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US 2022/0136700 A1Published application
Method of generating gas turbine fuel and gas turbine system
AssigneeAmtech Corporation
InventorsAsbjørn STRAND, Kumar Ranjan ROUT, De CHEN
Life of this patent
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Abstract
Disclosed herein is a fuel for use in a combustor of a gas turbine, wherein the fuel is a gas mixture that comprises hydrogen and exhaust gas from a total combustor.
Claims16
(canceled)
A fuel for use in a combustor of a gas turbine, wherein:
- the fuel is a gas mixture that comprises hydrogen and exhaust gas from a total combustor;
- and
- the fuel is produced according to a method that comprises:
- generating reformate using heat from a total combustor, wherein the reformate comprises hydrogen;
- and
- generating the fuel by mixing at least part of the reformate with at least part of the exhaust gas from the total combustor.
3 more elements
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A gas turbine system comprising:
- a gas turbine comprising a first combustor that, in use, receives a fuel that is a gas mixture that comprises hydrogen and an exhaust gas;
- a hydrogen producing system;
- a second combustor, wherein the second combustor is a total combustor and the second combustor is separate from the first combustor;
- and
- an air intake for receiving air;
- wherein:
- the hydrogen producing system is arranged to perform a reforming process on a carbonaceous gas, wherein the reforming process generates a reformate that comprises hydrogen;
- the total combustor is arranged to generate heat and an exhaust gas;
- and
- the combustor of the gas turbine is arranged to receive reformate output from the hydrogen producing system, exhaust gas from the total combustor, and air from the air intake.
7 more elements
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Dependencies are inferred from the claim text.