An aircraft propeller taper bore insert apparatus is provided. The apparatus includes a tapered outer surface and an inner surface. The outer surface is dimensioned and configured to fit within and be of substantially a same size and shape as an aircraft propeller taper bore or an aircraft propeller balancing tube. The inner surface defines an inner cavity configured to receive a balancing medium and includes a plurality of retention formations arranged thereon and configured to support the balancing medium.


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    Titel :

    AIRCRAFT PROPELLERS


    Beteiligte:
    SMITH BLAIR A (Autor:in) / GRULKE DAVID J (Autor:in)

    Erscheinungsdatum :

    2015-09-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft Propellers

    HAVILL, CLINTON H. | SAE Technical Papers | 1929


    Aircraft propellers

    Havill, C.H. | Engineering Index Backfile | 1929


    Aircraft propellers

    Havill, C.H. | Engineering Index Backfile | 1929



    PROPELLERS FOR AIRCRAFT

    TOWKAN MICHAEL FEDOR | Europäisches Patentamt | 2018

    Freier Zugriff