Air-fuel Premixer For Gas Turbine Combustor With Variable Swirler

The invention relates to and provides a swirler assembly in a gas turbine combustor. The swirler assembly includes a hub, a shroud, and a plurality of vanes connected between the hub (201) and the shroud (202). a vane angle of the plurality of vanes is adjustable.

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Bibliographic Details
Main Authors BATHINA MAHESH, PANDA AMULYA
Format Patent
LanguageChinese
English
Published 17.07.2013
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Abstract The invention relates to and provides a swirler assembly in a gas turbine combustor. The swirler assembly includes a hub, a shroud, and a plurality of vanes connected between the hub (201) and the shroud (202). a vane angle of the plurality of vanes is adjustable.
AbstractList The invention relates to and provides a swirler assembly in a gas turbine combustor. The swirler assembly includes a hub, a shroud, and a plurality of vanes connected between the hub (201) and the shroud (202). a vane angle of the plurality of vanes is adjustable.
Author BATHINA MAHESH
PANDA AMULYA
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Snippet The invention relates to and provides a swirler assembly in a gas turbine combustor. The swirler assembly includes a hub, a shroud, and a plurality of vanes...
SourceID epo
SourceType Open Access Repository
SubjectTerms AIR
BLASTING
BURNERS
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN
WEAPONS
Title Air-fuel Premixer For Gas Turbine Combustor With Variable Swirler
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