Results 111 to 120 of about 25,864 (144)
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ÐлекÑÑиÑеÑÐºÐ°Ñ ÑаÑÑÑ ÐолÑÑкой ÐÐС-2
2019The work presents the concept of the electrical part of the Kola NPP-2. There are analysis of the composition of the auxiliary section and selection of the scheme of the auxiliary section. The analysis of the modes of starting and self-starting of electric motors of the auxiliary section for the choice of the scheme of reserve power supply is carried ...
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 110 кÐ
2020ÐÑедÑÑÐ°Ð²Ð»ÐµÐ½Ð½Ð°Ñ ÑабоÑа поÑвÑÑена пÑоекÑиÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð°Ð²Ð¸Ð°Ñионного двигаÑÐµÐ»Ñ Ð´Ð»Ñ ÑÑеднемагиÑÑÑалÑного ÑамолеÑа на оÑнове пÑоÑоÑипа CFM56. ÐÑновнÑми паÑамеÑÑами, в болÑÑей ÑÑепени оказÑваÑÑими Ð²Ð»Ð¸Ñ ...
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 75 кÐ
2021The topic of the final qualification work: "The RD 33 turbojet engine with a thrust of 75 kN» In this paper, a two-shaft gas turbine engine with a thrust of 75 kN is calculated according to the prototype RD 33. In the course of the final qualification work, the following tasks were performed:: ⢠Thermal calculation ⢠Approximate calculation of the
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 165 кÐ
2020Ð¦ÐµÐ»Ñ ÑабоÑÑ - ÑпÑоекÑиÑоваÑÑ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ ÑÑгой 165 кРна оÑнове пÑоÑоÑипа газоÑÑÑбинного авиаÑионного двигаÑÐµÐ»Ñ ÐС â 90Ð. РабоÑа ÑоÑÑÐ¾Ð¸Ñ Ð½Ð° воÑÑми оÑновнÑÑ Ð³Ð»Ð°Ð². ÐеÑÐ²Ð°Ñ Ð³Ð»Ð°Ð²Ð° поÑвÑÑена пÑедваÑиÑел
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ÐлекÑÑоÑÑаÑиÑеÑкие ионнÑе ловÑÑки
2008РаÑÑмоÑÑÐµÐ½Ñ Ð¼Ð°ÑемаÑиÑеÑкие оÑÐ½Ð¾Ð²Ñ Ð¿ÑоекÑиÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑовÑеменнÑÑ Ð¼Ð°ÑÑ-ÑпекÑÑомеÑÑиÑеÑÐºÐ¸Ñ Ð¿ÑибоÑов Ñипа ÑлекÑÑоÑÑаÑиÑеÑÐºÐ¸Ñ Ð¸Ð¾Ð½Ð½ÑÑ Ð»Ð¾Ð²ÑÑек. ÐÑновное внимание Ñделено оÑигиналÑнÑм маÑемаÑиÑеÑки
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 150 кÐ
2020Рданной вÑпÑÑкной квалиÑикаÑионной ÑабоÑе бакалавÑа пÑÐ¸Ð²ÐµÐ´ÐµÐ½Ñ ÑезÑлÑÑаÑÑ ÑаÑÑеÑа и пÑоекÑиÑование двÑÑ ÐºÐ¾Ð½ÑÑÑного авиаÑионного двигаÑÐµÐ»Ñ ÑÑгой 150 кÐ, ÑабоÑаÑÑего на кеÑоÑине.
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ÐлекÑÑомагниÑÐ½Ð°Ñ ÑÐºÐ¾Ð»Ð¾Ð³Ð¸Ñ Ñеловека
2008РаÑÑмаÑÑиваÑÑÑÑ Ð²Ð¾Ð¿ÑоÑÑ Ð¶Ð¸Ð·Ð½ÐµÐ´ÐµÑÑелÑноÑÑи Ñеловека в ÑлекÑÑомагниÑнÑÑ Ð¿Ð¾Ð»ÑÑ ÐµÑÑеÑÑвенного и иÑкÑÑÑÑвенного пÑоиÑÑ Ð¾Ð¶Ð´ÐµÐ½Ð¸Ñ. ÐÐ·Ð»Ð¾Ð¶ÐµÐ½Ñ ÐºÐ¾Ð½ÑепÑии Ð¼ÐµÑ Ð°Ð½Ð¸Ð·Ð¼Ð¾Ð² биологиÑеÑкого дейÑÑÐ²Ð¸Ñ ÑлекÑÑомР...
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 40 кÐ
2020The subject of the graduate qualification work is âDouble-circuit engine with a 40 kN thrustâ. The aim of the presented work is the design of the aircraft engine based on the prototype AI-22. The main parameters that affect the presented calcula-tion to a greater extent are the temperature behind the combustion chamber, the degree of two-circuit ...
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 120 кÐ
2020This bachelor thesis includes calculation and engineering of a gas turbine engine CFM56-5Ð running by kerosene. Engine designed for passenger aircraft. This gas turbine engine meets the requirements for fifth-generation engines, has high power and reliability, which is necessary for high airliner lift.The explanatory note contains a description of the
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ÐоÑÑÐºÐ°Ñ ÐÐУ на оÑновании Ñипа ÑÑипод
2021РбакалавÑÑкой ÑабоÑе ÑаÑÑмаÑÑиваеÑÑÑ ÑаÑÑÐµÑ Ð²ÐµÑÑоÑнеÑгеÑиÑеÑкой ÑÑÑановки на воздейÑÑвие внеÑÐ½Ð¸Ñ Ð½Ð°Ð³ÑÑзок, Ñак же в данной ÑабоÑе бÑли ÑаÑÑÑиÑÐ°Ð½Ñ ÑÑÑойÑивоÑÑÑ ÑооÑÑÐ¶ÐµÐ½Ð¸Ñ Ð½Ð° опÑокидÑвание и
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