Unitized rotor assembly

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11180997
APP PUB NO 20210087935A1
SERIAL NO

16577385

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Abstract

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A method of making a rotor assembly of a turbojet includes building the rotor assembly via layer-by-layer additive manufacturing. A turbine portion is formed and a compressor portion is integrally formed with the turbine portion. A shaft portion is integrally formed with the compressor portion. A material of the rotor assembly includes a nickel based alloy.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Binek, Lawrence A Glastonbury, US 96 56
Boy, Jesse R Middletown, US 1 0
Butcher, Evan J Suffield, US 20 33
Garcia, Jesus A San Diego, US 8 20
Kennedy, Matthew B Vernon, US 18 43
Zarandi, Faramarz Vernon, US 1 0

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