LOCKING MECHANISM, SPECIFICALLY FOR AN AIRCRAFT LANDING GEAR OR AN AIRCRAFT LANDING GEAR DOOR

摘要

the invention relates to a coupling device.in particular for the attachment of a landing gearfor a discussion of aircraft and landing gearan aircraft, comprising a housing in which is arranged aset of elements including at least one articulated.the locking hook and a hook lever connected to thatby the spring, which may be associated with hookby acting on the lever to unlock the lockingin a first mode of actuation in anormal operation, with a relief in advance of the.the mechanism is in a second modein one mode of operation of the brake system.according to the invention, the secondwith the operation mode of the actuator systemelectro mechanical actuator is an electrically operatedthe actuator has two motors independently.with a power of irreversible processa differential output shaft, controla release lever pivot emergency cooperationthe locking lever is used in operationnormal.