A blade shank assembly (100) for an aircraft propeller blade includes a blade shank (101); a split blade retention race (103) encircling the blade shank, the split blade retention race including two splits (104), wherein the split blade retention race comprises: inner chamfers (201) located between the blade shank and the split blade retention race at each of the two splits; and outer chamfers (202) located adjacent to a race surface of the split blade retention race at each of the two splits; and a plurality of ball bearings (102) located on the race surface of the split blade retention race.


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    Titel :

    Split blade retention race with inner and outer chamfers


    Weitere Titelangaben:

    Geteilter Blatthalterlaufring mit inneren und äußeren Fasen
    Bague de rétention de pale divisée avec des chanfreins internes et externes


    Beteiligte:
    VENTURA PETER (Autor:in) / SOULE MATTHEW (Autor:in)

    Erscheinungsdatum :

    22.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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