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.
INSTALLATION PROPULSIVE HYBRIDE ET PROCÉDÉ DE COMMANDE D'UNE TELLE INSTALLATION
HYBRID PROPULSIVE INSTALLATION AND METHOD FOR CONTROLLING SUCH AN INSTALLATION
HYBRIDANTRIEBSVORRICHTUNG UND VERFAHREN ZUR STEUERUNG EINER SOLCHEN VORRICHTUNG
08.03.2023
Patent
Elektronische Ressource
Französisch
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