Fuel nozzle for a gas turbine with radial swirler and axial swirler and gas turbine
AssigneeNuovo Pignone Tecnologie Srl
InventorMatteo CERUTTI
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Abstract
The fuel nozzle for the gas turbine includes a radial swirler and an axial swirler. The radial swirler is arranged to swirl a first flow of a first oxidant-fuel mixture and the axial swirler is arranged to swirl a second flow of a second oxidant-fuel mixture. The first flow may be fed by a central conduit and the second flow may be fed by an annular conduit surrounding the central conduit
Claims14
A fuel nozzle for a gas turbine comprising a radial swirler and an axial swirler, wherein the radial swirler is arranged to swirl a first flow of a first oxidant-fuel mixture and the axial swirler is arranged to swirl a second flow of a second oxidant-fuel mixture.
Dependencies are inferred from the claim text.