The invention relates to an automated method for influencing a gust load of an aircraft (6), wherein the torque (MI) at least of an electromotive thrust generating unit (1) arranged on a wing (4) of the aircraft (6) is modified such that the root bending torque (M2) of the wing (4) generated by the gust load is reduced. The invention also relates to an associated apparatus and an aircraft and a computer program product and a computer-readable medium for carrying out the method.


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    Titel :

    GUST LOAD REDUCTION IN AN AIRCRAFT



    Medientyp :

    Patent


    Format :

    Elektronische Ressource



    Gust load reduction in an aircraft

    SCHILDT PHILIPP / DILCHER ANTON / KOLEM PASCAL et al. | Europäisches Patentamt | 2024

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