Aircraft propulsion systems and aircraft are described. The aircraft propulsion systems include aircraft systems having at least one hydrogen tank and an aircraft-systems heat exchanger and engine systems having at least a main engine core, a high pressure pump, a hydrogen-air heat exchanger, and an expander, wherein the main engine core comprises a compressor section, a combustor section having a burner, and a turbine section. Hydrogen is supplied from the at least one hydrogen tank through a hydrogen flow path, passing through the aircraft-systems heat exchanger, the high pressure pump, the hydrogen-air heat exchanger, and the expander, prior to being injected into the burner for combustion.
TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS
28.09.2023
Patent
Elektronische Ressource
Englisch
TURBO EXPANDERS FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS
Europäisches Patentamt | 2024
|Turbo expanders for turbine engines having hydrogen fuel systems
Europäisches Patentamt | 2024
|Hybrid electric power for turbine engines having hydrogen fuel systems
Europäisches Patentamt | 2024
|HYBRID ELECTRIC POWER FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS
Europäisches Patentamt | 2024
|