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A pre-mixer assembly associated with a fuel supply system for mixing of air and fuel upstream from a main combustion zone in a gas turbine engine. The pre-mixer assembly includes a swirler assembly disposed about a fuel injector of the fuel supply system and a pre-mixer transition member. The swirle

A pre-mixer assembly associated with a fuel supply system for mixing of air and fuel upstream from a main combustion zone in a gas turbine engine. The pre-mixer assembly includes a swirler assembly disposed about a fuel injector of the fuel supply system and a pre-mixer transition member. The swirler assembly includes a forward end defining an air inlet and an opposed aft end. The pre-mixer transition member has a forward end affixed to the aft end of the swirler assembly and an opposed aft end defining an outlet of the pre-mixer assembly. The aft end of the pre-mixer transition member is spaced from a base plate such that a gap is formed between the aft end of the pre-mixer transition member and the base plate for permitting a flow of purge air therethrough to increase a velocity of the air/fuel mixture exiting the pre-mixer assembly.

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1. A fuel supply system in a gas turbine engine, the fuel supply system comprising: a plurality of main fuel injectors surrounding a center pilot nozzle; anda plurality of pre-mixer assemblies, each pre-mixer assembly associated with a respective one of said main fuel injectors, said pre-mixer assem

1. A fuel supply system in a gas turbine engine, the fuel supply system comprising: a plurality of main fuel injectors surrounding a center pilot nozzle; anda plurality of pre-mixer assemblies, each pre-mixer assembly associated with a respective one of said main fuel injectors, said pre-mixer assemblies for effecting a mixing of air and fuel upstream from a main combustion zone in the gas turbine engine, each pre-mixer assembly comprising: a swirler assembly disposed about said respective main fuel injector, said swirler assembly including a forward end defining an air inlet and an opposed aft end;a pre-mixer transition member extending from said aft end of said swirler assembly toward the main combustion zone, said pre-mixer transition member including a forward end affixed to said aft end of said swirler assembly and an opposed aft end defining an outlet of said pre-mixer assembly to the main combustion zone, wherein said aft end of said pre-mixer transition member is spaced from a base plate such that a gap is formed between said aft end of said pre-mixer transition member and said base plate, said gap permitting a flow of purge air therethrough to effect an increase in a velocity of the air and fuel mixture exiting said pre-mixer assembly;wherein a plurality of apertures is formed in each of said swirler assembly and said pre-mixer transition member to allow additional purge air to flow therethrough, said additional purge air for effecting an increase in said velocity of the air and fuel mixture as the air and fuel mixture flows through said pre-mixer assembly proximate to a boundary layer of said pre-mixer assembly; andwherein said apertures formed in said pre-mixer transition member have a smaller diameter than a diameter of said apertures in said swirler assembly. 2. The fuel supply system according to claim 1, wherein said base plate includes an annular array of apertures formed therein, each of said apertures associated with a respective pre-mixer assembly of the engine and permits the air and fuel mixture in each associated pre-mixer assembly to flow from the respective pre-mixer assembly into the main combustion zone. 3. The fuel supply system according to claim 1, wherein a gap is formed between said swirler assembly and said pre-mixer transition member of each pre-mixer assembly to allow additional purge air to flow therethrough to effect an additional increase in said velocity of the air and fuel mixture as the air and fuel mixture flows through each pre-mixer assembly proximate to said boundary layer of each pre-mixer assembly. 4. The fuel supply system according to claim 1, wherein said apertures in at least one of said swirler assembly and said pre-mixer transition member of each pre-mixer assembly are arranged in at least one annular row. 5. The fuel supply system according to claim 1, wherein said apertures in both said swirler assembly and said pre-mixer transition member of each pre-mixer assembly are arranged in at least one annular row. 6. The fuel supply system according to claim 1, wherein said apertures formed in said pre-mixer transition member are staggered with respect to said apertures in said swirler assembly. 7. The fuel supply system according to claim 1, wherein said base plate is attached to a liner head. 8. The fuel supply system according to claim 1, wherein said base plate is attached to a radially inner surface of a liner. 9. The fuel supply system according to claim 1, wherein said pre-mixer transition member comprises a forward end radial dimension and an aft end radial dimension smaller than said forward end radial dimension. 10. The fuel supply system according to claim 1, wherein said swirler assembly and said pre-mixer transition member are integrally formed. 11. The fuel supply system according to claim 1, wherein said swirler assembly and said pre-mixer transition member are separately formed. 12. The fuel supply system according to claim 1, wherein said pre-mixer transition member and said base plate extend to about the same axial location and said gap between said pre-mixer transition member aft end and said base plate comprises a dimension in at least one of a radial direction and a circumferential direction. 13. The fuel supply system according to claim 1, further comprising a passageway formed between said base plate and a pilot cone associated with said center pilot nozzle, said passageway permitting cooling air to flow therethrough for effecting a cooling of at least one of said pilot cone and said base plate.