Combustion systems

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10578021
APP PUB NO 20160376997A1
SERIAL NO

14752318

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Importance

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Abstract

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A combustion system for a gas turbine engine includes a combustor dome. The combustor dome includes a fuel manifold with an inlet and nozzle components of a plurality of nozzles circumferentially spaced around the combustor dome. The fuel manifold and nozzle components are integrated with the combustor dome for fluid communication from the inlet to the nozzle components.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
COLLINS ENGINE NOZZLES INC811 4TH STREET P O BOX 65100 DES MOINES IA 50265

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Prociw, Lev A Johnston, US 71 320

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