A system for controlling landing gear subsystems may comprise a controller and a first motor drive unit in operable communication with the controller. A first electric motor and a second electric motor may be in operable communication with the first motor drive unit. A second motor drive unit may be in operable communication with the controller. A third electric motor and a fourth electric motor may be in operable communication with the second motor drive unit. An AC/DC converter may be electrically coupled to the first drive unit and the second motor drive unit.
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
ARCHITECTURE DE SYSTEME DE TRAIN D'ATTERRISSAGE REPARTIE POUR UN ACTIONNEMENT ELECTROMECANIQUE
2021-09-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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