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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Main Authors | , |
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Format | Patent |
Language | Chinese English |
Published |
17.07.2013
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Subjects | |
Online Access | Get full text |
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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. |
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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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Notes | Application Number: CN20121593065 |
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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... |
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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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