Rolls-Royce experience in ceramic matrix composite demonstration

Ceramic Gas Turbine Design and Test Expericence

Volumn 1, Issue , 2002, Pages 583-593

  Razzell, Anthony G ^a  

^a ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AFTERBURNERS (ENGINE); AIRCRAFT ENGINES; AIRFOILS; BORON COMPOUNDS; CARBON CARBON COMPOSITES; CERAMIC COATINGS; CERAMIC MATRIX COMPOSITES; GLASS CERAMICS; NOZZLES; SILICON CARBIDE; THERMAL CYCLING;

CHEMICAL VAPOR INFILTRATION; FLAMEHOLDERS; NOZZLE PETALS;

GAS TURBINES;

EID: 0141428953     PISSN: None     EISSN: None     Source Type: Book    
DOI: None     Document Type: Conference Paper

References (4)

1. Beesley, C., "The Application of CMCs in High Integrity Gas Turbine Engines," 1997, Key Engineering Materials, Vols. 127-131, pp. 165-174, Trans. Tech Publications, Switzerland.
2. Rolls-Royce High Temperature Abradable Seal, US Patent 5 780 146B, 1996.
3. Holmquist, M., Lundberg, R., Razzell, T., Sudre, O., Molliex, L., and Adlerborn, J., "Development of Ultra High Temperature Ceramic Composites for Gas Turbine Combustors," ASME paper 97-GT-413, presented at the ASME International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, USA, June 2-5, 1997.
4. Razzell, A.G., Moliex, L., Holmquist, M., and Sudre, O., "Oxide/Oxide Ceramic Matrix Composites in Gas Turbine Combustors," ASME paper 98-GT-30, presented at the ASME International Gas Turbine and Aeroengine Congress and Exhibition, Stockholm, Sweden, June 2-5, 1998.