ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ð¼Ð¾ÑноÑÑÑÑ 17 ÐÐÑ
2023The purpose of this work is to design a gas turbine engine with a capacity of 17 MW based on the NK-16 ST prototype. Tasks that were solved during the work: 1. Calculation of the thermal scheme, based on the results of which the degree of pressure increase in the compressor and the temperature at the turbine inlet are selected; 2.
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ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ð¼Ð¾ÑноÑÑÑÑ 10 ÐÐÑ
2023This work is aimed at designing a gas turbine plant with a capacity of 10 MW based on the GTK-10-4. Tasks that were solved during the study: 1. Calculation of the thermal scheme of the installation and selection of optimal parameters p_k and T_3 by means of the calculation program A2GTP; 2. Approximate calculation of the compressor; 3.
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ÐоÑмиÑование ÑоÑноÑÑи в маÑиноÑÑÑоении. Ч. 1
2014РаÑÑмоÑÑÐµÐ½Ñ Ð²Ð¾Ð¿ÑоÑÑ Ð½Ð¾ÑмиÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑоÑноÑÑи Ñ ÑелÑÑ Ð¾Ð±ÐµÑпеÑÐµÐ½Ð¸Ñ ÐºÐ°ÑеÑÑва изделий на оÑнове пÑинÑипов и ÑÑебований междÑнаÑоднÑÑ ÑÑандаÑÑов ÑеÑии ÐСР9000 и оÑеÑеÑÑвеннÑÑ Ð½Ð¾ÑмаÑивно-пÑавовÑÑ Ð´Ð¾Â ...
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Ðказание пеÑвой помоÑи поÑÑÑадавÑим пÑи пожаÑе
2019The paper deals with the organization: analysis of harmful and dangerous factors of fire, analysis of the most likely injuries caused by fire, analysis of modern methods of first aid and development of a universal algorithm for first aid in case of fire.
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ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ð¼Ð¾ÑноÑÑÑÑ 5,5 ÐÐÑ
2023The theme of the final qualification work: "Gas turbine unit with a capacity of 5.5 MW" The purpose of this work is to design a gas turbine unit with a capacity of 5.5 based on the NKâ12ST prototype Tasks that were solved in the course of work 1.
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ÐоÑмиÑование ÑоÑноÑÑи в маÑиноÑÑÑоении. Ч. 2
2014ЯвлÑеÑÑÑ Ð¿Ñодолжением пеÑвой ÑаÑÑи. Рнем ÑаÑÑмоÑÑÐµÐ½Ñ Ð²Ð¾Ð¿ÑоÑÑ Ð½Ð¾ÑмиÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑоÑноÑÑи и взаимозаменÑемоÑÑи ÑгловÑÑ ÑазмеÑов и коÂниÑеÑÐºÐ¸Ñ Ñоединений, паÑамеÑÑов ÑеÑÐ¾Ñ Ð¾Ð²Ð°ÑоÑÑи повеÑÑ Ð½Ð¾ÑÑи, ÑоÑ
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ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ð¼Ð¾ÑноÑÑÑÑ 32 ÐÐÑ
2023Тема вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ: «ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ð¼Ð¾ÑноÑÑÑÑ 32 ÐÐÑ». ÐÐ°Ð½Ð½Ð°Ñ Ð²ÑпÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑикаÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑабоÑа бакалавÑа поÑвÑÑена пÑоекÑиÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð³Ð°Ð·Ð¾ÑÑÑбинного двигаÑÐµÐ»Ñ Ð¼Ð¾Ñ ...
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ÐвиаÑионнÑй газоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 90кÐ
2017Рданной ÑабоÑе бÑл ÑаÑÑÑиÑан авиаÑионнÑй газоÑÑÑбиннÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 90 кÐ. РабоÑа Ñазделена на воÑÐµÐ¼Ñ Ð¾ÑновнÑÑ Ð³Ð»Ð°Ð², в коÑоÑÑÑ Ð±Ñли ÑаÑÑÑиÑÐ°Ð½Ñ Ð°Ð³ÑегаÑÑ ÑÑÑановки, Ñакие как венÑилÑÑоÑ, комп
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ÐазоÑÑÑбиннÑй двигаÑÐµÐ»Ñ ÐТÐ-1250
2022The topic of the final qualifying work: "Gas turbine unit GTP-1250".This work is devoted to the design of a gas turbine unit with a capacity of 1.2 MW based on the previously developed gas turbine unit GTD-1250. Tasks that were solved during the study:1. Calculation of the thermal scheme of the installation using the A2GTP program.2.
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ÐвиаÑионнÑй газоÑÑÑбиннÑй двигаÑÐµÐ»Ñ ÑÑгой 160 кÐ
2019Рданной вÑпÑÑкной квалиÑикаÑионной ÑабоÑе бÑло вÑполнено пÑоекÑиÑование авиаÑионного газоÑÑÑбинного двигаÑÐµÐ»Ñ (ÐТÐ) ÑÑгой 160 кÐ, на оÑнове двигаÑÐµÐ»Ñ ÐС-90а, ÑазÑабоÑанного ÐÐР«ÐвиадвигаÑелÑ»
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