title: ÐÐ²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ ÑÑÐ³Ð¾Ð¹ 100 ÐºÐ
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð±Ð°ÐºÐ°Ð»Ð°Ð²ÑÐ°
titleType: Subtitle
title: Turbofan engine with thrust 100 kN
Creators: name: Ð¢Ð°ÑÑÐ¾Ð², Ð¡ÐµÑÐ³ÐµÐ¹
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2019
Subjects: Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
ÐÐ¸Ð³-31
Ð-30
Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð´Ð»Ñ Ð²Ð¾ÐµÐ½Ð½Ð¾Ð¹ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¸
ÑÐ¾ÑÑÐ°Ð¶Ð½Ð°Ñ ÐºÐ°Ð¼ÐµÑÐ°
gas-turbine engine
turbo-fan engine
D-30
Mig-31
engine for military aircraft

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description: Annotation
In this final qualifying work, the design of a turbo-jet aircraft gas turbine engine (GTE) with trust 100 kN, based on the D-30. 
The graduate work includes an introduction, seven chapters and a conclusion. In addition, the work includes a special part devoted to the literature review on the topic reheat champer.
The contents of the explanatory note: 
1. Variant thermal calculations of the GTE cycle, selection of the optimal variant and refinement of the selected option; 
2. Gas-dynamic calculations of the compressor, combustion chambers and turbines; 
3. Strength calculations of the last stage of the turbine, compilation of the vibration diagram of the blade. 
In the process of designing the engine, in comparison with the prototype, the combustion chamber was shortened, and the flow part of the turbine was redesigned. At the same time, it was possible to maintain high efficiency and economy of the prototype engine.