The invention discloses a balance block for an aircraft. A clamping hook is manufactured by an aluminum alloy material, and is better in elasticity to bring convenience for operators to fixedly mount the balance block; a zinc coating layer coats the outer surfaces of the balance block and the clamping hook, and an epoxy resin layer coats the zinc coating layer, so that the balance block resists the corrosion, is long in service life, and protects the environment; a base of the balance block has the same radian with the edge of an aircraft wheel, so that the balance block is conveniently clamped at the edge of the aircraft wheel to prevent the friction between the base of the balance block and other structures on a tire; the inner layer of the clamping hook is coated with an adhesive layer, so that the clamping hook is tightly combined with the edge of the aircraft wheel, and is not easy to fall; and the balance block for the aircraft has the advantages of good safety, environmental protection, long service life and broad market prospect.


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    Titel :

    Balance block for aircraft


    Beteiligte:
    LIANG YUNTIAN (Autor:in)

    Erscheinungsdatum :

    06.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60B VEHICLE WHEELS , Räder für Fahrzeuge / B64C AEROPLANES , Flugzeuge



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