title: ÐÐ¸ÑÐ¾ÑÐ°ÑÐ¸Ð²Ð½Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð½Ð°Ñ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ° Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 100 ÐºÐ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: Low-powered birotational turbine installation of 100 kW
Creators: name: ÐÐ°ÑÐ°Ð¼Ð¾Ð½Ð¾Ð², ÐÐ¾Ð½ÑÑÐ°Ð½ÑÐ¸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: Ð¼Ð°Ð»Ð¾ÑÐ°ÑÑ Ð¾Ð´Ð½Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð°
Ð¼Ð¸ÐºÑÐ¾ÑÑÑÐ±Ð¸Ð½Ð½ÑÐ¹ Ð³ÐµÐ½ÐµÑÐ°ÑÐ¾Ñ
Ð²ÑÐ°ÑÐ°ÑÑÐ¸Ð¹ÑÑ ÑÐ¾Ð¿Ð»Ð¾Ð²Ð¾Ð¹ Ð°Ð¿Ð¿Ð°ÑÐ°Ñ
Ð±Ð¸ÑÐ¾ÑÐ°ÑÐ¸Ð²Ð½Ð°Ñ ÑÑÑÐ±Ð¸Ð½Ð°
ÑÑÐµÐ¿ÐµÐ½Ñ ÑÐ¶Ð°ÑÐ¸Ñ
ÐºÐ¾ÑÑÑÐ¸ÑÐ¸ÐµÐ½Ñ Ð¿Ð¾Ð»ÐµÐ·Ð½Ð¾Ð³Ð¾ Ð´ÐµÐ¹ÑÑÐ²Ð¸Ñ
Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ
low flow turbine
microturbine generator
rotating nozzle apparatus
birotational turbine
compression ratio
coefficient of performance
research

description: Ð¦ÐµÐ»ÑÑ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ ÑÐ²Ð»ÑÐµÑÑÑ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð±Ð¸ÑÐ¾ÑÐ°ÑÐ¸Ð²Ð½Ð¾Ð¹ Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð¹ ÑÑÑÐ°Ð½Ð¾Ð²ÐºÐ¸ Ð¼Ð¾ÑÐ½Ð¾ÑÑÑÑ 100 ÐºÐÑ. Ð ÐºÐ°ÑÐµÑÑÐ²Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° Ð±ÑÐ»Ð° Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð° ÑÑÑÐ±Ð¸Ð½Ð° Â«ÐÐ¢Ð-100Â». Ð Ð¿ÑÐ¾ÑÐµÑÑÐµ ÑÐ°Ð±Ð¾ÑÑ Ð±ÑÐ» Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½ ÑÐ°ÑÑÐµÑ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð¹ ÑÑÐµÐ¼Ñ Ð¸ Ð²ÑÐ±ÑÐ°Ð½Ð° Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½Ð°Ñ ÑÑÐµÐ¿ÐµÐ½Ñ Ð¿Ð¾Ð²ÑÑÐµÐ½Ð¸Ñ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ. ÐÑÐ¾Ð²Ð¾Ð´Ð¸Ð»ÑÑ ÑÐ°ÑÑÐµÑ ÑÐµÐ½ÑÑÐ¾Ð±ÐµÐ¶Ð½Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°. ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ Ð¸Ð½Ð´Ð¸Ð²Ð¸Ð´ÑÐ°Ð»ÑÐ½Ð¾Ð¹ ÐºÐ°Ð¼ÐµÑÑ ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ Ñ Ð¿Ð¾ÑÐ»ÐµÐ´ÑÑÑÐ¸Ð¼ Ð¿Ð¾Ð»ÑÑÐµÐ½Ð¸ÐµÐ¼ ÐµÑ Ð³ÐµÐ¾Ð¼ÐµÑÑÐ¸ÑÐµÑÐºÐ¸Ñ ÑÐ°Ð·Ð¼ÐµÑÐ¾Ð².
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description: The purpose of this work is to design the 100 kW birotating gas-turbine unit. The turbine "MTG-100" was used fs a prototype. In the course of work the calculation of the thermal scheme was executed and optimum pressure ratio was chosen.
 Calculation of the centrifugal compressor was carried out. Calculation of an individual combustion chamber with the subsequent obtaining its geometrical sizes was carried out.
 Gasdynamic calculation of the rotating nozzle diaphragm and the impeller of birotating GTU for the purpose of obtaining the given capacities of an electric generator was given in work. 
 In the course of calculation office package of Microsoft Office applications was used. As results of calculation triangles of speeds were constructed and simulated a feather of the rotor blade. 
 In the conclusion the drawing of a longitudinal section of GTU and the drawing of the impeller with blades was executed. Calculation on durability of structural elements (the impeller with blades and rotors) by means of the ANSYS Workbench and Mathcad software packages, with the subsequent material selection and creation of charts was executed.