The present invention relates to a hybrid-electric propulsion system for aircraft, specifically a propulsion system utilizing a propulsor driven by both an internal combustion engine and an electric machine. The hybrid-electric propulsion system includes an internal combustion engine such as a gas turbine, an electric machine (either motor or generator), and various subsystems including a thermal management subsystem for cooling flows, an electrical power supply system, a control system, and an electrochemical storage system.
HYBRID-ELECTRIC PROPULSION SYSTEM FOR AERONAUTICAL APPLICATIONS
HYBRIDELEKTRISCHES ANTRIEBSSYSTEM FÜR LUFTFAHRTANWENDUNGEN
SYSTÈME DE PROPULSION HYBRIDE-ÉLECTRIQUE POUR DES APPLICATIONS AÉRONAUTIQUES
2025-02-19
Patent
Electronic Resource
English
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
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