Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova

In order to understand the vapor injection flow characteristics of two-stage rotary compressor in the course of compression, a mathematical model based on mass conservation equation, energy equation and thermodynamic identity was established and proved by P-V diagram testing results. Some useful...

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Main Author: M. A. Fedorova
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2021-12-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
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Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2021/%D0%A2.%205,%20%E2%84%96%204%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/65-74%20%D0%99.%20%D0%A1.%20%D0%A5%D1%83,%20%D0%A5.%20%D0%A6%D0%B7.%20%D0%92%D1%8D%D0%B9,%20%D0%91.%20%D0%AE%D0%B9%20[%D0%B8%20%D0%B4%D1%80.].pdf
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author M. A. Fedorova
author_facet M. A. Fedorova
author_sort M. A. Fedorova
collection DOAJ
description In order to understand the vapor injection flow characteristics of two-stage rotary compressor in the course of compression, a mathematical model based on mass conservation equation, energy equation and thermodynamic identity was established and proved by P-V diagram testing results. Some useful conclusions about pressure in the intermediate chamber and mass flow of vapor injection in the course of compression were also given out. The results show that, gas backflow between the intermediate chamber and the vapor injection channel is an important defection of two-stage rotary compressor which can be solved by the application of injection valve in vapor injection channel. The injection valve can obviously reduce the gas backflow and the power loss in the course of compression while increasing the pressure fluctuation in the intermediate chamber. Experiments show that the COP of two-stage rotary compressor with the injection valve increased by over 2% in ASHRAE/T working condition.
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institution Kabale University
issn 2588-0373
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language English
publishDate 2021-12-01
publisher Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
record_format Article
series Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
spelling doaj-art-1dc5396fd7bf4c0bb7c49076e2150dbe2025-02-02T20:05:20ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2021-12-0154657410.25206/2588-0373-2021-5-4-65-74Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. FedorovaM. A. Fedorova0https://orcid.org/0000-0002-0899-6303Omsk State Technical UniversityIn order to understand the vapor injection flow characteristics of two-stage rotary compressor in the course of compression, a mathematical model based on mass conservation equation, energy equation and thermodynamic identity was established and proved by P-V diagram testing results. Some useful conclusions about pressure in the intermediate chamber and mass flow of vapor injection in the course of compression were also given out. The results show that, gas backflow between the intermediate chamber and the vapor injection channel is an important defection of two-stage rotary compressor which can be solved by the application of injection valve in vapor injection channel. The injection valve can obviously reduce the gas backflow and the power loss in the course of compression while increasing the pressure fluctuation in the intermediate chamber. Experiments show that the COP of two-stage rotary compressor with the injection valve increased by over 2% in ASHRAE/T working condition.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2021/%D0%A2.%205,%20%E2%84%96%204%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/65-74%20%D0%99.%20%D0%A1.%20%D0%A5%D1%83,%20%D0%A5.%20%D0%A6%D0%B7.%20%D0%92%D1%8D%D0%B9,%20%D0%91.%20%D0%AE%D0%B9%20[%D0%B8%20%D0%B4%D1%80.].pdfrefrigeration machinerotary compressorsteam injectionmathematical modelexperimentverification
spellingShingle M. A. Fedorova
Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
refrigeration machine
rotary compressor
steam injection
mathematical model
experiment
verification
title Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
title_full Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
title_fullStr Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
title_full_unstemmed Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
title_short Hu Y. S., Wei H. J., Yu B., Yang O. X., Wang J., Wu J. Research on the vapor injection of two-stage rotary compressor / trans. from Engl. M. A. Fedorova
title_sort hu y s wei h j yu b yang o x wang j wu j research on the vapor injection of two stage rotary compressor trans from engl m a fedorova
topic refrigeration machine
rotary compressor
steam injection
mathematical model
experiment
verification
url https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2021/%D0%A2.%205,%20%E2%84%96%204%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/65-74%20%D0%99.%20%D0%A1.%20%D0%A5%D1%83,%20%D0%A5.%20%D0%A6%D0%B7.%20%D0%92%D1%8D%D0%B9,%20%D0%91.%20%D0%AE%D0%B9%20[%D0%B8%20%D0%B4%D1%80.].pdf
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