The invention relates to a method for providing predefined desired drive characteristics (38, 50) in an aircraft, characterized by the following steps: —driving a thrust generation element of the aircraft by means of an electric motor that has actual drive characteristics (34) which include at least some of the desired drive characteristics (38, 50) but are also partly different therefrom; and—having a control device adjust operating points of the electric motor exclusively according to the desired drive characteristics (38, 50).


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    Title :

    VERFAHREN ZUM BEREITSTELLEN EINER VORBESTIMMTEN ANTRIEBSCHARAKTERISTIK IN EINEM FLUGZEUG UND ZUGEHÖRIGE ANTRIEBSVORRICHTUNG


    Additional title:

    METHOD FOR PROVIDING PREDEFINED DRIVE CHARACTERISTICS IN AN AIRCRAFT, AND ASSOCIATED DRIVE DEVICE
    PROCÉDÉ DE GÉNÉRATION D'UNE CARACTÉRISTIQUE DE PROPLULSION PRÉDÉFINIE DANS UN AVION ET DISPOSITIF DE PROPULSION ASSOCIÉ


    Contributors:

    Publication date :

    2016-08-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

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



    Verfahren und System zum Bereitstellen einer vorbestimmten pyrotechnischen Energieabgabe

    WINTER ANDREAS / LAWRENTZ ULF / BLEY ULRICH | European Patent Office | 2021

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