Electromechanical drive system (1) to control a transmission shaft (2) connected to the mechanical operating systems of an aircraft, comprising an electric machine (3), a two-way transmission rotation (8) and a clutch assembly (9) wherein the two-way transmission rotation (8) is configured, in any direction of rotation of the transmission shaft (2), to selectively allow the passage of torque either only between the electric machine (3) and the transmission shaft (2) when the torque is supplied by the electric machine (3) to the transmission shaft (2) or between the transmission shaft (2), the clutch assembly (9) and the electric machine ( 3 ) when the torque is supplied by the transmission shaft (2) to the electric machine (3).
ELECTROMECHANICAL DRIVE SYSTEM FOR AN AIRCRAFT
ELEKTROMECHANISCHES ANTRIEBSSYSTEM FÜR EIN FLUGZEUG
SYSTÈME D'ENTRAÎNEMENT ÉLECTROMÉCANIQUE POUR AÉRONEF
2024-09-04
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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