protection systems

Indexed keywords

CERAMIC MATRIX COMPOSITES; COMBUSTION; COMBUSTORS; PARTICULATE EMISSIONS; THERMAL BARRIER COATINGS;

COMBUSTION CHAMBER DESIGN; COOLING AIR; THERMAL EFFICIENCY; THERMAL PROTECTION SYSTEMS (TPS);

GAS TURBINES;

EID: 2942639835     PISSN: 13594311     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.applthermaleng.2003.11.019     Document Type: Conference Paper

References (8)

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2. M. van Roode et al., Ceramic Gas Turbine Development, ASME 1993-GT-309, 1993.
3. Shi J. Ceramic matrix composites for gas turbine engines. Strang A., et al. Advances in Turbine Materials Design and Manufacturing. 1997;IOM.
4. J. Price et al., Ceramic Stationery Gas Turbine Development Program, ASME 2000-GT-75, 2000.
5. D. Oates, Ceramic to metal joining for gas turbine combustion applications, PhD Thesis, University of Manchester Institute of Science and Technology, 1998.
6. K.L. More et al., Exposure of Ceramics and Ceramic Matrix Composites in Simulated and Actual Combustor Environments, ASME 99-GT-292, 1999.
7. H.E. Eaton et al., EBC Protection of SiC/SiC Composites in the Gas Turbine Combustion Environment, ASME 2000-GT-631, 2000.
8. J. Shi, tensile fatigue and life prediction of a SiC/SiC Composite, in: Proceedings of ASME TURBO EXPO 2001, New Orleans, USA, 2001-GT-0463.