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
FLUGGERÄT MIT HILFSTRIEBWERK UND VERFAHREN ZUR STEUERUNG DES HILFSTRIEBWERKS
VÉHICULE VOLANT AYANT UN PROPULSEUR AUXILIAIRE ET PROCÉDÉ DE COMMANDE DE PROPULSEUR AUXILIAIRE
2025-06-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / 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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