ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 32 ÐÐÑ
2020Тема вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ (ÐÐÐ ): «ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 32 ÐÐÑ». ÐÑи вÑполнении ÑабоÑÑ Ð² каÑеÑÑве пÑоÑоÑипа иÑполÑзована ÐÐÐ Ðадога 32.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 25 ÐÐÑ
2020ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑабоÑÑ ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 25 ÐÐÑ. РкаÑеÑÑве пÑоÑоÑипа бÑла вÑбÑана газоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка ÐТУ-25.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 26 ÐÐÑ
ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ Ð±Ð°ÐºÐ°Ð»Ð°Ð²Ñа ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование газоÑÑÑбинной ÑÑÑановки на оÑнове пÑоÑоÑипа ÐТУ-25Ð. ÐадаÑи, коÑоÑÑе вÑполнÑÑÑÑÑ Ð² пÑоÑеÑÑе иÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð³Ð°Ð ...openaire +1 more source
ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 4 ÐÐÑ
2019Рданной ÑабоÑе пÑедÑÑавлен ÑаÑÑÐµÑ Ð³Ð°Ð·Ð¾ÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 4 ÐÐÑ Ð´Ð»Ñ ÑкÑплÑаÑаÑии в ÑоÑÑаве газопеÑекаÑиваÑÑего агÑегаÑа компÑеÑÑоÑной ÑÑанÑии.
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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 2,3 ÐÐÑ
2019This work contain the method for creating a 2.3 MW gas-turbine plant based on the already existing prototype TB3-117. A general description of the prototype installation and some design features are given. The calculation of the thermal scheme, the approximate calculation of the compressor, the calculation of the combustion chamber, the gas-dynamic ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 17 ÐÐÑ
2019In this work the design technique and calculation of the 17 MW gas-turbine unit on the basis of already existing prototype of "AL-31ST" is explained. In work the general description of unit is given, calculation of the thermal scheme, approximate calculation of the axial compressor, calculation of a combustion chamber, gasodynamic calculation of a ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16 ÐÐÑ
2017ÐÐ°Ð½Ð½Ð°Ñ ÑабоÑа поÑвÑÑена ÑазÑабоÑке газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 16 ÐÐÑ Ð´Ð»Ñ Ð¿Ñивода нагнеÑаÑÐµÐ»Ñ Ð¿ÑиÑодного газа. Топливом данной ÑÑÑановки ÑвлÑеÑÑÑ ÑопливнÑй газ.
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 6,3 ÐÐÑ
2019In this work, the calculation of a 6,3 MW gas turbine unit. Calculation was based on 6,3 MW gas turbine engine NK-12ST. This calculation includes thermal scheme of GTU calculation, approximate axial compressor calculation, calculation of the combustion chamber, gasdynamic calculation of gas turbine, flow twist of last stage and approximate calculation ...
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ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 18 ÐÐÑ
The purpose of this bachelors final qualifying work is to design a gas turbine plant based on the AL-31ST prototype. Tasks that are performed during the research of a gas turbine engine: 1. Study of the design features of the AL-31ST prototype. 2. Thermal calculation of the engine with the selection of the optimal option. 3.openaire +1 more source

