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.
Device for reducing structural vibrations of airfoils
03.05.2016
Patent
Elektronische Ressource
Englisch
DEVICE FOR REDUCING VIBRATIONS IN CONDUCTIVE AIRFOILS
Europäisches Patentamt | 2019
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