Gas turbine nozzles with embossments in airfoil cavities

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United States of America Patent

PATENT NO 9745920
SERIAL NO

14483192

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Abstract

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The present application provides a nozzle for a gas turbine engine. The nozzle may include a band, a seal slot positioned within the band, an airfoil extending from the band, a cavity within the airfoil, and an embossment positioned about the band and the cavity.

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Patent Owner(s)

Patent OwnerAddress
GE INFRASTRUCTURE TECHNOLOGY LLC300 GARLINGTON RD GREENVILLE SC 29615

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Jasper, Martin James Simpsonville, US 8 5

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