Hydraulic system for an aircraft landing gear

摘要

A hydraulic system for retracting into and extending out of the body of an aircraft a landing gear for use in taking off and landing, comprises a housing unit (11) which has a hydraulic pump (20), a hydraulic actuator (35), a shuttle valve (42), an emergency valve (36), an actuator pressure releasing mechanism (60) and a mechanically locking mechanism (65) accommodated therein. The hydraulic actuator (35) has a piston rod assembly (36) received therein to be reciprocably moved by the hydraulic pump (20) to assume a retraction position (Pr) and an extended position (Pe). The shuttle valve (42) is movable with respect to the housing unit (11) for selectively changing the flow of the hydraulic fluid between the hydraulic pump (20) and the hydraulic actuator (35). The emergency valve (46) is movable with respect to the housing unit (11) to assume two different positions for selectively changing the flow of the hydraulic fluid between the hydraulic pump (20) and the hydraulic actuator (35) and the flow of the hydraulic pump (20) and the fluid pressure reservoir (71). The actuator pressure releasing mechanism (60) serves to release the hydraulic pressure in the hydraulic actuator (35) to allow the piston rod assembly (36) to be freely moved with respect to the housing unit (11) toward the extended position of the piston rod assembly (36). The mechanically locking mechanism (65) is provided selectively to lock the piston rod assembly (36) with the housing unit (11) and to unlock the piston rod assembly (36) from the housing unit (11) to be freely moved. <IMAGE>