FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Device for damping oscillation movements of aircraft wing incorporates gyromotor, rotor of which is made as a disk and outer frame of which is made as a ring, both are installed at the bearing frame of outer wing; and dampers. Rotor rotation axis is parallel to aircraft longitudinal axis. Dampers are made as a pair of fork outer wings, fixed on the bearing frame. Gyromotor is installed between pairs of fork outer wings.
EFFECT: damping efficiency improvement.
2 dwg
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