The invention discloses a method for optimizing
gas compressor stator blade root slotting
channel geometry based on an optimization
algorithm, and relates to the technical field of optimization algorithms and
impeller mechanical flow control.The method aims at obtaining optimal blade root
channel geometry through optimization calculation so that the angle area separation
control effect of a force suction face can be optimal.By means of the
gas compressor stator blade root slotting method based on the optimization
algorithm, all design parameters of blade root channels can be subjected to
coupling calculation and analysis, the optimal channel
control effect is proposed based on an optimization calculation result, the
coupling effect between the geometrical parameters of the channels can be comprehensively considered, and thus it is avoided that only changes of a
single parameter or a few of parameters are calculated in flow optimization control.The optimization
algorithm is a multi-target
function optimization algorithm based on a non-domination
ranking genetic algorithm, the S-shaped channels contracting to a force
suction surface from a pressure surface are subjected to optimization calculation, the optimization parameters include inlet positions and outlet positions of the channels, lengths and channel heights, and a target function includes a blade grid total pressure loss coefficient, a static pressure raising coefficient and a blade grid channel blockage coefficient.The
gas compressor stator blade root slotting method has the advantages that an optimization method and a blade grid flow control method are combined,
channel geometry is optimized on the condition that the original blade grid blade shape is fixed, and thus the
control effect is optimal.