BURNER WITH A COOLING SYSTEM ALLOWING AN INCREASED GAS TURBINE EFFICIENCY

A burner for a combustion chamber of a turbine, with an injection device for the introduction of at least one gaseous and/or liquid fuel into the burner is proposed. The injection device has at least one body arranged in the burner with at least two nozzles for introducing the at least one fuel into...

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Main Authors POYYAPAKKAM, Madhavan, LAUFFER, Diane, THEUER, Andre, BENZ, Urs, WINKLER, Anton
Format Patent
LanguageEnglish
French
German
Published 29.05.2019
Subjects
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Abstract A burner for a combustion chamber of a turbine, with an injection device for the introduction of at least one gaseous and/or liquid fuel into the burner is proposed. The injection device has at least one body arranged in the burner with at least two nozzles for introducing the at least one fuel into the burner, the body being configured with a streamlined cross-sectional profile which extends with a longitudinal direction perpendicularly or at an inclination to a main flow direction prevailing in the burner. The carrier air plenum is provided with holes such that carrier air exiting through the holes impinges an inner side of a leading edge portion of the body.
AbstractList A burner for a combustion chamber of a turbine, with an injection device for the introduction of at least one gaseous and/or liquid fuel into the burner is proposed. The injection device has at least one body arranged in the burner with at least two nozzles for introducing the at least one fuel into the burner, the body being configured with a streamlined cross-sectional profile which extends with a longitudinal direction perpendicularly or at an inclination to a main flow direction prevailing in the burner. The carrier air plenum is provided with holes such that carrier air exiting through the holes impinges an inner side of a leading edge portion of the body.
Author THEUER, Andre
LAUFFER, Diane
BENZ, Urs
WINKLER, Anton
POYYAPAKKAM, Madhavan
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DocumentTitleAlternate BRENNER MIT EINEM KÜHLSYSTEM FÜR ERHÖHTE GASTURBINENEFFIZIENZ
BRÛLEUR AVEC UN SYSTÈME DE REFROIDISSEMENT PERMETTANT D'ACCROÎTRE LE RENDEMENT D'UNE TURBINE À GAZ
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RelatedCompanies Ansaldo Energia Switzerland AG
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Snippet A burner for a combustion chamber of a turbine, with an injection device for the introduction of at least one gaseous and/or liquid fuel into the burner is...
SourceID epo
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SubjectTerms BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
Title BURNER WITH A COOLING SYSTEM ALLOWING AN INCREASED GAS TURBINE EFFICIENCY
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