A system for controlling landing gear subsystems may comprise a controller (122) and a first motor drive unit (130) in operable communication with the controller. A first electric motor (132) and a second electric motor (134) may be in operable communication with the first motor drive unit. A second motor drive unit (150) may be in operable communication with the controller. A third electric motor (136) and a fourth electric motor (142) may be in operable communication with the second motor drive unit. An AC/DC converter (200) may be electrically coupled to the first drive unit and the second motor drive unit.
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
VERTEILTE FAHRWERKSSYSTEMARCHITEKTUR FÜR ELEKTROMECHANISCHE BETÄTIGUNG
ARCHITECTURE DE SYSTÈME D'ATTERRISSAGE DISTRIBUÉE POUR ACTIONNEMENT ÉLECTROMÉCANIQUE
2021-11-17
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
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