Method for producing an abradable seal

Coating processes – Spray coating utilizing flame or plasma heat – Metal or metal alloy coating

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427455, C23C 406, C23C 410

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057801169

ABSTRACT:
A gas turbine abradable seal is prepared by plasma spraying an oxidation resistant metallic material and boron nitride. The resultant structure comprises a metallic matrix encompassing a lubricating amount of boron nitride, with porosity of less than about 15 percent and a fabricated surface roughness of less than about 600 microinches. The reduced surface roughness and substantially reduced permeability of this seal provide substantially enhanced engine efficiency, and improved durability.

REFERENCES:
patent: 3084064 (1963-04-01), Cowden et al.
patent: 4696855 (1987-09-01), Pettit, Jr. et al.
patent: 4731302 (1988-03-01), Weissmantel et al.
patent: 4743514 (1988-05-01), Strangman et al.
patent: 4783341 (1988-11-01), Packer et al.
patent: 5358753 (1994-10-01), Rao et al.
Japanese Patent Abstract, Publication No. JP1242786, published Sep. 27, 1989.
Japanese Patent Abstract, Publication No. JP3096601, published Apr. 22, 1991.

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