An aeronautical propulsion system including a turbine engine having a fan and an electric motor drivingly coupled to at least one of the fan or the turbine engine. The aeronautical propulsion system additionally includes a fuel cell for providing electrical energy to the electric motor, the fuel cell generating water as a byproduct. The aeronautical portion system directs the water generated by the fuel cell to the turbine engine during operation to improve an efficiency of the aeronautical propulsion system.
Hybrid propulsion system for a gas turbine engine including a fuel cell
15.09.2020
Patent
Elektronische Ressource
Englisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |
Cooling system in hybrid electric propulsion gas turbine engine
Europäisches Patentamt | 2020
|COOLING SYSTEM IN HYBRID ELECTRIC PROPULSION GAS TURBINE ENGINE
Europäisches Patentamt | 2019
|Distributed hybrid propulsion system with turbine engine and aircraft
Europäisches Patentamt | 2023
|AIRCRAFT INCLUDING PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM
Europäisches Patentamt | 2018
|HYBRID PROPULSION VESSEL HAVING FUEL CELL AND HYBRID PROPULSION DEVICE
Europäisches Patentamt | 2025
|