CN109779948B - A plasma tip clearance sealing method for improving the performance of an axial flow fan - Google Patents
A plasma tip clearance sealing method for improving the performance of an axial flow fan Download PDFInfo
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- CN109779948B CN109779948B CN201910042809.3A CN201910042809A CN109779948B CN 109779948 B CN109779948 B CN 109779948B CN 201910042809 A CN201910042809 A CN 201910042809A CN 109779948 B CN109779948 B CN 109779948B
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- 238000000034 method Methods 0.000 title claims abstract description 16
- 238000007789 sealing Methods 0.000 title claims abstract description 11
- 230000000903 blocking effect Effects 0.000 claims abstract description 4
- 230000005684 electric field Effects 0.000 claims abstract description 4
- 230000007935 neutral effect Effects 0.000 claims abstract description 4
- 239000002245 particle Substances 0.000 claims abstract description 4
- 239000011810 insulating material Substances 0.000 claims description 3
- 239000007858 starting material Substances 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 description 1
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Abstract
一种用于提高轴流风机性能的等离子式叶顶间隙密封方法,步骤为:将轴流风机的叶片和机匣更换为绝缘材料;在机匣外部设置等离子发生器,在叶片顶部安装负极,负极依次通过导线、叶轮轴引电器与等离子发生器负极接线端子相连;在与叶片顶部正对的机匣内壁上安装圆环形正极,正极通过导线与等离子发生器正极接线端子相连;启动轴流风机,启动等离子发生器,在正极与负极之间形成电场,使正极与负极之间的空气产生电离,随着叶片的高速旋转,将在叶片顶部与机匣之间的环形间隙内形成等离子体环幕,当叶片压力面的气流想要从间隙通过时,气流中的中性粒子将与等离子体环幕发生碰撞,进而对这部分气流产生阻挡效应,用以降低从间隙泄露出的气流量。
A plasma-type blade tip gap sealing method for improving the performance of an axial-flow fan. The negative electrode is connected to the negative terminal of the plasma generator through the wire and the impeller shaft lead in turn; the annular positive electrode is installed on the inner wall of the casing facing the top of the blade, and the positive electrode is connected to the positive terminal of the plasma generator through the wire; start the axial flow Fan, start the plasma generator, form an electric field between the positive electrode and the negative electrode, ionize the air between the positive electrode and the negative electrode, and with the high-speed rotation of the blade, a plasma will be formed in the annular gap between the top of the blade and the casing Ring curtain, when the airflow on the pressure surface of the blade wants to pass through the gap, the neutral particles in the airflow will collide with the plasma ring curtain, and then produce a blocking effect on this part of the airflow to reduce the amount of airflow leaking from the gap. .
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CN201910042809.3A CN109779948B (en) | 2019-01-17 | 2019-01-17 | A plasma tip clearance sealing method for improving the performance of an axial flow fan |
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CN201910042809.3A CN109779948B (en) | 2019-01-17 | 2019-01-17 | A plasma tip clearance sealing method for improving the performance of an axial flow fan |
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CN109779948A CN109779948A (en) | 2019-05-21 |
CN109779948B true CN109779948B (en) | 2021-01-05 |
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CN117948290B (en) * | 2024-03-22 | 2024-06-18 | 河北冀力重型机械设备有限公司 | Axial flow fan |
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KR100464902B1 (en) * | 2001-02-12 | 2005-01-05 | (주)에스이 플라즈마 | Apparatus for generating low temperature plasama at atmospheric pressure |
GB0411178D0 (en) * | 2004-05-20 | 2004-06-23 | Rolls Royce Plc | Sealing arrangement |
CN1793665A (en) * | 2006-01-12 | 2006-06-28 | 上海交通大学 | Low noise axial fan with rotary deflecting ring |
US7819626B2 (en) * | 2006-10-13 | 2010-10-26 | General Electric Company | Plasma blade tip clearance control |
WO2008154592A2 (en) * | 2007-06-11 | 2008-12-18 | University Of Florida Research Foundation, Inc. | Electrodynamic control of blade clearance leakage loss in turbomachinery applications |
US8282336B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system |
CN103133391A (en) * | 2011-12-01 | 2013-06-05 | 中国科学院工程热物理研究所 | Cartridge receiver processing system |
CN102913399A (en) * | 2012-11-06 | 2013-02-06 | 中国科学院工程热物理研究所 | Plasma flow control method for reducing the wake loss of a wind turbine |
CN103835888B (en) * | 2012-11-20 | 2016-05-11 | 中国科学院工程热物理研究所 | The Apparatus and system of wind energy conversion system brake |
CN104138712B (en) * | 2013-05-06 | 2016-02-24 | 孙红梅 | Wind wheel electrode discharge device |
CN103925152A (en) * | 2014-04-23 | 2014-07-16 | 哈尔滨工业大学 | Wind turbine blade based on dielectric barrier discharging plasma excitation |
JP2017053261A (en) * | 2015-09-08 | 2017-03-16 | 国立研究開発法人産業技術総合研究所 | Pressure loss reduction device for fluid machinery |
CN105673559B (en) * | 2016-04-13 | 2018-04-06 | 上海理工大学 | Efficient meridionally-accelerated axial flow fan with casing |
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Effective date of registration: 20210514 Address after: 330200 no.2377 hanghanghangcheng Avenue, high tech Zone, Nanchang City, Jiangxi Province Patentee after: Jiangxi Zhongfa Tianxin Aero Engine Technology Co.,Ltd. Address before: 110136, Liaoning, Shenyang moral and Economic Development Zone, No. 37 South Avenue moral Patentee before: SHENYANG AEROSPACE University |
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PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: A Plasma Blade Tip Gap Sealing Method for Improving the Performance of Axial Flow Fans Granted publication date: 20210105 Pledgee: CITIC Bank Nanchang branch of Limited by Share Ltd. Pledgor: Jiangxi Zhongfa Tianxin Aero Engine Technology Co.,Ltd. Registration number: Y2024980008468 |