The invention proposes an annular porous gas turbulence structure of a solid rocket motor gas flow regulating device, which premixes and evenly distributes the high-temperature and high-speed incoming gas, reduces the uneven erosion and aerodynamic impact of the gas on the valve core of the flow regulating device, and can also be used To filter some of the bulky debris entrained in solid rocket motor gases. The annular porous gas turbulence structure can process multiple air holes on the annular turbulence structure according to the incoming flow direction. The shape and number of air holes can be adjusted according to the area of the gas inlet and nozzle outlet. The periphery of the spool of the regulating device is fixed between the gas inlet and the spool of the flow regulating device through mechanical and adhesive means. The invention not only has the characteristics of simple structure, compactness, easy molding, convenient assembly, high temperature resistance, reliable operation, etc.; it also plays the role of premixed gas flow, uniform distribution of gas, and reduces local erosion and ablation of high-temperature and high-speed gas on the gas flow adjustment device. .