A method is provided for operating a piston engine in an airplane in an emergency operating mode, in which a minimum power output of the piston engine is ensured in that an emergency operating mode is activated that is as much as possible independent of measured values of respective sensors provided for an operation of the piston engine, in which the measured values of the sensors are substituted with firmly specified values. A corresponding airplane is provided as well as to an emergency operation control unit for carrying out the provided method.


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    Titel :

    EMERGENCY OPERATING MODE FOR A PISTON ENGINE IN AN AIRPLANE


    Beteiligte:
    ANDREAS HEYL (Autor:in) / DANIEL DAMM (Autor:in) / MARKUS HERBORD (Autor:in) / WILFRIED FEUCHTER (Autor:in) / NICOLAS SOMMER (Autor:in) / MATTHIAS WETTIG (Autor:in)

    Erscheinungsdatum :

    09.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen



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