Method for recirculation of exhaust gas and gas turbine for conducting said method

A method for recirculation of exhaust gas (18) from a combustion chamber (11) of a combustor (10) of a gas turbine back to the supply side of said combustor (10) is characterized in that a partial flow (18a) of the exhaust gas (18) in said combustion chamber (11) is directly extracted from said comb...

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Bibliographic Details
Main Authors THOMAS RUCK, HANSPETER KNOEPFEL, MICHELE PERETI
Format Patent
LanguageEnglish
Published 27.01.2016
Subjects
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A method for recirculation of exhaust gas (18) from a combustion chamber (11) of a combustor (10) of a gas turbine back to the supply side of said combustor (10) is characterized in that a partial flow (18a) of the exhaust gas (18) in said combustion chamber (11) is directly extracted from said combustion chamber (11) and internally fed back to an entrance of the combustor (10) through an internal channel (12) of said combustor (10).
Bibliography:Application Number: CN201510339608