Temperature sensor arrangement in combination with a gas turbine combustion chamber
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United States of America Patent
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Nov 7, 2000
Grant Date -
N/A
app pub date -
May 29, 1997
filing date -
Jul 18, 1996
priority date (Note) -
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Abstract
In a temperature-measuring device, in particular for measuring the flame temperature in a gas turbine combustion chamber, a number of optical measuring sensors (7) are arranged directly upstream of a flame front (8) in a premixing zone (3) of a burner (1). Each optical measuring sensor (7) is aligned essentially parallel to and/or coaxial with a fuel flow (5) directed into the gas turbine combustion chamber.
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