A self-lubricated actuator for a rotor blade flap of a helicopter having a housing; a motor having a shaft disposed in a bearing is provided. The actuator further has an output rod and a mechanism operatively associated with the motor and the output rod to transmit movement from the motor to the output rod. The housing includes a lubrication medium capable of substantially immersing the bearing, the motor shaft and the mechanism during operation.
SELF-LUBRICATED ACTUATOR FOR ON-BLADE ROTOR CONTROL
SELBSTSCHMIERENDER AKTUATOR FÜR ROTORSTEUERUNG AUF DER LAUFSCHAUFEL
ACTIONNEUR AUTOLUBRIFIÉ POUR UNE COMMANDE DE ROTOR SUR PALE
2019-01-23
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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