CN104507247A - Plasma stimulator system capable of controlling position of suction peak - Google Patents

Plasma stimulator system capable of controlling position of suction peak Download PDF

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Publication number
CN104507247A
CN104507247A CN201410616929.7A CN201410616929A CN104507247A CN 104507247 A CN104507247 A CN 104507247A CN 201410616929 A CN201410616929 A CN 201410616929A CN 104507247 A CN104507247 A CN 104507247A
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China
Prior art keywords
exciter
relay
emitter
suction peak
plasma
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CN201410616929.7A
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Chinese (zh)
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CN104507247B (en
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郝江南
高超
王玉玲
武斌
索涛
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Northwestern Polytechnical University
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Northwestern Polytechnical University
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Abstract

The present invention relates to a plasma stimulator system capable of controlling the position of a suction peak, wherein each bipolar plasma stimulator system comprises an emitter pole and a receiver pole, the emitter pole is connected with an electrode of a high voltage power supply by a switch, the receiver pole is connected with another electrode of the high voltage power supply by a switch, each switch is controlled by a relay, and each relay is controlled by a controller. Compared with existing simulators, the plasma stimulator system capable of controlling the position of the suction peak can achieve the effect of changing the position of the suction peak of the simulator through changing the position in the simulator where the plasma emitter pole appears at the first time. Such a simulator may form a suction peak continuously moving downstream in a large area on a surface of an object. With such action, the flowing of air flow can be effectively controlled.

Description

A kind of suction peak position confined plasma exciter system
Technical field
The invention belongs to fluid active flow control devices, relate to a kind of suction peak position confined plasma exciter system, be specifically a kind of can the equipment that control effectively of plasma exciter suction peak position.
Background technology
In order to increase the control effects of Plasma Actuator for flowing, increasing the large metering methods such as exciter area, raising operating voltage, change exciter structure and being conducted extensive research.The control effects of effective raising exciter means that plasma flow control technique can further effectively be used in actual production life.For aircraft, technique is particularly crucial.Effective flowing control can improve aeroplane performance, and reduce resistance, increase lift, the load improving aircraft reduces its energy consumption.For opportunity of combat, adopt the aircraft of effective plasma flow control to expand flight envelope, form new tactics, promote the operational efficiency of aircraft.
But compared with practical application, current Plasma Actuator also needs to promote for performance, solve the problems such as the exciter voltage faced at present is high, control range is less, control position is limited.
Summary of the invention
The technical problem solved
In order to avoid the deficiencies in the prior art part, the present invention proposes a kind of suction peak position confined plasma exciter system, more effectively controls the flowing of air-flow at body surface, the especially air current flow of aircraft surfaces.
Technical scheme
A kind of suction peak position confined plasma exciter system, is characterized in that comprising controller 1, high voltage source 2, multiple ambiplasma exciter 3, launching relay group 4 and receiving relay group 5; Each ambiplasma exciter comprises emitter and receiving pole, emitter passes through an Electrode connection of a switch and high voltage source 2, receiving pole and another Electrode connection by a switch and high voltage source 2, each switch is controlled by a relay, and each relay is controlled by controller 1.
Described high voltage source 2 adopt can the AC power of activated plasma, AC-DC coupling power supply or nanosecond power supply.
A kind of method utilizing described system change exciter first to occur the position of plasma emission pole, it is characterized in that: the suction peak position produced as required, the emitter of ambiplasma exciter or the relay of receiving pole that are positioned at the suction peak position of generation is connected by controller, make its conducting, connect the receiving pole of ambiplasma exciter or the relay of emitter of more than this ambiplasma exciter next stage simultaneously, make its conducting; The relay of the emitter after conducting or the relay work of receiving pole, make the normally opened contact controlling emitter and receiving pole close, and connects the excitation power supply circuit with high voltage source 2, produces suction peak in the suction peak position needing to produce.
Beneficial effect
A kind of suction peak position confined plasma exciter system that the present invention proposes, compared with existing exciter, there is the position of plasma emission pole in suction peak position confined plasma exciter system, can reach the effect changing exciter suction peak position by changing exciter first.This kind of exciter can form a suction peak constantly moved to downstream at body surface on a large scale.Under this kind of effect, air-flow can be controlled by effectively carrying out flowing.
Accompanying drawing explanation
Fig. 1: suction peak position confined plasma exciter system schematic diagram
Fig. 2: suction peak position confined plasma exciter system operating diagram (1# position, 2 grades of suction peaks)
Fig. 3: suction peak position confined plasma exciter system operating diagram (2# position, 2 grades of suction peaks)
1-controller, 2-power supply, 3-ambiplasma exciter, 4-emitter switch, 5-receiving pole switch, 7-1# emitter, 8-2# receiving pole, 9-1# position suction airstream, 10-2# emitter, 11-2# position suction airstream 12-3# receiving pole, J-relay, K-switch.
Embodiment
Now in conjunction with the embodiments, the invention will be further described for accompanying drawing:
The embodiment of the present invention is by controller 1, power supply 2, ambiplasma exciter 3, emitter switch group 4, receiving pole switches set 5.Wherein power supply can adopt AC power, AC-DC coupling power supply, nanosecond power supply etc. various can the power supply of activated plasma.Plasma excitation 3 adopts bipolarity plasma excitation device.According to concrete user demand, exciter can be processed to various shape.Emitter switch group 4 receiving pole switches set 5 is made up of relay J and K switch.
Controller 1 is switched on or switched off by certain or certain the several relay controlled in emitter relay group 4 and receiving pole relay group 5, and corresponding emitter or receiving pole and excitation power supply 2 are connected.
1st relay of emitter switch group 4 and the 2nd relay of receiving pole switches set 5,1st switch of control emitter switch group 4 and receiving pole switches set 5 the 2nd switch are closed, between 1# emitter 7 to 2# receiving pole 8, now just defines the ambiplasma exciter of 2 grades.After emitter 7, now have suction airstream 9 produce an obvious suction peak, now exciter can form an obvious downward suction for air-flow, and this suction is proportional to applied voltage.
Then, the 1st switch of control emitter switch group 4 is closed, controls its 2nd switch simultaneously and close, disconnect receiving pole switches set 5 the 2nd switch, closed disconnection receiving pole switches set 5 the 3rd switch.This just defines the ambiplasma exciter of 2 grades between 2# emitter 10 and 3# receiving pole 12, and now the position at suction peak is moved to 2# emitter 10 position and produces suction airstream 11 at this, carries out downwards by that analogy.According to different demands, the ambiplasma exciter of 3 grades or multistage can be selected according to actual needs.
The suction peak position confined plasma exciter course of work is: controller 1 controls the switch of power supply 2, provides folding and disconnection are carried out in instruction control to emitter switch group 4 and receiving pole switches set 5 simultaneously.By upper switch and the lower position of the switch poor, ambiplasma exciter is formed at transmitting and receiving interpolar, along with switches set does not stop to change position, the position of activated plasma is constantly changing first, so just guide the continuous occurrence positions change in suction peak, form one group continuously to the suction peak of downstream movement at object plane.

Claims (3)

1. a suction peak position confined plasma exciter system, is characterized in that comprising controller (1), high voltage source (2), multiple ambiplasma exciter (3) and launching relay group (4) and receiving relay group (5); Each ambiplasma exciter comprises emitter and receiving pole, emitter passes through an Electrode connection of a switch and high voltage source (2), receiving pole and another Electrode connection by a switch and high voltage source (2), each switch is controlled by a relay, and each relay is controlled by controller (1).
2. suction peak position confined plasma exciter system according to claim 1, is characterized in that: described high voltage source (2) adopt can the AC power of activated plasma, AC-DC coupling power supply or nanosecond power supply.
3. the method utilizing system described in claim 1 to carry out suction peak position control, it is characterized in that: the suction peak position produced as required, the emitter of ambiplasma exciter or the relay of receiving pole that are positioned at the suction peak position of generation is connected by controller, make its conducting, connect the receiving pole of ambiplasma exciter or the relay of emitter of more than this ambiplasma exciter next stage simultaneously, make its conducting; The relay of the emitter after conducting or the relay work of receiving pole, make the normally opened contact controlling emitter and receiving pole close, connect the excitation power supply circuit with high voltage source (2), produce suction peak in the suction peak position needing to produce.
CN201410616929.7A 2014-11-05 2014-11-05 Plasma stimulator system capable of controlling position of suction peak Active CN104507247B (en)

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CN104507247B CN104507247B (en) 2017-03-22

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110636685A (en) * 2019-09-10 2019-12-31 空气动力学国家重点实验室 Wall drag reduction mechanism based on plasma generator
CN110933832A (en) * 2019-07-16 2020-03-27 中国人民解放军空军工程大学 Single power supply driven array type plasma synthetic jet flow control device and flow control method

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101784155A (en) * 2009-01-21 2010-07-21 郝江南 Plasma bipolar exciting electrode
CN102114910A (en) * 2010-12-14 2011-07-06 大连海事大学 Plasma wing flow control method
JP2011238385A (en) * 2010-05-06 2011-11-24 Tokyo Metropolitan Univ Induced flow control surface plasma actuator
JP2012180799A (en) * 2011-03-02 2012-09-20 Nissan Motor Co Ltd Gas flow control device of internal combustion engine
JP2013155673A (en) * 2012-01-30 2013-08-15 Daihatsu Motor Co Ltd Internal combustion engine
CN103410680A (en) * 2013-06-19 2013-11-27 中国科学院电工研究所 Plasma control device and method for blades of wind driven generator
CN103661929A (en) * 2013-12-19 2014-03-26 南京航空航天大学 Plasma unmanned aerial vehicle
CN203872422U (en) * 2014-04-10 2014-10-08 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

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101784155A (en) * 2009-01-21 2010-07-21 郝江南 Plasma bipolar exciting electrode
JP2011238385A (en) * 2010-05-06 2011-11-24 Tokyo Metropolitan Univ Induced flow control surface plasma actuator
CN102114910A (en) * 2010-12-14 2011-07-06 大连海事大学 Plasma wing flow control method
JP2012180799A (en) * 2011-03-02 2012-09-20 Nissan Motor Co Ltd Gas flow control device of internal combustion engine
JP2013155673A (en) * 2012-01-30 2013-08-15 Daihatsu Motor Co Ltd Internal combustion engine
CN103410680A (en) * 2013-06-19 2013-11-27 中国科学院电工研究所 Plasma control device and method for blades of wind driven generator
CN103661929A (en) * 2013-12-19 2014-03-26 南京航空航天大学 Plasma unmanned aerial vehicle
CN203872422U (en) * 2014-04-10 2014-10-08 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

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
王斌等: "新型等离子体激励器对流动分离点控制", 《实验流体力学》 *
郝江南等: "双极性等离子体激励器流动控制特性研究", 《实验流体力学》 *
郝江南等: "多级双极性等离子体激励器加速气流的实验研究", 《中国科学: 物理学 力学 天文学》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110933832A (en) * 2019-07-16 2020-03-27 中国人民解放军空军工程大学 Single power supply driven array type plasma synthetic jet flow control device and flow control method
CN110636685A (en) * 2019-09-10 2019-12-31 空气动力学国家重点实验室 Wall drag reduction mechanism based on plasma generator
CN110636685B (en) * 2019-09-10 2021-09-28 空气动力学国家重点实验室 Wall drag reduction mechanism based on plasma generator

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