A propeller blade retention element (6) comprises a body portion (40) formed of a corrosion resistant metal, and at least one bearing race portion (42) attached to the body portion (40), the race portion (42) being formed of an induction hardenable, corrosion resistant metal.


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    Title :

    PROPELLER BLADES


    Additional title:

    PROPELLERSCHAUFELN
    PALES D'HÉLICE


    Contributors:

    Publication date :

    2019-01-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / C21D Veränderung der physikalischen Struktur von Eisenmetallen , MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS



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