The invention relates to a method for automatically controlling an operating mode of a turboshaft engine of a helicopter, comprising a step (10) of receiving data (27, 28, 29) that are representative of the flight of the helicopter; a step (11) of selecting the turboshaft engine for which a change of mode would be most relevant; a step (12) of determining an operating mode of said turboshaft engine, known as the selected mode, selected from a plurality of predetermined operating modes; and a step (14) of ordering the operating mode of said turboshaft engine into said selected mode. The invention also relates to a corresponding control device.


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    Title :

    PROCEDE DE COMMANDE AUTOMATIQUE DU REGIME DE FONCTIONNEMENT D'UN TURBOMOTEUR D'UN HELICOPTERE, DISPOSITIF DE COMMANDE CORRESPONDANT ET HELICOPTERE EQUIPE D'UN TEL DISPOSITIF


    Additional title:

    METHOD FOR AUTOMATICALLY CONTROLLING THE OPERATING SPEED OF A HELICOPTER TURBOSHAFT ENGINE, CORRESPONDING CONTROL DEVICE AND HELICOPTER PROVIDED WITH SUCH A DEVICE
    VERFAHREN ZUR AUTOMATISCHEN STEUERUNG DER BETRIEBSGESCHWINDIGKEIT EINES HUBSCHRAUBERWELLENTRIEBWERKS, ZUGEHÖRIGES STEUERUNGSVERFAHREN UND MIT SOLCH EINER VORRICHTUNG AUSGESTATTETER HUBSCHRAUBER


    Contributors:

    Publication date :

    2020-06-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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