This invention discloses a method and
system for analyzing the steady-state of a laminar
diffusion jet
flame, relating to the field of gas
turbine combustion technology. The method includes: obtaining the instantaneous propagation velocity of the laminar jet
diffusion flame when the
flame root reaches its final stable position during propagation towards the
nozzle. S d and the local
airflow velocity at that location U G ;according to S d and U G Determine the instantaneous
combustion rate; compare the instantaneous
combustion rate with... U G If the difference between the two is within a preset range, it indicates that the combustion rate and the local
airflow velocity are in
dynamic equilibrium, and it is determined to be a pusher flame; if the instantaneous combustion rate is greater than 1, it indicates that the combustion rate and the local
airflow velocity are in
dynamic equilibrium, and it is determined to be a pusher flame. U G If the difference exceeds a preset range, it indicates that the
flame propagation and the
extinction caused by heat loss are in equilibrium, and the flame is identified as an attached flame. This invention achieves precise identification of the flame's
stable state by quantifying the comparison between combustion rate and airflow rate, providing a quantitative basis for combustion adjustment and significantly reducing operational
blindness and time costs. A corresponding analysis
system is also provided.