The invention provides a landing gear strut for an aircraft which has the cross-section of an airfoil. The strut is mounted to the fuselage of the aircraft, preferably at a shallow downward angle from the horizontal, and preferably presents a positive angle of attack to the oncoming airflow. Due to the combination of an airfoil profile and a positive angle of attack, the strut is enabled to provide lift to the aircraft.


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    Titel :

    Lifting strut in the shape of a lifting airfoil for aircraft landing gear


    Beteiligte:
    MACBEAN ALASDAIR (Autor:in) / WOOD WILLIAM (Autor:in) / GAMBILL DAVID (Autor:in) / MERDINGER DORON (Autor:in)

    Erscheinungsdatum :

    05.08.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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