CN101784155B - Plasma bipolar exciting electrode - Google Patents
Plasma bipolar exciting electrode Download PDFInfo
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- CN101784155B CN101784155B CN2009100210085A CN200910021008A CN101784155B CN 101784155 B CN101784155 B CN 101784155B CN 2009100210085 A CN2009100210085 A CN 2009100210085A CN 200910021008 A CN200910021008 A CN 200910021008A CN 101784155 B CN101784155 B CN 101784155B
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Abstract
The invention relates to a device in the fluid active control technical field, in particular to a plasma bipolar exciting electrode. The technical key points thereof include that the exciting electrode is composed of a conductive electrode core with good conductivity as well as an insulating base and an insulating layer with good insulating property, part region of the conductive electrode core is covered by the insulating layer from left to right, the coverage area is 10-99%, the part of the conductive electrode core covered by the top part of the insulating layer is formed into the cathode of the bipolar electrode, and the naked part is formed into the anode of the bipolar electrode. N groups of bipolar electrodes are arranged on the insulating base in parallel at certain interval, and high potential and low potential of a high frequency high voltage power supply are respectively connected with the bipolar electrodes at the first stage and the last stage, thus forming the plasma bipolar exciting electrode. The invention can improve exciting effect, efficiency and control of plasma to fluid.
Description
Technical field
The present invention relates to a kind of device of fluid active control technical field, particularly a kind of plasma bipolar exciting electrode.
Background technology
Plasma is the 4th kind of state that material exists, and 99% material exists with plasma state in the universe.Plasma also has the characteristics of fluid except having electrology characteristic.Exactly because plasma has the characteristic of electricity and fluid simultaneously; The research of in two fields of aerospace, using plasma to carry out mobile control of plasma or even plasma propelling is carried out on a large scale, and plasma is human breakover points on the Aero-Space cause.The experimental study stage ionic medium body of present stage has been applied to aspects such as wing drag reduction, the control of wing aerofoil underlying surface layer, the raising of aerofoil stalling angle, body of revolution FLOW CONTROL by success.General plasma exciter is made up of upper and lower electrode, and wherein top electrode is exposed in the air, and bottom electrode is insulated material and covers.When high-frequency high-voltage was loaded on upper and lower electrode, the air between the upper and lower utmost point was produced plasma by ionization.The plasma excitation device directly acts on fluid, produces plasma at atmospheric environment ionic medium exciter through ionized air, and through the direction motion according to the rules of driven plasma, has reached the purpose of drive air.In the outer space, the plasma exciter directly acts on the free plasma generation thrust in outer space.Along with the research of article on plasma body FLOW CONTROL deepens continuously, the research and development of people's article on plasma body exciter are more and more paid attention to, and have proposed para-electric excitation and two kinds of incentive modes of wriggling excitation.But these two kinds of energisation modes are all very limited for the arousal effect of fluid, and usefulness is low, the big plasma progress of research that restricted of equipment cost.
Summary of the invention
The purpose of this invention is to provide a kind of plasma bipolar exciting electrode, the new mode of utilization plasma bipolarity excitation uses the plasma bipolar exciting electrode can improve arousal effect and the usefulness of plasma for fluid.
The scheme that the present invention solves the prior art problem is: ambiplasma exciting electrode, and the bipolarity plasma exciter that can design according to its characteristic.Bipolar electrode is made up of electric conductivity favorable conductive electrode cores and insulation property good insulation performance base plate and top layer.The conductive electrode core is covered covering area range 10% to 99% in part zone from left to right by top layer.The part that the conductive electrode core is covered by top layer is formed the negative pole of bipolar electrode, and exposed part has been formed the positive pole of bipolar electrode.Conductive electrode core and top layer parallelization are on insulating base.For the chosen material of bipolar electrode, also can use the composite material that has insulation and electric conductivity simultaneously.Be laid in the bipolar electrode on the insulating base by N group according to parallel at certain interval, N >=2 wherein, the high potential of high-frequency and high-voltage power supply links to each other with the last grade bipolar electrode with the first order respectively with electronegative potential, has promptly formed the plasma bipolar exciter.
Operation principle of the present invention is: N level ambiplasma exciting electrode is arranged on the insulating material according to specific parameter, and the live wire of high-frequency and high-voltage power supply and zero line put on the first order and the last grade electrode.When energized; Under operating frequency and voltage effect; Glow discharge produces between first utmost point and second utmost point; Air is produced plasma by ionization at this moment accordingly, and to second level motion, near the air in this process, driving has produced the control effect to air to plasma under the effect of voltage.Because isoionic electrology characteristic; Electric current is conducted to the negative pole of second utmost point by the positive pole of the first order; The negative pole of second utmost point and positive pole are inner conductings; This moment, there was voltage in the negative pole at the partial positive pole and the 3rd utmost point, and same discharge excitation process produces at the negative pole of the partial positive pole and the third level once more.Along with the generation of plasma and the propagation of electric current, same discharge excitation process is constantly carried out being dissipated to until electric weight and is lower than plasma exciatiaon voltage.Each time glow discharge is not only and is produced plasma and carry out the process to Atmospheric Flow control in this process, and its also is the process that energy is propagated simultaneously.
Compare with existing plasma excitation electrode; The effect of bipolarity plasma exciting electrode has obtained improving significantly; It has changed the electrode effect, single electrode has been had plasma and the effect of accepting energy take place, and isoionic electricity and fluid behaviour are given full play to and utilized to bipolar electrode; And in this process, owing to enlarged area and time of contact that plasma contacts with atmosphere, more effective energy is used for exciting of plasma and induced air.
Description of drawings
Fig. 1, for the structure construction sketch map of bipolar electrode of the present invention,
Fig. 2, bipolar electrode exciter schematic diagram for utilizing the present invention to realize,
Fig. 3, be exciter article on plasma of the present invention stream and air current control schematic diagram.
Among the figure 1, insulating base, 2, the conductive electrode core, 3, top layer, 4, high-frequency and high-voltage power supply; 5, first order bipolar electrode, 6, second level bipolar electrode, 7, third level bipolar electrode, 8, terminal bipolar electrode; 9, power line, 10, plasma, 11, air stream.
Specific embodiment
Claims (2)
1. plasma bipolar exciting electrode; Form by electric conductivity favorable conductive electrode cores (2) and insulation property good insulation performance base plate (1) and top layer (3); It is characterized in that: conductive electrode core (2) is covered by top layer (3) in part zone from left to right; Covering area range 10% to 99%; The part that conductive electrode core (2) is covered by top layer (3) is formed the negative pole of plasma bipolar exciting electrode; And exposed part has been formed the positive pole of plasma bipolar exciting electrode; The plasma bipolar exciting electrode that N group is laid on the insulating base (1) according to parallel at certain interval has promptly formed the plasma bipolar exciter, N >=2 wherein, and the high potential of high-frequency and high-voltage power supply (4) links to each other with the last grade plasma bipolar exciting electrode (8) with first order plasma bipolar exciting electrode (5) respectively with electronegative potential.
2. plasma bipolar exciting electrode according to claim 1 is characterized in that: high-frequency and high-voltage power supply (4) output frequency and voltage are adjustable.
Priority Applications (1)
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CN2009100210085A CN101784155B (en) | 2009-01-21 | 2009-01-21 | Plasma bipolar exciting electrode |
Applications Claiming Priority (1)
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CN2009100210085A CN101784155B (en) | 2009-01-21 | 2009-01-21 | Plasma bipolar exciting electrode |
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CN101784155A CN101784155A (en) | 2010-07-21 |
CN101784155B true CN101784155B (en) | 2012-05-02 |
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CN2009100210085A Expired - Fee Related CN101784155B (en) | 2009-01-21 | 2009-01-21 | Plasma bipolar exciting electrode |
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Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN104185354A (en) * | 2014-04-10 | 2014-12-03 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Dielectric barrier discharge plasma exciter and system |
CN104314690A (en) * | 2014-10-21 | 2015-01-28 | 西北工业大学 | Plasma phase-changing control air inlet passage and control method |
CN104507247B (en) * | 2014-11-05 | 2017-03-22 | 西北工业大学 | Plasma stimulator system capable of controlling position of suction peak |
CN105676293B (en) * | 2016-01-20 | 2017-12-12 | 浙江大学 | A kind of plasma focus transmitting battle array based on micro-porous electrode structure |
CN108243549B (en) * | 2018-03-15 | 2018-10-30 | 哈尔滨工业大学 | Plasma Actuator with fluting ventilation device |
CN112441057B (en) * | 2020-11-18 | 2022-01-18 | 西南交通大学 | Bidirectional plasma drag reduction braking system and use method thereof |
Citations (4)
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US7380756B1 (en) * | 2003-11-17 | 2008-06-03 | The United States Of America As Represented By The Secretary Of The Air Force | Single dielectric barrier aerodynamic plasma actuation |
CN101296842A (en) * | 2005-10-17 | 2008-10-29 | 贝尔直升机特克斯特龙有限公司 | Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
EP1995173A1 (en) * | 2007-05-25 | 2008-11-26 | The Boeing Company | Plasma flow control actuator system and method |
CN101332871A (en) * | 2007-05-25 | 2008-12-31 | 波音公司 | Airfoil trailing edge plasma flow control apparatus and method |
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2009
- 2009-01-21 CN CN2009100210085A patent/CN101784155B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7380756B1 (en) * | 2003-11-17 | 2008-06-03 | The United States Of America As Represented By The Secretary Of The Air Force | Single dielectric barrier aerodynamic plasma actuation |
CN101296842A (en) * | 2005-10-17 | 2008-10-29 | 贝尔直升机特克斯特龙有限公司 | Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
EP1995173A1 (en) * | 2007-05-25 | 2008-11-26 | The Boeing Company | Plasma flow control actuator system and method |
CN101332871A (en) * | 2007-05-25 | 2008-12-31 | 波音公司 | Airfoil trailing edge plasma flow control apparatus and method |
Non-Patent Citations (3)
Title |
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Thomas C. Corke, et al..SDBD plasma enhanced aerodynamics: concepts, optimization and applications.《Progress in Aerospace Sciences》.2007,第43卷193-217. * |
ThomasC.Corke et al..SDBD plasma enhanced aerodynamics: concepts |
李钢等.介质阻挡放电等离子体流动控制技术的研究进展.《科技导报》.2008,第26卷(第4期),87-92. * |
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