A fire seals system positioned in a corner of a region of attachment between a rear engine mount and a pylon and comprising a metal shoe comprising a fitting comprising two first vanes forming an L fixed in the corner and a lower second vane between the lower edges of the two first vanes and an upper second vane between the upper edges of the two first vanes, and a flexible tongue having a fixed upstream end and a free downstream end in which an intermediate part of the tongue is arranged between the lower second vane and the upper second vane, and a longilinear seal attached to a thrust reverser cowl with one end of the longilinear seal bearing against the tongue. Such a fire seals system makes it possible to limit the spread of flames and to absorb movements of the nacelle.


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    Titel :

    SYSTEME DE JOINTS FEU METALLIQUES POUR UNE ATTACHE MOTEUR D'UN AERONEF


    Weitere Titelangaben:

    METAL FIRE JOINT SYSTEM FOR AN AIRCRAFT ENGINE MOUNT
    SYSTEM MIT METALL-BRANDSCHUTZDICHTUNGEN FÜR MOTORBEFESTIGUNG EINES LUFTFAHRZEUGS


    Beteiligte:
    CASSAGNE JÉRÔME (Autor:in) / GELIOT JEAN (Autor:in)

    Erscheinungsdatum :

    26.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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