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
Subjects
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
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Summary: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.
Bibliography:Application Number: CN20121593065