The disclosure relates to a machining system for aircraft structural components, comprising a first frame for mounting a workpiece, and a second frame for mounting a tool pair including an upper tool and a lower tool cooperating therewith. The workpiece is positioned between the upper tool and the lower tool. The second frame is formed to be displaceable at least in a longitudinal direction with respect to a base. The tool pair is held in the second frame such that it is displaceable in a transverse direction which is at an angle to the longitudinal direction. The second frame is held on at least one swivel bearing so that the second frame can be adjustably swiveled together with the tool pair about a swivel axis.


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    Titel :

    MACHINING SYSTEM FOR AIRCRAFT STRUCTURAL COMPONENTS


    Beteiligte:

    Erscheinungsdatum :

    18.10.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B21J FORGING , Schmieden / B23B Drehen , TURNING / B23Q DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING , Einzelheiten, Bestandteile oder Zubehör für Werkzeugmaschinen, z.B. Anordnungen zum Kopieren oder Steuern / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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