CENTRIFUGAL COMPRESSOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY

A fluid transfer assembly (16) for use in a gas turbine engine includes a rotor shaft, a stationary assembly (102) circumscribing the rotor shaft, and a rotating component (100) coupled to the rotor shaft and positioned radially inward of the stationary assembly. The rotating assembly includes a hub...

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Bibliographische Detailangaben
Hauptverfasser:	ROSE, Joseph George, MONIZ, Thomas Ory
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PISTONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	A fluid transfer assembly (16) for use in a gas turbine engine includes a rotor shaft, a stationary assembly (102) circumscribing the rotor shaft, and a rotating component (100) coupled to the rotor shaft and positioned radially inward of the stationary assembly. The rotating assembly includes a hub (104) coupled to the rotor shaft, a plurality of rotor blades (106) coupled to the hub, and a shroud (108) coupled to the plurality of rotor blades.