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
27.11.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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