FUEL-AIR PREMIXER FOR A GAS TURBINE
The present disclosure relates to a fuel-air premixer (12) for a turbine system (10). The fuel-air premixer includes a swirler (50) and a centerbody (52). The swirler is configured to direct a flow of air through the premixer, and the centerbody is configured to inject fuel into the flow of air. Add...
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Main Authors | , , , , , , , |
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Format | Patent |
Language | English French German |
Published |
08.09.2021
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Subjects | |
Online Access | Get full text |
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