title: ÐÐ°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ° Ð´Ð»Ñ Ð¿ÑÐ¸Ð²Ð¾Ð´Ð° Ð½Ð°Ð³Ð½ÐµÑÐ°ÑÐµÐ»Ñ Ð¿ÑÐ¸ÑÐ¾Ð´Ð½Ð¾Ð³Ð¾ Ð³Ð°Ð·Ð° Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 16 ÐÐÑ
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: Gas turbine installation for a 16 MW natural gas blower drive
Creators: name: ÐÐ²Ð°Ð½Ð¾Ð², ÐÐ»ÐµÐºÑÐ°Ð½Ð´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: 2020
Subjects: Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
ÑÑÑÐ±Ð¸Ð½Ð°
ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ
ÐºÐ°Ð¼ÐµÑÐ° ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ
ÑÐ¸Ð»Ð¾Ð²Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð°
Ð»Ð¾Ð¿Ð°ÑÐºÐ°
Ð´Ð¸ÑÐº
ÑÐ¾ÑÐ¾Ñ
gas-turbine engine
turbine
compressor
combustion chamber
power turbine
shovel
disc
rotor

description: Ð Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÐµ Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸ Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 16 ÐÐÐ¢. Ð ÐºÐ°ÑÐµÑÑÐ²Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° Ð¸ÑÐ¿Ð¾Ð»ÑÐ·ÑÐµÑÑÑ ÐÐ¢Ð ÐÐ-16 Ð¡Ð¢. Ð Ð¿ÑÐ¾ÑÐµÑÑÐµ Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ð¸Ñ ÑÐ°Ð±Ð¾ÑÑ Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ ÑÐ°ÑÑÐµÑÐ° Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² ÑÐ°Ð±Ð¾ÑÐµÐ³Ð¾ Ð¿ÑÐ¾ÑÐµÑÑÐ° Ð² ÑÐ°ÑÐ°ÐºÑÐµÑÐ½ÑÑ ÑÐµÑÐµÐ½Ð¸ÑÑ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ñ A2GTP. ÐÑÐ¾Ð°Ð½Ð°Ð»Ð¸Ð·Ð¸ÑÐ¾Ð²Ð°Ð² ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ Ð±ÑÐ» Ð²ÑÐ±ÑÐ°Ð½ Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½ÑÐ¹ ÑÐµÐ¶Ð¸Ð¼ ÑÐ°Ð±Ð¾ÑÑ ÑÑÑÐ±Ð¸Ð½Ñ Ð¸ Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð¹ ÑÑÐµÐ¼Ñ. ÐÐ°Ð»ÐµÐµ Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ¾Ð² Ð½Ð¸Ð·ÐºÐ¾Ð³Ð¾ Ð¸ Ð²ÑÑÐ¾ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ. Ð Ð°ÑÑÐµÑ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ¾Ð² Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼ Ð´Ð»Ñ ÑÐ¾Ð³Ð¾, ÑÑÐ¾Ð±Ñ Ð¿ÑÐ¸ÑÑÑÐ¿Ð¸ÑÑ Ðº Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¾Ð¼Ñ ÑÐ°ÑÑÐµÑÑ ÑÑÑÐ±Ð¸Ð½Ñ, Ð² ÑÐ¾Ð´Ðµ ÐºÐ¾ÑÐ¾ÑÐ¾Ð³Ð¾ Ð±ÑÐ»Ð¸ Ð¿Ð¾Ð»ÑÑÐµÐ½Ñ Ð³Ð°Ð±Ð°ÑÐ¸ÑÐ½ÑÐµ Ð´Ð°Ð½Ð½ÑÐµ Ð´Ð»Ñ Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ð¸Ñ ÑÐµÑÑÐµÐ¶Ð° Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ. ÐÐ° ÑÑÐ´Ñ Ñ ÑÑÐ¸Ð¼ Ð±ÑÐ»Ð¾ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¾ Ð¿ÑÐ¾ÑÐ¸Ð»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ½Ð¾Ð¹ ÑÐ°ÑÑÐ¸, Ð¾Ð¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ð¸Ðµ Ð¼Ð¾ÑÐ½Ð¾ÑÑÐ¸ Ð¸ ÐÐÐ, Ð° ÑÐ°ÐºÐ¶Ðµ ÑÐ°ÑÑÐµÑ Ð·Ð°ÐºÑÑÑÐºÐ¸ Ð¿Ð¾ÑÐ¾ÐºÐ° Ð¿Ð¾ÑÐ»ÐµÐ´Ð½ÐµÐ¹ ÑÑÑÐ¿ÐµÐ½Ð¸ ÑÑÑÐ±Ð¸Ð½Ñ Ð¸ Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ñ Ð¿ÑÐ¾ÑÐ¸Ð»Ð¸ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸ Ð¿Ð¾ Ð¿ÑÑÐ¸ ÑÐ°ÑÑÑÐ¸ÑÐ°Ð½Ð½ÑÐ¼ ÑÐµÑÐµÐ½Ð¸ÑÐ¼. ÐÐ¾ Ð¿ÑÐ¾ÑÐ¸Ð»ÑÐ¼ ÑÐµÑÐµÐ½Ð¸Ð¹ Ð¸ Ð¸Ñ ÑÐµÐ½ÑÑÐ°Ð¼ Ð¼Ð°ÑÑ Ð±ÑÐ»Ð° Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ð° Ð¾Ð±ÑÐµÐ¼Ð½Ð°Ñ Ð¼Ð¾Ð´ÐµÐ»Ñ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸. ÐÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ Ð½Ð° Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÑ ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ¾Ð² ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ (ÑÐ°Ð±Ð¾ÑÐµÐ¹ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸, Ð´Ð¸ÑÐºÐ°, ÑÐ¾ÑÐ¾ÑÐ°) Ñ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼ ANSYS Workbench Ð¸ MathCad. ÐÑÐ¾Ð±Ð¾Ðµ Ð²Ð½Ð¸Ð¼Ð°Ð½Ð¸Ðµ ÑÐ´ÐµÐ»ÑÐµÑÑÑ Ð¾Ð¿Ð¸ÑÐ°Ð½Ð¸Ñ ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ¾Ð² ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸: ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾Ñ Ð²ÑÑÐ¾ÐºÐ¾Ð³Ð¾ Ð¸ Ð½Ð¸Ð·ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ, ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ½ÑÐµ ÑÑÑÐ±Ð¸Ð½Ñ, ÑÐ¸Ð»Ð¾Ð²Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð°, Ð¿Ð¾Ð´ÑÐ¸Ð¿Ð½Ð¸ÐºÐ¸, Ð¿ÑÑÐºÐ¾Ð²Ð¾Ðµ ÑÑÑÑÐ¾Ð¹ÑÑÐ²Ð¾. ÐÐ°Ð²ÐµÑÑÐ°ÐµÑ ÑÑÑ ÑÐ°Ð±Ð¾ÑÑ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ° ÑÐ°ÑÑÐµÑÐ° ÑÐµÑÑÑÑÐ° ÑÐ°Ð±Ð¾ÑÑ Ð¿Ð¾Ð´ÑÐ¸Ð¿Ð½Ð¸ÐºÐ¾Ð²ÑÑ Ð¾Ð¿Ð¾Ñ ÑÐ¾ÑÐ¾ÑÐ°.
description: In this work, a gas turbine unit with a capacity of 16 MW is calculated. As a prototype, the gas turbine engine NK-16 ST is used. In the process of performing work, the calculation of the calculation of the parameters of the working process in characteristic sections of the flowing part of the gas turbine engine using the A2GTP program was performed. After analyzing the results, the optimal mode of operation of the turbine was selected and the thermal circuit was calculated. Next, the calculation of low and high pressure compressors. The calculation of compressors is necessary in order to start the gas-dynamic calculation of the turbine, during which dimensional data were obtained for constructing the engine drawing. Along with this, profiling of the flow part, determination of power and efficiency, as well as calculation of the swirl of the flow of the last stage of the turbine were carried out, and the profiles of the blade were constructed for five calculated sections. Using the profiles of the sections and their centers of mass, a volumetric model of the blade was constructed. Strength analysis of structural elements (rotor blades, discs, rotors) was performed using ANSYS Workbench and MathCad programs. Particular attention is paid to the description of the installation elements: high and low pressure compressor, compressor turbines, power turbine, bearings, starting device. The work is completed by the method of calculating the service life of the bearing support of the rotor.