A propeller shaft assembly for an aircraft engine includes a shaft having a bore extending through the shaft at a front end thereof, the front end of the shaft having an outer surface facing radially outwardly from the shaft and an inner surface spaced apart from the outer surface and facing radially inwardly to the bore. A front flange extends radially outwardly on the outer surface, the front flange defining a hub side surface adapted to abut with a propeller hub. A reinforcement rib extends radially inwardly towards a central axis of the shaft. At least part of the reinforcement rib is radially aligned with the front flange.


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    Titel :

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE


    Weitere Titelangaben:

    ARBRE PORTE-HELICE COMPRENANT UNE BRIDE AVANT RENFORCEE


    Beteiligte:

    Erscheinungsdatum :

    2024-03-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTYNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTYNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTYNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTYNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff