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.
FLUID TUBE ASSEMBLY FOR GAS TURBINE ENGINE
FLÜSSIGKEITSROHRANORDNUNG FÜR GASTURBINENMOTOR
ENSEMBLE DE TUBE DE FLUIDE POUR MOTEUR À TURBINE À GAZ
2020-04-08
Patent
Elektronische Ressource
Englisch
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 |