A fitting for attaching the horizontal tail stabilizer of an aircraft, allowing the formation of a lighter component, without a fatigue failure mode and with a significant reduction in the installation time. The fitting comprises: a core piece having a regular thickness, the core piece having a U configuration, according to a plan view, thereby being composed of two lateral areas and a central area located between the lateral areas, at least one central reinforcement having a regular thickness and joined to one side of the central area and comprising a flange located on an inner edge of the core piece, at least two lateral reinforcements having a regular thickness and each lateral reinforcement being joined to one side of a different lateral area and comprising a flange located on the inner edge of the core piece.


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    Titel :

    FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    06.02.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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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