The present technology is related to a structurally bonded arrangement (160) for structurally bonding a first component (210) to a second component (220). The structurally bonded arrangement includes a first connecting area (215) of the first component (210), a second connecting area (225) of the second component (220) that is spaced apart from the first connecting area (215) to form an interspace (230), and multiple interconnecting components (270) arranged across the interspace (230). First and second interconnecting components (270a, 270b) of the multiple interconnecting components (270) are structurally bonded separate from each other to the first connecting area (215) at separate first bonding areas (280a, 280b) and to the second connecting area (225) at separate second bonding areas (290a, 290b) thereby structurally bonding the first component (210) to the second component (220). The present technology is also related to a rotorcraft (100) with such a structurally bonded arrangement (160).


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    Titel :

    A STRUCTURALLY BONDED ARRANGEMENT


    Weitere Titelangaben:

    STRUKTURVERBUNDENE ANORDNUNG
    AGENCEMENT LIÉ STRUCTURELLEMENT


    Beteiligte:
    BLACHA MARTIN (Autor:in) / BUESING SEBASTIAN (Autor:in) / PABST KEVIN (Autor:in)

    Erscheinungsdatum :

    13.08.2025


    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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