Aircraft landing gear unlock actuator
Aircraft landing gear unlock actuator
- Neue Suche nach: COLLINS ANDREW JOHN
- Neue Suche nach: COLLINS ANDREW JOHN
This disclosure relates to a landing gear system that includes a landing gear strut rotatable between stowed and deployed positions. A lock-stay is connected to the landing gear strut and is movable between locked and unlocked conditions. An unlock actuator (24) is connected to the lock-stay and includes first (44) and second (48) members movable relative to one another. The first member is movable between first and second positions that correspond to the locked and unlocked conditions. A controller is in communication with the unlock actuator and is configured to command the unlock actuator between the first and second positions in response to an input. The second member is permitted to free-drive relative to the first member between the stowed and deployed positions with the lock-stay in the unlocked condition.
Dokumentinformationen
Aircraft landing gear unlock actuator
Entriegelungsstellglied für ein Flugzeugfahrwerk
Actionneur de déverrouillage de train d'atterrissage d'avion
2018-05-30
Patent
Elektronische Ressource
Englisch
| IPC: | B64C AEROPLANES , Flugzeuge |