CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE

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United States of America Patent

APP PUB NO 20180347470A1
SERIAL NO

16108616

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Abstract

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A fuel injection system for a gas turbine engine includes a fuel nozzle with a fuel injection aperture to inject a fuel jet and a multiple of airflow passages in the fuel nozzle to communicate a multiple of air streams to interact with the fuel jet.

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Patent Owner(s)

Patent OwnerAddress
RAYTHEON TECHNOLOGIES CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032-2568

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bellows, Benjamin Glastonbury, US 3 24
Lovett, Jeffery A Tolland, US 27 362

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