GAS TURBINE ENGINE ASSEMBLY COMPRISING DAMPED FLUID TRANSFER TUBE

GAS TURBINE ENGINE ASSEMBLY COMPRISING DAMPED FLUID TRANSFER TUBE

An assembly (20) is provided for a gas turbine engine. This assembly (20) includes a stationary structure (40) configured with a first side (44), a second side (46) and a bore (54) that extends through the stationary structure (40) between the first side (44) and the second side (46). The assembly (...

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Bibliographische Detailangaben
1. Verfasser: ANGLIN, Christopher T
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Beschreibung
Zusammenfassung:An assembly (20) is provided for a gas turbine engine. This assembly (20) includes a stationary structure (40) configured with a first side (44), a second side (46) and a bore (54) that extends through the stationary structure (40) between the first side (44) and the second side (46). The assembly (20) also includes a fluid transfer tube (38) extending within the bore (54) and forming a plenum (108) between a sidewall (72) of the fluid transfer tube (38) and the stationary structure (40). The fluid transfer tube (38) is configured with a first end (68) at the first side (44), a second end (70) at the second side (46), a flowpath (74) and an aperture (94). The flowpath (74) is at least partially formed by the sidewall (72) and extends through the fluid transfer tube (38) between the first end (68) and the second end (70). The aperture (94) fluidly couples the flowpath (74) with the plenum (102).