Annular combustion chamber of a gas turbine

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United States of America Patent

PATENT NO 9435538
APP PUB NO 20130192232A1
SERIAL NO

13746467

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Abstract

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The present invention relates to an annular combustion chamber of a gas turbine with—relative to the engine axis—a radially outer combustion chamber wall and a radially inner combustion chamber wall, with the combustion chamber walls forming an annular combustion space, with a combustion chamber head having a plurality of fuel nozzles and air inlet openings, with the respective central axes of the fuel nozzles forming an envelope rotationally symmetrical to the engine axis, the envelope dividing the combustion chamber into an annular and radially outer area and an annular and radially inner area, with the radially outer area and the radially inner area having the same volumes.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG15827 BLANKENFELDE-MAHLOW

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Clemen, Carsten Mittenwalde, DE 69 450

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