Centrifugal compressor assembly for use in a turbine engine and method of assembly

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United States of America Patent

PATENT NO 10227879
APP PUB NO 20170234147A1
SERIAL NO

15041467

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Abstract

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A fluid transfer assembly for use in a gas turbine engine includes a rotor shaft, a stationary assembly circumscribing the rotor shaft, and a rotating component coupled to the rotor shaft and positioned radially inward of the stationary assembly. The rotating assembly includes a hub coupled to the rotor shaft, a plurality of rotor blades coupled to the hub, and a shroud coupled to the plurality of rotor blades.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 RIVER ROAD SCHENECTADY NY 12345

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Moniz, Thomas Ory Loveland, US 117 2249
Rose, Joseph George Mason, US 15 15

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