A power plant comprising two engine groups and a main power transmission gearbox. Each engine group drives the main gearbox mechanically in order to rotate a main rotor of an aircraft at a frequency of rotation NR. A first engine group comprising two main engines is regulated on a first setpoint NR* for the frequency of rotation NR, while a second engine group comprising a secondary engine is regulated on a second setpoint W2* for power of the second engine group. In addition, each engine operates with margins relative to operating limits. The second setpoint W2* for power is determined so that each secondary engine operates with a lowest second margin that is equal to the lowest first margin of the first engine group.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PROCEDE DE REGULATION D'UNE INSTALLATION MOTRICE TRIMOTEUR POUR UN AERONEF A VOILURE TOURNANTE


    Beteiligte:
    ROSSOTTO REGIS (Autor:in)

    Erscheinungsdatum :

    2018-05-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    PROCEDE DE REGULATION D'UNE INSTALLATION MOTRICE TRIMOTEUR POUR UN AERONEF A VOILURE TOURNANTE

    ROSSOTTO RÉGIS | Europäisches Patentamt | 2016

    Freier Zugriff

    PROCEDE DE REGULATION D'UNE INSTALLATION MOTRICE TRIMOTEUR POUR UN AERONEF A VOILURE TOURNANTE

    ROSSOTTO RÉGIS | Europäisches Patentamt | 2017

    Freier Zugriff


    INSTALLATION MOTRICE TRIMOTEUR REGULEE POUR UN AERONEF A VOILURE TOURNANTE

    ROSSOTTO REGIS / BOIE HANNO | Europäisches Patentamt | 2016

    Freier Zugriff

    INSTALLATION MOTRICE HYBRIDE POUR AERONEF A VOILURE TOURNANTE BIMOTEUR

    GROJO HOPDJANIAN MARIE LAURE / MARIOTTO DAMIEN / MEIFFRE LOIC | Europäisches Patentamt | 2017

    Freier Zugriff