Ceramic Composite Liner Material for Gas Turbine Combustors

Advanced commercial and military gas turbine engines may operate at combustor outlet temperatures in excess of 1920 K (3000 K). At these temperatures combustors liners experience extreme convective and radiative heat fluxes. The ability of plasma sprayed ceramic coating to reduce liner metal tempera...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Ercegovic,D B, Walker,C L, Norgren,C T
Format:	Report
Sprache:	eng
Schlagworte:	Ceramic coatings Ceramic materials Ceramics, Refractories and Glass Coatings, Colorants and Finishes Combustion and Ignition Combustion chamber liners Combustors Gas turbines Heat flux High temperature Linings Thermal properties Thermal resistance Thermal stability
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