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


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

    Erscheinungsdatum :

    07.10.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Gust load reduction in an aircraft

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

    Freier Zugriff

    Gust Load Alleviation Control for Very Flexible Aircraft

    Dillsaver, M. / Cesnik, C. / Kolmanovsky, I. | British Library Conference Proceedings | 2011


    "Robust Gust Load Alleviation for a Flexible Aircraft"

    Aouf, N. / Boulet, B. / Botez, R. et al. | British Library Conference Proceedings | 2000


    Gust Load Alleviation Control for Very Flexible Aircraft

    Dillsaver, Matthew / Cesnik, Carlos / Kolmanovsky, Ilya | AIAA | 2011


    Gust Load Alleviation Control for Very Flexible Aircraft

    Dillsaver, M. / Cesnik, C. / Kolmanovsky, I. et al. | British Library Conference Proceedings | 2011