The invention relates to the technical field of ignition systems of
gas turbines, and discloses a special
ignition system for a gas
turbine, which comprises a monitoring
control layer, an
energy distribution layer and a
combustion optimization layer. The monitoring
control layer monitors parameters such as
combustion chamber pressure fluctuation in real time through multiple types of sensors and executes
phase synchronization and injection control. The
energy distribution layer is provided with a multi-stage energy release strategy and a self-adaptive
time sequence matching mechanism, a stable ignition energy field is constructed, and physical and digital space linkage regulation and control are achieved through a multi-
modal energy interface; and the
combustion optimization layer establishes a multi-dimensional mapping combustion
state control model based on a dynamic combustion
algorithm and real-
time data, and adopts a collaborative optimization
algorithm to calibrate an ignition
time sequence, regulate and control a fuel
mixing ratio and maintain
flame stability. According to the
system, through multi-dimensional energy fusion,
model parameter dynamic correction and intelligent
algorithm application, the accuracy, stability and multi-working-condition adaptability of the gas
turbine ignition process are remarkably improved, and the
system is suitable for gas
turbine efficient combustion control in the fields of
aerospace,
electric power and the like.