FIELD: energy.
SUBSTANCE: invention relates to power engineering. Method for auto-configuration of fuel combustion system of gas turbine includes selection of a first adjustment curve from multiple adjustment curves for gas turbine, disbalance of stable operating point of gas turbine by changing one or more working parameters based on a predetermined set of instructions, determining adjusting parameters and saving thereof, while current operating point of gas turbine is returned to said first adjustment curve, and formation of a backup copy of adjusting parameters for recovery of stable working point. Invention also discloses a controller, versions of a gas turbine and machine-readable medium.
EFFECT: minimising combustion dynamics, which also enables to reduce risk of errors and need for manual adjustment of curve.
15 cl, 8 dwg
