A hybrid propulsion installation for an aircraft, including an internal combustion engine having at least one combustion chamber; at least one electricity generator; an electrical propulsion system; electromechanical protection mechanism arranged between the or each electricity generator and the electrical propulsion system; wherein the installation also includes: an electronic computer configured to: receive at least one piece of information on a position of the electromechanical protection mechanism; receive at least one piece of information on a speed of rotation of a shaft of the internal combustion engine; and control the flow of fuel supplying the combustion chamber depending on the information received.


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    Title :

    INSTALLATION PROPULSIVE HYBRIDE ET PROCÉDÉ DE COMMANDE D'UNE TELLE INSTALLATION


    Additional title:

    HYBRID PROPULSIVE INSTALLATION AND METHOD FOR CONTROLLING SUCH AN INSTALLATION
    HYBRIDANTRIEBSVORRICHTUNG UND VERFAHREN ZUR STEUERUNG EINER SOLCHEN VORRICHTUNG


    Contributors:

    Publication date :

    2023-03-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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