A method is provided for operating a system of an aircraft. During this method, rotation of a propulsor rotor is driven using mechanical power output by a powerplant. The powerplant includes a first drive device and a second drive device. The first drive device generates a first portion of the mechanical power. The second drive device generates a second portion of the mechanical power. A ratio between the first portion of the mechanical power and the second portion of the mechanical power is adjusted to control vibrations of the powerplant.
ADJUSTING AIRCRAFT POWERPLANT POWER SPLIT TO CONTROL POWERPLANT VIBRATI ONS
REGLAGE DE LA REPARTITION DE LA PUISSANCE D~UN GROUPE MOTOPROPULSEUR D~AERONEF POUR CONTROLER LES VIBRATIONS DU GROUPE MOTOPROPULSEUR
2023-12-21
Patent
Elektronische Ressource
Englisch
ADJUSTING AIRCRAFT POWERPLANT POWER SPLIT TO CONTROL POWERPLANT VIBRATIONS
Europäisches Patentamt | 2023
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