Sequential combustion with dilution gas mixer
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United States of America Patent
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Jun 25, 2019
Grant Date -
Aug 13, 2015
app pub date -
Apr 22, 2015
filing date -
Oct 24, 2012
priority date (Note) -
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Abstract
The invention refers to a sequential combustor arrangement including a first burner, a first combustion chamber, a mixer for admixing a dilution gas to the hot gases leaving the first combustion chamber during operation, a second burner, and a second combustion chamber arranged sequentially in a fluid flow connection. The mixer includes a plurality of injection pipes pointing inwards from the side walls of the mixer for admixing the dilution gas to cool the hot flue gases leaving the first combustion chamber with a low pressure drop. The disclosure further refers to a method for operating a gas turbine with such a combustor arrangement.
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