A hybrid propulsion system for propelling an aircraft (100) comprises a first propulsion system (11) based on fuel cells and a second propulsion (12) system based on one or more combustion engines (15, 16). The first propulsion system (11) is fully providing a base thrust (A). The second propulsion system (12) is providing a peak thrust (B) needed for take-off of the aircraft (100) and/or is assisting the first propulsion system (11) in propelling the aircraft (100) when the peak thrust (B) is needed or in failure conditions.
HYBRID PROPULSION SYSTEM FOR PROPELLING AN AIRCRAFT, METHOD OF OPERATING SAME, AND HYBRID AIRCRAFT
HYBRIDANTRIEBSSYSTEM ZUM ANTREIBEN EINES FLUGZEUGES, VERFAHREN ZU DESSEN BETRIEB UND HYBRIDFAHRZEUG
SYSTÈME DE PROPULSION HYBRIDE POUR PROPULSER UN AÉRONEF, SON PROCÉDÉ DE FONCTIONNEMENT ET AÉRONEF HYBRIDE
2023-05-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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