Repair or remanufacture of liner panels for a gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10094242
APP PUB NO 20150240661A1
SERIAL NO

14628263

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Abstract

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A method of remanufacturing a liner panel for a gas turbine engine includes removing a bushing from a damaged component; and molding the bushing with a material charge. A liner panel for a gas turbine engine includes a forward fan exit case liner panel with a donor bushing from a damaged forward fan exit case liner panel. A liner panel for a gas turbine engine includes a forward fan exit case liner panel molded from a material charge that includes a multiple of layers. At least one of the multiple of layer includes a discontinuity.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bogue, William Hebron, US 55 256
Gates, Brandon A DeWitt, US 10 26
Holland, Brian K Lansing, US 16 55
Morden, Michael A Holt, US 9 20

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