Effect of thermal aging on microstructure and functional properties of zirconia-base thermal barrier coatings

Journal of Thermal Spray Technology

Volumn 18, Issue 2, 2009, Pages 201-208

  Markocsan, Nicolaie ^a   Nylen P ^a,b   Wigren, J ^b   Li, X H ^c   Tricoire, A ^b  

^a UNIVERSITY WEST   (Sweden)

^b VOLVO AERO CORPORATION   (Sweden)

^c Siemens Industrial Turbomachinery AB   (Sweden)

Author keywords

Heat treatment; Plasma spray; Porosity; TBCs; Thermal conductivity; Zirconia

Indexed keywords

ADHESION STRENGTHS; ATMOSPHERIC PLASMAS; COATING MICROSTRUCTURES; COATING MORPHOLOGIES; COMBUSTION TEMPERATURES; FEEDSTOCK MATERIALS; FUEL EFFICIENCIES; FUNCTIONAL PROPERTIES; GAS TURBINE ENGINES; HEAT TREATMENT CONDITIONS; LONG SERVICE LIVES; LOW THERMAL CONDUCTIVITIES; METAL COMPONENTS; MICROSTRUCTURE ANALYSIS; OPERATING CONDITIONS; PARTIALLY STABILIZED ZIRCONIAS; PLASMA SPRAY; PLASMA SPRAYED; SPRAY CONDITIONS; SURFACE TEMPERATURES; TBCS; YTTRIA PARTIALLY STABILIZED ZIRCONIAS;

AIR CLEANERS; COATINGS; ENERGY EFFICIENCY; GAS EMISSIONS; GAS TURBINES; HEAT TREATMENT; LEAKAGE (FLUID); MICROSTRUCTURE; PLASMA JETS; PLASMA SPRAYING; PLASMAS; POROSITY; THERMAL AGING; THERMAL CONDUCTIVITY; THERMOANALYSIS; THERMOELECTRICITY; YTTRIA STABILIZED ZIRCONIA; ZIRCONIA;

THERMAL BARRIER COATINGS;

EID: 67349229749     PISSN: 10599630     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11666-009-9313-6     Document Type: Conference Paper

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