A nose landing gear system is disclosed. In various embodiments, the nose landing gear system includes an electro-hydraulic actuator 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
2021-03-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
NTIS | 1979
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