A propeller shaft assembly for an aircraft engine includes a shaft having: an annular wall extending circumferentially about a shaft axis and circumscribing a hollowed interior defining a cavity in a front end portion of the shaft, the annular wall having an outer surface and an inner surface facing radially inwardly to the cavity; and a front flange projecting radially outwardly from the annular wall. The front flange includes a hub side surface defining an interface plane and adapted to abut with a propeller hub. The shaft also includes a reinforcement web defining an end wall of the cavity, the reinforcement web extending radially inwardly from the inner surface of the annular wall. At least part of the reinforcement web is radially aligned with the front flange. At least one perforation extends axially through the reinforcement web.


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    Titel :

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE


    Beteiligte:

    Erscheinungsdatum :

    21.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTYNSKI TOMASZ | Europäisches Patentamt | 2024

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    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

    PROPELLER SHAFT WITH REINFORCED FRONT FLANGE

    KESEK MATEUSZ / ROZPUTNSKI TOMASZ | Europäisches Patentamt | 2024

    Freier Zugriff