Abstract The computer-aided design (CAD) system is specified for the preproduction engineering of the aircraft engine compressor blades. This system is characterized by a high quality of designing the finishing cutoff and reducing dies. It is shown that a high level of unification and integration in CAD permits the time of designing the punch tool sets to be significantly reduced.


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    Titel :

    Computer-aided design of blank forging production facilities for aircraft engine compressor blades


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2014-04-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch







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