Multi-stage combustor with a linear actuator controlling a variable air bypass

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United States of America Patent

PATENT NO 10041681
APP PUB NO 20160040884A1
SERIAL NO

14452568

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Abstract

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The present application provides a combustor for use with a gas turbine engine. The combustor may include a primary stage nozzle in communication with a linear actuator and a number of stationary secondary nozzles surrounding the primary stage nozzle in whole or in part. The linear actuator varies the position of the primary stage nozzle with respect to the stationary secondary nozzles.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 NEUMANN WAY MAIL DROP F16 EVENDALE OH 45215-6301

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Citeno, Joseph Vincent Greenville, US 12 172
Johnson, Thomas Edward Greer, US 130 2441

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