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US 12,577,914 B2Granted
Methods and systems for starting hydrogen powered gas generators
AssigneeRtx Corporation
InventorsMarc J. Muldoon, Carroll V. Sidwell
Life of this patent
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Abstract
Aircraft hydrogen fuel systems and methods and systems of starting such systems are described. The aircraft hydrogen fuel systems include a hydrogen burning main engine, a main tank configured to contain liquid hydrogen to be supplied to the main engine during a normal operation, and a starter tank configured to contain gaseous hydrogen to be used during a startup operation of the main engine. Methods and processes for starting and/or restarting such systems are described.
Claims7
A method of performing a startup operation of a hydrogen-burning turbine engine, the method comprising:
- controlling a valve to supply liquid hydrogen from a fuel supply to a first hydrogen-burning turbine engine to convert the liquid hydrogen to gaseous hydrogen in a first fuel conditioning heat exchanger using waste heat generated by the first hydrogen-burning turbine engine and combusting the gaseous hydrogen in the first hydrogen-burning turbine engine during a normal operation;
- determining that the first hydrogen-burning turbine engine has a combustor flame-out condition;
- upon determining the first hydrogen-burning turbine engine has the combustor flame-out condition, controlling the valve to stop supplying the liquid hydrogen to the first hydrogen-burning turbine engine and to route the liquid hydrogen from the fuel supply to a second hydrogen-burning engine, wherein a second fuel conditioning heat exchanger of the second hydrogen-burning engine is configured to convert the liquid hydrogen to gaseous hydrogen;
- supplying the gaseous hydrogen to the first hydrogen-burning turbine engine from the second fuel conditioning heat exchanger to perform the startup operation via combustion of the gaseous hydrogen within the first hydrogen-burning turbine engine;
- and
- after the first hydrogen-burning turbine engine is started and returned to the normal operation, controlling the valve to redirect the liquid hydrogen from the fuel supply to the first hydrogen-burning turbine engine to convert the liquid hydrogen to gaseous hydrogen in the first fuel conditioning heat exchanger using the waste heat generated by the first hydrogen-burning turbine engine during the normal operation.
3 more elements
Dependencies are inferred from the claim text.