Focusing on the combustion characteristics and engineering application value of the constant-pressure sequential burner equipped in the GT36-S5 gas turbine
the structural principles and combustion adjustment mechanisms of the burner in actual operation were systematically elucidated. The effects of characteristic parameters
such as fuel staging ratio
combustion pressure pulsation frequency
and temperature distribution
on the operational stability of the unit were analyzed. By analyzing the process parameters of combustion adjustments under actual operating conditions
the nonlinear response laws of the gas turbine combustion during dynamic load changes were revealed. Specifically addressing the low-temperature operating scenario in winter
the effects of various factors
including fuel staging ratios at various stages
the MET setpoint
and
C
2+
content
on combustion stability
pulsations in different frequency bands and NO
x
emissions were analyzed. Results show that the obtained combustion characteristic analysis provides a critical basis for the operation and maintenance of the unit. It can guide on-site personnel to improve combustion stability and equipment reliability in complex environments by adjusting the gas turbine load
the residence time at different load stages
offering significant engineering reference value for the operation optimization of similar heavy-duty gas turbines.
关键词
Keywords
references
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