초록 ▼

An injector for a gas turbine combustor including a catalyst coated surface forming a passage for feed gas flow and a channel for oxidant gas flow establishing an axial gas flow through a flow conditioner disposed at least partially within an inner wall of the injector. The flow conditioner includes

An injector for a gas turbine combustor including a catalyst coated surface forming a passage for feed gas flow and a channel for oxidant gas flow establishing an axial gas flow through a flow conditioner disposed at least partially within an inner wall of the injector. The flow conditioner includes a length with an interior passage opening into upstream and downstream ends for passage of the axial gas flow. An interior diameter of the interior passage smoothly reduces and then increases from upstream to downstream ends.

대표청구항 ▼

1. An injector for a gas turbine combustor comprising: an inner wall,at least one catalyst coated surface disposed within said inner wall and forming at least one passage adapted to provide a feed gas flow through the injector,at least one channel disposed within said inner wall and adapted for pass

1. An injector for a gas turbine combustor comprising: an inner wall,at least one catalyst coated surface disposed within said inner wall and forming at least one passage adapted to provide a feed gas flow through the injector,at least one channel disposed within said inner wall and adapted for passage of an oxidant gas flow through the injector,at least one of the feed gas flow or the oxidant gas flow establishing an axial gas flow through the inner wall and to the combustor,a mix zone downstream of the channel and the passage wherein the oxidant gas flow and feed gas flow mix,a flow conditioner disposed within said axial gas flow downstream of the mix zone, said flow conditioner including an elongated body having a length, an upstream end, a downstream end, an exterior surface at least partially disposed within the inner wall, and an interior passage for passage of said axial gas flow, the interior passage extending along the length, opening into the upstream and downstream ends and including an interior diameter, the interior diameter substantially smoothly reducing and then increasing from the upstream end to the downstream end, wherein the exterior surface of the flow conditioner includes a plurality of vanes, the vanes and the inner wall defining at least one substantially longitudinally extending channel for passage of said axial gas flow. 2. The injector of claim 1 wherein the injector includes a main injector and a catalytic pilot injector. 3. The injector of claim 2 wherein the inner wall is formed by the catalytic pilot injector. 4. The injector of claim 2 wherein the inner wall is formed by the catalytic pilot injector and the main injector, and the flow conditioner is disposed at least partially within the inner wall formed by the catalytic pilot injector. 5. The injector of claim 2 wherein the catalytic pilot injector is disposed at least partially within the main injector. 6. The injector of claim 1 wherein the vanes are disposed in a substantially spiral arrangement around the exterior surface. 7. An injector for a gas turbine combustor comprising: an inner wall,at least one catalyst coated surface disposed within said inner wall and forming at least one passage adapted to provide a feed gas flow through the injector,at least one channel disposed within said inner wall and adapted for passage of an oxidant gas flow through the injector,at least one of the feed gas flow or the oxidant gas flow establishing an axial gas flow through the inner wall and to the combustor,a mix zone downstream of the channel and the passage wherein the oxidant gas flow and feed gas flow mix,a flow conditioner disposed within said axial gas flow downstream of the mix zone, said flow conditioner including an elongated body having a length,an upstream end,a downstream end,an exterior surface along the length, at least a portion of the exterior surface being spaced away from and disposed within the inner wall, the exterior surface of the flow conditioner and the inner wall of the injector defining at least one substantially longitudinally extending channel for passage of said axial gas flow, wherein the exterior surface includes a plurality of substantially longitudinally extending vanes including an outer perimeter configured to be disposed within the inner wall, the at least one substantially longitudinally extending channel of the flow conditioner including a plurality of substantially longitudinally extending vane channels for passage of said axial gas flow,and an interior passage for passage of said axial gas flow, the interior passage extending along the length, opening into the upstream and downstream ends and including an interior diameter, the interior diameter substantially smoothly reducing and then increasing from the upstream end to the downstream end. 8. The injector of claim 7 including at least one longitudinally extending tube having an interior and an exterior, the interior of the tube forming said at least one channel and the exterior forming the at least one catalyst coated surface. 9. The injector of claim 7 wherein the vanes are disposed in a substantially spiral arrangement about the exterior surface. 10. The injector of claim 7 wherein the vanes are disposed at a vane angle on the order of 10° to 25°. 11. The injector of claim 10 wherein the vanes are disposed at a vane angle on the order of 15°. 12. The injector of claim 7 wherein the interior diameter reduces on the order of 35% to 50%. 13. The injector of claim 7 wherein the interior diameter reduces over 75% to 90% of the length before increasing. 14. The injector of claim 7 wherein the vanes are disposed at a vane angle on the order of 10° to 25°, the interior diameter reduces on the order of 35% to 50%, over 75% to 90% of the length of the flow conditioner. 15. The injector of claim 7 further including a main swirl injector disposed about the flow conditioner.