Combustor liner attachment assembly for gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 11293637
APP PUB NO 20200116356A1
SERIAL NO

16189730

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A combustor liner panel attachment assembly. The assembly includes a first liner extending from a first end to a second end, and circumferentially to partially define a combustion zone. The assembly also includes a second liner disposed circumferentially adjacent to the first liner. The assembly further includes a radial support having a shoulder in contact with a radially inner surface of each of the first liner and the second liner to radially retain the first liner and the second liner, the radial support allowing the first liner and the second liner to thermally grow axially.

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Patent Owner(s)

  • RAYTHEON TECHNOLOGIES CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
White, Kevin W Jupiter, US 6 28

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