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A counter-flow system for use in a turbine for selecting various mixtures of fluids for use with the system. The system may be used for a combustor for a gas powered turbine which employs a heat exchanger to combust a fuel without the emission of undesired chemical species. A gas powered turbine req

A counter-flow system for use in a turbine for selecting various mixtures of fluids for use with the system. The system may be used for a combustor for a gas powered turbine which employs a heat exchanger to combust a fuel without the emission of undesired chemical species. A gas powered turbine requires expanding gases to power the turbine blades. Fuel is combusted to produce the required gases. An oxidizer is introduced into the counter-flow system in a first direction before a first portion of fuel is introduced into the oxidizer. The fuel and oxidizer mixture is then flowed through a second pathway wherein the fuel and oxidizer mixture obtains a selected amount of thermal energy. Moreover, in a second pathway an equivalence ratio of the fuel and oxidizer mixture may be altered from the original fuel and oxidizer mixture.

대표청구항 ▼

What is claimed is: 1. A counter-flow combustor apparatus for use in a turbine for combusting a fuel in the presence of an oxidizer, the apparatus comprising: an oxidizer flow pathway defined by a first plurality of paths to direct a flow of a first portion of an oxidizer in a first direction along

What is claimed is: 1. A counter-flow combustor apparatus for use in a turbine for combusting a fuel in the presence of an oxidizer, the apparatus comprising: an oxidizer flow pathway defined by a first plurality of paths to direct a flow of a first portion of an oxidizer in a first direction along a first axis; a first fuel inlet to provide a first portion of fuel to said first portion of said oxidizer; a first mixing section to allow said oxidizer and said first portion of said fuel to mix, thereby forming a first oxidizer-fuel mixture; a first oxidizer-fuel pathway defined by a second plurality of paths to direct a flow of said first oxidizer-fuel mixture in a second direction along said first axis; and a second oxidizer inlet to form a second oxidizer-fuel mixture by allowing a second portion of said oxidizer to mix with the first oxidizer-fuel mixture. 2. The counter-flow combustor apparatus of claim 1, further comprising: a combustion chamber into which said second oxidizer-fuel mixture flows. 3. A counter-flow combustor apparatus for use in a turbine for combusting a fuel in the presence of an oxidizer, the apparatus comprising: an oxidizer flow pathway to direct a flow of a first portion of an oxidizer in a first direction along a first axis; a first fuel inlet to provide a first portion of fuel to said first portion of said oxidizer; a first mixing section to allow said oxidizer and said first portion of said fuel to mix, thereby forming a first oxidizer-fuel mixture; a first oxidizer-fuel pathway to direct a flow of said first oxidizer-fuel mixture in a second direction along said first axis; a second oxidizer inlet to form a second oxidizer-fuel mixture by allowing a second portion of said oxidizer to mix with the first oxidizer-fuel mixture; a second oxidizer-fuel pathway to direct a flow in said second direction; a second fuel inlet substantially near an outlet of said second oxidizer-fuel pathway; and wherein a second portion of fuel is injected into said second oxidizer-fuel mixture to be combusted in a combustion chamber. 4. The counter-flow combustor apparatus of claim 3, wherein said second oxidizer-fuel pathway defines said second oxidizer inlet; and wherein said first oxidizer-fuel mixture flows through said second oxidizer-fuel pathway to be mixed with said second portion of the oxidizer. 5. The counter-flow of combustor apparatus of claim 3, wherein said second oxidizer-fuel pathway is substantially parallel with said first axis. 6. The counter-flow combustor apparatus of claim 3, wherein said first oxidizer-fuel mixture flows through said second oxidizer-fuel pathway in said second direction; wherein said second direction is generally about 180째 relative to said first direction. 7. The counter-flow apparatus of claim 3, wherein said first oxidizer-fuel pathway and said second oxidizer-fuel pathway are selected from a group comprising at least one of a tube, a fin, a column, and combinations thereof. 8. The counter-flow combustor apparatus of claim 3, wherein: said second oxidizer inlet includes a port defined by said second oxidizer-fuel pathway; said second oxidizer-fuel pathway is a tube. 9. A combustor for use in a gas powered turbine, the combustor comprising: a first oxidizer inlet for receiving a first volume of an oxidizer; a first flow conduit for directing the first volume oxidizer to a first injection area, wherein a first portion of fuel is injected into the oxidizer to form a first oxidizer-fuel mixture; a second flow conduit for directing the first oxidizer-fuel mixture; and a second oxidizer inlet associated with said second flow conduit to receive a second volume of the oxidizer into the first oxidizer-fuel mixture to form a second oxidizer-fuel mixture; an oxidizer pathway to direct the oxidizer; a first fuel inlet associated with said oxidizer pathway; and wherein a volume of fuel is injected into said oxidizer pathway as the first volume of the oxidizer moves through said oxidizer pathway. 10. The combustor of claim 9, wherein said oxidizer pathway operatively interconnects said first oxidizer inlet and said first flow conduit such that the oxidizer entering said first oxidizer inlet is directed towards and through said first flow conduit. 11. The combustor of claim 9, wherein: said second flow conduit includes a tube for directing the flow of the first oxidizer-fuel mixture; and said tube includes a wall substantially enclosing a flow pathway for flowing the first oxidizer-fuel mixture. 12. The combustor of claim 11, wherein: said second oxidizer inlet includes a bore defined by said tube of said second flow conduit; and the second volume of the oxidizer moves into said second flow conduit through said bores. 13. The combustor of claim 9, wherein: said second flow conduit includes a wall; and said second oxidizer inlet includes a bore of a selected size such that the second volume of the oxidizer is substantially controlled. 14. The combustor of claim 13, wherein: said bore includes a plurality of bore pathways, such that a selected plurality and a selected size for each of said selected plurality of said bore pathways substantially controls the second volume of the oxidizer. 15. The combustor of claim 9, wherein: said first oxidizer-fuel mixture includes a first equivalent ratio; said second oxidizer-fuel mixture includes a second equivalence ratio; wherein said first equivalence ratio and said second equivalence ratio are selected to be at least one of the group comprising: the first equivalence ratio equal to the second equivalence ratio; and the first equivalence ratio greater than the second equivalence ratio.