Combustion chamber of a combustor for a gas turbine
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United States of America Patent
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Feb 6, 2018
Issued Date -
N/A
app pub date -
Dec 21, 2012
filing date -
Jan 5, 2012
priority date (Note) -
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Abstract
A combustion chamber of a combustor for a gas turbine is provided. A combustion chamber includes a plurality of segments arranged annularly about an axis of the combustion chamber, each segment comprising a radial inner wall portion and a radial outer wall portion, a first section comprising an opening for the installation of a burner, and a second section at which at least one airfoil extends between the radial inner wall portion and radial outer wall portion of the segment.
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