An embodiment flying vehicle includes a fuel cell installed in a fuselage and configured to supply power to the fuselage and an auxiliary thruster installed in the fuselage and configured to provide an auxiliary thrust force by ejecting combustion gas generated by burning a portion of fuel to be supplied to the fuel cell.
FLYING VEHICLE HAVING AUXILIARY THRUSTER AND METHOD FOR CONTROLLING AUXILIARY THRUSTER
2025-06-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / 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 |
FLYING VEHICLE HAVING AUXILIARY THRUSTER AND METHOD FOR CONTROLLING AUXILIARY THRUSTER
European Patent Office | 2025
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