A system architecture for operation of aircraft flaps is provided. The system architecture includes a first pair of motor drive units, the first pair comprising a first motor drive unit (MD1) and a second motor drive unit (MD3), and a second pair of motor drive units, the second pair comprising a third motor drive unit (MD2) and a fourth motor drive unit (MD4). The system further includes a first plurality of switches connected between the first motor drive unit (MD1) and the second motor drive unit (MD3), said first plurality of switches configured to operate a first electric motor (201) and a second electric motor (202), and a second plurality of switches connected between the third motor drive unit (MD2) and the fourth motor drive unit (MD4), said second plurality of switches configured to operate a third electric motor (203) and a fourth electric motor (204).
SYSTEM ARCHITECTURE FOR OPERATION OF AIRCRAFT FLAPS
ARCHITECTURE DE SYSTEME POUR L'OPERATION DE VOLETS D'AERONEF
2023-05-03
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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