A fluid tube assembly includes a first fluid tube (102) extending through a duct liner (104), a portion of the first fluid tube disposed radially outward of the duct liner and a portion of the first fluid tube disposed radially inward of the duct liner. Also included is a second fluid tube (112) located radially inward of the duct liner. Further included is a clamp (120) located radially inward of the duct liner and having an inner wall defining an interior space. Yet further included is a nut (116) at least partially disposed within the interior space, the nut having an outer geometry corresponding to a geometry of a portion of the inner wall of the clamp, the first fluid tube and the second fluid tube each having a portion disposed within the nut, the clamp and the nut providing anti-rotation during assembly of the fluid tube assembly.


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    Titel :

    FLUID TUBE ASSEMBLY FOR GAS TURBINE ENGINE


    Weitere Titelangaben:

    FLÜSSIGKEITSROHRANORDNUNG FÜR GASTURBINENMOTOR
    ENSEMBLE DE TUBE DE FLUIDE POUR MOTEUR À TURBINE À GAZ


    Beteiligte:

    Erscheinungsdatum :

    2020-04-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F16L PIPES , Rohre



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