The turbofan jet engine with an afterburner AL-31F with thrust 80 kN
| Jazyk: | ruština |
|---|---|
| Rok vydání: | 2022 |
| Předmět: |
turbofan aircraft engine
двÑÑ ÐºÐ¾Ð½ÑÑÑнÑй авиаÑионнÑй двигаÑÐµÐ»Ñ axial compressor turbine компÑеÑÑÐ¾Ñ prototype AL-31F ÑÑÑбоÑеакÑивнÑй ÑÑÑбина afterburner двигаÑÐµÐ»Ñ ÐºÐ°Ð¼ÐµÑа ÑгоÑÐ°Ð½Ð¸Ñ Ð¿ÑоÑоÑип ÐÐ-31 Ñ ÑоÑÑÐ°Ð¶Ð½Ð°Ñ ÐºÐ°Ð¼ÐµÑа ÑгоÑÐ°Ð½Ð¸Ñ turbojet engine combustor |
| DOI: | 10.18720/spbpu/3/2022/vr/vr22-2991 |
| Popis: | Тема вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ: «ТÑÑбоÑеакÑивнÑй двÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑоÑÑажной камеÑой ÑгоÑÐ°Ð½Ð¸Ñ ÐÐ-31Ф Ñ ÑÑгой 80 клРданной ÑабоÑе пÑоизведен ÑаÑÑÐµÑ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑного ÑÑÑбоÑеакÑивного двигаÑÐµÐ»Ñ Ñ ÑоÑÑажной камеÑой ÑгоÑÐ°Ð½Ð¸Ñ Ð¿Ð¾ пÑоÑоÑÐ¸Ð¿Ñ ÐÐ-31Ф.Ð Ñ Ð¾Ð´Ðµ вÑпÑÑкной квалиÑикаÑионной ÑабоÑе вÑполнен ÑаÑÑеÑ:Тепловой ÑÑ ÐµÐ¼Ñ.ÐÑиближеннÑй ÑаÑÑÐµÑ ÐºÐ¾Ð¼Ð¿ÑеÑÑоÑа.РаÑÑÐµÑ ÑÑÑбинÑ.РаÑÑÐµÑ ÐºÐ°Ð¼ÐµÑÑ ÑгоÑаниÑ.ÐÑоÑноÑÑной ÑаÑÑÐµÑ Ð»Ð¾Ð¿Ð°Ñки, диÑка поÑледней ÑÑÑпени и ÑаÑÑÐµÑ ÑоÑоÑа на виибÑонадежноÑÑÑ.ÐпиÑана конÑÑÑÑкÑÐ¸Ñ Ð´Ð²Ð¸Ð³Ð°ÑелÑ.РаÑÑмоÑÑено ÑиÑÑема Ð¾Ñ Ð»Ð°Ð¶Ð´ÐµÐ½Ð¸Ñ Ð¿Ð¾Ð´Ñипников. Bachelor thesis: «The turbofan jet engine with an afterburner AL-31F with thrust 80 kN». In the following thesis the calculation of an AL-31F prototype afterburning turbofan aircraft jet engine was performed.In the course of the graduation work following operations were carried out:Thermal calculation.Approximate calculation of the axial compressor.The combustor calculation.Turbine calculation.Strength calculation of the turbine blade and disc; vibration resistance calculation of the rotor.The design of the engine is described.The bearing cooling system was considered. |
| Databáze: | OpenAIRE |
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