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Studyofdelaminationindrillingcarbonfiberreinforced
plastics(CFRP)usingdesignexperiments
J.P.Davim*,PedroReis
DepartmentofMechanicalEngineering,UniversityofAveiroCampusSantiago,3810-193Aveiro,Portugal
Abstract
Inthispaperispresentedanewcomprehensiveapproachtoselectcuttingparametersfordamage-freedrillingincarbonfiberreinforcedepoxycompositematerial.TheapproachisbasedonacombinationofTaguchiÕstechniquesandontheanalysisofvariance(ANOVA).Aplanofexperiments,basedonthetechniquesofTaguchi,wasperformeddrillingwithcuttingparametersprefixedinanautoclavecarbonfiberreinforcedplastic(CFRP)laminate.TheANOVAisemployedtoinvestigatethecuttingcharacteristicsofCFRPÕsusinghighspeedsteel(HSS)andCementedCarbide(K10)drills.Theobjectivewastoestablishacor-relationbetweencuttingvelocityandfeedratewiththedelaminationinaCFRPlaminate.Thecorrelationwasobtainedbymultiplelinearregression.Finally,confirmationtestswereperformedtomakeacomparisonbetweentheresultsforeseenfromthementionedcorrelation.
Ó2002ElsevierScienceLtd.Allrightsreserved.
Keywords:Drilling;Carbonfiberreinforcedplastics;Delaminationfactor;TaguchiÕstechniques;Analysisofvariance
1.Introduction
Owingtothegrowinguseofcompositematerials,specificallythefiberreinforcedplastics(FRP)outsidethedefenceindustryandtheaerospaceindustry,theunitcostreplacestheperformanceatanycostasthemainconcernforproduction.So,theproductiontechno-logies,especiallythemachiningofcomposites,areas-sumingamoreandmoresignificantroleastheyconditiontheeconomicviabilityoftheproduct.
Machiningcompositematerialsisarathercomplextaskowingtoitsheterogeneity,heatsensitivity,andtothefactthatreinforcementsareextremelyabrasive.Con-ventionalmachiningmethodsshouldbeadaptedinsuchawaythattheydiminishthermalandmechanicaldamage.
Drillingisafrequentlypracticedmachiningprocessinindustryowingtotheneedforcomponentassemblyinmechanicalpiecesandstructures.
Thedrillingoflaminatecompositematerialsissig-nificantlyaffectedbythetendencyofthesematerialstodelaminateandthefiberstobondfromthematrixundertheactionofmachiningforces(thrustforceandtorque).
*Correspondingauthor.Fax:+351-234-370953.E-mailaddress:pdavim@mec.ua.pt(J.P.Davim).
Manyauthors[1–3],whenreportingaboutthedrill-ingoflaminatedcompositematerialsbyconventionaltools,haveshownthatthequalityofthecutsurfacesisstronglydependentonthedrillingparameters,toolge-ometryandtoolmaterial.Aninappropriatechoiceoftheseparameterscanleadtounacceptablematerialde-gradation,suchasfiberpull-out,matrixcratering,thermaldamageanddelamination.Amongthedefectscausedbydrilling,delaminationappearstobethemostcritical.
LaminatedfiberreinforcedplyÕsundermachiningforcesaresubjecttotheriskofinterlaminarcrackpropagation,calleddelamination.
Koenigetal.,studiedin1985themachiningoffiberreinforcedplasticsandconcludedthatahighfeedrateofdrillingwillcauseacrackaroundtheexitedgeofthehole[4].
Millerpresentedin1987adatabaseonoptimumcuttingparametersfordrillingholeswithminimumlocalmachiningdamage[5].
HochengandPuw[1],in1992presentedastudyofthechipformationandassessesthemachinabilityoftwocompositematerials(Thermoset-basedandThermo-plastics-based)andconcludedthatfromcuttingchipstheformerpresentsalargeamountofdeformationinchipformation,whilethelattertendstofracture.He
0263-8223/03/$-seefrontmatterÓ2002ElsevierScienceLtd.Allrightsreserved.PII:S0263-8223(02)00257-X
482J.P.Davim,P.Reis/CompositeStructures59(2003)481–487
alsonoticedthatcarbon/ABSissuperiortocarbon/epoxyforsurfacequalityandbothholeedges.
ChambersandBishop[6]in1995investigatedtheeffectofthecuttingparametersondrillingcarbon/epoxyandcarbon/peekandconcludedthatthedrillingofcarboncompositesisdependentuponthecharacteristicsofthematrixandthehelicalPCDdrillgeometrygavethebestoverallperformance.
Inadditiontotheproblemsoftoolwear,itisverydifficulttoachievethequalityofsurfaceneededfortheaccurateassemblyofcomponentsinmechanicalstruc-tures.
Linetal.[7]in1996,carriedoutastudyondrillingofcarbonfiberreinforcedcompositeathighspeedandconcludedthatanincreaseofthecuttingvelocityleadsaincreasingofthedrillwear.Inthiswaythefactofincreasingthewearofdrillcausesarisingofthrustforce.
Wen-ChouChen[3]in1997studiedthevariationsofcuttingforceswithorwithoutonsetdelaminationduringthedrillingoperationsandconcludedthatthedelami-nation-freedrillingprocessesmaybeobtainedbytheproperselectionsoftoolgeometryanddrillingpara-meters.
Piquetetal.[8]in2000carriedoutastudyofdrillingthincarbon/epoxylaminateswithtwotypesofdrills,ahelicaldrillandadrillofspecialgeometry,andcon-cludedthatbothdrillsleadsadamageattheentranceinthewallandtheexitofthehole,withtheexceptionofspecialgeometrydrillwhichispossibleasignificantre-ductioninthefinaldamage.
Enemuohetal.[9]in2001,realizethatwiththeap-plicationofthetechniqueofTaguchiandothermeth-ods,werepossibletoachievethecuttingparametersthatallowedtheabsenceofdamageinthedrillingoffiberreinforcedplastics.
Alltheaboveworkscontributestothepracticeofcuttingcompositematerials,buttheydonotshowthebasicmechanismsofcutandthecharacterizationofthemachinability.
2.Experimentalprocedure2.1.Meansandmaterials
Inordertoachievetheobjectiveofthisexperimentalwork,mainlytheestablishingofcorrelationsbetweenthecuttingconditionswiththedelamination,machiningissueswereeffectuatedwithdifferentcuttingconditions,andwereusedcarbonfiberreinforcedplastics(CFRPÕs)(Epoxymatrixreinforcedwith55%ofcarbonfiber)fortests.
Thiscompositematerialwasproducedbyautoclavewithafiberorientationof0/90degrees,aswecanob-serveonFig.1.
Theexperimentshadbeencarriedoutinanautoclavelaminatemadeupof16layersoffiberswith4mmofthickness,usingthreedifferenttypesof5mmdiameterdrillspresentedintheFig.2.Ahelicalflutehighspeed
Fig.1.Plateproducedbyautoclavewithafiberorientationof0/90degrees.
Fig.2.(a)HelicalfluteHSSdrill;(b)four-fluteK10drill;(c)helicalfluteK10drill.
J.P.Davim,P.Reis/CompositeStructures59(2003)481–487483
steel(HSS)drill(R415.5-0500-50-8C0),afour-flutece-mentedcarbide(K10)drill(R950.01H10F)andfinallyahelicalfluteK10carbidedrill(R415.5-0500-30-AC0),accordingtoISO1832.
Adrillingmachinewith2,2kWspindlepowerandamaximumspindlespeedof2500rpmwasusedtoper-formtheexperiments.
Theuseddrillshavean118°pointangle.
Thesqueezeofthelaminate,inthepressofjawofthedrillingmachinewasmadebyasystemofclamps,tomakesurethatvibrationsanddisplacementdoesnotexist,aswecanobserveinFig.3.
Thedamagearoundtheholeswasmeasuredwithashopmicroscope,MitutoyoTM500,with30Âmagni-ficationand1lmresolution.
2.2.Planofexperiments(Taguchi’stechniques)TaguchiÕstechniqueshavebeenusedwidelyinengi-neeringanalysis.Thesetechniquesconsistofaplanofexperimentswiththeobjectiveofacquiringdatainacontrolledway,executingtheseexperiments,inordertoobtaininformationaboutthebehaviorofagivenpro-cess.
Thetreatmentoftheexperimentalresultsisbasedontheanalysisaverageandtheanalysisofvariance(AN-OVA)[10–13].
FortheelaborationofexperimentsplanweusedthemethodofTaguchifortwofactorsatthreelevels.Bylevelswemeanthevaluestakenbythefactors.Table1indicatesthefactorstobestudiedandtheassignmentofthecorrespondinglevels.
ThearraychosenwastheL9(24),whichhasninerowscorrespondingtothenumberoftests(eightdegreesoffreedom)withtwocolumnsatthreelevels,asshowninTable2.Thefactorsandtheinteractionsareassignedtothecolumns.
Theplanofexperimentsismadeofninetests(arrayrows)inwhichthefirstcolumnwasassignedtothecuttingvelocityðVÞandthesecondcolumntothefeed
Fig.3.Squeezeoftheplateinthepressofjawofthedrillingmachine.
Table1
AssignmentofthelevelstothefactorsLevelRevolutionnFeedratefCuttingvelocity(rpm)(mm/rev)V(m/min)110000.0416215000.08243
2000
0.15
32
Table2
OrthogonalarrayL9(24)ofTaguchi[10]L9(24)Test123411111212223133342123522316231273132832139
3
3
2
1
LineargraphL9ð24Þ[10].
rateðfÞandtheremainingwereassignedtotheinter-actions.TheresponsetobestudiedisthedelaminationfactorðFdÞinCFRPlaminate.
3.Resultsanddiscussion
3.1.Influenceofthecuttingparametersinthedelami-nationfactor
ThedamagearoundtheholeswasmeasuredusingashopmicroscopeMitutoyoTM-500,followingtheschemapresentedintheFig.4.
AftermeasuringthemaximumdiameterðDmaxÞinthedamagezone,i.e.aroundeachhole,wecarriedouttodeterminedthevalueofthedelaminationfactorðFdÞ.ThisfactorisdeterminedbytheratiothemaximumdiameterðDmaxÞofthedamagezonetotheholediameterðDÞ.
Fig.4.SchemaofthemeasurementofthemaximumdiameterðDmaxÞwithashopmicroscopeMitutoyoTM500.
484J.P.Davim,P.Reis/CompositeStructures59(2003)481–487
ThevalueofdelaminationfactorðFdÞcanbeobtainedbythefollowingequation:FDmaxd¼
Dð1Þ
being,DmaxthemaximumdiameterofthedamageholeinlmandDthediameteroftheholeinlm.
Table3showstheresultsofthedelaminationfactorðFdÞ,forthethreesetsofdrillingtests,obtainedbytheEq.(1)infunctionofthecuttingparameters.
IntheFigs.5and6wecanobservetheevolutionofthedelaminationfactorðFdÞwiththefeedforthedif-ferentcuttingspeedvalues.
InFig.5wecanevidencethattheFdincreaseswiththefeedrate,andwiththecuttingspeed.Accordingtothegraph,wecanobservethatthecarbidedrillpresentsabetterperformancethantheHSSdrill,i.e.underthesamecuttingconditions(cuttingspeedandfeedrate),theHSSdrillcausesalwaysabiggerdelaminationfac-tor,witchmeanshigherdamageinthecompositelami-nate.
WealsocanobservethatinFig.6,theFdincreaseswiththefeedrate,andwiththecuttingspeed.
Table3
ValuesofdelaminationfactorðFdÞinfunctionofthecuttingparame-tersTest
V(m/f(mm/DelaminationfactorðFdÞmin)rev)HelicalfluteFour-fluteHelicalfluteHSSdrillK10drillK10drill116
0.041.0441.01.04220.081.0521.0661.04530.151.0511.0661.047424
0.041.0611.0691.05750.081.0701.0711.060.151.0791.0781.0732
0.041.0631.0731.05280.081.0691.0751.0629
0.15
1.078
1.080
1.069
)1.09dFV = 16 m/min(r 1.08oV = 24 m/mintcaf1.07V = 32 m/min noit1.06V = 16 m/minnaiV = 24 m/minma1.05V = 32 m/minelD1.04HSS drillK10 drill1.030.020.060.10.140.18feed (mm/rev)Fig.5.DelaminationfactorðFdÞinfunctionofthecuttingparameterstodrills,fortwotoolmaterials,whichhavethesamegeometry.1.10)dV = 16 m/minF1.09(V = 24 m/minrot1.08V = 32 m/mincaf1.07V = 16 m/minno1.06V = 24 m/minitanV = 32 m/minim1.05a4 flutes (K10)le1.04Dhelical flute1.03(K10)0.020.060.10.140.18feed (mm/rev)Fig.6.DelaminationfactorðFdÞinfunctionofthecuttingparameterstodrills,fortwotoolmaterials,whicharemanufacturedwiththesamematerial.Wecanevidencethatthehelicalflute(K10)drillpresentsabetterperformancethanthefour-flute(K10)drill,i.e.underthesamecuttingconditions(cuttingspeedandfeedrate).Thefour-flutedrillcausesalwaysabiggerdelaminationfactor,exceptinthetestwhichhavethehigherfeedrateandthelowercuttingvelocity.
Geometricaldifferencesbetweenthetwotypesofdrillmaybethereasonforthisfact.
Withanopticalmicroscope(OM)waspossibletoobservethedamagearoundtheholes,andnoticetheinfluenceofthecuttingvelocityðVÞhaveonthede-laminationfactorðFdÞ,aswecanseeonFig.7.
InFig.7,wecanevidencethat,foraconstantafeedrate,anincreaseofthecuttingvelocityincreasesthedelaminationfactorðFdÞaswell.
Ananalysisofvarianceofthedatawiththedelami-nationfactorðFdÞinCFRPlaminate,withtheobjectiveofanalyzingtheinfluenceofthecuttingvelocityðVÞ,offeedrateðfÞonthetotalvarianceoftheresults.
Thestatisticaltreatmentofthedatawasmadeintwophases.Thefirstphasewasconcernedwiththeanalysisofvarianceandtheeffectofthefactorsandofthein-teractions.Thesecondphaseallowedustoobtainthecorrelationbetweentheparameters(Vandf).
Tables4–6showtheresultsoftheanalysisofvariancewiththedelaminationfactorðFdÞinCFRPlaminate.FromtheanalysisofTable4,wecanobservethatthecuttingvelocityðP¼72:5%ÞandthefeedratefactorðP¼20:5%Þ,havestatisticalandphysicalsignificanceonthedelaminationfactorðFdÞobtained,especiallythecuttingvelocityfactor.
Thefactors(Vandf)presentastatisticalsignificancetestF>Fa¼5%.NoticethattheerrorassociatedtothetableANOVAfortheFdwasapproximately7%.FromtheanalysisofTable5,wecanobservethatthecuttingvelocityfactorðP¼65:9%Þ,havestatisticalandphysicalsignificanceontheFdobtained.
ThefactorfeedrateðP¼19:3%ÞdoesnotpresentpercentageofstatisticalsignificanceofcontributionontheFd.
J.P.Davim,P.Reis/CompositeStructures59(2003)481–487485
Fig.7.DelaminationfactorðFdÞinfunctionofthecuttingspeed,MO:amplificationof30Â.
Table4
ANOVAforthedelaminationfactorðFdÞtothehelicalfluteHSSdrillSourceofvarianceV(m/min)f(mm/rev)ErrorTotal
SDQ8.7E)42.6E)44E)51.17E)3
gl2248
Variance4.3E)41.3E)41E)5/
TestF42.2612.69//
Fa¼5%6.946.94//
P72.520.57.0100.0
SDQ––sumofsquares,gl––degreesoffreedom,P––percentageofcontribution.
Table5
ANOVAforthedelaminationfactorðFdÞtothefour-fluteK10drillSourceofvarianceV(m/min)f(mm/rev)ErrorTotal
SDQ1.7E)46E)52E)52.5E)4
gl2248
Variance9E)53E)55E)6/
TestF18.816.20//
Fa¼5%6.946.94//
P65.919.314.8100.0
SDQ––sumofsquares,gl––degreesoffreedom,P––percentageofcontribution.Table6
ANOVAforthedelaminationfactorðFdÞtothehelicalfluteK10drillSourceofvarianceV(m/min)f(mm/rev)ErrorTotal
SDQ4.6E)41.5E)41E)46.7E)4
gl2248
Variance2.3E)47E)52E)5/
TestF14.114.//
Fa¼5%6.946.94//
P63.517.119.4100.0
SDQ––sumofsquares,gl––degreesoffreedom,P––percentageofcontribution.
ThefactorcuttingvelocitypresentastatisticalsignificancetestF>Fa¼5%,witchdoesnothap-penstothefactorfeedratebecausethetestF FromtheanalysisofTable6,wecanobservethatthecuttingvelocityfactorðP¼63:5%Þ,havestatisticalandphysicalsignificanceontheFdobtained.ThefactorfeedrateðP¼17:1%ÞdoesnotpresentpercentageofphysicalsignificanceofcontributionontheFd,becausePðpercentageofcontributionÞ NoticethattheerrorassociatedtothetableANOVAfortheFdwasapproximately19.4%. 486J.P.Davim,P.Reis/CompositeStructures59(2003)481–487 3.2.Correlation(delaminationfactor/cuttingparameters)Thecorrelationsbetweenthefactors(cuttingvelocity,feedrate)andthedelaminationfactorðFdÞinCFRPlaminatewereobtainedbymultiplelinearregression.Theequationsobtainedwereasfollow:HelicalfluteHSSdrillÀFd¼1:021þ1:31Â10À3 Vþ0:117fR¼0:76ð2Þ Four-fluteK10drillÀFd¼1:037þ1:0Â10 À3Vþ0:158fR¼0:74ð3Þ HelicalfluteK10drillÀ Fd¼1:010À1:16Â10À4Vþ0:097f R¼0:86 ð4Þ being,Vthecuttingofvelocityinm/min,andfthefeedrateinmm/rev.3.3.Confirmationtests Table7showsthecuttingconditionsusedontheconfirmationtests. Theresultsobtainedbyacomparisonbetweentheforeseenvaluesbythebythemodelsdevelopedinthepresentwork(Eqs.(2)–(4))andtheexperimentallyob-tainedresultsbydelaminationfactorðFdÞ,areshowninTable8.Fromtheanalysisoftherefereedtable,wecanobservethatthegainedthroughtheactualmodelshowamaximumerrorofabout2%.WealsocanconsiderthatEqs.(2)–(4),correlatestheevolutionofthedelamination Table7 CuttingconditionsusedindrillingconfirmationtestsTypeofdrillTestRevolutionnV(m/min)f(mm/rev)(rpm)HelicalfluteHSS1c1250200.082c1750270.08Four-fluteK103c1250200.084c1750270.08HelicalfluteK10 5c1250200.086c 1750 27 0.08 Table8 ExperimentalplanconfirmationdrillingtestsandtheircomparisonwiththeresultsTestDelaminationfactorðFdÞExperimentalvaluesModelEqs.(2)–(4)Error(%)11.0471.0560.8721.0711.0660.4031.0841.0691.3241.0921.0771.3651.0231.0101.316 1.041 1.033 0.73 factorðFdÞinthelaminatewiththecuttingconditions(cuttingvelocityandfeed)withagooddegreeofap-proximation. 4.Conclusions Fromthisstudyondelaminationwhen,drillingofCFRPs,thefollowingconclusionscanbedrawn:•ThehelicalfluteK10drillpromoteslessdamageonthecompositelaminatethanthefour-flutecarbide(K10)drill,i.e.,thedelaminationfactorðFdÞissmal-ler. •ThehelicalfluteK10drill,presentsabetterperfor-mance,thanhelicalfluteHSSdrill,i.e.,thecarbidedrillisthebetterchoicefordrillingCFRP. •Thedelaminationfactorincreaseswithbothcuttingparameters,whichmeansthatthecompositedamageisbiggerforhighercuttingspeedandforhigherfeed.•ThecuttingvelocityisthecuttingparameterthathasthehighestphysicalaswellstatisticalinfluencethedelaminationfactorinCFRPlaminate(63.91%and65.9%),forthethreedrills. •Bothcarbidedrillsshowsanalmostnullwearlandintheflanksurface,whiletheHSSdrillpresentsawearvalueof0.012mm,measuredat1/4thedrillradius,apartfromthecorner. •Theconfirmationtestsshowedthattheerrorassoci-atedtothedelaminationfactorðFdÞ(maximumvalue2%andminimum0.4%)isexcellent. Acknowledgements TheauthorsacknowledgeProfessorAnto nioTorresMarques,fromINEGI/FEUP,forprovidingthecom-positematerialusedinthedrillingtests.Theyacknowl-edgealsototheMechanicalEngineerPedroMadalenofortheirparticipationintheexperimentalwork. References [1]HochengH,PuwH.Ondrillingcharacteristicsoffibre-reinforced thermosetandthermoplastics.IntJMachToolsManufact1992;32(4):583–92. [2]HochengH,PuwH,YaoK.Experimentalaspectsofdrillingof somefibrereinforcedplastics.In:Proceedingsofthemachiningofcompositematerialssymposium.ChicagoIllinois:ASMMaterialsweek;1992.p.127–38. [3]ChenW.Someexperimentalinvestigationsinthedrillingof carbonfibre-reinforcedplastic(CFRP)compositelaminates.IntJMachToolsManufact1997;37(8):1097–108. [4]KoenigW,WulfC,GrassP,WillerscheidH.Machiningoffiber reinforcedplastics.ManufactTechCIRPAnn1985;34(2):537–48.[5]MillerJA.Drillinggraphite/epoxyatLockheed.AmMachAutom Manufact1987:70–1. J.P.Davim,P.Reis/CompositeStructures59(2003)481–487 [6]ChambersA,BishopG.Thedrillingofcarbonfibrepolymer matrixcomposites.ProcessManufact1995;III:565–72. [7]LinSC,ChenIK.Drillingofcarbonfiber-reinforcedcomposite materialathighspeed.IntJMacToolsManufact1996:156–62.[8]PiquetR,FerretB,LachaudF,SwiderP.Experimentalanalysis ofdrillingdamageinthincarbon/epoxylaminateusingspecialdrills.IntJMacToolsManufact2000:1107–15. [9]UgoEnemuohE,SherifEl-GizawyA,ChukwujekwuOkaforA.An approachfordevelopmentofdamage-freedrillingofcarbonfiberreinforcedthermosets.IntJMacToolsManufact2001:1795–814. 487 [10]RossP.Taguchitechniquesforqualityengineering-lossfunction, orthogonalexperiments,parameterandtolerancedesign.NewYork:McGraw-Hill;1988.p.10–50. [11]TaguchiG,KonishiS.Taguchimethods,orthogonalarraysand lineargraphs,toolsforqualityengineering.AmericanSupplierInstitute;1987.p.35–8. [12]PhadkeMS.Qualityengineeringusingrobustdesign.Englewood CliffsNJ:Prentice-Hall;19.p.1–50. [13]TaguchiG.Taguchionrobusttechnologydevelopmentmethods. NewYork:ASMEPress;1993.p.1–40. 因篇幅问题不能全部显示,请点此查看更多更全内容
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