ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16 ÐÐÑ
2019In this paper, the methods for creating a 16 MW gas turbine plant based on the existing prototype PS-90GP-2 are presented. Calculation of the thermal scheme, approximate calculation of the compressor, calculation of the combustion chamber, gas-dynamic calculation of the compressor turbine (CT) and free force turbine (FT), calculation of the twist of ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 160ÐÐÑ
2021This work is devoted to the development and design of a stationary gas turbine power plant with a free turbine with a useful capacity of 160MW. Tasks solved dur ing the design process: 1. Calculation of the thermal scheme of a gas turbine installation; 2. Calculation of the combustion chamber; 3.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16 ÐÐÑ
2022This work is devoted to the design of a stationary gas turbine with a power of 16 MW, based on the prototype V94, used to produce electricity in a simple and combined cycle. Tasks that were solved during the study: 1. Perform the calculation of the thermal circuit; 2. Make an approximate gas-dynamic calculation of the axial compressor and design of the
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16,8 ÐÐÑ
2022Рданной ÑабоÑе изложена меÑодика ÑÐ¾Ð·Ð´Ð°Ð½Ð¸Ñ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки (ÐТУ) моÑноÑÑÑÑ 16,8 ÐÐÑ Ð½Ð° оÑнове Ñанее ÑазÑабоÑанной газоÑÑÑбиннойÑÑÑановки ÐÐ-31СТ.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑ 10,3 ÐÐÑ
2020The prototype for the GTU considered in this work is GTU-10P, made on the basis of the PS-90 aircraft engine. The aim of the work is the research, calculation and design of a gas turbine unit with a capacity of 10,3 MW. Tasks that were solved during the study: ï ¬Calculation of a thermal arrangement, which data is used in choice of the optimal ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑ 15 ÐÐÑ
2020The aim of this work is the design and calculation of a gas turbine unit with a capacity of 15 MW, as well as its optimization. As a prototype, the PS-90GP-2 installation is used. In the course of the work, the calculation of the thermal circuit is carried out, based on the data obtained, the optimal degree of pressure increase in the compressor is ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16.8 ÐÐÑ
2020The aim of this work is to design a gas turbine plant with a capacity of 16.8 MW. The gas turbine unit AL-31ST was chosen as a prototype. In the course of the work produced: 1) calculation of the thermal scheme, on the basis of the results of which the optimal degree of pressure increase in the compressor is selected; 2) an approximate calculation of ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 25,6 ÐÐÑ
2020ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑабоÑÑ ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование и ÑаÑÑÐµÑ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 25,6 ÐÐÑ, пÑоÑоÑипом коÑоÑой ÑвлÑеÑÑÑ ÐТУ ÐС-90ÐÐ-2.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16,8 ÐÐÑ
2021ÐвигаÑÐµÐ»Ñ ÐÐ-31СТ пÑедназнаÑен Ð´Ð»Ñ Ð¿Ñивода ÑоÑоÑа нагнеÑаÑÐµÐ»Ñ Ð³Ð°Ð·Ð¾Ð¿ÐµÑекаÑиваÑÑего агÑегаÑа. ÐонÑÑÑÑкÑивно двигаÑÐµÐ»Ñ Ð²Ñполнен в виде двÑÑ Ð¼Ð¾Ð´Ñлей: газогенеÑаÑоÑа и Ñвободной ÑÑÑбинÑ.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð°Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 1600кÐÑ
2016РнаÑÑоÑÑей ÑабоÑе пÑоизведен ÑаÑÑÐµÑ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки, а Ñакже модиÑикаÑÐ¸Ñ ÑÑÑÐ±Ð¸Ð½Ñ Ð¿ÑÑем ÑокÑаÑÐµÐ½Ð¸Ñ ÐºÐ¾Ð»Ð¸ÑеÑÑва ÑÑÑпеней и ÑазÑабоÑки ÑабоÑей лопаÑки пеÑвой ÑÑÑпени.
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