Segmented surface-stabilized gas burner and method of use with gas turbines
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United States of America Patent
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Sep 24, 2002
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N/A
app pub date -
Mar 15, 2001
filing date -
Mar 15, 2001
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Abstract
A segmented surface-stabilized 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 surface-stabilized 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 relative flow of compressed air into the segments of the burner remains unchanged.
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