In order to reduce the mass of a primary structure of a mounting pylon for an engine of an aircraft, the mounting pylon includes a box and a rear sub-structure fastened to the box which includes two lateral panels, each equipped at its rear end with a first linking portion through which passes a first connection orifice that is designed to receive a connection pin of a lateral front wing attachment. The rear sub-structure is made in one piece and includes two opposite lateral flanks that are respectively fastened to the two lateral panels of the box by fastening elements. Each lateral flank has a second linking portion through which passes a second connection orifice that is aligned with the first connection orifice, and is also designed to receive the connection pin of the lateral front wing attachment.


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    Titel :

    STRUCTURE PRIMAIRE ALLEGEE POUR MAT D'ACCROCHAGE DE MOTEUR D'AERONEF


    Weitere Titelangaben:

    LIGHT PRIMARY STRUCTURE FOR AIRCRAFT ENGINE MOUNTING STRUT
    LEICHTE PRIMÄRSTRUKTUR FÜR AUFHÄNGEMAST EINES TRIEBWERKS EINES LUFTFAHRZEUGS


    Beteiligte:
    JULE PASCAL (Autor:in)

    Erscheinungsdatum :

    2019-10-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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