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
08.06.2016
Patent
Elektronische Ressource
Französisch
Procédé automatique de régulation d'un groupe de motorisation d'aéronef, dispositif et aéronef
Europäisches Patentamt | 2016
|PROCEDE AUTOMATIQUE DE REGULATION D'UN GROUPE DE MOTORISATION D'AERONEF, DISPOSITIF ET AERONEF
Europäisches Patentamt | 2016
|Europäisches Patentamt | 2019
|Europäisches Patentamt | 2019
|Europäisches Patentamt | 2018
|