The effects of bond and thermal barrier coating compositions, thicknesses, and densities on air plasma spray deposited Ni-Cr-Al-Y/ZrO2-Y2O3 life were evaluated in cyclic furnace oxidation tests at temperatures from 1110 to 1220 C. An empirical relation was developed to give life as a function of the above parameters. The thermal barrier system tested which had the longest life consisted of Ni-35.0 wt% Cr-5.9 wt% Al-0.95 wt% Y bond coating and ZrO2-6.1 wt% Y2O3 thermal barrier coating
Coatings are presently applied to Space Shuttle Main Engine (SSME) turbine blades for protection aga...
The durability of thermal barrier coatings (TBCs) can dictate the life of the hot section engine com...
A Mach 0.3 burner rig test program was conducted to determine how the fuel to air mass ratio affects...
A cyclic furnace study was conducted on thermal barrier systems to evaluate the effects of yttrium, ...
The aim of this study was to investigate the thermal cycling behaviour of NiCr-Al-Co-Y2O3 bond coati...
A promising two-layer thermal barrier coating system (TBS), Ni-16.4Cr-5.1A1-0.15Y/ZrO2-6.1Y2O3 (all ...
Initial experiments conducted on thermal barrier coatings prepared in the newly upgraded research pl...
This research was directed at developing the fundamentals that will facilitate the fabrication of ai...
Calcium silicate and yttria stabilized zirconia/MCrAlY thermal barrier coating systems on air-cooled...
Thermal barrier coatings were exposed to the high temperature and high heat flux produced by a 30 kW...
Eight plasma sprayed bond coatings were evaluated for their potential use with ZrO2-Y2O3 thermal bar...
Complex thermal barrier coating systems are one the most efficient high-temperature surface treatmen...
This is the second of two reports which discuss initial experiments on thermal barrier coatings prep...
Furnace thermal cycling lifetime and microstructural degradation are reported for thermal barrier co...
Furnace thermal cycling lifetime and microstructural degradation are reported for thermal barrier co...
Coatings are presently applied to Space Shuttle Main Engine (SSME) turbine blades for protection aga...
The durability of thermal barrier coatings (TBCs) can dictate the life of the hot section engine com...
A Mach 0.3 burner rig test program was conducted to determine how the fuel to air mass ratio affects...
A cyclic furnace study was conducted on thermal barrier systems to evaluate the effects of yttrium, ...
The aim of this study was to investigate the thermal cycling behaviour of NiCr-Al-Co-Y2O3 bond coati...
A promising two-layer thermal barrier coating system (TBS), Ni-16.4Cr-5.1A1-0.15Y/ZrO2-6.1Y2O3 (all ...
Initial experiments conducted on thermal barrier coatings prepared in the newly upgraded research pl...
This research was directed at developing the fundamentals that will facilitate the fabrication of ai...
Calcium silicate and yttria stabilized zirconia/MCrAlY thermal barrier coating systems on air-cooled...
Thermal barrier coatings were exposed to the high temperature and high heat flux produced by a 30 kW...
Eight plasma sprayed bond coatings were evaluated for their potential use with ZrO2-Y2O3 thermal bar...
Complex thermal barrier coating systems are one the most efficient high-temperature surface treatmen...
This is the second of two reports which discuss initial experiments on thermal barrier coatings prep...
Furnace thermal cycling lifetime and microstructural degradation are reported for thermal barrier co...
Furnace thermal cycling lifetime and microstructural degradation are reported for thermal barrier co...
Coatings are presently applied to Space Shuttle Main Engine (SSME) turbine blades for protection aga...
The durability of thermal barrier coatings (TBCs) can dictate the life of the hot section engine com...
A Mach 0.3 burner rig test program was conducted to determine how the fuel to air mass ratio affects...