A primary structure of an aircraft pylon, which comprises upper and lower spars, right-hand and left-hand lateral panels, transverse reinforcers that are disposed in transverse planes and, each have a square or rectangular contour and at least one sole to which the upper and lower spars and the right-hand and left-hand lateral panels are fastened. At least one of the transverse reinforcers of the primary structure has first and second link rods that are oriented along diagonals of the transverse reinforcer, and connecting systems that each connect first and second ends of the first and second link rods to the sole or to one of the soles.


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    Title :

    STRUCTURE PRIMAIRE D'UN MÂT D'AÉRONEF COMPORTANT AU MOINS UN RENFORT TRANSVERSAL ÉQUIPÉ DE DEUX BIELLES DISPOSÉES EN DIAGONALE ET AÉRONEF COMPRENANT UNE TELLE STRUCTURE PRIMAIRE


    Additional title:

    PRIMARY STRUCTURE OF AN AIRCRAFT MOUNT COMPRISING AT LEAST ONE TRANSVERSE REINFORCEMENT PROVIDED WITH TWO RODS ARRANGED DIAGONALLY AND AIRCRAFT COMPRISING SUCH A PRIMARY STRUCTURE
    PRIMÄRSTRUKTUR EINES FLUGZEUGTRIEBWERKTRÄGERS, DIE MINDESTENS EINE QUERVERSTEIFUNG MIT ZWEI DIAGONAL ANGEORDNETEN STREBEN UMFASST, UND LUFTFAHRZEUG MIT EINER SOLCHEN PRIMÄRSTRUKTUR


    Contributors:

    Publication date :

    2021-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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