A propeller blade mounting system includes a mounting system (4) on rolling bearings between a propeller hub (3) and a propeller blade (2), wherein: at least one bearing outer ring (9) is connected in rotationally fixed manner to the propeller blade (2); at least one bearing inner ring (15, 16, 17) is mounted on the propeller hub (3); a sleeve-shaped central section (13) connected to the propeller blade (2) is disposed radially inside the bearing inner ring (15, 16, 17); and a lubricant chamber (18) is formed between the bearing outer ring (9) and the central section (13) in the radial direction, relative to the rotational axis (R) of the propeller hub (3), and is closed towards the exterior.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Propeller blade mounting system


    Beteiligte:
    SEBALD WILHELM (Autor:in)

    Erscheinungsdatum :

    2019-06-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16C SHAFTS , Wellen



    PROPELLER BLADE MOUNTING SYSTEM

    SEBALD WILHELM | Europäisches Patentamt | 2020

    Freier Zugriff

    PROPELLER BLADE MOUNTING SYSTEM

    ZEBALD VILGELM | Europäisches Patentamt | 2018

    Freier Zugriff

    PROPELLER BLADE MOUNTING SYSTEM

    SEBALD WILHELM | Europäisches Patentamt | 2016

    Freier Zugriff

    Straight-blade propeller mounting method and mounting base

    DENG ZHIBO | Europäisches Patentamt | 2020

    Freier Zugriff

    Propeller blade mounting and measuring tool

    YANG ZIMENG / YU JINGBO / LIU BINGBING et al. | Europäisches Patentamt | 2021

    Freier Zugriff