Results 101 to 110 of about 9,844 (146)
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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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2021
The work is devoted to research in the field of energy efficiency of structural solutions of the building envelope. The aim of the work was to select a rational constructive solution for the enclosing structure in both economic and energy-efficient aspects.
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The work is devoted to research in the field of energy efficiency of structural solutions of the building envelope. The aim of the work was to select a rational constructive solution for the enclosing structure in both economic and energy-efficient aspects.
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ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ ÑÑгой 78кÐ
2020ÐÐ°Ð½Ð½Ð°Ñ ÑабоÑа поÑвÑÑена пÑоекÑиÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑного ÑÑÑбоÑеакÑивного двигаÑелÑ, моÑноÑÑÑÑ 78 кÐ,пÑедназнаÑенного Ð´Ð»Ñ ÑÑеднемагиÑÑÑалÑнÑÑ Ð¿Ð°ÑÑажиÑÑÐºÐ¸Ñ Ð¿ÐµÑевозок.
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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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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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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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ÐеÑод опÑимизаÑии ÑигналÑнÑÑ ÐºÐ¾Ð½ÑÑÑÑкÑий ÐÐÐ
2020Ð ÑабоÑе пÑедлагаеÑÑÑ Ð¼ÐµÑод опÑимизаÑии ÑигналÑнÑÑ ÐºÐ¾Ð½ÑÑÑÑкÑий квадÑаÑÑÑной амплиÑÑдной манипÑлÑÑии (ÐÐÐ), в коÑоÑом паÑамеÑÑами опÑимизаÑии ÑвлÑÑÑÑÑ Ð²ÐµÐ»Ð¸ÑÐ¸Ð½Ñ ÐºÐ²Ð°Ð´ÑаÑÑÑ ÑигналÑнÑÑ ÑоÑек.
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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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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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ÐвиаÑионнÑй двÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 90кÐ
2021In this work, the design of a turbofan aircraft gas turbine engine with thrust of 90 kN was performed. GE F404 chosen as a prototype. Graduation qualifying work includes an introduction, seven chapters and a conclusion. In addition, the work includes a special part devoted to spectrum-diagnostics of defects in GTE rotors.
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