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.
VORRICHTUNG ZUR REDUZIERUNG VON STRUKTURSCHWINGUNGEN VON TRAGFLÜGELN
DEVICE FOR REDUCING STRUCTURAL VIBRATIONS OF AEROFOILS
DISPOSITIF POUR LA RÉDUCTION DES OSCILLATIONS DE LA STRUCTURE D'AILES PORTANTES
2019-05-22
Patent
Electronic Resource
German
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