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IRJET - Optical Emission Technique for Understanding the Spark Gap Discharge and Life Time Analysis
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 02 | Feb 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 2633 OpticalemissiontechniqueforunderstandingtheSparkgapDischarge andlifetimeanalysis CSReddy1 1AdamascienceandTechnologyUniversity, Adama,Ethiopia. ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - This paper presents the Optical Emission Spectroscopy(OES)techniquetostudytheSparkgapdischarge in Argon, Nitrogen and helium gasses at 0-2 kg/cm2 pressure range. The life time is also estimated for the gas ambiance for varyingpressureconditions.Basedonthelifetimeprofiles,the plasmatemperatureandelectrondensityaredeterminedbythe intensity ratio of emission lines of excited atoms. The obtained resultsareinagreementoverawideelectrondensityrange108- 1015 cm-3. Key Words: Spark gap, Breakdown, spectroscopy, plasma temperature,electrondensity. 1. INTRODUCTION One of the most conventional high peak power switching deviceisthesparkgap.Thesparkgaphasmultipleadvantage touseasaswitchinpulsedpowercircuitduetoitssimplicity, wideoperatingvoltageandcurrentrange,highdv/dt.Oneof themajordrawbackswithrepetitivepulsedpowersparkgapis recovery of spark gap voltage. The lower pressure spark gap recover greater than their breakdown voltage of first pulse undercertaincondition,whichiscalled“overrecovery”[1,2]. Tounderstandthedischargepropertiesthemeasurementof electrondensityandtemperatureisessential. There are two major factors influences the insulation characteristicsofgasswitch.Oneistherateofdecreaseinthe gas temperature and the other is the vanishing of electron followingtheextinctionofarccurrent,thevolumebetweenthe twoelectrodesisfilledwithhotdecayingplasmainwhichthe degreeofionizationisrapidlydecreasing.Butthemetalhotgas remainforarelativelylongtimeandiscooledbytheheatflow to the surrounding ambient gas and the electrodes, the recovery characteristics are governed entirely on the gas temperature[3]. It is essential to understand the local temperature variation due to plasma formation during breakdown process and influenceofvariousspeciesformedduetoconstitutionofthe mediumontherecoveryvoltageprocesshastobeascertained. Havingknownallthis,inthepresentstudy,anattempthasbeen made to understand the mechanism of spark gap discharge under the influence of different gas discharge. The emission spectra, plasma temperature and electron density are also investigated. 2. EXPERIMENTALSETUP Figure 1 shows the experimental set up for the emission spectroscopy measurements with spark gap chamber. The supply voltage (0-230 V, AC) was stepped up using a transformerandfedtoavoltagedoublerscircuit.Thecapacitor was charged through the voltage doublers circuit and dischargedthroughthesparkgapwhichwasconnectedacross thechamber. Animpulsegeneratorconsistsofacapacitorthatischargedto the required voltage and discharged through a circuit. The circuitparameterscanbeadjustedtogiveanimpulsevoltageof the desired shapes. An equivalent circuit of an Experimental setupisshowninFigure2,wherethecapacitorCG(10000pf)is chargedfromaDCsourceuntilthesparkgapbreaksdown.The voltage is then impressed upon the object using a capacitor havingcapacitanceCL(1200pf).Thewaveshapingresistors,Rf (416Ω)andRt (10kΩ),controlthefrontandtailoftheimpulse voltage available across CL, respectively. Overall, the wave shapeisdeterminedbythevaluesofthegeneratorcapacitance (CG),theloadcapacitance(CL),andthewavecontrolresistances, RfandRt.Ifthetailtime,Tt,issufficientlygreaterthanthefront time,Tf,andthetotalloadcapacitance,CL,islessthan1/5ofthe generator capacitance, CG(i.e., stage capacitance/number of stages), then an approximation to the wave shape can be determinedfrom Theoutputvoltagewaveformcanbedefined accuratelyby 3. AnalysisofOpticalEmissionSignalduringSpark gapdischargeprocess: TheOpticalemissionspectroscopy(OES)Techniqueisused tostudythebehaviorofsparkgapdischargewith
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 02 | Feb 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 2634 Figure-1:ExperimentalSetup Nitrogen, Argon and Helium gasses from zero 2 kg/cm2 pressurerange.Animpulsevoltage(doubleexponentialpulse withafronttimeof1.2usandtailtimeof50us)isappliedtothe sparkgapofwhichelectrodesareofrogowskyprofiletypeand thickness of 15mm having an inter electrode gap of 10mm. Applied voltage is measured using a CuSo4resistive divider havingdivisionratioof1800:1.Opticalemissionduringspark gapdischargeondifferentgassesiscollected,usingafiberlens withafocallength150mmanditiscoupledtoaspectrometer (Oceanoptics,USB2000)usingamultimodeopticalfiberwitha corediameterof400um. -50 0 50 100 0 10 20 30 40 50 Voltage(kV) Time (us) Figure-2:Voltagepulseappliedtothesparkgap Anattemptwasmadetoestimatetemporaldistributionof plasmatemperaturefromthelife-timeprofile.Fig3,4and5 showstheopticalemissionspectraofArgon,Nitrogenand Heliumgasambienceat2kg/cm2pressure. 300 400 500 600 700 800 900 0 100 200 300 400 500 600 700 ArII ArII ArI ArI ArII Ar 2 Kg/cm 2 Wavelength(nm) Intensity(arbs) Figure-3:Opticalemissionspectraobtainedduringthespark gapdischargeintheArgonambienceat2kg/cm2 300 400 500 600 700 800 900 0 100 200 300 400 500 NII NII NII Intensity(arbs) Wavelength(nm) N 2 Kg/cm2 NI Figure-4:Opticalemissionspectraobtainedduringthespark gapdischargeintheNitrogenambienceat2kg/cm2.
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 02 | Feb 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 2635 300 400 500 600 700 800 900 0 100 200 300 400 500 600 700 HeI HeII HeI Intensity(arbs) Wavelength(nm) He 2 Kg/cm2 Figure-5:Opticalemissionspectraobtainedduringthespark gapdischargeintheHeliumambienceat2kg/cm2. 4. LifetimeResults: Life-timeprofileofaparticularemissionwavelength,givesthe instantaneousvaluesofintensityandfromwhichtemperature can be estimated based on Boltzmann’s distribution. Two atomicemissionlineintensitiesofArIIat434.8and487.9nm were sampled at different instants and estimate the plasma temperature.Similarlytheprocedurecontinuedfornitrogen and Helium gas line intensities to find the respective plasma temperature. The atomic emission lines and spectroscopic parameters used in estimating plasma temperature are summarizedinTable1. Line Waveleng th (nm) Upper energy level Ek (c/m) Configuration gk*Ak (1/s) N II 500.5 186652.49 2s22p(2P0)3p-2s22p(2P0)3d 1.03e9 N II 567.9 166678.64 2s22p(2P0)3s-2s22p(2P0)3p 3.47e8 N I 746.8 96750.840 2s22p2(3p)3s-2s22p2(3d)3p 7.84e7 Ar II 434.8 157234.0196 3s23p4(3p)4s-3s23p4(3p)4p 9.36e8 Ar II 487.9 158730.2995 3s23p4(3p)4s-3s23p4(3p)4p 4.94e8 ArI 696.5 107496.4166 3p5(2p0 )4s-3p5(2p0 )4p 3/2 1/2 1.92e7 Ar I 763.5 106237.5518 3p5(2p0 )4s-3p5(2p0 )4p 3/2 3/2 1.22e8 He I 587.6 186101.592 1s2p-1s3d 8.83e7 He II 656.1 426717.460 6.27e6 He I 667.8 186104.966 1s2p-1s-3d 3.18e8 Table1.SpectroscopicparametersofNitrogen,ArgonandHeliumusedfor plasmatemperature The life time was estimated at 1/e of the maximum emission intensity. The figures 6, 7, and 8 show the lifetime profiles of Nitrogen,HeliumandArgonrespectively. Thesefiguresshow clearlytheeffectofpressureontheemissionlifetime. 0 10 20 30 0.00 0.02 0.04 0.06 0.08 Intensity(arbs) N II 567.9 life time (us) 1 kg/cm 2 1.5 kg/cm 2 2 kg/cm 2 Figure-6:Life-timeprofileofNitrogenlines1kg/cm2at NII567.9 0 10 20 30 40 50 60 0.00 0.01 0.02 0.03 0.04 Intensity(arbs) He II 656.1 life time (us) 0.5 kg/cm 2 1 kg/cm 2 1.5 kg/cm 2 2 kg/cm 2 Figure-7:Life-timeprofileofHeliumlines0.5-2kg/cm2 atHe II656.1 0 10 20 30 40 0.00 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 Intensity(arbs) Ar II 487.9 life time (us) 0.5kg/cm 2 1kg/cm 2 1.5kg/cm 2 2kg/cm 2 Figure-9:Life-timeprofileofArgonlines0.5-2kg/cm2 at(d) Ar IIat487.9
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 02 | Feb 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 2636 5.ELECTRONDENSITY Electron density can be determined using modified Saha equation [4] which involves ion-atom line intensity ratio. Based on the experimentally observed emission spectra, electrondensity,ne. WhereEiandEaaretheenergiesoftheupperstates,EionistheIst ionizationpotential. TheEstimationofelectrondensityconsideringlocalthermal equilibrium in Argon [5] ambient gas at 2 kg/cm2 pressure valueisshowninfigure10andEstimationofelectrondensity considering local thermal equilibrium indifferent ambient gaseswithvariouspressurevaluesisshowninfigure11. 0 0.5 1 1.5 2 2.5 3 3.5 x 10 -5 -2 0 2 4 6 8 10 12 x 10 15 Time. Electrondensity(cm- 3) Figure-10:Estimationofelectrondensityconsideringlocal thermalequilibriuminArgonambientgasat2kg/cm2 pressurevalue. 6. CONCLUSION Optical emission spectroscopy is used to understand the dischargeproperties.Argon,nitrogenandheliumgasseswere usedasdielectricmediumat0-2kg/cm2.Itwasobservedthat theelectrontemperaturewashighintheArgoncomparedwith Nitrogenenvironment.Theaverageelectrondensityoverthe emissiontimewasrangingfrom109 to1015 cm-3.Theplasma temperature and density estimated from time integrated spectra were an average value not giving any temporal distributiondetails. 0.0 0.5 1.0 1.5 2.0 6.566E7 4.85165E8 3.58491E9 2.64891E10 1.9573E11 1.44626E12 1.06865E13 7.8963E13 5.83462E14 Electrondensity(cm^-3) Pressure (kg/cm^2) Nitrogen Argon Helium Figure-14:Estimationofelectrondensityconsideringlocal thermalequilibriumindifferentambientgaseswithvarious pressurevalues. REFERENCES [1] K.V.Nagesh,P.H.Ron,g.R.Hagabhushana,andR.S.Nema, “Overrecoveryinlowpressuresparkgaps-Confirmation of pressure reduction in over recovery”, IEEE Trans. PlasmaSci.,Vol.27,No.6,pp.1559-1565,February1999. [2] C.S.Reddy, et. al,“Voltage Recovery Characteristics of Spark gap using Repetitive Pulse Power System” IEEE International Power Modulator and High Voltage Conference(IPMHVC),USA,June-2014. [3] C.S.Reddy,et.al.,,“RecoveryAnalysisofSparkgapbyAnode Temperature Decay method for Different Materials."International Journal of Applied Electromagnetics and Mechanics, Vol 47, pp 643-651, 2015.PublishedbyIOSpress. [4] J.K.Antony,N.J.Vasa, S.R.Chakravarthy,andR.Sarathi,. “Understanding the mechanism of nano-aluminum particleformationbywireexplosionprocessusingoptical emissiontechnique,”J.Quant.Spectrosc.Radiat.Transfer, Vol.111,No.17-18,pp.2509-2516, 2010. [5] C.S.Reddy, et. al ,“ Experimental Investigations of Pulse Charged Spark Gap Recovery Times and Influencing Factors,”IEEE Transactions on Plasma Science, Vol.44, Issue3,pp.331-337,2016.
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