
Работа включает в ÑÐµÐ±Ñ Ð²Ð²ÐµÐ´ÐµÐ½Ð¸Ðµ, 5 глав и заключение.Выполнен раÑчет цилиндра Ñреднего Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ Ð¿Ð°Ñ€Ð¾Ð²Ð¾Ð¹ турбины на базе прототипа К-1200-240, который Ñодержит раÑчет тепловой Ñхемы паротурбинной уÑтановки, газодинамичеÑкий раÑчет по Ñреднему диаметру, раÑчет параметров потока поÑледней Ñтупени цилиндра, прочноÑтной раÑчет лопатки и ротора. Также была Ñоздана и опиÑана программа газодинамичеÑкого раÑчета турбины.
The work includes an introduction, 5 chapters and a conclusion.The calculation of the medium-pressure cylinder of a steam turbine based on the prototype К-300-240-2, which includes the steam turbine thermal scheme calculation, the gas-dynamic calculation for the average diameter, the swirl blade calculation of the last cylinder stage, the strength blade and rotor calculation. A program for the gas-dynamic calculation of the turbine was also created and described.
газодинамиÑеÑкий ÑаÑÑеÑ, Ñепловой ÑаÑÑеÑ, medium pressure cylinder, steam turbine, Ð-1200-240, пÑоÑноÑÑной ÑаÑÑеÑ, паÑоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка, blade profiling, K-1200-240, пÑоÑилиÑование лопаÑки, thermal calculation, ÑÐ¸Ð»Ð¸Ð½Ð´Ñ ÑÑеднего давлениÑ, gasâdynamic calculation, strength calculation
газодинамиÑеÑкий ÑаÑÑеÑ, Ñепловой ÑаÑÑеÑ, medium pressure cylinder, steam turbine, Ð-1200-240, пÑоÑноÑÑной ÑаÑÑеÑ, паÑоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка, blade profiling, K-1200-240, пÑоÑилиÑование лопаÑки, thermal calculation, ÑÐ¸Ð»Ð¸Ð½Ð´Ñ ÑÑеднего давлениÑ, gasâdynamic calculation, strength calculation
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