The application discloses a
turbine rotating-static spacing design method for inhibiting wave
system interference, and the method comprises the following steps: obtaining
turbine overall design input parameters; establishing a rotating-static axial spacing quantitative calculation model based on the input parameters; satisfying supersonic
airflow local blockage conditions; and inhibiting wave
system interference through induced shock
waves. The optimal spacing is calculated by using the model, so that the rotor blade is swept by three times of extended, reflected and induced shock
waves when passing through the guide vane channel, and aerodynamic excitation spectrum is widely distributed. The spacing is output to the
turbine stage axial
layout design. The application optimizes the
axial distance between the rotor blade and the
stator guide vane, directly reduces the turbine stage axial size, and through the accurate control of the axial spacing, the rotor blade is swept by three times of extended, reflected and induced shock
waves when passing through the guide vane channel, the wide distribution of the aerodynamic excitation
energy spectrum is realized, and the aerodynamic excitation on the
turbine rotor blade is significantly reduced.