DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION

DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION

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...

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Bibliographische Detailangaben
Hauptverfasser: JOSYULA, Anil Prasad, VENKATESHA, Harish Gondihalli, CEPIC, Adnan, VIJAY, Ashish
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Zusammenfassung: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.