A locking device locks a landing gear mounted in rotation on an aircraft and includes a deployment hydraulic jack including a first chamber connected to a first hydraulic supply and a second chamber connected to a second hydraulic supply. The locking device includes a hydraulic actuator connected to a rotary distributor. The rotary distributor includes a coupling operationally connecting the rotary distributor to a strut of the landing gear, a first supply port fluidly connected to the first hydraulic supply, and a first outlet port fluidly connected to the hydraulic actuator.
DISPOSITIF DE VERROUILLAGE D'ATTERRISSEUR
LANDING GEAR LOCKING DEVICE
VERRIEGELUNGSVORRICHTUNG FÜR EIN FAHRWERK
2023-04-26
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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