Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition
The outlet flow fields of a low-speed repeating-stage compressor with bowed stator stages are measured with five-hole probe under the near stall condition when the rotor/stator axial gap varies. The performances of the straight stator stages are investigated and compared to those of the bowed stator...
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Veröffentlicht in: | Chinese journal of aeronautics 2008-06, Vol.21 (3), p.215-222 |
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creator | Huawei, Lu Fu, Chen Jilin, Wan Zhongqi, Wang |
description | The outlet flow fields of a low-speed repeating-stage compressor with bowed stator stages are measured with five-hole probe under the near stall condition when the rotor/stator axial gap varies. The performances of the straight stator stages are investigated and compared to those of the bowed stator stages. The results show that using bowed stator stages could alleviate the flow separation at both upper and low corners of the suction surface and the endwalls, and decrease the losses along the flow passage as well as the outlet flow angle. As the rotor/stator axial gap decreases, although the diffusion capacity of the compressor increases obviously, the outlet flow field in the straight stator stages deteriorates quickly. By contrast, little changes occur in the bowed stator stages, indicating that as the rotor/stator axial gap decreases, improved performance is achieved in the bowed stator stages. |
doi_str_mv | 10.1016/S1000-9361(08)60028-X |
format | Article |
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The performances of the straight stator stages are investigated and compared to those of the bowed stator stages. The results show that using bowed stator stages could alleviate the flow separation at both upper and low corners of the suction surface and the endwalls, and decrease the losses along the flow passage as well as the outlet flow angle. As the rotor/stator axial gap decreases, although the diffusion capacity of the compressor increases obviously, the outlet flow field in the straight stator stages deteriorates quickly. By contrast, little changes occur in the bowed stator stages, indicating that as the rotor/stator axial gap decreases, improved performance is achieved in the bowed stator stages.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/S1000-9361(08)60028-X</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>bowed stator ; compressor ; corner separation ; near stall condition ; rotor/stator axial gap ; 压缩机 ; 弓形定子 ; 转子/定子轴向缝隙</subject><ispartof>Chinese journal of aeronautics, 2008-06, Vol.21 (3), p.215-222</ispartof><rights>2008 Chinese Journal of Aeronautics</rights><rights>Copyright © Wanfang Data Co. Ltd. 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By contrast, little changes occur in the bowed stator stages, indicating that as the rotor/stator axial gap decreases, improved performance is achieved in the bowed stator stages.</description><subject>bowed stator</subject><subject>compressor</subject><subject>corner separation</subject><subject>near stall condition</subject><subject>rotor/stator axial gap</subject><subject>压缩机</subject><subject>弓形定子</subject><subject>转子/定子轴向缝隙</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNqFkE1P3DAQhnNopVLan1DJ6qEfh9Bx7CTOqYJtF5AQHCgSN8uxx7uGrL3YWRb-Pc4u4trTSKPnmdH7FsUXCkcUaPPrmgJA2bGG_gDxswGoRHn7rjh4W38oPqZ0B8C6lsJBEedD2JK5w8GQ89U6hkdcoR9J_0xOwhYNuR7VGOI0FpiI80SRWcggppTXWzcuyR9nLcbJOn5yaiCnap3IjTcYySWqnTsM2fLGjS74T8V7q4aEn1_nYXEz__tvdlZeXJ2ez44vSs15M5aM1lYoBcxYVfWNFVZUTYXGUsZZ1TZtb4xAw0WjwSIK5FpwWmNvoIau7dhh8X1_d6u8VX4h78Im-vxRLu-feokVgAAGwDP5bU_m_A8bTKNcuaRxGJTHsEmSsbrmjE5gvQd1DClFtHId3UrFZ0lBTv3LXf9yKlqCkLv-5W32fu89zHkfHUaZtEOv0biIepQmuP9e-Pr6eRn84sHlOL3S99YNKKuW87ZrW_YCGZSaqg</recordid><startdate>20080601</startdate><enddate>20080601</enddate><creator>Huawei, Lu</creator><creator>Fu, Chen</creator><creator>Jilin, Wan</creator><creator>Zhongqi, Wang</creator><general>Elsevier Ltd</general><general>School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>W92</scope><scope>~WA</scope><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>20080601</creationdate><title>Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition</title><author>Huawei, Lu ; Fu, Chen ; Jilin, Wan ; Zhongqi, Wang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c446t-315f8aa03dfa2b6f8f8262edf13432767bdd8ed486c0fee8e4c8415ebd0509793</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>bowed stator</topic><topic>compressor</topic><topic>corner separation</topic><topic>near stall condition</topic><topic>rotor/stator axial gap</topic><topic>压缩机</topic><topic>弓形定子</topic><topic>转子/定子轴向缝隙</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Huawei, Lu</creatorcontrib><creatorcontrib>Fu, Chen</creatorcontrib><creatorcontrib>Jilin, Wan</creatorcontrib><creatorcontrib>Zhongqi, Wang</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库-工程技术</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>Chinese journal of aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Huawei, Lu</au><au>Fu, Chen</au><au>Jilin, Wan</au><au>Zhongqi, Wang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition</atitle><jtitle>Chinese journal of aeronautics</jtitle><addtitle>Chinese Journal of Aeronautics</addtitle><date>2008-06-01</date><risdate>2008</risdate><volume>21</volume><issue>3</issue><spage>215</spage><epage>222</epage><pages>215-222</pages><issn>1000-9361</issn><abstract>The outlet flow fields of a low-speed repeating-stage compressor with bowed stator stages are measured with five-hole probe under the near stall condition when the rotor/stator axial gap varies. The performances of the straight stator stages are investigated and compared to those of the bowed stator stages. The results show that using bowed stator stages could alleviate the flow separation at both upper and low corners of the suction surface and the endwalls, and decrease the losses along the flow passage as well as the outlet flow angle. As the rotor/stator axial gap decreases, although the diffusion capacity of the compressor increases obviously, the outlet flow field in the straight stator stages deteriorates quickly. By contrast, little changes occur in the bowed stator stages, indicating that as the rotor/stator axial gap decreases, improved performance is achieved in the bowed stator stages.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/S1000-9361(08)60028-X</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
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source | Access via ScienceDirect (Elsevier); EZB-FREE-00999 freely available EZB journals |
subjects | bowed stator compressor corner separation near stall condition rotor/stator axial gap 压缩机 弓形定子 转子/定子轴向缝隙 |
title | Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition |
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