Premix burner for a gas turbine
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United States of America Patent
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Oct 11, 2011
Grant Date -
Oct 28, 2010
app pub date -
May 27, 2010
filing date -
Nov 27, 2007
priority date (Note) -
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Abstract
A premix burner is provided, with a swirl generator and a downstream mixer tube for combusting gaseous and liquid fuel which during entry of combustion air is introduced into the burner interior space of the swirl generator and/or is introduced into the burner interior of the swirl generator on a burner axis, and also with a fuel lance which is arranged on the burner axis. The premix burner, in the transition section from the swirl generator to the mixer tube, includes at least one additional feed for introducing gaseous and/or liquid premix fuel from the wall region into the burner interior space of the mixer tube.
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