Development of Programs for Digital Anti-Surge Protection Systems to Optimize the Control of Electrical Circuits of the Gas Pumping Station Operation Mode

Development of programs for digital protection systems to prevent surging processes at compressor stations. Within the framework of the boundary layer theory, an analytical solution to the problem of the boundary layer of a compressible gas between slightly curved impeller blades is a obtained. To determine the distribution of the gas flow velocity between the boundary layers of two adjacent impeller blades, which ensures a continuous flow of gas in the boundary layers, which prevents the appearance of surging due to sudden changes in flow rate.