NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine applications. This report discusses the history of TBCs emphasizing the role NASA has played beginning with (1) frit coatings in the 1940s and 1950s; (2) thermally sprayed coatings for rocket application in the 1960s and early 1970s; (3) the beginnings of the modern era of turbine section coatings in the mid 1970s; and (4) failure mechanism and life prediction studies in the 1980s and 1990s. More recent efforts are also briefly discussed
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magn...
Interest in thermal protection systems for high-speed vehicles is increasing because of the stringen...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
This document contains papers from the 1997 Thermal Barrier Coatings Workshop, sponsored by the TBC ...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Thermal barrier coatings (TBCs) are absolutely critical to the efficient and safe operation of gas t...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
This document contains the agenda and presentation abstracts for the Thermal Barrier Coating Worksho...
This report describes the work performed on a thermal barrier coating support technology task of the...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The program focuses on predicting the lives of two types of strain-tolerant and oxidation-resistant ...
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magn...
Interest in thermal protection systems for high-speed vehicles is increasing because of the stringen...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...
This document contains papers from the 1997 Thermal Barrier Coatings Workshop, sponsored by the TBC ...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Thermal barrier coatings (TBCs) are absolutely critical to the efficient and safe operation of gas t...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
The potential of thermal barrier coatings for use in utility gas turbines was assessed. Pressurized ...
This document contains the agenda and presentation abstracts for the Thermal Barrier Coating Worksho...
This report describes the work performed on a thermal barrier coating support technology task of the...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
The program focuses on predicting the lives of two types of strain-tolerant and oxidation-resistant ...
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magn...
Interest in thermal protection systems for high-speed vehicles is increasing because of the stringen...
Ceramic coatings have low thermal conductivity. They provide potential for increased engine performa...