Low emissions combustor premixer
AssigneeGeneral Electric Company
InventorAnthony John Dean
Life of this patent
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Abstract
A low emissions combustor includes a premixer for premixing liquid fuel and compressed air for achieving low NOx emissions without water or steam injection. The premixer includes a centerbody disposed in a shroud defining an annular flow channel extending between an inlet and outlet of the shroud. A plurality of fuel injection orifices are spaced circumferentially around the centerbody with each having an outlet being substantially flush with an outer surface of the centerbody. The fuel injection orifices inject liquid fuel into the flow channel wherein it is atomized by compressed air channeled through the shroud inlet. In a preferred embodiment, the fuel injection orifices are inclined at an acute angle for injection the fuel toward the shroud inlet to increase differential mixing velocity with the compressed air.
Claims6
A pre-mixer for pre-mixing liquid fuel and compressed air for flow to a gas turbine engine low NOx combustion chamber comprising:
- a tubular shroud having an inlet at one end thereof for receiving said compressed air, and an outlet at an opposite end thereof;
- a centerbody having an outer surface and disposed coaxially in said shroud and spaced radially inward therefrom to define a flow channel from said shroud inlet to said shroud outlet;
- a plurality of fuel injection orifices spaced circumferentially apart around said center body and each having an outlet being substantially flush with said center body outer surface;
- a fuel supply circuit extending in said centerbody in flow communication with said fuel injection orifices for supplying said liquid fuel to said orifices for discharge therefrom into said flow channel for pre-mixing said air prior to discharge from said shroud outlet;
- wherein said fuel injection orifices are positioned axially between said shroud inlet and said shroud outlet for defining a pre-mixing region in said flow channel extending to said shroud outlet, with said pre-mixing region being unobstructed;
- wherein said fuel injection orifices are inclined at an acute angle with respect to said centerbody outer surface for injecting said fuel toward said shroud inlet to increase the differential mixing velocity with said compressed air;
- said pre-mixer in combination with a gas turbine engine compressor disposed in flow communication with said shroud outlet for channeling compressed discharge air into said shroud inlet, said combustion chamber is disposed in flow communication with said shroud outlet and said fuel outlets are spaced axially upstream from said shroud outlet;
- and
- wherein said fuel supply circuit comprises an annular manifold disposed in said centerbody in flow communication with said fuel injection orifices, a center bore extending in said centerbody for channeling said fuel, and a plurality of fuel spokes extending radially outwardly from said center bore to said manifold for distributing said fuel to said manifold.
Dependencies are inferred from the claim text.