Ð“Ð°Ð·Ð¾Ñ‚ÑƒÑ€Ð±Ð¸Ð½Ð½Ð°Ñ ÑƒÑтановка мощноÑтью 65 МВт
Ð“Ð°Ð·Ð¾Ñ‚ÑƒÑ€Ð±Ð¸Ð½Ð½Ð°Ñ ÑƒÑтановка мощноÑтью 65 МВт
Ð”Ð°Ð½Ð½Ð°Ñ Ð²Ñ‹Ð¿ÑƒÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸Ñ„Ð¸ÐºÐ°Ñ†Ð¸Ð¾Ð½Ð½Ð°Ñ Ñ€Ð°Ð±Ð¾Ñ‚Ð° бакалавра поÑвÑщена разработке и проектированию Ñтационарного газотурбинного Ð´Ð²Ð¸Ð³Ð°Ñ‚ÐµÐ»Ñ Ð¼Ð¾Ñ‰Ð½Ð¾ÑÑ‚ÑŒ 65 МВт. Данное проектирование включает в ÑÐµÐ±Ñ Ñ‚ÐµÐ¿Ð»Ð¾Ð²Ð¾Ð¹ раÑчет, приближенный раÑчет компреÑÑора, раÑчет камеры ÑгораниÑ, газодинамичеÑкий раÑчет, прочноÑтной раÑчет, опиÑание и оÑновные характериÑтики турбины, а также ÑÐ¿ÐµÑ†Ð¸Ð°Ð»ÑŒÐ½Ð°Ñ Ñ‡Ð°ÑÑ‚ÑŒ.
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 turbine, as well as a special part.
пÑоÑоÑÐ½Ð°Ñ ÑаÑÑÑ, газодинамиÑеÑкий ÑаÑÑеÑ, оÑевой компÑеÑÑоÑ, calculation of the thermal circuit microturbine, axial compressor, камеÑа ÑгоÑаниÑ, gas turbine unit, vibration reliability, вибÑонадежноÑÑÑ, пÑоÑилиÑование лопаÑки, disc, strength calculation, turbine, combustion chamber, пÑоÑноÑÑÑ, ÑаÑÑÐµÑ Ð½Ð° пÑоÑноÑÑÑ, blade, ÑÑÑбина, flow part, ÑаÑÑÐµÑ Ñепловой ÑÑ ÐµÐ¼Ñ Ð¼Ð¸ÐºÑоÑÑÑбинÑ, газоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка, blade profiling, gas dynamic calculation, диÑк, лопаÑка, rotor, strength, ÑоÑоÑ
пÑоÑоÑÐ½Ð°Ñ ÑаÑÑÑ, газодинамиÑеÑкий ÑаÑÑеÑ, оÑевой компÑеÑÑоÑ, calculation of the thermal circuit microturbine, axial compressor, камеÑа ÑгоÑаниÑ, gas turbine unit, vibration reliability, вибÑонадежноÑÑÑ, пÑоÑилиÑование лопаÑки, disc, strength calculation, turbine, combustion chamber, пÑоÑноÑÑÑ, ÑаÑÑÐµÑ Ð½Ð° пÑоÑноÑÑÑ, blade, ÑÑÑбина, flow part, ÑаÑÑÐµÑ Ñепловой ÑÑ ÐµÐ¼Ñ Ð¼Ð¸ÐºÑоÑÑÑбинÑ, газоÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑановка, blade profiling, gas dynamic calculation, диÑк, лопаÑка, rotor, strength, ÑоÑоÑ
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