Thermal barrier coating inside cooling channels

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United States of America Patent

PATENT NO 9869183
SERIAL NO

14799994

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a rotor disk rotatable about an axis and a gas path wall coupled to and radially outward of the rotor disk. The gas path wall bounds a radially inward portion of a gas path. A plurality of rotor spokes are radially intermediate the rotor disk and the gas path wall. The plurality of rotor spokes is circumferentially spaced to define a plurality of cooling channels intermediate the rotor disk and the gas path wall. A thermal barrier coating is disposed on a surface of at least one of the plurality of cooling channels. A method of cooling a rotor assembly is also disclosed.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hill, James D Tolland, US 92 968
Lord, Wesley K South Glastonbury, US 91 1458
Merry, Brian D Andover, US 210 3873
Suciu, Gabriel L Glastonbury, US 580 8113

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges13727914531101 - 1011 - 2021 - 3031 - 4051 - 6061 - 70020406080100120140160180200220240260280300

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