The method involves operating a two-position selector to stop an engine i.e. turbomotor (3), or to set the engine into operation, during a selection step. The engine is controlled automatically to implement an idling mode of operation if collective pitch of blades (301) is less than a threshold, and if an aircraft (1) is standing on ground during a regulation step. Original speed of rotation is determined for regulating rotation speed at a level defined by a manufacturer to ensure operation of the aircraft outside a ground resonance range. An independent claim is also included for a regulation device for regulating a power plant of an aircraft.
Procédé automatique de régulation d'un groupe de motorisation d'aéronef à voilure tournante, dispositif et aéronef
Automatic method for controlling a rotorcraft engine group, device and rotorcraft
Automatisches Einstellverfahren der Motorenanlage eines Drehflügelflugzeugs, Vorrichtung und Drehflügelflugzeug
2016-06-08
Patent
Electronic Resource
French
PROCEDE AUTOMATIQUE DE REGULATION D'UN GROUPE DE MOTORISATION D'AERONEF, DISPOSITIF ET AERONEF
European Patent Office | 2016
|Procédé automatique de régulation d'un groupe de motorisation d'aéronef, dispositif et aéronef
European Patent Office | 2016
|European Patent Office | 2019
|European Patent Office | 2018
|European Patent Office | 2019
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