The invention discloses a sealing method for an integral tank of an airplane. The sealing method for the integral tank of the airplane is characterized in that during assembly of the wall-plate integral tank, faying surfaces and fillets are sealed through two-component modified polysulfide sealant so as to achieve sealing of assembled gaps, and a detachable covering cap of the oil tank is sealed through low-adhesion modified polysulfide sealant. The sealing method for the integral tank of the airplane has the beneficial effects that the quantity of the needed sealant components is small in the assembling process of the integral tank; the manufacturability is good; the operation is simple, the detachable position of the tank is sealed through the low-adhesion sealant, and the advantage of convenient disassembly and maintenance is achieved. Besides, the tank sealing has the advantages of corrosion prevention, good economical property and high sealing reliability.


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    Titel :

    Sealing method for integral tank of airplane


    Beteiligte:
    XING YILIN (Autor:in) / SUN KANG (Autor:in) / LIU GANG (Autor:in) / LI XIMIN (Autor:in)

    Erscheinungsdatum :

    06.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / C09K Materialien für Anwendungen, soweit nicht anderweitig vorgesehen , MATERIALS FOR APPLICATIONS NOT OTHERWISE PROVIDED FOR



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