Premixer for a combustor

1. A premixer for a combustor, comprising:

a centerbody disposed along an axis of symmetry, the centerbody including a hollow interior cavity;

a swirler assembly disposed radially outward of the centerbody, the swirler assembly including at least one swirler configured to impart a tangential velocity component to an air flow passing therethrough;

an annular peripheral wall disposed radially outward of the centerbody and the swirler assembly such that a mixing duct is defined by the annular peripheral wall and the centerbody, downstream from the swirler assembly;

an annular splitter positioned radially inward of the swirler assembly and radially outward of the centerbody such that a radial gap is defined between the annular splitter and an outer surface of the centerbody, wherein the annular splitter includes a trailing edge which extends axially aft of the swirler assembly;

a fuel gallery disposed inside the hollow interior cavity of the centerbody, the fuel gallery defined by a tubular conduit that extends longitudinally within the hollow interior cavity of the centerbody; and

a plurality of tubular fuel injectors extending radially outward from the fuel gallery and spanning the hollow interior cavity and passing through a plurality of injector ports communicating with an outer surface of the annular splitter,

wherein the plurality of injector ports are located downstream of the swirler assembly.

2. The premixer of claim 1 wherein a plurality of struts span the radial gap between the annular splitter and the outer surface of the centerbody, so as to divide the radial gap into a plurality of slots.

3. The premixer of claim 2 wherein the plurality of struts are configured so they do not impart a tangential velocity component to air passing through the plurality of slots.

4. The premixer of claim 2 wherein the plurality of struts are configured so they impart a tangential velocity component to air passing through the plurality of slots.

5. The premixer of claim 4 wherein the plurality of struts are configured so they impart the tangential velocity component to air passing through the plurality of slots which is less than the tangential velocity component imparted by the swirler assembly to air passing therethrough.

6. The premixer of claim 1 wherein the swirler assembly includes:

an inner swirler and an outer swirler separated from each other by an annular hub.

7. The premixer of claim 6 wherein the inner and outer swirlers are counterrotating.

8. The premixer of claim 1 , wherein the centerbody has an upstream end and a downstream end, the centerbody including a cylindrically-shaped first body portion and a conical second body portion downstream of the first body portion, the conical second body portion radially narrowing from the cylindrically-shaped first body portion towards the downstream end, the conical second body portion defining an exit at the downstream end.

9. A combustor for a gas turbine engine, comprising:

an annular inner liner;

an annular outer liner spaced apart from the annular inner liner;

a domed end disposed at an upstream end of the annular inner and outer liners, the

domed end including at least one annular dome, wherein each annular dome includes an annular array of premixers according to claim 1 .