Active tip clearance control system for gas turbine engine

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United States of America Patent

PATENT NO 10781756
APP PUB NO 20190242303A1
SERIAL NO

15887181

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Abstract

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An active tip clearance control system of a gas turbine engine and an associated method are disclosed. The system comprises a Coanda effect fluidic device configured to control a flow of clearance control fluid to a turbine section of the gas turbine engine for active tip clearance control.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADA CORP1000 MARIE VICTORIN BLVD LONGUEUIL QU J4G 1A1

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Alecu, Daniel Brampton, CA 90 429
Menheere, David Norval, CA 76 449

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