Varying thickness thermal barrier for combustion turbine...

Details Varying thickness thermal barrier for combustion turbine... Varying thickness thermal barrier for combustion turbine...

F - Mech Eng,Light,Heat,Weapons

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F02C 3/14 (2006.01) F02C 7/30 (2006.01) F23R 3/00 (2006.01) F23R 3/08 (2006.01)

Patent

CA 1231240

ABSTRACT OF THE DISCLOSURE This improvement for the combustor of a combus- tion turbine provides a tapered thickness insulating (above 10% porosity is desirable) ceramic coating on the interior of a metallic combustor. There is little or no coating adjacent to the air inlets and the thickness increases in the downstream direction. Both peak tempera- ture and the temperature gradient of the combustor are significantly reduced.

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