The present disclosure relates to a fastening arrangement for plate-shaped facing components. The fastening arrangement includes at least one profiled rail comprising legs in a cross-section, an intermediate space being formed between these legs and configured to hold a peripheral portion of at least one of the facing components. A first one of the legs of the profiled rail includes at least one opening which extends into the first leg in a transverse direction of the profiled rail. The fastening arrangement also includes at least one fixing element which is equipped with at least one extension. The extension is designed such that it can be pressed into the opening in the first leg to fix the facing component so that the extension protrudes into the intermediate space and portions thereof come into frictional contact with the peripheral portion of the facing component held in the intermediate space.


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    Titel :

    Fastening arrangement for plate-shaped facing components, facing arrangement and aircraft or spacecraft


    Beteiligte:
    SPELLER JOHN (Autor:in)

    Erscheinungsdatum :

    22.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64C AEROPLANES , Flugzeuge



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