A landing gear system, comprising: a nose gear door motor (132); a nose gear motor drive unit (130) in operable communication with the nose gear door motor; a nose gear retraction-extension motor (134) in operable communication with the nose gear motor drive unit; an alternating current direct current converter (200) electrically coupled to the nose gear motor drive unit; a controller (122) in operable communication with the nose gear motor drive unit; and a tangible, non-transitory memory configured to communicate with the controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a pilot command; determining, by the controller, a nose landing gear power sequence for providing power to the nose gear door motor and the nose gear retraction-extension motor in response to receiving the pilot command; and outputting, by the controller, a first command to the nose gear motor drive unit, wherein the nose gear motor drive unit is configured to power either the nose gear door motor or the nose gear retraction-extension motor based on the first command from the controller.
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
VERTEILTE FAHRWERKSSYSTEMARCHITEKTUR FÜR ELEKTROMECHANISCHE BETÄTIGUNG
ARCHITECTURE DE SYSTÈME DE TRAIN D'ATTERRISSAGE DISTRIBUÉ POUR ACTIONNEMENT ÉLECTROMÉCANIQUE
2025-01-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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