An integrated three function valve (ITFV) for an actuator of a flight control surface. The ITFV includes: an inner spool configured to be actuated in a first direction and a second direction responsive to a pressure differential acting across the inner spool; and an intermediate spool configured to be actuated in the first direction and second direction between an active position and a bypass position. The inner spool is located within the intermediate spool.
HYDRAULIC VALVE
03.07.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |