REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30
In this paper redesign process of an axial compressor of a Gas Turbine for mechanical drive is discussed together with computational results and experimental data. The goal of the project was to reduce compressor mass flow by 30% and at the same time to increase compressor specific work by about 10%...
Gespeichert in:
| Veröffentlicht in: | WIT Transactions on Ecology and the Environment 2019-01, Vol.222, p.93 |
|---|---|
| Hauptverfasser: | , , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | 93 |
| container_title | WIT Transactions on Ecology and the Environment |
| container_volume | 222 |
| creator | SEDUNIN, VIACHESLAV ALEKSEEVICH YURII MIRONOVICH BRODOV KOMAROV, OLEG VIACHESLAVOVICH Blinov, Vitaliy Leonidovich SKOROKHODOV, ALEXANDER VLADIMIROVICH SERKOV, SERGEY ALEKSANDROVICH |
| description | In this paper redesign process of an axial compressor of a Gas Turbine for mechanical drive is discussed together with computational results and experimental data. The goal of the project was to reduce compressor mass flow by 30% and at the same time to increase compressor specific work by about 10%. This could not be achieved by conventional methods such as re-staggering of Inlet Guide Vanes. Throughflow and CFD calculations were performed for redesigned versions. As a result an updated compressor was produced for the real engine and achieved design objectives. This paper shows how the swept area distribution along the compressor affects stage loading distribution and surge limits. |
| doi_str_mv | 10.2495/EQ180091 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest</sourceid><recordid>TN_cdi_proquest_miscellaneous_2255717919</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2255717919</sourcerecordid><originalsourceid>FETCH-LOGICAL-p1371-bda7b63db09019d6462240397fb5e411721f78146b6fa541275c0c5f156c9d343</originalsourceid><addsrcrecordid>eNotjl1LwzAYRoMoOObAn5BLb6p5kzdJcyOUmm6FbtG2Y7sbTT9gUN007v9vTK_Oc3F4OIQ8AnvmaOSL_YCYMQM3ZAIaRSQkwu11qwgx3t6TWQh7z1AKkIKzCXkt7Zut8vmKuowmK5ps86SgqVu-l7aqXEk3eb2gy6SqaFa4Db3o67TO3dUX7IHcDc0Y-tk_p2Sd2TpdRIWb52lSREcQGiLfNdor0XlmGJhOoeIcmTB68LJHAM1h0DGg8mpoLs1cy5a1cgCpWtMJFFPy9Pd7_Dl8n_rwu_vch7Yfx-arP5zCjnMpNWgDRpwB8oRD2g</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2255717919</pqid></control><display><type>article</type><title>REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30</title><source>Alma/SFX Local Collection</source><creator>SEDUNIN, VIACHESLAV ALEKSEEVICH ; YURII MIRONOVICH BRODOV ; KOMAROV, OLEG VIACHESLAVOVICH ; Blinov, Vitaliy Leonidovich ; SKOROKHODOV, ALEXANDER VLADIMIROVICH ; SERKOV, SERGEY ALEKSANDROVICH</creator><creatorcontrib>SEDUNIN, VIACHESLAV ALEKSEEVICH ; YURII MIRONOVICH BRODOV ; KOMAROV, OLEG VIACHESLAVOVICH ; Blinov, Vitaliy Leonidovich ; SKOROKHODOV, ALEXANDER VLADIMIROVICH ; SERKOV, SERGEY ALEKSANDROVICH</creatorcontrib><description>In this paper redesign process of an axial compressor of a Gas Turbine for mechanical drive is discussed together with computational results and experimental data. The goal of the project was to reduce compressor mass flow by 30% and at the same time to increase compressor specific work by about 10%. This could not be achieved by conventional methods such as re-staggering of Inlet Guide Vanes. Throughflow and CFD calculations were performed for redesigned versions. As a result an updated compressor was produced for the real engine and achieved design objectives. This paper shows how the swept area distribution along the compressor affects stage loading distribution and surge limits.</description><identifier>ISSN: 1746-448X</identifier><identifier>EISSN: 1743-3541</identifier><identifier>DOI: 10.2495/EQ180091</identifier><language>eng</language><publisher>Southampton: W I T Press</publisher><subject>Computer applications ; Gas turbines ; Guide vanes ; Mass flow ; Mechanical drives ; Redesign ; Stress concentration ; Time compression ; Turbocompressors</subject><ispartof>WIT Transactions on Ecology and the Environment, 2019-01, Vol.222, p.93</ispartof><rights>2019. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the associated terms available at https://www.witpress.com/elibrary .</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>SEDUNIN, VIACHESLAV ALEKSEEVICH</creatorcontrib><creatorcontrib>YURII MIRONOVICH BRODOV</creatorcontrib><creatorcontrib>KOMAROV, OLEG VIACHESLAVOVICH</creatorcontrib><creatorcontrib>Blinov, Vitaliy Leonidovich</creatorcontrib><creatorcontrib>SKOROKHODOV, ALEXANDER VLADIMIROVICH</creatorcontrib><creatorcontrib>SERKOV, SERGEY ALEKSANDROVICH</creatorcontrib><title>REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30</title><title>WIT Transactions on Ecology and the Environment</title><description>In this paper redesign process of an axial compressor of a Gas Turbine for mechanical drive is discussed together with computational results and experimental data. The goal of the project was to reduce compressor mass flow by 30% and at the same time to increase compressor specific work by about 10%. This could not be achieved by conventional methods such as re-staggering of Inlet Guide Vanes. Throughflow and CFD calculations were performed for redesigned versions. As a result an updated compressor was produced for the real engine and achieved design objectives. This paper shows how the swept area distribution along the compressor affects stage loading distribution and surge limits.</description><subject>Computer applications</subject><subject>Gas turbines</subject><subject>Guide vanes</subject><subject>Mass flow</subject><subject>Mechanical drives</subject><subject>Redesign</subject><subject>Stress concentration</subject><subject>Time compression</subject><subject>Turbocompressors</subject><issn>1746-448X</issn><issn>1743-3541</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNotjl1LwzAYRoMoOObAn5BLb6p5kzdJcyOUmm6FbtG2Y7sbTT9gUN007v9vTK_Oc3F4OIQ8AnvmaOSL_YCYMQM3ZAIaRSQkwu11qwgx3t6TWQh7z1AKkIKzCXkt7Zut8vmKuowmK5ps86SgqVu-l7aqXEk3eb2gy6SqaFa4Db3o67TO3dUX7IHcDc0Y-tk_p2Sd2TpdRIWb52lSREcQGiLfNdor0XlmGJhOoeIcmTB68LJHAM1h0DGg8mpoLs1cy5a1cgCpWtMJFFPy9Pd7_Dl8n_rwu_vch7Yfx-arP5zCjnMpNWgDRpwB8oRD2g</recordid><startdate>20190101</startdate><enddate>20190101</enddate><creator>SEDUNIN, VIACHESLAV ALEKSEEVICH</creator><creator>YURII MIRONOVICH BRODOV</creator><creator>KOMAROV, OLEG VIACHESLAVOVICH</creator><creator>Blinov, Vitaliy Leonidovich</creator><creator>SKOROKHODOV, ALEXANDER VLADIMIROVICH</creator><creator>SERKOV, SERGEY ALEKSANDROVICH</creator><general>W I T Press</general><scope>7SN</scope><scope>7ST</scope><scope>ABUWG</scope><scope>AEUYN</scope><scope>AFKRA</scope><scope>ATCPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BHPHI</scope><scope>C1K</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>PATMY</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PYCSY</scope><scope>SOI</scope></search><sort><creationdate>20190101</creationdate><title>REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30</title><author>SEDUNIN, VIACHESLAV ALEKSEEVICH ; YURII MIRONOVICH BRODOV ; KOMAROV, OLEG VIACHESLAVOVICH ; Blinov, Vitaliy Leonidovich ; SKOROKHODOV, ALEXANDER VLADIMIROVICH ; SERKOV, SERGEY ALEKSANDROVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p1371-bda7b63db09019d6462240397fb5e411721f78146b6fa541275c0c5f156c9d343</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Computer applications</topic><topic>Gas turbines</topic><topic>Guide vanes</topic><topic>Mass flow</topic><topic>Mechanical drives</topic><topic>Redesign</topic><topic>Stress concentration</topic><topic>Time compression</topic><topic>Turbocompressors</topic><toplevel>online_resources</toplevel><creatorcontrib>SEDUNIN, VIACHESLAV ALEKSEEVICH</creatorcontrib><creatorcontrib>YURII MIRONOVICH BRODOV</creatorcontrib><creatorcontrib>KOMAROV, OLEG VIACHESLAVOVICH</creatorcontrib><creatorcontrib>Blinov, Vitaliy Leonidovich</creatorcontrib><creatorcontrib>SKOROKHODOV, ALEXANDER VLADIMIROVICH</creatorcontrib><creatorcontrib>SERKOV, SERGEY ALEKSANDROVICH</creatorcontrib><collection>Ecology Abstracts</collection><collection>Environment Abstracts</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest One Sustainability</collection><collection>ProQuest Central UK/Ireland</collection><collection>Agricultural & Environmental Science Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Natural Science Collection</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>Environmental Science Database</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Environmental Science Collection</collection><collection>Environment Abstracts</collection><jtitle>WIT Transactions on Ecology and the Environment</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>SEDUNIN, VIACHESLAV ALEKSEEVICH</au><au>YURII MIRONOVICH BRODOV</au><au>KOMAROV, OLEG VIACHESLAVOVICH</au><au>Blinov, Vitaliy Leonidovich</au><au>SKOROKHODOV, ALEXANDER VLADIMIROVICH</au><au>SERKOV, SERGEY ALEKSANDROVICH</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30</atitle><jtitle>WIT Transactions on Ecology and the Environment</jtitle><date>2019-01-01</date><risdate>2019</risdate><volume>222</volume><spage>93</spage><pages>93-</pages><issn>1746-448X</issn><eissn>1743-3541</eissn><abstract>In this paper redesign process of an axial compressor of a Gas Turbine for mechanical drive is discussed together with computational results and experimental data. The goal of the project was to reduce compressor mass flow by 30% and at the same time to increase compressor specific work by about 10%. This could not be achieved by conventional methods such as re-staggering of Inlet Guide Vanes. Throughflow and CFD calculations were performed for redesigned versions. As a result an updated compressor was produced for the real engine and achieved design objectives. This paper shows how the swept area distribution along the compressor affects stage loading distribution and surge limits.</abstract><cop>Southampton</cop><pub>W I T Press</pub><doi>10.2495/EQ180091</doi><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1746-448X |
| ispartof | WIT Transactions on Ecology and the Environment, 2019-01, Vol.222, p.93 |
| issn | 1746-448X 1743-3541 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_2255717919 |
| source | Alma/SFX Local Collection |
| subjects | Computer applications Gas turbines Guide vanes Mass flow Mechanical drives Redesign Stress concentration Time compression Turbocompressors |
| title | REDESIGN OF AN AXIAL COMPRESSOR WITH MASS FLOW REDUCTION OF 30 |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-13T19%3A31%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=REDESIGN%20OF%20AN%20AXIAL%20COMPRESSOR%20WITH%20MASS%20FLOW%20REDUCTION%20OF%2030&rft.jtitle=WIT%20Transactions%20on%20Ecology%20and%20the%20Environment&rft.au=SEDUNIN,%20VIACHESLAV%20ALEKSEEVICH&rft.date=2019-01-01&rft.volume=222&rft.spage=93&rft.pages=93-&rft.issn=1746-448X&rft.eissn=1743-3541&rft_id=info:doi/10.2495/EQ180091&rft_dat=%3Cproquest%3E2255717919%3C/proquest%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2255717919&rft_id=info:pmid/&rfr_iscdi=true |