FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to rotors. Proposed rotor comprises disk with blades. Proposed rotor represents a disk, which can be either bladed in sector sections of the disk or flexible with flexibility increasing from rotational axis to periphery, the disk oscillating and being attached unorthogonally to vertical or horizontal shaft.
EFFECT: simplified design.
5 cl, 3 dwg
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