Heat exchanger bypass ejector

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12098676
SERIAL NO

18238669

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Abstract

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An aircraft propulsion system includes a core engine for generating an exhaust gas flow that is expanded through a turbine to generate shaft power. A heat exchanger is in communication with a partial portion of the exhaust gas flow and an exit flow is emitted from the heat exchanger. An ejector is configured to increase a pressure of the exit flow with a motive flow taken from the core flow path.

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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
Ikeda, Michael K West Hartford, US 13 86
MacDonald, Malcolm P Bloomfield, US 14 2
Taylor, Stephen H East Hartford, US 21 29

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