Method for detecting combustion conditions in combustors
First Claim
1. A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of:
- measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine;
obtaining a distribution pattern of said measured concentration; and
examining said distribution pattern to detect combustion conditions in said combustors.
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Abstract
A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes the combustors and a gas turbine driven by combustion gas from the combustors, comprises a step for measuring concentration of unburnt component in the combustion gas by means of a plurality of sensors disposed on the downstream side of the gas turbine, a step for obtaining a distribution pattern of the measured concentration, and a step for investigating the distribution pattern to detect combustion conditions in the combustors.
47 Citations
9 Claims
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1. A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of:
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measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; and examining said distribution pattern to detect combustion conditions in said combustors. - View Dependent Claims (2, 3, 4)
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5. A control method for controlling combustion in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of:
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measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; examining said distribution pattern to detect combustion conditions in said combustors; and adjusting flow rates of air and/or fuel to be fed to the respective combustors in dependence upon detected combustion conditions. - View Dependent Claims (6, 7, 8, 9)
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Specification