Gas turbine engine component having a thermal-insulating multila

Stock material or miscellaneous articles – Structurally defined web or sheet – Including components having same physical characteristic in...

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123 1R, 244 35R, 244123, 428218, 4283128, 4283166, 4283191, B32B 326, B64C 320

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061656003

ABSTRACT:
A method of forming a multilayer ceramic coating system on a substrate that requires thermal protection from a hostile thermal environment. The method generally entails forming at least one tape that contains ceramic particles dispersed in an organic constituent, such as a binder and/or plasticizer. If a single tape is used, the tape is formed of multiple layers of different compositions and applied as a unit to the substrate, thereby forming at least an innermost layer and an outermost layer on the substrate. If multiple tapes are used, a first tape is applied to the substrate to form the innermost layer, and a second tape is applied to form the outermost layer. The tape/tapes are then sintered to form innermost and outermost ceramic layers, respectively, on the substrate. The tape/tapes are formed and processed such that the innermost ceramic layer has submicron voids to provide a desired level of porosity, while the outermost ceramic layer is thinner, smoother and less porous than the innermost ceramic layer.

REFERENCES:
patent: 4061816 (1977-12-01), Kitamura
patent: 4552800 (1985-11-01), Blasch et al.
patent: 4698255 (1987-10-01), Pineau
patent: 5139977 (1992-08-01), Dwivedi
patent: 5942316 (1999-08-01), Luhrsen et al.

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