Fitting for attaching the horizontal tail stabilizer of an aircraft, allowing to obtain a lighter component, without fatigue failure mode and with a significant reduction in the installation time, wherein the fitting comprises:- a core piece (1) having a regular thickness, the core piece (1) having U configuration, according to a plan view, thereby being composed by two lateral areas (1') and a central area (1") located between the arm areas (1'),- at least one central reinforcement (2) having a regular thickness and joined to one side of the central area (1") and comprising a flange (2') located in an inner edge (1"') of the core piece (1),- at least two lateral reinforcements (3) having a regular thickness and each lateral reinforcement (3) being joined to one side of a different lateral area (1') and comprising a flange (3') located in the inner edge (1"') of the core piece (1).


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    Titel :

    FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT


    Weitere Titelangaben:

    BESCHLAG ZUR BEFESTIGUNG DES HORIZONTALEN HÖHENLEITWERKSTABILISATORS EINES FLUGZEUGS
    FERRURE POUR FIXER LE STABILISATEUR D'EMPENNAGE HORIZONTAL D'UN AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    26.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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