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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    Title :

    LIFTING STRUT FOR AIRCRAFT LANDING GEAR


    Contributors:

    Publication date :

    2025-07-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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