A hybrid propulsion system including a turbine engine including a high-pressure spool and a low-pressure spool, the low-pressure spool including reduction gear, the reduction gear forming part of a transmission gearbox which is positioned axially at a front end of the propulsion system; —first and second electric machines mechanically and respectively connected to the high-pressure and low-pressure spools, the electric machines being configured to operate in modes referred to as motor and generator, the first and second electric machines being fixed to the transmission gearbox; —a control system which is configured to allow the transfer of power between the high-pressure and low-pressure spools via the first and second electric machines.
SYSTEME PROPULSIF HYBRIDE POUR UN AERONEF
HYBRID PROPULSION SYSTEM FOR AN AIRCRAFT
HYBRIDANTRIEBSSYSTEM FÜR EIN FLUGZEUG
28.05.2025
Patent
Elektronische Ressource
Französisch