title: ÐÐ°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ° Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 14 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 unit capacity of 14 MW
Creators: name: ÐÐ°Ð½ÑÐµÐ², Ð Ð¾Ð¼Ð°Ð½
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¸Ð½Ð½Ð°Ñ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ°
Ð¿Ð°ÑÐ¾ÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ°
gas turbine installation
steam turbine installation

description: Ð¦ÐµÐ»ÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ ÑÐ²Ð»ÑÐ»Ð¾ÑÑ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸ Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 14ÐÐÑ. ÐÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð¾Ð¼ Ð²ÑÐ±ÑÐ°Ð½ ÐÐ-12Ð¡Ð¢.
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ÐÐ° Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð¸Ð¸ Ð²ÑÑÐµÐ¸Ð·Ð»Ð¾Ð¶ÐµÐ½Ð½Ð¾Ð³Ð¾, ÑÐ°Ð·ÑÐ°Ð±Ð°ÑÑÐ²Ð°ÐµÑÑÑ ÑÐµÑÑÐµÐ¶ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸. Ð ÐºÐ¾Ð½ÐµÑÐ½Ð¾Ð¼ Ð¸ÑÐ¾Ð³Ðµ Ð¿ÑÐ¾Ð²ÐµÑÐºÑ Ð½Ð° Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÑ Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ðµ ANSYS Ð¿ÑÐ¾ÑÐ¾Ð´ÑÑ ÑÐ°ÐºÐ¸Ðµ ÑÐ»ÐµÐ¼ÐµÐ½ÑÑ ÐºÐ°Ðº Ð»Ð¾Ð¿Ð°ÑÐºÐ°, Ð´Ð¸ÑÐº Ð¸ ÑÐ¾ÑÐ¾Ñ ÑÐ¸Ð»Ð¾Ð²Ð¾Ð¹ ÑÑÑÐ±Ð¸Ð½Ñ.
ÐÐ¿Ð¸ÑÑÐ²Ð°ÐµÑÑÑ ÐºÐ¾Ð½Ð²ÐµÑÑÐ°ÑÐ¸Ñ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð² ÑÑÐ°ÑÐ¸Ð¾Ð½Ð°ÑÐ½ÑÐ¹.
description: The purpose of this work was to design a gas turbine plant with a capacity of 14 MW. The prototype selected NK-12ST.
In the process of doing the work, the thermal circuit is calculated, after which the optimum degree of pressure increase in the compressor is selected.
The calculation of the axial compressor is given, the most suitable number of compressor steps is selected.
Next, the combustion chamber is calculated to obtain its geometric dimensions and various coefficients.
The gas-dynamic calculation of the flow part of the CT and CT for approximate construction is performed. The optimal number of steps, the height of the blades of the first and last steps is determined. The flow twist is calculated, with the help of which the velocity triangles are built, which allow you to draw a profile. After constructed a geometric model of the working blade of the last stage.
Based on the above, an installation drawing is being developed. Ultimately, such elements as the blade, disk and rotor of the power turbine pass the ANSYS strength test.
Conversion of the aircraft engine to the stationary one is described.