The invention is particularly concerned with sealing thermal barrier coating systems of the type in use and being contemplated for use in diesel and other internal combustion engines. The invention also would find application in moderately high temperature regions of gas turbine engines and any other application employing a thermal barrier coating at moderate temperatures. Ni-35Cr-6Al-1Y, Ni-35Cr-6Al-1Yb, or other metallic alloy denoted as MCrAlx is applied over a zirconia-based thermal barrier overlayer. The close-out layer is glass-bead preened to densify its surface. This seals and protects the thermal barrier coating system
This document contains papers from the 1997 Thermal Barrier Coatings Workshop, sponsored by the TBC ...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Application of thermal barrier coatings deposited by thermal spray, physical vapor and possibly othe...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A thin, light-weight, multi-layer coating is provided for protecting metals and their alloys from en...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
Thermal barrier coatings for aero-propulsion operation have been in use since the 1960s. These therm...
Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engin
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
This document contains papers from the 1997 Thermal Barrier Coatings Workshop, sponsored by the TBC ...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Application of thermal barrier coatings deposited by thermal spray, physical vapor and possibly othe...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A thin, light-weight, multi-layer coating is provided for protecting metals and their alloys from en...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
Thermal barrier coatings for aero-propulsion operation have been in use since the 1960s. These therm...
Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engin
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
This document contains papers from the 1997 Thermal Barrier Coatings Workshop, sponsored by the TBC ...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Application of thermal barrier coatings deposited by thermal spray, physical vapor and possibly othe...