title: ÐÐ²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ ÑÑÐ³Ð¾Ð¹ 120 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: Two-circuit engine with 120 kN thrust
Creators: name: Ð¢ÑÐ¸ÑÐ¾Ð½Ð¾Ð²Ð°, ÐÐ»ÐµÐ½Ð°
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: 2020
Subjects: Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
Ð¡FM56-5B
ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½Ñ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
Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ.
gas turbine engine
CFM56-5B
turbojet engine
turbojet two-circuit engine
aircraft engine.

description: Ð Ð´Ð°Ð½Ð½Ð¾Ð¹ Ð²ÑÐ¿ÑÑÐºÐ½Ð¾Ð¹ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÐµ Ð±Ð°ÐºÐ°Ð»Ð°Ð²ÑÐ° Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ñ ÑÐ°ÑÑÑÑ Ð¸ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ CFM56-5Ð, ÑÐ°Ð±Ð¾ÑÐ°ÑÑÐµÐ³Ð¾ Ð½Ð° ÐºÐµÑÐ¾ÑÐ¸Ð½Ðµ.Ð¡Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð¿ÑÐµÐ´Ð½Ð°Ð·Ð½Ð°ÑÐ°ÐµÑÑÑ Ð´Ð»Ñ Ð¿Ð°ÑÑÐ°Ð¶Ð¸ÑÑÐºÐ¸Ñ ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ¾Ð². ÐÐ°Ð½Ð½ÑÐ¹ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð¾ÑÐ²ÐµÑÐ°ÐµÑ ÑÑÐµÐ±Ð¾Ð²Ð°Ð½Ð¸ÑÐ¼, Ð¿ÑÐµÐ´ÑÑÐ²Ð»ÑÐµÐ¼ÑÐ¼ Ðº Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÑÐ¼ Ð¿ÑÑÐ¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ,Ð¾Ð±Ð»Ð°Ð´Ð°ÐµÑ Ð²ÑÑÐ¾ÐºÐ¾Ð¹ Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ Ð¸ Ð½Ð°Ð´ÑÐ¶Ð½Ð¾ÑÑÑÑ, ÑÑÐ¾ Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼Ð¾ Ð´Ð»Ñ Ð²ÑÑÐ¾ÐºÐ¾Ð¹ Ð¿Ð¾Ð´ÑÐµÐ¼Ð½Ð¾Ð¹ ÑÐ¸Ð»Ñ Ð°Ð²Ð¸Ð°Ð»Ð°Ð¹Ð½ÐµÑÐ°.ÐÐ¾ÑÑÐ½Ð¸ÑÐµÐ»ÑÐ½Ð°Ñ Ð·Ð°Ð¿Ð¸ÑÐºÐ° ÑÐ¾Ð´ÐµÑÐ¶Ð¸Ñ Ð² ÑÐµÐ±Ðµ Ð¾Ð¿Ð¸ÑÐ°Ð½Ð¸Ðµ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ,ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð¹ ÑÐ°ÑÑÐµÑ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ, ÑÐ°ÑÑÐµÑÑ Ð²ÐµÐ½ÑÐ¸Ð»ÑÑÐ¾ÑÐ°, Ð¾ÑÐ½Ð¾Ð²Ð½ÑÑ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð²Ð½ÑÑ Ð¸ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, ÑÑÐ¾ÑÐ½ÐµÐ½Ð½ÑÐ¹ Ð¿Ð¾ÑÑÑÐ¿ÐµÐ½ÑÐ°ÑÑÐ¹ ÑÐ°ÑÑÐµÑ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ° Ð½Ð° ÑÑÐµÐ´Ð½ÐµÐ¼ ÑÐ°Ð´Ð¸ÑÑÐµ, ÑÑÑÐ±Ð¸Ð½Ñ Ð¿Ð¾ ÑÑÐµÐ´Ð½ÐµÐ¼Ñ Ð´Ð¸Ð°Ð¼ÐµÑÑÑ, Ð³ÐµÐ¾Ð¼ÐµÑÑÐ¸ÑÐµÑÐºÐ¸Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² ÑÑÑÐ¿ÐµÐ½ÐµÐ¹ ÑÑÑÐ±Ð¸Ð½Ñ, ÑÐ°ÑÑÐµÑ Ð·Ð°ÐºÑÑÑÐºÐ¸ Ð¿Ð¾ÑÐ¾ÐºÐ° Ð½Ð° Ð¿Ð¾ÑÐ»ÐµÐ´Ð½ÐµÐ¹ ÑÑÑÐ¿ÐµÐ½Ð¸ ÑÑÑÐ±Ð¸Ð½Ñ,ÑÐ°ÑÑÑÑ Ð½Ð° Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÑ ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ¾Ð² ÑÑÑÐ±Ð¸Ð½Ñ Ð½Ð¸Ð·ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ, Ð° ÑÐ°Ðº Ð¶Ðµ ÑÐ¿ÐµÑÐ¸Ð°Ð»ÑÐ½ÑÑ ÑÐ°ÑÑÑ Ð½Ð° ÑÐµÐ¼Ñ ÑÐµÑÐ½Ð¾Ð»Ð¾Ð³Ð¸Ð¸ Ð¸Ð·Ð³Ð¾ÑÐ¾Ð²Ð»ÐµÐ½Ð¸Ñ ÑÐ°Ð±Ð¾ÑÐµÐ¹ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸ Ð¿ÐµÑÐ²Ð¾Ð¹ ÑÑÑÐ¿ÐµÐ½Ð¸ ÑÑÑÐ±Ð¸Ð½Ñ. Ð ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐµ ÑÐ°ÑÑÑÑÐ° Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð¼Ñ Ð´Ð¾ÑÑÐ¸Ð³Ð»Ð¸ Ð½ÑÐ¶Ð½ÑÑ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð²,Ð¿Ð¾ÑÑÐ¸ Ð½Ðµ Ð¸Ð·Ð¼ÐµÐ½Ð¸Ð² Ð´Ð¸Ð°Ð¼ÐµÑÑÐ°Ð»ÑÐ½ÑÐµ ÑÐ°Ð·Ð¼ÐµÑÑ Ð²Ð½ÑÑÑÐµÐ½Ð½ÐµÐ³Ð¾ ÐºÐ¾Ð½ÑÑÑÐ°, ÑÐ¾ÑÑÐ°Ð½Ð¸Ð² Ð¿ÑÐ¸ ÑÑÐ¾Ð¼ ÑÐ¾ÑÐ¾ÑÐ¸Ð¹ ÐºÐ¾ÑÑÑÐ¸ÑÐ¸ÐµÐ½Ñ Ð¿Ð¾Ð»ÐµÐ·Ð½Ð¾Ð³Ð¾ Ð´ÐµÐ¹ÑÑÐ²Ð¸Ñ Ð¸ ÑÐ´ÐµÐ»ÑÐ½ÑÐ¹ ÑÐ°ÑÑÐ¾Ð´.
description: This 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 design of aircraft engine, thermal calculation of the motor parameters, the calculations of fan, main design and gas-dynamic parameters of the compressor, gradually refined the calculation of the compressor at the average radius of the turbine by the average diameter, the geometric parameters of turbine stages, the calculation of the spin flow at the last stage of the turbine, the strength calculation of the elements of the low pressure turbine, and a special piece on the theme of manufacturing technology of the rotor blade of the first turbine stage.As result of calculating the engine, we achieved the necessary parameters, almost without changing the diameter of the internal contour, while maintaining a good efficiency and specific consumption.