Results 151 to 157 of about 581 (157)

Газотурбинная установка мощностью 2,3 МВт

2019
This work contain the method for creating a 2.3 MW gas-turbine plant based on the already existing prototype TB3-117. A general description of the prototype installation and some design features are given. The calculation of the thermal scheme, the approximate calculation of the compressor, the calculation of the combustion chamber, the gas-dynamic ...
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Газотурбинная установка мощностью 17 МВт

2019
In this work the design technique and calculation of the 17 MW gas-turbine unit on the basis of already existing prototype of "AL-31ST" is explained. In work the general description of unit is given, calculation of the thermal scheme, approximate calculation of the axial compressor, calculation of a combustion chamber, gasodynamic calculation of a ...
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Газотурбинная установка мощностью 16 МВт

2017
Данная работа посвящена разработке газотурбинной установки мощностью 16 МВт для привода нагнетателя природного газа. Топливом данной установки является топливный газ.
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Газотурбинная установка мощностью 6,3 МВт

2019
In this work, the calculation of a 6,3 MW gas turbine unit. Calculation was based on 6,3 MW gas turbine engine NK-12ST. This calculation includes thermal scheme of GTU calculation, approximate axial compressor calculation, calculation of the combustion chamber, gasdynamic calculation of gas turbine, flow twist of last stage and approximate calculation ...
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Газотурбинная установка мощностью 18 МВт

The purpose of this bachelors final qualifying work is to design a gas turbine plant based on the AL-31ST prototype. Tasks that are performed during the research of a gas turbine engine: 1. Study of the design features of the AL-31ST prototype. 2. Thermal calculation of the engine with the selection of the optimal option. 3.
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Газотурбинная установка мощностью 1,4 МВт

Целью данной выпускной квалификационной работы бакалавра является проектирование газотурбинной установки на основе прототипа ГТУ-ТВ3-117. В работе изложена методика создания газотурбинной уст
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Газотурбинная установка мощностью 65 МВт

This bachelors graduation thesis is devoted to the development and design of a stationary gas turbine engine with a capacity of 65 MW. This design includes thermal calculation, approximate calculation of the compressor, calculation of the combustion chamber, gas dynamic calculation, strength calculation, description and main characteristics of the ...
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