A drive system of at least one rotor of an aircraft via electrical energy in addition to or as a replacement of a mechanical system. The electrical energy is provided at least in part by at least one device for recovering thermal energy from hot gases of an internal combustion engine of the aircraft.


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    Titel :

    Aircraft propulsion architecture integrating an energy recovery system


    Beteiligte:
    RECHAIN BRUNO (Autor:in) / SMAOUI HICHEM (Autor:in) / JOUBERT EMMANUEL (Autor:in) / BEZES GILLES (Autor:in) / SAUTREUIL MATTHIEU (Autor:in)

    Erscheinungsdatum :

    06.02.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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