Gas turbine plant with ammonia decomposition system

US12398663B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12398663-B2
Application numberUS-202418677558-A
CountryUS
Kind codeB2
Filing dateMay 29, 2024
Priority dateMay 30, 2023
Publication dateAug 26, 2025
Grant dateAug 26, 2025

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present disclosure relates to a gas turbine plant which decomposes ammonia and supplies it as fuel to a combustor of the gas turbine. The gas turbine plant supplies sufficient heat to the ammonia in order to thermally decompose the ammonia effectively, and separates the residual ammonia present in the decomposition gas and supplies it to a combustor of the gas turbine.

First claim

Opening claim text (preview).

What is claimed is: 1. A gas turbine plant with an ammonia decomposition system, the gas turbine plant comprising: a storage tank configured to store liquid ammonia; a supply pump configured to supply the liquid ammonia of the storage tank; a preheater configured to preheat the liquid ammonia supplied by the supply pump; a vaporizer configured to vaporize the liquid ammonia preheated by the preheater; a superheater configured to superheat gaseous ammonia vaporized by the vaporizer; a decomposition reactor configured to thermally decompose the gaseous ammonia superheated by the superheater; a separator configured to separate residual ammonia from decomposition gas decomposed by the decomposition reactor; and a second combustor configured to generate combustion gas in such a way as to supply heat to the decomposition reactor, wherein synthesis gas consisting of hydrogen and nitrogen with the residual ammonia removed by the separator is supplied to a first combustor of a gas turbine, wherein a heat transfer fluid absorbs heat from the combustion gas or the decomposition gas and supplies the heat to the liquid ammonia, the gaseous ammonia, the synthesis gas supplied to the first combustor, or fuel supplied to the second combustor; wherein a heat transfer fluid circuit through which the heat transfer fluid flows comprises: a pump; a first heat exchanger that absorbs heat by heat exchange with the combustion gas or the decomposition gas; and a second heat exchanger that supplies heat by heat exchange with the liquid ammonia, the gaseous ammonia, the synthesis gas supplied to the first combustor, or fuel supplied to the second combustor; wherein exhaust gas discharged from the gas turbine is supplied to a heat recovery steam generator, wherein steam generated by heat of the exhaust gas in the heat recovery steam generator is supplied to a steam turbine and drives the steam turbine, and then flows into a condenser, and water condensed in the condenser is supplied back to the heat recovery steam generator, wherein a portion of the water condensed in the condenser is supplied as the heat transfer fluid to the heat transfer fluid circuit, and wherein the heat transfer fluid circuit further comprises an internal heat exchanger in which the water discharged from the condenser and the water entering the condenser exchange heat. 2. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein the second heat exchanger is any one of the preheater, the vaporizer, and the superheater. 3. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein the second heat exchanger is disposed such that the synthesis gas supplied from the separator to the first combustor passes through the second heat exchanger. 4. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein the second heat exchanger is disposed such that the fuel supplied to the second combustor passes through the second heat exchanger. 5. The gas turbine plant with an ammonia decomposition system of claim 4 , wherein a portion of the decomposition gas decomposed by the decomposition reactor or a portion of the synthesis gas from which the residual ammonia has been removed in the separator is supplied as fuel for the second combustor. 6. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein a portion of the synthesis gas from which the residual ammonia has been removed in the separator is supplied as fuel for the second combustor, and wherein the second heat exchanger is disposed such that the synthesis gas from the separator passes through the second heat exchanger before being branched. 7. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein the water discharged from the condenser absorbs heat while passing through the internal heat exchanger, absorbs heat while passing through the first heat exchanger, and then supplies the heat while passing through the second heat exchanger, and supplies the heat while passing through the internal heat exchanger, and then flows back into the condenser. 8. The gas turbine plant with an ammonia decomposition system of claim 1 , wherein the combustion gas supplies heat while passing through the decomposition reactor and the superheater, and wherein the heat transfer fluid absorbs heat from the combustion gas that has passed through the decomposition reactor and the superheater. 9. A gas turbine plant with an ammonia decomposition system, the gas turbine plant comprising: a storage tank configured to store liquid ammonia; a supply pump configured to supply the liquid ammonia of the storage tank; a preheater configured to preheat the liquid ammonia supplied by the supply pump; a vaporizer configured to vaporize the liquid ammonia preheated by the preheater; a superheater configured to superheat gaseous ammonia vaporized by the vaporizer; a decomposition reactor configured to thermally decompose the gaseous ammonia superheated by the superheater; and a separator configured to separate residual ammonia from decomposition gas decomposed by the decomposition reactor, wherein synthesis gas consisting of hydrogen and nitrogen with the residual ammonia removed by the separator is supplied to a first combustor of a gas turbine, wherein a heat transfer fluid absorbs heat from the decomposition gas and supplies the heat to the liquid ammonia, the gaseous ammonia, or the synthesis gas supplied to the first combustor, wherein a heat transfer fluid circuit through which the heat transfer fluid flows comprises: a pump; a first heat exchanger that absorbs heat by heat exchange with the decomposition gas; and a second heat exchanger that supplies heat by heat exchange with the liquid ammonia, the gaseous ammonia, or the synthesis gas supplied to the first combustor; wherein exhaust gas discharged from the gas turbine is supplied to a heat recovery steam generator, wherein steam generated by heat of the exhaust gas in the heat recovery steam generator is supplied to a steam turbine and drives the steam turbine, and then flows into a condenser, and water condensed in the condenser is supplied back to the heat recovery steam generator, wherein a portion of the water condensed in the condenser is supplied as the heat transfer fluid to the heat transfer fluid circuit; and wherein the heat transfer fluid circuit further comprises an internal heat exchanger in which the water discharged from the condenser and the water entering the condenser exchange heat. 10. The gas turbine plant with an ammonia decomposition system of claim 9 , wherein the second heat exchanger is any one of the preheater, the vaporizer, and the superheater. 11. The gas turbine plant with an ammonia decomposition system of claim 9 , wherein the second heat exchanger is disposed such that the synthesis gas supplied from the separator to the first combustor passes through the second heat exchanger. 12. The gas turbine plant with an ammonia decomposition system of claim 9 , wherein the water discharged from the condenser absorbs heat while passing through the internal heat exchanger, absorbs heat while passing through the first heat exchanger, and then supplies the heat while passing through the second heat exchanger, and supplies the heat while passing through the internal heat exchanger, and then flows back into the condenser.

Assignees

Inventors

Classifications

  • having at least one combustion gas turbine · CPC title

  • F01K11/02Primary

    the engines being turbines · CPC title

  • Process efficiency · CPC title

  • Separation of ammonia from gases and vapours {(as part of the ammonia synthesis process C01C1/04)} · CPC title

  • Separation of ammonia from ammonia liquors, e.g. gas liquors {(as part of the ammonia synthesis process C01C1/04)} · CPC title

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What does patent US12398663B2 cover?
The present disclosure relates to a gas turbine plant which decomposes ammonia and supplies it as fuel to a combustor of the gas turbine. The gas turbine plant supplies sufficient heat to the ammonia in order to thermally decompose the ammonia effectively, and separates the residual ammonia present in the decomposition gas and supplies it to a combustor of the gas turbine.
Who is the assignee on this patent?
Doosan Enerbility Co Ltd
What technology area does this patent fall under?
Primary CPC classification F01K11/02. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 26 2025 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).