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:
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