A rotor (8a) comprises at least two rotor blades (10), and each rotor blade (10) of the at least two rotor blades (10) rotates around a rotor axis (Y) and performs pitching around a pitch axis (X). The rotor axis (Y) and the pitch axis (X) intersect in a rotor center (P0). The rotor (8a) is characterized in that each rotor blade (10) comprises at least one permanent magnet (25) having a first spherical magnet surface (19). Each rotor blade (10) further comprises a pitch control apparatus (20) for controlling the pitching of the at least two rotor blades (10). The pitch control apparatus (20) comprises electrically controlled magnets (24) having a second spherical magnet surface (15).
A ROTOR WITH PITCH CONTROL APPARATUS
ROTOR MIT BLATTVERSTELLUNGSVORRICHTUNG
ROTOR À APPAREIL DE COMMANDE DE PAS
2022-12-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |