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Disclosed is an arrangement for expanding an annular fluid flow and a center fluid flow, comprising a combustor including a venturi and a centerbody, the centerbody including an upstream end and a downstream end, and a venturi throat defined by the venturi and disposed upstream of 0.19 inches downst

Disclosed is an arrangement for expanding an annular fluid flow and a center fluid flow, comprising a combustor including a venturi and a centerbody, the centerbody including an upstream end and a downstream end, and a venturi throat defined by the venturi and disposed upstream of 0.19 inches downstream of the downstream end of the centerbody.

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1. An arrangement for expanding an annular fluid flow and a center fluid flow in a gas turbomachine, the arrangement comprising: a gas turbomachine combustor including a combustion chamber, a venturi and a centerbody arranged within the combustion chamber, the venturi including a converging section

1. An arrangement for expanding an annular fluid flow and a center fluid flow in a gas turbomachine, the arrangement comprising: a gas turbomachine combustor including a combustion chamber, a venturi and a centerbody arranged within the combustion chamber, the venturi including a converging section and a diverging section, said centerbody including an upstream end and a downstream end; anda venturi throat defined by said venturi between the converging section and diverging section, said venturi throat being disposed entirely upstream of the downstream end of the centerbody. 2. An arrangement according to claim 1, wherein said venturi throat is disposed from about 0.31 inches upstream of said downstream end of said centerbody to about 0.5 inches upstream of said downstream end of said centerbody. 3. An arrangement according to claim 1, wherein said combustor is a dry low NOx combustor. 4. The arrangement according to claim 1, wherein the venturi is V-shaped in cross-section. 5. An arrangement for expanding an annular fluid flow and a center fluid flow in a gas turbomachine, the arrangement comprising: a gas turbomachine combustor disposed in a gas flow path between a compressor and a turbine within a gas turbine, said gas turbomachine combustor including a combustion chamber, a venturi and a centerbody arranged within the combustion chamber, the venturi including a converging section and a diverging section, said centerbody including an upstream end and a downstream end; anda venturi throat defined by said venturi between the converging section and diverging section, said venturi throat being disposed entirely upstream of the downstream end of the centerbody. 6. The arrangement according to claim 5, wherein the venturi is V-shaped in cross-section. 7. A method for arranging components to produce an expansion of an annular fluid flow and a center fluid flow in a gas turbomachine combustor, the method comprising: disposing a venturi throat arranged between a converging section and a diverging section of a venturi positioned within a combustion chamber radially outwardly of a centerbody of the gas turbomachine combustor; anddisposing said venturi throat entirely upstream of a downstream end of the centerbody. 8. A method according to claim 7, wherein said disposing includes said venturi throat being disposed from about 0.31 inches upstream of the downstream end of said centerbody to about 0.5 inches upstream of said downstream end of said centerbody. 9. A method for reducing NOx emissions by enhancing flame stability and reducing CO emissions in a gas turbomachine combustor, the method comprising: directing an annular fluid flow through a converging section of a venturi toward a centerbody of the gas turbomachine combustor including a combustion chamber, said directing occurring entirely upstream of a downstream end of the centerbody;expanding said annular fluid flow away from said centerbody through a diverging section of the venturi, said expanding occurring entirely upstream of the downstream end of the centerbody;drawing a center fluid flow radially outwardly via said expanding; andincreasing a centerline recirculation region size. 10. A method according to claim 9, wherein said directing of said annular fluid toward said centerbody is occurring from about 0.31 inches upstream of said downstream end of said centerbody to about 0.5 inches upstream of said downstream end of said centerbody. 11. A method according to claim 9, wherein said expanding of said annular fluid away from said centerbody is occurring substantially coplanar relative to said downstream end of said centerbody. 12. A method according to claim 9, wherein said expanding of said annular fluid away from said centerbody is occurring from less than 0.19 inches downstream of said downstream end of said centerbody to about 0.5 inches upstream of said downstream end of said centerbody. 13. A method according to claim 12, wherein said expanding of said annular fluid away from said centerbody is occurring from about 0.31 inches upstream of said downstream end of said centerbody to about 0.5 inches upstream of said downstream end of said centerbody.