An automated method for influencing a gust load of an aircraft is provided. A torque at least of an electromotive thrust generating unit arranged on a wing of the aircraft is modified such that a root bending torque of the wing generated by the gust load is reduced. An associated apparatus, an aircraft, a computer program product, and a computer-readable medium for carrying out the method are also provided.


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    Titel :

    Gust load reduction in an aircraft


    Beteiligte:
    SCHILDT PHILIPP (Autor:in) / DILCHER ANTON (Autor:in) / KOLEM PASCAL (Autor:in) / OTTO OLAF (Autor:in) / PFLAUM FREDERIC (Autor:in)

    Erscheinungsdatum :

    2024-02-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    GUST LOAD REDUCTION IN AN AIRCRAFT

    SCHILDT PHILIPP / DILCHER ANTON / KOLEM PASCAL et al. | Europäisches Patentamt | 2021

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