In a rotor mast for a rotorcraft, the rotor mast can be coupled in a rotationally fixed manner to a drive unit of a helicopter rotor transmission, which allows a particularly smooth running operation. This is achieved in that the rotor mast is configured in two parts, and comprises a bearing mast and an outer mast, with the outer mast, configured as a hollow body, is mounted, concentrically surrounding the bearing mast, such that it can rotate about a central axis relative to the bearing mast. The outer mast can be operatively connected with the helicopter rotor transmission, and the bearing mast can be mounted in the rotorcraft in a locationally and rotationally fixed manner, such that the outer mast can be coupled with a main rotor in a rotationally fixed manner, and can be set in rotation with the helicopter rotor transmission.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor mast


    Beteiligte:
    KÖSTLI ROMAN (Autor:in) / STUCKI MARTIN (Autor:in)

    Erscheinungsdatum :

    2020-08-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



    ROTOR MAST

    KOESTLI ROMAN / MARTIN STUCKI | Europäisches Patentamt | 2018

    Freier Zugriff

    Rotor Mast

    KÖSTLI ROMAN / STUCKI MARTIN | Europäisches Patentamt | 2018

    Freier Zugriff

    Rotor mast assembly

    ELLIOTT DAVID / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2018

    Freier Zugriff

    ROTARY AIRCRAFT HYBRID ROTOR MAST

    MESSINGER STAN / MESSINGER CLAYTON | Europäisches Patentamt | 2022

    Freier Zugriff

    ROTARY AIRCRAFT HYBRID ROTOR MAST

    MESSINGER STAN / MESSINGER CLAYTON | Europäisches Patentamt | 2022

    Freier Zugriff