The invention relates to a method (100) for correcting the thrust vector created by a thrust assembly associated with electrical means for correcting said thrust vector. Such a thrust assembly comprises a mechanical rotor rotated by a rotary shaft of an internal combustion engine (12a-e) in response to a power command (PC). Such a method (100) comprises a step (110) of producing said power command (PC) so as to decrease the difference (RSE) between a setpoint rotational speed (RSI) and a measured rotational speed (RSM) of the shaft of the internal combustion engine (12a-e) and thereby feedback controlling the speed of the shaft of the internal combustion engine (12a-e). The method further comprises a step (120) of producing an actuation command (AC) for actuating electrical means (19a-e) for correcting the thrust vector, said command being produced on the basis of said difference (RSE) separately from the step of feedback controlling the speed of the shaft of the internal combustion engine (12a-e).


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    Title :

    PROCÉDÉ DE PILOTAGE D'UN GROUPE DE POUSSÉE POUR DISPOSITIF DE PROPULSION


    Additional title:

    METHOD FOR CONTROLLING A THRUST ASSEMBLY FOR A PROPULSION DEVICE
    VERFAHREN ZUR STEUERUNG EINER SCHUBANORDNUNG FÜR EINE ANTRIEBSVORRICHTUNG


    Contributors:

    Publication date :

    2023-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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