The invention relates to an assembly comprising a structure (2) and a tubular element (6), which is mounted isostatically in the structure (2), said tubular element (6) comprising a first end (7) connected to said structure by at least four connecting rods 10a-10b-10c-10d, thus setting four first degrees of freedom, and a second end (8) connected to said structure (2) by an attachment means (20) that sets two second degrees of freedom, said connecting rods comprising a means for adjusting the length thereof. In particular, it relates to an exhaust suitable for an auxiliary power unit in the compartment thereof and to the mounting method for aligning them.


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    Title :

    SUSPENSION D'UN ÉLÉMENT TUBULAIRE DANS UN COMPARTIMENT D'AÉRONEF


    Additional title:

    SUSPENSION OF A TUBULAR ELEMENT IN AN AIR CRAFT COMPARTMENT
    AUFHÄNGUNG EINES ROHRFÖRMIGEN TEILS IN EINEM LUFTFAHRZEUGBEREICH


    Contributors:

    Publication date :

    2019-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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