A stability control augmentation system and method for a flight control surface of an aircraft. The system comprises an actuator 200 operable for actuating the flight control surface, and a control valve 100 comprising a spool 140 and an integrated augmentation mechanism 130, 150. The spool 140 and the actuation mechanism 130, 150 are both moveable to open and close a fluid flow path through the control valve 100 to control the actuator 200.
STABILITY CONTROL AUGMENTATION SYSTEM AND METHOD
SYSTEM UND VERFAHREN ZUR ERHÖHUNG DER STABILITÄTSKONTROLLE
SYSTÈME ET PROCÉDÉ D'AUGMENTATION DE CONTRÔLE DE STABILITÉ
2024-07-31
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |