The invention belongs to the technical field of aero-engine cooling design and flow heat exchange optimization, and provides a
turbine blade cooling turbulence rib construction method,
system and configuration based on
level set topological optimization and a blade. The method comprises the steps that a fluid-
solid coupling calculation model containing a
cooling channel fluid domain and a blade wall surface
solid domain is constructed, defining a
level set function to implicitly represent the two-phase region; establishing a unified
control equation set covering a full computational domain based on the function, and introducing a flow velocity suppression mechanism into a
solid domain to carry out single-domain
coupling solution of fluid flow and solid heat conduction; according to the
physical field solution, constructing an optimization model taking the cooling performance as a target function and the
volume fraction of the turbulent flow rib as a constraint, and calculating the sensitivity of the target function to a
level set function; using the sensitivity to drive a
level set function update to evolve a
spoiler rib boundary; iterating until convergence and outputting the final
geometric configuration of the turbulent flow rib. According to the invention, the irregular turbulent flow structure with
high heat exchange efficiency and low flow resistance can be automatically generated without presetting a rib type.