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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 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 5 ÐÐÑ
ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ Ð±Ð°ÐºÐ°Ð»Ð°Ð²Ñа ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 5 ÐÐÑ Ð½Ð° оÑнове пÑоÑоÑипа ÐÐ-12СТ. ÐадаÑи, коÑоÑÑе бÑли ÑеÑÐµÐ½Ñ Ð² Ñ Ð¾Ð´Ðµ ÑабоÑÑ:openaire +1 more source
ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 65 ÐÐÑ
This bachelors graduation thesis is devoted to the development and design of a stationary gas turbine engine with a capacity of 65 MW. This design includes thermal calculation, approximate calculation of the compressor, calculation of the combustion chamber, gas dynamic calculation, strength calculation, description and main characteristics of the ...openaire +1 more source
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