Results 121 to 130 of about 260 (130)
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This paper calculates and designs a twin-shaft gas turbine engine with a thrust of 120 kN based on the prototype CFM-56-5. During the final qualification work, the following tasks were performed: ⢠Variative thermal calculation of the engine. ⢠Compressor calculation. ⢠Combustion chamber calculations.
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The aim of the work is to develop a turbojet twinâcircuit engine (turbojet engine) with a thrust of 85 kN based on a prototype - the AL-31F aviation turbojet engine. The main part of the work is devoted to the careful calculation of the parameters of the working process of the engine.
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The purpose of this work is to design an aviation engine with a thrust of 77 kN based on the prototype of the SaM 146. Tasks that were solved during the work: 1. Calculation of the thermal circuit, 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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ÐÐ°Ð½Ð½Ð°Ñ ÑабоÑа поÑвÑÑена пÑоекÑиÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑÑÑбоÑеакÑивного двÑÑ
конÑÑÑного авиаÑионного двигаÑÐµÐ»Ñ Ð½Ð° базе пÑоÑоÑипа ÐС-90Ð. ÐадаÑи, коÑоÑÑе вÑполнÑлиÑÑ Ð² пÑоÑеÑÑе иÑÑледованиÑ: 1) ÐзÑÑение оÑоР...
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2018
ÐбÑекÑом овеÑдÑаÑÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð´Ð¸Ð¿Ð»Ð¾Ð¼Ð½Ð¾Ð¹ ÑинанÑовое ÑабоÑÑ, ÑвлÑеÑÑÑ ÑиÑÑема ÑиÑки ÑинанÑового ÑолÑко ÑпÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ ÐÐР«ТиÑаÑполÑÑкий ÑÑÑка ÐºÐ¾Ð¼Ð±Ð¸Ð½Ð°Ñ Ñ Ð»ÐµÐ±Ð¾Ð¿ÑодÑкÑов».
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ÐбÑекÑом овеÑдÑаÑÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð´Ð¸Ð¿Ð»Ð¾Ð¼Ð½Ð¾Ð¹ ÑинанÑовое ÑабоÑÑ, ÑвлÑеÑÑÑ ÑиÑÑема ÑиÑки ÑинанÑового ÑолÑко ÑпÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ ÐÐР«ТиÑаÑполÑÑкий ÑÑÑка ÐºÐ¾Ð¼Ð±Ð¸Ð½Ð°Ñ Ñ Ð»ÐµÐ±Ð¾Ð¿ÑодÑкÑов».
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2016
ЦелÑÑ Ð²ÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ Ð±Ð°ÐºÐ°Ð»Ð°Ð²Ñа ÑвлÑеÑÑÑ ÑазÑабоÑка инÑеÑÑейÑа Ð´Ð»Ñ Ð¼Ð¾Ð±Ð¸Ð»Ñного пÑиложениÑ, иÑÑ Ð¾Ð´Ñ Ð¸Ð· ÑезÑлÑÑаÑов, полÑÑеннÑÑ Ð¿Ñи анализе даннÑÑ ÐºÐ¾Ð½ÑакÑного ÑенÑÑа ÐÐР«Ðега
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ЦелÑÑ Ð²ÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ Ð±Ð°ÐºÐ°Ð»Ð°Ð²Ñа ÑвлÑеÑÑÑ ÑазÑабоÑка инÑеÑÑейÑа Ð´Ð»Ñ Ð¼Ð¾Ð±Ð¸Ð»Ñного пÑиложениÑ, иÑÑ Ð¾Ð´Ñ Ð¸Ð· ÑезÑлÑÑаÑов, полÑÑеннÑÑ Ð¿Ñи анализе даннÑÑ ÐºÐ¾Ð½ÑакÑного ÑенÑÑа ÐÐР«Ðега
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This final qualification work is devoted to the calculation and design of a turbojet two-circuit twin-shaft aviation engine of 147 kN directional thrust based on the ÐÐ-14 prototype, a Russian 5th generation turbofan engine intended for the medium-haul narrow-body passenger aircraft ÐС-21.
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2017
Темой дипломной ÑабоÑÑ ÑвлÑеÑÑÑ Â«ÐонÑÑÑÑкÑивнÑе ÑеÑÐµÐ½Ð¸Ñ ÑÑÐµÑ ÑÑажного многокваÑÑиÑного жилого дома». ÐеÑÑо ÑÑÑоиÑелÑÑÑва г. СанкÑ-ÐеÑеÑбÑÑг, ÐÑимоÑÑкийм Ñайон, ÐÐ¾Ð½Ð½Ð¾Ð»Ð°Ñ ÑинÑкий пÑ., д. 34..
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Темой дипломной ÑабоÑÑ ÑвлÑеÑÑÑ Â«ÐонÑÑÑÑкÑивнÑе ÑеÑÐµÐ½Ð¸Ñ ÑÑÐµÑ ÑÑажного многокваÑÑиÑного жилого дома». ÐеÑÑо ÑÑÑоиÑелÑÑÑва г. СанкÑ-ÐеÑеÑбÑÑг, ÐÑимоÑÑкийм Ñайон, ÐÐ¾Ð½Ð½Ð¾Ð»Ð°Ñ ÑинÑкий пÑ., д. 34..
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