Combustion bypass passive valve system for a gas turbine

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United States of America Patent

PATENT NO 10337739
APP PUB NO 20180051882A1
SERIAL NO

15237795

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Abstract

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A combustor for a gas turbine, including: a combustor chamber; a casing enclosing the combustor chamber and defining an area therebetween for passing compressor discharge air into the combustor chamber for use in combustion; and at least one passive bypass valve for selectively extracting a portion of the compressor discharge air from the area between the combustor chamber and the casing to adjust a temperature in the combustor.

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Patent Owner(s)

Patent OwnerAddress
GE INFRASTRUCTURE TECHNOLOGY LLC300 GARLINGTON ROAD GREENVILLE SC 29615

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Miranda, Carlos Miguel Greer, US 24 232
Widener, Stanley Kevin Greer, US 51 1000

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