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- W604893096 abstract "Fuel variability is a highly desired capability in a gas turbine combustor. A combustor design allowing for fuel interchangeability without an effect on its operational range would decrease costs associated with the use of alternative fuels. Therefore, it is necessary to understand the fuel variability capable by current gas turbine combustor designs. This research endeavor investigated the effects of swirl flows on the fuel flexibility of a gas turbine combustor since swirl flows are a common method of flame stabilization in gas turbine combustors. Two swirlers were fabricated and fourteen fuel blend compositions were combusted for a total of nineteen swirler/fuel blend combinations. The velocity and turbulence intensity distribution induced by each swirler was recorded using air as the flowing medium. These measurements showed that the angular velocity increases as the swirl van angle increases. Blowout velocities were also recorded for the nineteen swirler/fuel blend conditions to generate stability maps. The stability maps revealed that the combustion stability improved as the methane content is increased. However, fuel flexibility seemed to be feasible in all cases. It was also noticed that the burner obtained greater stability with the lower swirl vane angle." @default.
- W604893096 created "2016-06-24" @default.
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- W604893096 date "2005-12-01" @default.
- W604893096 modified "2023-09-27" @default.
- W604893096 title "Effects of Swirl on Fuel Variability in Gas Turbine Combustors" @default.
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