A tilt actuation apparatus for tilting a propulsion system of an aircraft, the tilt actuation apparatus comprising: a tilt actuator comprising a rotor; a gear set, wherein the rotor is coupled to the gear set, a worm gear concentrically coupled to an output of the gear set, a worm wheel meshed with the worm gear, a gear shaft concentrically coupled to the worm wheel, a pinion concentrically coupled to the gear shaft, and an output shaft coupled to an output of the pinion, the output shaft configured to be fixed to a frame of the aircraft.
SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
05.06.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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