Vehicle microturbine system and method of operating the same
US-2020158017-A1 · May 21, 2020 · US
US11512606B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-11512606-B1 |
| Application number | US-202117472258-A |
| Country | US |
| Kind code | B1 |
| Filing date | Sep 10, 2021 |
| Priority date | Sep 10, 2021 |
| Publication date | Nov 29, 2022 |
| Grant date | Nov 29, 2022 |
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The electrical power generation system including a micro-turbine including a combustor, a first stage turbine configured to be driven by a combustor exhaust from the combustor, at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor, a catalytic converter configured convert the combustor exhaust to a catalytic exhaust that includes at least exothermic heat, a second stage turbine configured to be driven by the catalytic exhaust from the catalytic converter, and one or more shafts connecting the first stage turbine and the second stage turbine to the at least one compressor such that rotation of the first stage turbine and the second stage turbine drives rotation of the at least one compressor.
Opening claim text (preview).
What is claimed is: 1. An electrical power generation system, comprising: a micro-turbine alternator, comprising: a combustor; a first stage turbine configured to be driven by a combustor exhaust from the combustor; at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor; a catalytic converter configured to receive the combustor exhaust from the first stage turbine and to convert the combustor exhaust to a catalytic exhaust that comprises at least exothermic heat; a second stage turbine configured to be driven by the catalytic exhaust from the catalytic converter; one or more shafts connecting the first stage turbine and the second stage turbine to the at least one compressor such that rotation of the first stage turbine and the second stage turbine drives rotation of the at least one compressor; and an exhaust turbine reheat cycle configured to transfer heat from i) the combustor exhaust exiting the combustor prior to entering the first stage turbine to ii) the combustor exhaust exiting the first stage turbine prior to entering the catalytic converter. 2. The electrical power generation system of claim 1 , wherein the exhaust turbine reheat cycle further comprises: a heat exchanger comprising: one or more heat rejection passageways; and one or more heat absorption passageways. 3. The electrical power generation system of claim 2 , wherein the exhaust turbine reheat cycle further comprises: a first passageway extending from the combustor to the one or more heat rejection passageways and fluidly connecting the combustor to the one or more heat rejection passageways. 4. The electrical power generation system of claim 2 , wherein the exhaust turbine reheat cycle further comprises: a second passageway extending from the one or more heat rejection passageways to the first stage turbine and fluidly connecting the one or more heat rejection passageways to the first stage turbine. 5. The electrical power generation system of claim 2 , wherein the exhaust turbine reheat cycle further comprises: a third passageway extending from the first stage turbine to the one or more heat absorption passageways and fluidly connecting the first stage turbine to the one or more heat absorption passageways. 6. The electrical power generation system of claim 2 , further comprising: a fourth passageway extending from the one or more heat absorption passageways to the catalytic converter and fluidly connecting the one or more heat absorption passageways to the catalytic converter. 7. The electrical power generation system of claim 1 , further comprising: a fifth passageway extending from the catalytic converter to the second stage turbine and fluidly connecting the catalytic converter to the second stage turbine. 8. The electrical power generation system of claim 1 , further comprising: a sixth passageway extending from the second stage turbine to a turbine of an auxiliary turbo charger and fluidly connecting the second stage turbine to the turbine. 9. The electrical power generation system of claim 3 , wherein the exhaust turbine reheat cycle further comprises: a second passageway extending from the one or more heat rejection passageways to the first stage turbine and fluidly connecting the one or more heat rejection passageways to the first stage turbine. 10. The electrical power generation system of claim 9 , wherein the exhaust turbine reheat cycle further comprises: a third passageway extending from the first stage turbine to the one or more heat absorption passageways and fluidly connecting the first stage turbine to the one or more heat absorption passageways. 11. The electrical power generation system of claim 10 , further comprising: a fourth passageway extending from the one or more heat absorption passageways to the catalytic converter and fluidly connecting the one or more heat absorption passageways to the catalytic converter. 12. The electrical power generation system of claim 11 , further comprising: a fifth passageway extending from the catalytic converter to the second stage turbine and fluidly connecting the catalytic converter to the second stage turbine. 13. The electrical power generation system of claim 12 , further comprising a sixth passageway extending from the second stage turbine to a turbine of an auxiliary turbo charger and fluidly connecting the second stage turbine to the turbine. 14. The electrical power generation system of claim 2 , wherein the one or more heat absorption passageways are thermally connected to the one or more heat rejection passageways. 15. The electrical power generation system of claim 2 , wherein the one or more heat absorption passageways are physically connected to the one or more heat rejection passageways. 16. The electrical power generation system of claim 1 , wherein the at least one compressor further comprises: a first stage compressor; and a second stage compressor located aft of the first stage compressor, the first stage compressor and the second stage compressor being operably connected to the combustor to provide the compressed airflow to the combustor. 17. The electrical power generation system of claim 16 , further comprising: an electric generator disposed along the one or more shafts such that electrical power is generated via rotation of the one or more shafts, wherein the electric generator is disposed along the one or more shafts between the first stage compressor and the second stage compressor. 18. The electrical power generation system of claim 17 , wherein at least one of the one or more shafts passes through the electric generator. 19. A vehicle, comprising: a propulsion system; and an electrical power generation system operably connected to the propulsion system, comprising: a micro-turbine alternator, comprising: a combustor; a first stage turbine configured to be driven by a combustor exhaust from the combustor; at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor; a catalytic converter configured to receive the combustor exhaust from the first stage turbine and to convert the combustor exhaust to a catalytic exhaust that comprises at least exothermic heat; a second stage turbine configured to be driven by the catalytic exhaust from the catalytic converter; one or more shafts connecting the first stage turbine and the second stage turbine to the at least one compressor such that rotation of the first stage turbine and the second stage turbine drives rotation of the at least one compressor and; an exhaust turbine reheat cycle configured to transfer heat from i) the combustor exhaust exiting the combustor prior to entering the first stage turbine to ii) the combustor exhaust exiting the first stage turbine prior to entering the catalytic converter.
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