In an asymmetric operating regime, a first engine is operating in an active mode to provide motive power to an aircraft while a second engine is operating in a standby mode and de-clutched from a gearbox of the aircraft. In response to an emergency exit request, the second engine's speed is increased, at a maximum permissible rate, to a re-clutching speed while increasing the first engine's power output at a maximum permissible rate. When the re-clutching speed is reached, the second engine's power output is increased at a maximum permissible rate. In response to a normal exit request, the second engine's speed is increased to the re-clutching speed at a rate lower than the maximum permissible rate. When the re-clutching speed is reached, the second engine's power output is increased at a rate lower than the maximum permissible rate.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2023-06-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    MULTI-ENGINE AIRCRAFT AND METHOD OF OPERATING A MULTI-ENGINE AIRCRAFT

    MITROVIC LAZAR | Europäisches Patentamt | 2024

    Freier Zugriff

    System and method for operating a multi-engine aircraft

    BEAUCHESNE-MARTEL PHILIPPE / BIBOR OLIVIER | Europäisches Patentamt | 2024

    Freier Zugriff

    System and method for operating a multi-engine aircraft

    BEAUCHESNE-MARTEL PHILIPPE / BIBOR OLIVIER | Europäisches Patentamt | 2023

    Freier Zugriff

    SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFT

    BEAUCHESNE-MARTEL PHILIPPE / BIBOR OLIVIER | Europäisches Patentamt | 2023

    Freier Zugriff

    SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFT

    BEAUCHESNE-MARTEL PHILIPPE / BIBOR OLIVIER | Europäisches Patentamt | 2024

    Freier Zugriff