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.
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
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
2020-06-17
Patent
Elektronische Ressource
Französisch
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