The present embodiments relate to a cyclic pitch angle adjustment apparatus 200 for a rotor 110 or propeller, to a rotor 110 with such a cyclic pitch angle adjustment apparatus 200, and to a rotorcraft with such a rotor 110. The cyclic pitch angle adjustment apparatus 200 may include levers that rotate rotor blades around associated pitch axes, rods 240 that mechanically link the levers with a bearing 220 such that the rods 240 are movable relative to a central point 223, the bearing 220 being attached to a central rod 250 that is movable by means of a motor 510 and adapted for adjusting the cyclic pitch angle of the rotor blades from one pitch angle in one position to another pitch angle in another position.
A CYCLIC PITCH ANGLE ADJUSTMENT APPARATUS
VORRICHTUNG ZUR ZYKLISCHEN NEIGUNGSWINKELEINSTELLUNG
APPAREIL DE RÉGLAGE D'ANGLE DE PAS CYCLIQUE
2022-11-16
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |