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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    Title :

    EMERGENCY OPERATING MODE FOR A PISTON ENGINE IN AN AIRPLANE


    Contributors:

    Publication date :

    2015-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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    Zeyns, J. | Engineering Index Backfile | 1938


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