An electric actuator (1), comprising: an output section (30) receiving a reduced output from a first motor (11) through a rotational member (24B) supported by a bearing and through an internal gear (24A), wherein the output section (30) receives an output from a second motor (21) through a planetary gear mechanism that includes the internal gear (24A), a sun gear (22), and a planetary gear (23). Fig.1


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    Title :

    ELECTRIC ACTUATOR AND GEAR MECHANISM


    Additional title:

    ELEKTRISCHER STELLANTRIEB UND GETRIEBEMECHANISMUS
    ACTIONNEUR ÉLECTRIQUE ET MÉCANISME D'ENGRENAGE


    Contributors:

    Publication date :

    2020-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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