The Electron Beam (EB) welding process has gained widespread acceptance in the aerospace industry as an efficient, precise, high quality joining process. Because its optimum performance is realized in a vacuum environment, its use has been limited to welding of fairly small components, where Xray quality, high strength welds are required with minimal part distortion. Larger components can be welded; however, the equipment and operating costs increase with the correspondingly larger vaccum chambers used to house the parts to be welded.


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    Titel :

    EB Welding of Launch Vehicles


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Szabo, Attila (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1991



    Erscheinungsdatum :

    1991-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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