title: ÐÐ¾Ð´ÐµÑÐ½Ð¸Ð·Ð¸ÑÐ¾Ð²Ð°Ð½Ð½ÑÐ¹ ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½ÑÐ¹ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ ÑÐ¾ÑÑÐ°Ð¶Ð½Ð¾Ð¹ ÐºÐ°Ð¼ÐµÑÐ¾Ð¹ Ð Ð-33
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: Upgraded turbojet dual engine with afterburner RD-33
Creators: name: ÐÐ»ÑÐ±ÑÐ°Ð½Ð´Ñ, ÐÐµÐ½Ð¸Ñ
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: ÑÐ°ÑÑÐµÑ
Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½ÑÐ¹ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ ÑÐ¾ÑÑÐ°Ð¶Ð½Ð¾Ð¹ ÐºÐ°Ð¼ÐµÑÐ¾Ð¹
Ð Ð-33
ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
calculation
gas turbine engine
turbojet dual-circuit engine with afterburner
RD-33
aircraft engine

description: ÐÑÐ¾Ð¸Ð·Ð²Ð¾Ð´Ð¸ÑÑÑ ÑÐ°ÑÑÑÑ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° Ð Ð-33.
ÐÐ°Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð¿ÑÐ¸Ð¼ÐµÐ½ÑÑÑÑ Ð½Ð° ÑÐ²ÐµÑÑÐ·Ð²ÑÐºÐ¾Ð²ÑÑ Ð¼Ð½Ð¾Ð³Ð¾ÑÐµÐ»ÐµÐ²ÑÑ Ð¸ÑÑÑÐµÐ±Ð¸ÑÐµÐ»ÑÑ, Ð½Ð°Ð¿ÑÐ¸Ð¼ÐµÑ, ÐÐ¸Ð-29. Ð Ð´Ð°Ð½Ð½Ð¾Ð¼Ñ ÐºÐ»Ð°ÑÑÑ Ð¾ÑÐ½Ð¾ÑÑÑÑÑ ÑÐ°ÐºÐ¸Ðµ ÑÐ¾Ð²ÑÐµÐ¼ÐµÐ½Ð½ÑÐµ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ð¸ ÐºÐ°Ðº GE F404, GE F414. 
ÐÐ²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð Ð-33 Ð¸, Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ð½ÑÐ¹ Ð½Ð° ÐµÐ³Ð¾ Ð±Ð°Ð·Ðµ Ð Ð-33ÐÐ, ÑÐ²Ð»ÑÑÑÑÑ Ð½Ð°Ð¸Ð±Ð¾Ð»ÐµÐµ ÑÐ°ÑÐ¿ÑÐ¾ÑÑÑÐ°Ð½ÑÐ½Ð½ÑÐ¼Ð¸ Ð² ÑÐ²Ð¾ÐµÐ¼ ÐºÐ»Ð°ÑÑÐµ Ð¼Ð¾ÑÐ½Ð¾ÑÑÐ¸ Ð¸ Ð°ÐºÑÐ¸Ð²Ð½Ð¾ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·ÑÑÑÑÑ Ð½Ðµ ÑÐ¾Ð»ÑÐºÐ¾ Ð½Ð° ÑÐµÑÑÐ¸ÑÐ¾ÑÐ¸Ð¸ Ð Ð¾ÑÑÐ¸Ð¸ Ð¸ Ð² ÑÑÑÐ°Ð½Ð°Ñ Ð¡ÐÐ, Ð½Ð¾ Ð¸ Ð² Ð´ÑÑÐ³Ð¸Ñ ÑÑÑÐ°Ð½Ð°Ñ ÑÐ°ÐºÐ¸Ñ ÐºÐ°Ðº ÐÐ½Ð´Ð¸Ñ Ð¸ ÐÐ¸ÑÐ°Ð¹. ÐÐ¾ÑÐ°Ð±Ð¾ÑÐºÐ° Ð¸ Ð¼Ð¾Ð´ÐµÑÐ½Ð¸Ð·Ð°ÑÐ¸Ñ ÑÑÐ¸Ñ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹ ÑÐ²Ð»ÑÑÑÑÑ ÑÑÑÐ°ÑÐµÐ³Ð¸ÑÐµÑÐºÐ¸Ð¼Ð¸ Ð·Ð°Ð´Ð°ÑÐ°Ð¼Ð¸ Ð´Ð»Ñ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¾ÑÑÐºÐ¸Ñ Ð±ÑÑÐ¾. ÐÑÑÐ¾Ð´Ñ Ð¸Ð· Ð¿ÐµÑÐµÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ð³Ð¾, ÑÐµÐ¼Ñ Ð¼Ð¾Ð¶Ð½Ð¾ ÑÑÐ¸ÑÐ°ÑÑ Ð°ÐºÑÑÐ°Ð»ÑÐ½Ð¾Ð¹.
ÐÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð²ÐºÐ»ÑÑÐ°ÐµÑ Ð² ÑÐµÐ±Ñ:
1. ÐÐ°ÑÐ¸Ð°Ð½ÑÐ½ÑÐ¹ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð¹ ÑÐ°ÑÑÐµÑ ÑÐ¸ÐºÐ»Ð° ÐÐ¢Ð, Ð²ÑÐ±Ð¾Ñ Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½ÑÑ Ð´Ð°Ð½Ð½ÑÑ;
2. ÐÐ°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ°ÑÑÑÑ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°;
3. ÐÐ°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ°ÑÑÑÑ ÐºÐ°Ð¼ÐµÑÑ ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ;
4. ÐÐ°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ°ÑÑÑÑ ÑÑÑÐ±Ð¸Ð½Ñ;
5. Ð Ð°ÑÑÐµÑ Ð½Ð° Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÑ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸ Ð¸ Ð´Ð¸ÑÐºÐ° ÑÐ¾ÑÐ¾ÑÐ° ÑÑÑÐ±Ð¸Ð½Ñ;
6. Ð¡Ð¿Ð¾ÑÐ¾Ð±Ñ ÑÐ½Ð¸Ð¶ÐµÐ½Ð¸Ñ ÑÑÐ¼Ð° ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ.
Ð ÑÐ°Ð±Ð¾ÑÐµ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¾ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¿Ð¾ Ð·Ð½Ð°ÑÐ¸ÑÐµÐ»ÑÐ½Ð¾Ð¼Ñ ÑÐ²ÐµÐ»Ð¸ÑÐµÐ½Ð¸Ñ ÑÑÐ³Ð¸ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð·Ð° ÑÑÐµÑ ÑÐ²ÐµÐ»Ð¸ÑÐµÐ½Ð¸Ñ ÑÐ°ÑÑÐ¾Ð´Ð° Ð²Ð¾Ð·Ð´ÑÑÐ°, Ð¿ÑÐ¾ÑÐ¾Ð´ÑÑÐµÐ³Ð¾ ÑÐµÑÐµÐ· ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ.
description: The calculation of parameters of the aviation turbojet engine based on the prototype RD-33.
This engine will be used on supersonic light fighters, for example, MiG-29. This class includes such modern engines as the GE F404, GE F414.
The RD-33 engine and the RD-33MK built on its base are the most common in its power class and are actively used not only in Russia and in the CIS countries, but also in other countries such as India and China. Refinement and modernization of these engines are priority objectives for design offices. Based on the above, the topic can be considered relevant.
Graduation qualification work includes following:
1. Variant thermal calculation of the gas turbine engine cycle, selection of optimal data;
2. Gas dynamic calculation of the compressor;
3. Gas dynamic calculation of the combustion chamber;
4. Gas dynamic calculation of the turbine;
5. Calculation of the strength of the blade and the rotor disk of the turbine;
6. Ways to reduce the noise of a turbojet engine.
Research conducted a study of a significant increase in engine thrust by increasing the flow rate of air passing through the compressor.