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Тема выпускной квалификационной работы: «Двухконтурный двигатель с тягой 75 кН» В данной работе произведен расчет двухвального газотурбинного двигателя тягой 75 кН по прототипу РД 33. В ходе выпускной квалификационной работы были выполнены: • Вариантный тепловой расчет двигателя • Приближенный расчет компрессора • Расчеты турбины • Произведен прочностной расчет лопатки, диска последней ступени. • Так же изучили технология шумоподавления камеры сгорания РД 33.
The 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 compressor • Calculations of the turbine • The strength calculation of the blade, the disk of the last stage, as well as the low-pressure rotor was performed. • Also studied the combustion chamber noise reduction technology of the RD 33 .
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