A nose landing gear system (206) is disclosed. In various embodiments, the nose landing gear system includes an electro-hydraulic actuator (244) configured to raise and lower a nose shock strut assembly; a first electro-mechanical actuator configured to steer the nose shock strut assembly; and a second electro-mechanical actuator configured to open and close a fairing door.
ELECTRIC NOSE LANDING GEAR ARCHITECTURE
ELEKTRISCHE BUGFAHRWERKSARCHITEKTUR
ARCHITECTURE ÉLECTRIQUE DE TRAIN D'ATTERRISSAGE AVANT
2021-03-24
Patent
Electronic Resource
English
NTIS | 1979
|Emerald Group Publishing | 2000