Disclosed is a hybrid propulsion system for an aircraft, comprising an internal combustion engine (1) and a dedicated electrical power circuit, which are connected in parallel to a transmission system (5) for rotating a propeller (7), characterized in that it further comprises a decoupling free wheeling unit (60) between the internal combustion engine (1) from the transmission system (5).
SYSTEME DE PROPULSION HYBRIDE POUR UN AERONEF
2022-12-23
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |