A rotor blade (200) for a rotary wing aircraft includes a leading edge (204) and a trailing edge (206) defining a chordwise direction. The leading edge defines a forward end of the rotor blade and the trailing edge defines an aft end of the rotor blade. The rotor blade has a center of gravity (224) and an aerodynamic center (226) along the chordwise direction. The center of gravity is aft of the aerodynamic center.


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    Title :

    METHOD OF STABILIZING ARTICULATED ROTOR BLADE


    Additional title:

    VERFAHREN ZUR STABILISIERUNG EINES GELENKIGEN ROTORBLATTS
    PROCÉDÉ DE STABILISATION D'UNE PALE DE ROTOR ARTICULÉE



    Publication date :

    2024-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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