An exemplary high-speed hybrid propulsion system for a tiltrotor aircraft (10) includes two pivotal nacelles (18a, 18b), each nacelle comprising an electric motor (40) coupled to a proprotor; an electric aircraft system (45); an electric generator (38); an electrical bus (44) electrically connected to the electric generator (38), the electric motors (40), and the electric aircraft system (45); and a convertible turbofan engine (24) coupled to an electric generator (38) through a drive shaft (36).


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    Title :

    HIGH-SPEED HYBRID PROPULSION FOR AIRCRAFT


    Additional title:

    HOCHGESCHWINDIGKEITSHYBRIDANTRIEB FÜR FLUGZEUGE
    PROPULSION HYBRIDE HAUTE VITESSE POUR AÉRONEF


    Contributors:

    Publication date :

    2021-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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 / F41H Panzerung , ARMOUR



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