A head for a rotor of a rotorcraft, the head comprising a cap extending radially from an axis of rotation in elevation towards a periphery and extending in azimuth over 360 degrees, the cap extending in thickness between an inside face that is to face a hub of the rotor and an outside face overlying the inside face, the periphery being crenellated to define a succession of crenellations and of notches, each notch allowing a blade of the rotor to perform flapping motion.
COUPOLE DE ROTOR, ROTOR ET GIRAVION
ROTOR HUB CAP, ROTOR AND ROTORCRAFT
ROTORVERKLEIDUNG, ROTOR UND DREHFLÜGELFLUGZEUG
2017-12-13
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
DISPOSITIF DE BUTEE INFERIEUR D'UN ROTOR POUR GIRAVION, ROTOR DE GIRAVION ET GIRAVION
European Patent Office | 2018
|European Patent Office | 2016
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