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 моÑноÑÑÑÑ 18 ÐÐÑ
2021The aim of the work is the design and calculation of a gas turbine unit with a capacity of 18 MW, the prototype of the NK â 16 â 18ST gas turbine engine is taken as the basis. Calculations of the GTU thermal circuit, calculation of low-and medium-pressure compressors, detailed gas-dynamic calculation of the gas generator turbine and the power ...
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ÐикÑоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 200 кÐÑ
2018РнаÑÑоÑÑей ÑабоÑе пÑоизведен ÑаÑÑÐµÑ Ð¼Ð°Ð»Ð¾Ð³Ð°Ð±Ð°ÑиÑной газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 200 кÐÑ. РаÑÑÐµÑ Ð²ÐºÐ»ÑÑÐ°ÐµÑ Ð² ÑебÑ: ÑаÑÑÐµÑ Ñепловой ÑÑ ÐµÐ¼Ñ ÐТУ, пÑиближеннÑй ÑаÑÑÐµÑ ÑенÑÑобежного компÑеÑÑоÑа,
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 1,2 ÐÐÑ
2023ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑабоÑÑ ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 1,2 ÐÐÑ Ð½Ð° оÑнове Ñанее ÑазÑабоÑанной газоÑÑÑбинной ÑÑÑановки ÐТÐ-1250.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 25 ÐÐÑ
2018Рданной вÑпÑÑкной квалиÑикаÑионной ÑабоÑе бакалавÑа изложена меÑодика ÑÐ¾Ð·Ð´Ð°Ð½Ð¸Ñ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 25 ÐÐÑ Ð½Ð° оÑнове пÑоÑоÑипа ÐТÐ-25 УТÐÐ, вÑполненной ÐÐ "УÑалÑÑкий ÑÑÑбиннÑй зР...
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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 6,3 ÐÐÑ
2018Ð ÑабоÑе пÑоизведен ÑаÑÑÑÑ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 6,3 ÐвÑ. РаÑÑÐµÑ Ð±Ñл пÑоизведÑн на оÑновании газоÑÑÑбинного двигаÑÐµÐ»Ñ ÐÐ-12СТ моÑноÑÑÑÑ 6,3 ÐвÑ.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 2,1 ÐÐÑ
2017Рданной ÑабоÑе пÑедÑÑавлен ÑаÑÑÑÑ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 2,1 ÐÐÑ Ð´Ð»Ñ ÑкÑплÑаÑаÑии в ÑоÑÑаве газопеÑекаÑиваÑÑего агÑегаÑа компÑеÑÑоÑной ÑÑанÑии.
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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 16,8 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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