To provide systems and methods for fastening floor panels to an aircraft floor support structure.SOLUTION: A floor panel connection system for attaching a floor panel to an aircraft airframe is disclosed. The connection system includes a vertical load resisting coupling device and a shear load resisting coupling device to connect the floor panel to the airframe and resist forces applied to the panel. The vertical load resisting coupling device is configured to resist forces perpendicular to a top facial plane of the floor panel, without significantly resisting lateral forces. The shear load resisting coupling device is configured to resist forces parallel to the top facial plane of the floor panel, without significantly resisting vertical forces.SELECTED DRAWING: None

    【課題】フロアパネルを航空機フロア支持構造体に締結するためのシステム及び方法を提供する。【解決手段】フロアパネルを航空機の機体に装着するためのフロアパネル接続システムが開示される。接続システムは、フロアパネルを機体に接続し、パネルに印加される力に耐える、垂直荷重抵抗連結装置及びせん断荷重抵抗連結装置を含む。垂直荷重抵抗連結装置は、横方向の力に大きく抵抗することなく、フロアパネルの上部表面に垂直な力に耐えるように構成されている。せん断荷重抵抗連結装置は、垂直な力に大きく抵抗することなく、フロアパネルの上部表面に平行な力に耐えるように構成されている。【選択図】なし


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    Title :

    AIRCRAFT FLOOR PANEL FLOATING CONNECTION SYSTEM


    Additional title:

    航空機フロアパネルフローティング接続システム


    Contributors:

    Publication date :

    2019-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



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