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.


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    Title :

    SELF-LUBRICATED ACTUATOR FOR ON-BLADE ROTOR CONTROL


    Additional title:

    SELBSTSCHMIERENDER AKTUATOR FÜR ROTORSTEUERUNG AUF DER LAUFSCHAUFEL
    ACTIONNEUR AUTOLUBRIFIÉ POUR UNE COMMANDE DE ROTOR SUR PALE


    Contributors:

    Publication date :

    2019-01-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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