A gas turbine includes a compressor with a plurality of pressure plates, a combustor downstream from the compressor, and a turbine downstream from the combustor and axially aligned with the compressor. The combustor produces combustion gases that flow to the turbine. A first manifold connected to th
A gas turbine includes a compressor with a plurality of pressure plates, a combustor downstream from the compressor, and a turbine downstream from the combustor and axially aligned with the compressor. The combustor produces combustion gases that flow to the turbine. A first manifold connected to the combustor contains a first process gas for combustion in the combustor. A second manifold connected upstream of the turbine contains a second process gas, and a portion of the second process gas flows to the plurality of pressure plates.
대표청구항▼
1. A gas turbine, comprising: a. a compressor, the compressor comprising a plurality of pressure plates that extend radially in the compressor to prevent fluid flow through the compressor;b. at least one combustor downstream from the compressor;c. a turbine downstream from the at least one combustor
1. A gas turbine, comprising: a. a compressor, the compressor comprising a plurality of pressure plates that extend radially in the compressor to prevent fluid flow through the compressor;b. at least one combustor downstream from the compressor;c. a turbine downstream from the at least one combustor and axially aligned with the compressor, wherein the at least one combustor produces combustion gases that flow to the turbine;d. a first manifold connected to the at least one combustor, the first manifold containing a first process gas for combustion in the at least one combustor;e. a second manifold connected upstream of the turbine, the second manifold containing a second process gas, wherein a portion of the second process gas flows to the plurality of pressure plates. 2. The gas turbine as recited in claim 1, further including a plurality of combustors. 3. The gas turbine as recited in claim 2, wherein the first manifold is connected to each of the plurality of combustors. 4. The gas turbine as recited in claim 1, wherein the second process gas is carbon dioxide or nitrogen. 5. The gas turbine as recited in claim 1, wherein the second process gas enters the gas turbine and flows away from the turbine. 6. The gas turbine as recited in claim 1, further including an extraction port on the compressor proximate to the plurality of pressure plates, wherein a third process gas flows through the extraction port for cooling the pressure plates. 7. A gas turbine, comprising: a. a compressor, the compressor comprising a plurality of pressure plates that extend radially in the compressor to prevent fluid flow through the compressor;b. at least one combustor downstream from the compressor;c. a turbine downstream from the at least one combustor and axially aligned with the compressor, wherein the at least one combustor produces combustion gases that flow to the turbine;d. a first manifold connected to the gas turbine upstream of the turbine, the first manifold containing a first process gas for combustion in the at least one combustor;e. a second manifold connected upstream of the turbine, the second manifold containing a second process gas, wherein a portion of the second process gas flows to the plurality of pressure plates. 8. The gas turbine as recited in claim 7, further including a plurality of combustors. 9. The gas turbine as recited in claim 8, wherein the first manifold is connected to each of the plurality of combustors. 10. The gas turbine as recited in claim 7, wherein the second process gas is carbon dioxide or nitrogen. 11. The gas turbine as recited in claim 7, wherein the second process gas enters the gas turbine and flows away from the turbine. 12. The gas turbine as recited in claim 7, further including an extraction port on the compressor proximate to the plurality of pressure plates, wherein a third process gas flows through the extraction port for cooling the pressure plates. 13. A method for operating a gas turbine, the gas turbine having a compressor, a plurality of combustors, and a turbine, the method comprising: a. removing compressor blades from the compressor;b. installing a plurality of pressure plates in the compressor to prevent fluid flow through the compressor;c. supplying a first process gas to the gas turbine upstream of the turbine;d. combusting the first process gas in at least one of the plurality of combustors;e. supplying a second process gas to the gas turbine upstream of the turbine; andf. directing at least a portion of the second process gas to the plurality of pressure plates. 14. The method of claim 13, further including supplying the first process gas to each of the plurality of combustors. 15. The method of claim 13, further including mixing the first process gas with the second process gas prior to combustion. 16. The method of claim 13, wherein the second process gas is carbon dioxide or oxygen. 17. The method of claim 13, further including cooling at least one of the plurality of pressure plates with a third process gas.
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Fonda-Bonardi G. (2075 Linda Flora Dr. L Los Angeles CA 90077), Apparatus for generating electricity.
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