A helicopter rotor transmission in which the average lubricant monitoring and replenishment intervals are to be significantly increased. The helicopter rotor transmission has a central cavity, in which runs a bearing mast that is fixed in a locationally and rotationally manner, which is held passing through the gear housing at least partially in the direction of the central axis. An internally toothed gear ring of a rotatable rotor mast can be rotated about the central axis, with fixed rotation of the planetary gears about their planetary gear axes, such that the rotor mast can be set in rotation by means of a gear ring driver attached to the gear ring.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Редуктор несущего винта вертолета


    Erscheinungsdatum :

    2019-05-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




    КОМПЛЕКТ ДЛЯ ВЕРТОЛЕТА

    Europäisches Patentamt | 2021

    Freier Zugriff

    РУЛЕВОЙ ВИНТ ВЕРТОЛЕТА

    Europäisches Patentamt | 2018

    Freier Zugriff

    ВАЛ НЕСУЩЕГО ВИНТА

    Europäisches Patentamt | 2019

    Freier Zugriff

    СИСТЕМА ЛОПАСТЕЙ НЕСУЩЕГО ВИНТА

    Europäisches Patentamt | 2018

    Freier Zugriff