Dual fuel nozzle with swirling axial gas injection for a gas turbine engine

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United States of America Patent

PATENT NO 10228137
APP PUB NO 20160209038A1
SERIAL NO

14914802

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Abstract

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A fuel nozzle for a combustor of a gas turbine engine includes an outer air swirler along an axis, the outer air swirler defines an outer annular air passage. An inner air swirler along the axis defines an annular fuel gas passage around the axis between the outer air swirler and the inner air swirler, the annular fuel gas passage terminates with a multiple of skewed slots.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS RD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dai, Zhongtao Manchester, US 48 279
Kopp-Vaughan, Kristin East Hartford, US 9 101
Smith, Randolph J Ellington, US 11 173
Snyder, Timothy S Glastonbury, US 85 1234

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