A device for reducing structural vibrations of airfoils in an aircraft comprises, in the region of the airfoil tips, at least one force generator acting substantially in the direction of movement of the vibrations. This arrangement has the advantage that such a force generator is considerably less susceptible to wear than conventional aerodynamic flaps and therefore effective vibration damping is possible with a reduced outlay on maintenance and greater efficiency.


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    Title :

    VORRICHTUNG ZUR REDUZIERUNG VON STRUKTURSCHWINGUNGEN VON TRAGFLÜGELN


    Additional title:

    DEVICE FOR REDUCING STRUCTURAL VIBRATIONS OF AEROFOILS
    DISPOSITIF POUR LA RÉDUCTION DES OSCILLATIONS DE LA STRUCTURE D'AILES PORTANTES


    Contributors:

    Publication date :

    2019-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





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