Method of using segmented gas burner with gas turbines
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United States of America Patent
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Oct 29, 2002
Grant Date -
Oct 17, 2002
app pub date -
Jun 11, 2002
filing date -
Mar 15, 2001
priority date (Note) -
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Abstract
A segmented radiant gas burner features wide modulation of thermal output simply by the independent control of fuel gas flow to each burner segment. The burner also features a porous fiber burner face, preferably having dual porosities, and a metal liner positioned to provide a compact combustion zone adjacent the burner face. The segmented radiant burner is ideally suited for use with gas turbines not only because of its compactness and broad thermal modulation but also because only the flow of fuel gas to each burner segment requires control while the flow of compressed air into all segments of the burner remains unchanged.
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