Spoked spacer for a gas turbine engine

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United States of America Patent

PATENT NO 8944762
SERIAL NO

13283733

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Abstract

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A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation and a plurality of core gas path seals which extend from the rotor ring, each of the plurality of core gas path seals extend from the rotor ring at an interface, the interface defined along a spoke.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dye, Christopher M San Diego, US 119 2646
Muron, Stephen P Columbia, US 8 66
Suciu, Gabriel L Glastonbury, US 580 8113

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