Gas turbine plant with a capacity of 16 MW
| Jazyk: | ruština |
|---|---|
| Rok vydání: | 2022 |
| Předmět: | |
| DOI: | 10.18720/spbpu/3/2022/vr/vr22-2431 |
| Popis: | Тема: «ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка моÑноÑÑÑÑ 16 ÐÐÑ».ÐвÑоÑ: ÐлаÑов ТимÑÑ ÐнаÑолÑевиÑ, ÑÑÑÐ´ÐµÐ½Ñ 4 кÑÑÑа ÐнÑÑиÑÑÑа ÑнеÑгеÑики СÐбÐУ им. ÐеÑÑа Ðеликого.Ð ÑвÑзи Ñ ÑÐµÑ Ð½Ð¸ÑеÑкими пÑоблемами и ÑложноÑÑÑми, Ñема данной вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ Ð¾ÑлиÑаеÑÑÑ Ð¾Ñ Ð¾ÑиÑиалÑной, пÑопиÑанной в пÑиказе («ÐазоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка ÐТÐ16ТÐл). ЦелÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑабоÑÑ ÑвлÑеÑÑÑ Ð¿ÑоекÑиÑование газоÑÑÑбинной ÑÑÑановки моÑноÑÑÑÑ 16 ÐÐÑ Ð½Ð° оÑнове Ñанее ÑазÑабоÑанной газоÑÑÑбинной ÑÑÑановки ÐÐ-16СТ.Рданной ÑабоÑе пÑоизводÑÑÑÑ ÑаÑÑÐµÑ Ñепловой ÑÑ ÐµÐ¼Ñ, пÑиближеннÑй ÑаÑÑÐµÑ ÐºÐ¾Ð¼Ð¿ÑеÑÑоÑа низкого Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ (ÐÐÐ) и компÑеÑÑоÑа вÑÑокого Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ (ÐÐÐ), ÑаÑÑÐµÑ ÐºÐ°Ð¼ÐµÑÑ ÑгоÑÐ°Ð½Ð¸Ñ (ÐС) Ñ Ð¿Ð¾Ð»ÑÑением ее геомеÑÑиÑеÑÐºÐ¸Ñ ÑазмеÑов и Ñ Ð°ÑакÑеÑиÑÑик ÑабоÑего пÑоÑеÑÑа, подÑобнÑй газодинамиÑеÑкий ÑаÑÑÐµÑ Ð¿ÑоÑоÑной ÑаÑÑи ÑÑÑÐ±Ð¸Ð½Ñ Ð²ÑÑокого Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ (ТÐÐ), ÑÑÑÐ±Ð¸Ð½Ñ Ð½Ð¸Ð·ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ (ТÐÐ) и Ñиловой ÑÑÑÐ±Ð¸Ð½Ñ (СТ) Ñ Ð¿Ð¾Ð»ÑÑением геомеÑÑиÑеÑÐºÐ¸Ñ ÑазмеÑов пÑоÑоÑной ÑаÑÑи, ÑаÑÑеÑÑ Ð·Ð°ÐºÑÑÑки поÑока в поÑледней ÑÑÑпени СТ, на оÑновании коÑоÑÑÑ ÑÑÑоÑÑÑÑ ÑÑеÑголÑники ÑкоÑоÑÑей данной ÑÑÑпени в ÑазлиÑнÑÑ ÑеÑениÑÑ Ð¸ пÑоизводиÑÑÑ Ð¼Ð¾Ð´ÐµÐ»Ð¸Ñование лопаÑки, ÑаÑÑеÑÑ Ð½Ð° пÑоÑноÑÑÑ ÑоÑоÑнÑÑ ÑлеменÑов поÑледней ÑÑÑпени СТ в пÑогÑамме ANSYS.РабоÑа ÑодеÑÐ¶Ð¸Ñ 172 ÑÑÑаниÑÑ, 62 ÑиÑÑнка, 27 ÑаблиÑ, 1 пÑиложение, иÑполÑзовано 27 иÑÑоÑников. Theme: "Gas turbine plant with a capacity of 16 MW".Author: Platov Timur Anatolyevich, 4th year student of the Institute of Energy of the Peter the Great St. Petersburg Polytechnic University.Due to technical problems and difficulties, the theme of this diploma work differs from the official one ("Gas turbine plant GTN16TMZ"). The objective of this work is to design a 16 MW gas turbine plant based on the previously developed NK-16ST gas turbine plant.During this work, calculations of the thermal scheme, the approximate calculation of a low-pressure compressor (LPC) and a high-pressure compressor (HPC), the calculation of the combustion chamber (CC), a detailed gas-dynamic calculation of the flow path of a high-pressure turbine (HPT), a low-pressure turbine (LPT) and a power turbine (PT) in order to obtain the geometric dimensions of the flow-through part, calculations of the flow swirling in the last stage of the PT, on the basis of the results of which the velocity triangles of the considered stage are constructed in various sections and the blade is modeled, calculations for the strength of the rotor elements of the last stage of the PT are performed in the software package ANSYS. |
| Databáze: | OpenAIRE |
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