Add to ORKGThermal barrier ceramic coatings of stabilized zirconia over a bond coat of Ni Cr Al Y were tested for durability on air cooled turbine rotor blades in a research turbojet engine. Zirconia stabilized with either yttria, magnesia, or calcia was investigated. On the basis of durability and processing cost, the yttria stabilized zirconia was considered the best of the three coatings investigated
A program was conducted with the objective of developing advanced thermal barrier coating (TBC) syst...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
As part of a NASA program to reduce fuel consumption of current commercial aircraft engines, methods...
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magn...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
An analysis was made to determine the potential benefits of using a ceramic thermal insulation coati...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
Recent developments include the use of thermal barrier coatings to increase the efficiency of the mo...
Complex thermal barrier coating systems are one the most efficient high-temperature surface treatmen...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A simple, two-layer plasma-sprayed thermal barrier coating system was developed which has the potent...
A program was conducted with the objective of developing advanced thermal barrier coating (TBC) syst...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
As part of a NASA program to reduce fuel consumption of current commercial aircraft engines, methods...
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magn...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
An analysis was made to determine the potential benefits of using a ceramic thermal insulation coati...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
Recent developments include the use of thermal barrier coatings to increase the efficiency of the mo...
Complex thermal barrier coating systems are one the most efficient high-temperature surface treatmen...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A simple, two-layer plasma-sprayed thermal barrier coating system was developed which has the potent...
A program was conducted with the objective of developing advanced thermal barrier coating (TBC) syst...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
As part of a NASA program to reduce fuel consumption of current commercial aircraft engines, methods...