Abstract
Methods for converting aviation gas turbine engines when creating a gas-turbine-driven compressor plant for driving a gas compressor unit when transporting gas and gas turbine power plants in the power industry, various options for changing workflow and power circuits are considered. Using simulation modeling, the authors analyzed the parameters and characteristics of various options for creating a gas-turbine-driven compressor plant for a gas-compressor unit on the basis of the AL-31F aviation two spool turbojet engine with afterburner. The article shows the successive stages of the modernization of the scheme and changes in the parameters of the model of the aviation two spool turbojet engine with an afterburner with various conversion options in the gas-turbine-driven compressor plants for ground application. The criteria used are the full efficiency, the net power of the free turbine, the specific fuel consumption, the introduced structural changes and the overhaul life of the gas-turbine-driven compressor plant.
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