The invention provides an aero-engine
high pressure turbine disc optimization design
system based on particle swarm and method, and relates to a
design technology field of the aero-engine. The
system comprises a definition module of the optimization task of the aero-engine
high pressure turbine disc, a primary particle swarm / file and a grid generation module, a
global optimum selection module based on a gridding neighborhood, a particle update module, a file update module and a
file size control module based on the gridding neighborhood, first the gridding jam index precision is improved by using
active volume of file in gridding, then the particle jam distance is calculated in the finite region by using the gridding neighborhood message, the confidence level
operand is provided for selecting the
global optimum and deleting the file particle, the obtained ultimately file is the result of a plurality of the target optimization. During designing a plurality of the target optimization for the aero-engine
high pressure turbine disc, starting from increasing precision of the
global optimum in
particle swarm optimization and of the non-particle deleting, the
system and method provides the high-quality result of a plurality of the target optimization.