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Improving the Efficiency of Fuel Combustion in a 2.5-MW Contact-Type Gas Turbine Engine Using the Cross-Flow Plasma-Fuel Nozzle
The analysis of the possibilities of using the cross-flow plasma-fuel nozzle for supporting stable combustion of gaseous fuel in a combustion chamber of the contact-type gas turbine engine with steam injection is presented. Experimental studies of the plasma-fuel nozzle were carried out, which prove...
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Published in: | IEEE transactions on plasma science 2022-06, Vol.50 (6), p.1675-1680 |
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creator | Serbin, Serhiy I. Vilkul, Serhiy V. Patlaichuk, Volodymyr M. |
description | The analysis of the possibilities of using the cross-flow plasma-fuel nozzle for supporting stable combustion of gaseous fuel in a combustion chamber of the contact-type gas turbine engine with steam injection is presented. Experimental studies of the plasma-fuel nozzle were carried out, which proved the stability of its operation in a wide range of changes in the flow rates of plasma feedstock air. Indicators of the efficiency of the thermal scheme of the contact-type gas turbine engine as well as the characteristics of a low-emission combustion chamber with plasma assistance are obtained. |
doi_str_mv | 10.1109/TPS.2022.3173561 |
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Experimental studies of the plasma-fuel nozzle were carried out, which proved the stability of its operation in a wide range of changes in the flow rates of plasma feedstock air. Indicators of the efficiency of the thermal scheme of the contact-type gas turbine engine as well as the characteristics of a low-emission combustion chamber with plasma assistance are obtained.</description><identifier>ISSN: 0093-3813</identifier><identifier>EISSN: 1939-9375</identifier><identifier>DOI: 10.1109/TPS.2022.3173561</identifier><identifier>CODEN: ITPSBD</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Combustion ; Combustion chambers ; Cross flow ; Electron tubes ; Emission ; Engines ; Flow rates ; Flow velocity ; Fuel combustion ; Fuels ; gas turbine engine ; Gas turbine engines ; Gas turbines ; Gaseous fuels ; Nozzles ; plasma activation ; Plasma temperature ; plasma-assisted combustion ; Plasmas ; Turbines</subject><ispartof>IEEE transactions on plasma science, 2022-06, Vol.50 (6), p.1675-1680</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. 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Indicators of the efficiency of the thermal scheme of the contact-type gas turbine engine as well as the characteristics of a low-emission combustion chamber with plasma assistance are obtained.</description><subject>Combustion</subject><subject>Combustion chambers</subject><subject>Cross flow</subject><subject>Electron tubes</subject><subject>Emission</subject><subject>Engines</subject><subject>Flow rates</subject><subject>Flow velocity</subject><subject>Fuel combustion</subject><subject>Fuels</subject><subject>gas turbine engine</subject><subject>Gas turbine engines</subject><subject>Gas turbines</subject><subject>Gaseous fuels</subject><subject>Nozzles</subject><subject>plasma activation</subject><subject>Plasma temperature</subject><subject>plasma-assisted combustion</subject><subject>Plasmas</subject><subject>Turbines</subject><issn>0093-3813</issn><issn>1939-9375</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNo9kM1Lw0AQxRdRsFbvgpcFzxtnd5tu9ijF1kLVgikew24yqSn5qNlEaS_-6ya2enowvPdm5kfINQePc9B34fLVEyCEJ7mS_pifkAHXUjMtlX9KBgBaMhlweU4unNsA8JEPYkC-58W2rj6zck2bd6QPaZrFGZbxjlYpnbaY00lV2NY1WVXSrKSGCs9nT2_duGxM3LBwt0U6M46GbW2zsqso172s3F_npK6cY9O8-qLL3LjCsN_e52q_z_GSnKUmd3h11CFZTR_CySNbvMzmk_sFi7mvG4bKJjIRkBqpAuBoVSyl9VPFgQsIrLXJyGjrAyJPweg4SbRBHCcKbWB1LIfk9tDbffvRomuiTdXWZbcyEmPVgQpAyc4FB1fc31xjGm3rrDD1LuIQ9ZijDnPUY46OmLvIzSGSIeK_XSulAiXkDxiOeZE</recordid><startdate>20220601</startdate><enddate>20220601</enddate><creator>Serbin, Serhiy I.</creator><creator>Vilkul, Serhiy V.</creator><creator>Patlaichuk, Volodymyr M.</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7U5</scope><scope>8FD</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0002-3423-2681</orcidid><orcidid>https://orcid.org/0000-0002-9506-6023</orcidid><orcidid>https://orcid.org/0000-0001-6849-2492</orcidid></search><sort><creationdate>20220601</creationdate><title>Improving the Efficiency of Fuel Combustion in a 2.5-MW Contact-Type Gas Turbine Engine Using the Cross-Flow Plasma-Fuel Nozzle</title><author>Serbin, Serhiy I. ; Vilkul, Serhiy V. ; Patlaichuk, Volodymyr M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c159t-e7bd3d20fa37801eb7c33b5f7101208bbbd4a9b50ee1f0a9cdd9aee6d7eb8b9c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Combustion</topic><topic>Combustion chambers</topic><topic>Cross flow</topic><topic>Electron tubes</topic><topic>Emission</topic><topic>Engines</topic><topic>Flow rates</topic><topic>Flow velocity</topic><topic>Fuel combustion</topic><topic>Fuels</topic><topic>gas turbine engine</topic><topic>Gas turbine engines</topic><topic>Gas turbines</topic><topic>Gaseous fuels</topic><topic>Nozzles</topic><topic>plasma activation</topic><topic>Plasma temperature</topic><topic>plasma-assisted combustion</topic><topic>Plasmas</topic><topic>Turbines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Serbin, Serhiy I.</creatorcontrib><creatorcontrib>Vilkul, Serhiy V.</creatorcontrib><creatorcontrib>Patlaichuk, Volodymyr M.</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Xplore</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>IEEE transactions on plasma science</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Serbin, Serhiy I.</au><au>Vilkul, Serhiy V.</au><au>Patlaichuk, Volodymyr M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Improving the Efficiency of Fuel Combustion in a 2.5-MW Contact-Type Gas Turbine Engine Using the Cross-Flow Plasma-Fuel Nozzle</atitle><jtitle>IEEE transactions on plasma science</jtitle><stitle>TPS</stitle><date>2022-06-01</date><risdate>2022</risdate><volume>50</volume><issue>6</issue><spage>1675</spage><epage>1680</epage><pages>1675-1680</pages><issn>0093-3813</issn><eissn>1939-9375</eissn><coden>ITPSBD</coden><abstract>The analysis of the possibilities of using the cross-flow plasma-fuel nozzle for supporting stable combustion of gaseous fuel in a combustion chamber of the contact-type gas turbine engine with steam injection is presented. 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subjects | Combustion Combustion chambers Cross flow Electron tubes Emission Engines Flow rates Flow velocity Fuel combustion Fuels gas turbine engine Gas turbine engines Gas turbines Gaseous fuels Nozzles plasma activation Plasma temperature plasma-assisted combustion Plasmas Turbines |
title | Improving the Efficiency of Fuel Combustion in a 2.5-MW Contact-Type Gas Turbine Engine Using the Cross-Flow Plasma-Fuel Nozzle |
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