The invention is related to a rotor assembly 1 for a rotorcraft, comprising a rotor shaft 8, a torque transmission unit 4 that is non-rotatably mounted to the rotor shaft, a rotor hub 7 that is rotatably mounted to the rotor shaft 8 via an associated angular displacement enabling component 9, and at least two rotor blades 2b, 2d that are connected to the rotor hub 7, wherein the torque transmission unit 4 is coupled to the at least two rotor blades on a rotor assembly outflow side via a pitch control unit 10, wherein the pitch control unit transmits to the at least two rotor blades 2b, 2d torque that is applied from the rotor shaft 8 to the torque transmission unit 4, and wherein the pitch control unit 10 increases a respective pitch angle of the at least two rotor blades 2b, 2d if the torque is increased.
A ROTOR ASSEMBLY FOR A ROTORCRAFT WITH TORQUE CONTROLLED COLLECTIVE PITCH
ROTORANORDNUNG FÜR EIN ROTORFLUGZEUG MIT DREHMOMENTGESTEUERTER KOLLEKTIVER STEIGUNG
ENSEMBLE ROTOR POUR UN GIRAVION COMPORTANT UN PAS COLLECTIF CONTRÔLÉ PAR UN COUPLE
2019-11-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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