ContentslistsavailableatScienceDirect
Additive
Manufacturing
j o ur na l h o me pa g e :w w w . e l s e v i e r . c o m / l o c a t e / a d d m a
Assessing
the
capability
of
in-situ
nondestructive
analysis
during
layer
based
additive
manufacture
Matthias
Hirsch
a,b,
Rikesh
Patel
a,
Wenqi
Li
a,
Guangying
Guan
b,
Richard
K.
Leach
b,
Steve
D.
Sharples
a,
Adam
T.
Clare
b,∗aOpticsandPhotonicsGroup,FacultyofEngineering,TheUniversityofNottingham,NottinghamNG72RD,UnitedKingdom
bAdvancedComponentEngineeringLaboratory(ACEL),FacultyofEngineering,TheUniversityofNottingham,NottinghamNG72RD,UnitedKingdom
a
r
t
i
c
l
e
i
n
f
o
Articlehistory: Received2August2016 Receivedinrevisedform 16September2016 Accepted17October2016 Availableonlinexxx
Keywords:
Nondestructiveevaluation Additivemanufacturing Processcontrol In-situanalysis
a
b
s
t
r
a
c
t
Unlikemoreestablishedsubtractiveorconstantvolumemanufacturingtechnologies,additive manufac-turingmethodssufferfromalackofin-situmonitoringmethodologieswhichcanprovideinformation relatingtoprocessperformanceandtheformationofdefects.In-processevaluationforadditive manu-facturingisbecomingincreasinglyimportantinordertoassuretheintegrityofpartsproducedinthis way.Thispaperaddressesthegenericperformanceofinspectionmethodssuitableforadditive man-ufacturing.Keyprocessandmeasurementparametersareexploredandtheimpactsthesehaveupon productionratesaredefined.Essentialworkingparametersarehighlighted,withinwhichthespatial opportunityandtemporalpenaltyformeasurementallowforcomparisonofthesuitabilityofdifferent nondestructiveevaluationtechniques.Anewmethodofbenchmarkingin-situinspectioninstruments andcharacterisingtheirsuitabilityforadditivemanufacturingprocessesispresentedtoactasadesign tooltoaccommodateenduserrequirements.Twoinspectionexamplesarepresented:spatiallyresolved acousticspectroscopyandopticalcoherencetomographyforscanningselectivelasermeltingand selec-tivelasersinteringparts,respectively.Observationsmadefromtheanalysespresentedshowthatthe spatialcapabilityarisingfromscanningparametersaffectsthetemporalpenaltyandhenceimpactupon productionrates.Acasestudy,createdfromsimulateddata,hasbeenusedtooutlinethespatial per-formanceofagenericnondestructiveevaluationmethodandtoshowhowadecreaseindatacapture resolutionreducestheaccuracyofmeasurement.
©2016TheAuthors.PublishedbyElsevierB.V.ThisisanopenaccessarticleundertheCCBYlicense (http://creativecommons.org/licenses/by/4.0/).
1. Introduction
Throughthecontinueddevelopmentofadditive manufactur-ing(AM)processespartmanufactureforhighvalueapplicationsis continuingtogaintraction(e.g.inaerospace,medicalandtooling industries)[1].AnAMprocessuseslocalisedmaterialadditionon alayerperlayerbasistobuildupthree-dimensional(3D)parts[2]. Mordfinetal.definethreemainassumptionsaboutmanufactured materials[3]:(1)allmaterialscontaindefects;(2)thesedefectsare expectedanddonotdefinitivelymeanthepartisunfitforuse(i.e. forservicelife);and(3)thedetectabilityofdefectsincreaseswith thesizeofthedefects.Theseassumptionsholdtrueforparts pro-ducedwithAMprocesses,henceitcanbededucedthatinspection isessentialinhighvaluecomponentsinordertoassurethatthe manufacturedpartisfitforuse.
∗Correspondingauthor.
E-mailaddress:[email protected](A.T.Clare).
Inspection can be conducted destructively, where statistical informationcanbegatheredinordertogiveaconfidence inter-valforapartproducedundersimilarconditions(e.g.basematerial consistency, temperatureand atmosphere).However, for many applicationsinthehighvalueaddedindustries,destructive inspec-tion maynot besuitable (where individual partinformation is required).Nondestructiveevaluation(NDE)ofapartis,therefore, oftentheonlymethodthatcanbeemployedtogatherthedefect datarequired.Evertonetal.havereviewedrecentresearchon in-situmonitoringtechniquesofmetalAMprocesses[4];anoverview isgivenofthedirectandindirectmeasurementinstrumentation currentlyemployedtomeasurepartsandmachineoperationinAM, whichhasbeenfoundtobelimitedtoasmallnumberof commer-cialsystems;however,thereisarangeofinspectiontechniquesthat arecurrentlybeingdeveloped[4]andyetthereisnooverarching contributionwhichexplorestheirutilisation.
MeasurementmethodscurrentlybeingconsideredforAMcan besortedintotwoprincipalcategories:indirectanddirect.Indirect measurement techniques investigate effects on part
manufac-http://dx.doi.org/10.1016/j.addma.2016.10.004
areevaluatedinconventionalmanufacturing.However,AM pro-videsagoodopportunityforpartstobeinspectedastheyarebeing built−in-situ.NDEmethodsthatcaninspectthesurfaceand/or thesubsurfaceregioncannowbeusedtobuildupanimageofthe internalstructureofamanufacturedpart,ensuringitisproduced tomeetdesignparameters.Inaddition,measurementsmadeand analysedin-situcandetecterrorswithinthebuildprocess; feed-backcouldthenbeusedtopausethebuildtoavoidscrappageof theflawedcompletepart,reducingmaterialwaste.Alternatively, thescandatacanbeusedtoenabletotheAMmachinetoreact autonomouslyandreworkthedefectivelayer,‘saving’thebuild[8]. TheseapproachesmayimprovetheeconomicviabilityofusingAM processesandimproveitsadoptionintomorefields[9].Whilethe underpinningmachinetooltechnologytoallowin-siturepairisnot availableincurrentgenerationmachines,thispresentsan interest-ingresearchareawhichwillsignificantlyenhancethecapabilityof AMtools.
In-processmonitoringisanimportantnextstepinAMmethods duetouser,machineandmaterialinducederrorsaffectingthe suc-cessofmanufacturefromageometricalandmaterialpointofview [4].Thestudypresentedhereinvestigatesgenericparametersof NDEtoolsandtheirinfluenceontheproductivityontherapidly advancingAMprocesswhenincorporatedin-situ.Analysingthe spatialopportunityandtemporalpenaltyassociatedwithit,that theAMprocesspresentsforameasurementsystem,isakey con-cernwhendesigningandselectinginstruments.AnNDEcapability analysisapproachisdemonstratedintwocasestudiesand simu-lateddefectdataisusedtooutlinetheeffectsoflowNDEspatial capabilities.
1.1. Currentinspectionmethods
In order to frame the methodology of determining and optimising inspection strategies, it is useful to review current measurement strategies. Indirect NDEmethods currentlybeing investigated include thermal and optical analysis − conducted eitherin-situoronline,haveshowntoyielddatathatcanbeused forfeedback inselective lasermelting (SLM)[10,11].Meltpool analysisenablespartfailuredetection.Theprocesswillinfer for-mationofdefectsbasedonobservationsofthemeltpool.Inwork byKraussetal.,artificialdefectsinarangeof40mto500m wereintroducedintoanSLMbuildatthedesignstage[12].During partmanufacture withInconel718powder,thebuildwas ana-lysedusingthermography(detectingwithaninfraredcamera)with defectsoflessthan100midentifiedbydetectingavariationinthe coolingrate.However,asanindirectmeasurementmethod,the siz-ingandnatureofthedefectswerenotobtained.Doubenskaiaetal. haveshownthatanopticalsystemcanbeusedforsolidversus unfusedpowderdifferentiation(whilstalsodeterminingthe geom-etryofthepartin-situ)[13].Similarly,Schwerdtfegeretal.have shownthatinfraredimaging,usedin-situinelectron-beam pow-derbedfusionprocesses,yieldslayerperlayerdatathatoutlines areasofdefectsasareductioninintensity[14]−inthisstudythe minimumsamplingsizecorrespondedto830m.Thesizerange
cessmonitoringwithsurfaceandsubsurfaceinformation.Thiswas shown byGuan etal. scanningpolymer test samplesproduced usinganSLSsystemwithembeddedartificialdefects[8].Surface defectsandroughnesswavelengthswithaminimumof9mcould beresolvedandidentificationofloosepowderundersintered mate-rialwaspossibledownto200mbelowthesurface.Subsurface defectsupto100minsizecouldbeidentified.
Directex-situpartinterrogationmethodsincludetheuseof X-raycomputedtomography(XCT)(see[7]forathoroughreview), whichcandelivermeasurementsconsistingofa highresolution data set of the build. For a full 3D data acquisition, Tammas-Williams et al. utilised a high resolution XCT system to scan electron-beampowderbedfusionsampleswithbothcoarseand fine scans to detect defects and relate the distribution to the processingenvironment[15].TheXCTanalysisofelectron-beam powderbedfusionsampleshasbeenshowntoenablethe deter-minationofdefectslargerthan120m.Maskeryetal.conducted aporecharacterisationandquantificationstudyonAlSi10Mg
sam-plesproducedusingSLM[18].TheXCTresultsweresegmented andporeswerecharacterisedbasedonrelativecountandshape descriptors.Relativeporositiesofthesampleswerecalculatedto belessthan0.1%andpredictionsofservicelifeweremadebased ontheporedistributions,showingthatXCTisavalidapproachto SLMmonitoring.
2. DefiningNDEcapability
GiventhelevelofresearchactivityintheareaofNDEforAM parts,alongsidetheemergenceofnewAMmachines,thereisaneed toevaluatehowmeasurementtechniquesperforminservice.The timelineofabasicin-situanalysisforanAMprocessisoutlined inFig.1(a).Inthiscase,employinganNDEmethodbetweenthe manufactureofasinglelayerwillextendthetimetopart comple-tion;themanufactureandmeasurementprocessneedtooccurin succession.Onlineanalysis,outlinedinFig.1(b),assumesthatNDE measurementscanbeconductedduringthemanufacturingprocess andprocessmeasurementdataon-the-fly,reducingthebottleneck apparentinthelayercompletiontime.Fullonlinemonitoring sys-temscanonlyyieldindirectmeasurementsasthesolidificationof thematerialinthemanufacturingstagehastohaveoccurredbefore collectingdirectinformation.
Therequirementsformeasurementinstrumentationare depen-dent onthe type of AMprocess, thematerials tobe used,the expecteddefectsandtheendusertolerances.Thisincludesthe spa-tialopportunityandtemporalpenaltyaffordedtotheinstrument. AdefinitionofcapabilityofanNDEinstrumentisneededinorder toascertainthatitmeetstheserequirements.
Onerequirementthatanendusermayhaveforproductionis thepartcompletiontime,tmanufacture,andisgivenby
tmanufacture=tbuild+treset (1)
Fig.1.(a)measurementopportunitytimelineforin-situmeasurementofAMprocesses,whereallprocessingstepsarelinearandparallelprocessingmaynotbepossible. (b)measurementopportunitytimelineforonlinemeasurementofAMprocesseswheresomeparallelprocessingcanbedoneinordertooptimiseonNDEevaluationtime inrelationtoAMbuildtime.
manufacturingspeed,andincludesthetimetakenforthematerial tosolidifyfromamoltenstate.Theresetstageisthetimebetween thelayerbuildstagewherenomeltingoccurs,whereprocesses suchasretractionofthepartinthez-axis,recoatingwithpowder material(inpowderbedfusionprocesses)orresettingtoorigin pointsforthenextlayer(indirectedenergydepositionprocesses) occurs.
IfeachlayerismeasuredwithNDEinstrumentation,theoverall manufacturingtime(tmanufactureNDE)extendsbyafactorthatcanbe definedasthetemporalpenalty(Pt)suchthat
tmanufactureNDE=tmanufacture×Pt. (2)
ScantimesoftheNDEinstrumentarebasedonvariablesdefined asscan speeds(tscan) perdata point, N,and processing/latency speeds (tlatency) per data point, N. For the model presented in
Fig.1(a),a sequential interaction of production and analysis is observed.TheAMmanufacturingwithNDEtimebecomes
tmanufactureNDE=tbuild+N
tscan+tlatency
+treset. (3) FromEq.(3),thetemporalcapabilitycanbedefined,wherealower valueindicatesafasterscanningoftheAMpartinproduction,thus
Pt=N
tscan+tlatency
/(tbuild+treset)+1. (4) ThemodelpresentedinFig.1(b),onlineanalysis,outlinesthat thescanningofthelayerisoccurringinparalleltomanufacture.As such,scantimeandlatencytimepenaltiescanbedisregardedand theoveralltemporalpenaltybecomes1.
Inorder fortheNDEinstrumentationtobedeemedsuitable forintegrationintoaparticularAMmethodology,theaccuracyof thedataitfeedsbackneedstobedefined.Furthermore,thereisa relationshipbetweenthescantime(temporalpenalty)andthe res-olutionofthedata(e.g.pixelsize)oftheinstrumentationthatcan beoptimised.Theimportanceoftheresolutionofdataisshownin anexampleinFig.2,whereamaterialdefectisshownatits orig-inalsize.Theeffectofresizingthisimageisshowntocompletely loseinformationaboutthisdefectandadescriptionofitbecomes impossible.
To quantify the resolution of the data, a spatial capability index(Cs)isdefinedasfollows.Assumingthedataacquisitionof theNDEmethodhasbeenoptimisedtoyielddatawhich isnot under-sampled,theequivalentpixel size (discrimination ofthe instrument)is dependentonboththestep size(h)and resolu-tion(r)ofthemeasuringinstrument.Thestepsize(h)isdefined asthedistancebetweensampleddatapointsandthedefinitionof resolution(r),here,istheminimumdistancebetweentwo resolv-ablepoints,i.etheRayleighcriterion.Scanninginthexyplanewill yieldthedatasetofthelayerbut,sincesomeprocesses(suchas OCT,SRASand XCT)havetheabilitytopenetrate subsurfaceor near-subsurface,thereis asubsurface datasetresolvedin 2D(a tomograph).Thestepsizecould,hence,notbeuniforminall
direc-Fig.2.Anexampleofhowresolutionofthedataisessential.Anoriginaldefectis shownandcontinuouslyresizedtoshowtheeffectoflossofdatatoapointwhere noinformationaboutthedefectcanbeobtained.
tionsandassuchmustbedefinedforeachdimensionseparately, whichwouldthenyielddistinctspatialcapabilitiesforeach dimen-sion.
h=hX,hY,hZ. (5)
Foragivenprocess,therequiredspatialcapabilityofan instru-ment needs to be defined by the minimum defect size, Dmin,
requiredtobeinvestigatedinordertodetermineifthepart pro-ducedisfitforservice,e.g.inSLMdefectsofapproximately10m areexpected[15,16].IfhX,hY,hZ<Dminandtheratioofstepsizeand
resolutionisadequate,thentheinstrumentcanbeclassedviable foruse.However,generallymorethanonepixelisnecessaryfor thedeterminationofwhetheradefectispresentornot.Forthis,a multiplyingfactor,theminimumclustersize(Clmin)needstobe defined.Combiningtheminimumdefectsizeandminimumcluster sizeresultsinacapabilityoftheNDEmethodtoobtaindata,the spatialcapability:(ClminhX,hY,hZ)/r<Dmin.Ifthisspatialcapability isexpressedasafactor,itcanberewrittenas
Cs=rDmin/Clmin(hX,hY,hZ). (6) Aminimumrequiredspatialcapabilityinrelationtothe mini-mumdefectsizeis1atwhichpointtheNDEprocessingparameters will yield data with no lack of information. The outcomes of employingsub-optimalparameters(Cs below1)areoutlinedin Section4.3.
eval-tiononthespatialcapabilityispresented,basedonsimulatedsets ofscandatamimickingcommonlyobservedSLMbaseddefects.
Forthefirstcasestudy,anNDEtechniqueknownasspatially resolvedacousticspectroscopy(SRAS)isusedtoshowthe differ-encebetweenahighresolutionandlowresolutionscan.SRAShas beenoutlinedasaviablecandidateasanNDEmethodfor metal-basedAM[19]andcanbeusedforthedeterminationofsurfaceand nearsubsurfacefeaturedetection.Furthermore,currentresearchis ongoingtomakeSRASapplicableforobtainingsurfacedefectand graininformationonroughsurfaces[20]and,hence,applicablefor AM.Inthepast,SRAShasbeenemployedtoscanoveroptically smoothsurfacesinordertodeterminemicrostructureandgrain orientationofmetalsforhighvalueapplicationsthroughchanges insurfaceacousticwave(SAW)velocityorsignaldropout. Specif-icallySRAShasbeenemployedonAMsampleswiththeintentof developingitintoanin-situinvestigationtechnology[21].SRAS isalaserultrasoundtechniquethatusestwoseparatelasers;one lasergeneratesaSAWontoasampleprojectedthroughadefined grating,andthesecondlaserisusedtopickuptheperturbation causedbythewave,enablingmappingthesurfacethroughpoint scans[22].Processingdatawasobtainedthroughthetimestampsof datacollectionandsetupofscanparameters.Theprocessingtime wasextrapolatedthroughtimestampsofanalysisdatacreation.
For the second case study, example scanning scenarios are shown,usingopticalcoherencetomography(OCT)asanNDE tech-niqueforSLSofpolymerpowdermaterials.IntheworkbyGuan etal.,itwasshownthatOCTiscapabletoscanfordefectsand geom-etryfeaturesonpolymer-basedAMprocesses,bothonthesurface andsubsurface[8].TheOCTsignalisderivedfromback-scattering oflight,hence,ahigherintensityisaresultofhigherback scatter-ingpropertiesofthesample.Theimagedepthisdependentonthe penetrationdepth,whichisdeterminedbythepropertiesofOCT lightsourceandtheopticalpropertiesofthetargetsample.The OCTcasestudywasconstructedtoanalysethespatialcapability andtemporalpenaltyoftwocommerciallyavailableOCTsystems (ZeissCirrusHD-OCT5000[23]andTopcon3DOCT-2000[24]).
3.1. Spatialcapabilityonsimulateddefectdata
Asimulateddatasetwascreatedtodemonstratetheeffectsof changeininstrumentspatialcapability.Thedatasetwasbasedon atypicaldefectarrayforanSLMcomponentwithdefectsizesof approximately100m.Asamplecubeofside10mmwasdefined forthecreationoflayer-basedscaninformation.Inordertomimic a data set that could be obtained with an NDE instrument, a ‘tomograph-like’stackofimageswascreatedatascaleof25m/px. Theselayersweredefinedtohaveathicknessof30m;a com-monlayerthicknessinSLMmanufacture.Thedataforeachlayer wasgenerated withthesolidnoiserender function ata random seedwithinanopen-sourcesoftwarepackagedetailedelsewhere [25].Apseudo-randomnumbergeneratorbasedoncurrenttimewas utilisedtoproduce seedsin therangeof0 to2 ˆ31-1,producing cloud-likevariations.
Forthepurposeofshowingtheeffectofareductioninscaleon spatialcapability,thedatasetimageresolutionwasresizedinsteps
ofthepore.Thefirstdescriptor,fcirc,isdefinedas
fcirc=4A/P2 (7)
whereAisthecross-sectionalareaandPistheperimeterlength ofthepore.Themeasurefcircliesintherange0<fcirc≤1,where
1representsaperfectlycircularcross-section.Thesecondshape descriptor,faspectisdefinedas
faspect=dminor/dmajor (8)
where the dminor and dmajor are the minimum and maximum orthogonaldimensionsofthepores’bestfittingellipse.faspectcan beexpressedwithvalues0<faspect≤1,whereavalueof1indicates aperfectlysphericalporeandapproachingthevalueof0indicates aneedle-likeshape.
4. Casestudies
InordertooutlinehowtheNDEcapabilitiescanbecomparedfor AMpurposes,casestudiesarepresentedinthissection.Scanning environmentswillbepresentedanddiscussedinrelationtotheir applicabilitytoAMprocessesassupportedbytheliterature.
4.1. Casestudy1:SRASforSLM
SRAShasbeenoutlinedasaviablecandidatefor the inspec-tionofpartsproducedusingtheSLMAMprocesspreviously[21]. AschematicofthesetupofaSRASinstrumentisshowninFig.3(a). ThedetectedperturbationfrequencyindicatestheSAWvelocity, wherethevelocitycontrastorwaveabsencecanbeusedtoobtain boththematerialsurfacemicrostructureanddefectinformation. DependingontheSAWwavelength,somesubsurfacedefect infor-mationcanalsobeobtained.ThetypicalSRASscansyielddataas showninFig.3:theopticalmap(b),whichdirectlyindicatesthe surfacecracksandporesandthevelocitymap(c),whichimages themicrostructureofthesamplealongwithdefects.
TheSRAS setupis a scalablesystemand can becustomised dependingontheuser’srequirements;thereisatrade-offbetween accuracyandspeed.Intheworkpublished,therearetwosetsof SRASworkingparametersthatareused,showninTable1(with
saw=24m).IntheworkpresentedbySmithetal.,scanswere conductedex-situonpreparedTi-6Al–4Vsamples.InTable1,the scantimeandlatencytimeoftheinstrumenthavebeencombined. Thedesignoftheinstrumentallowsforindividualselectionofstep sizeaccordingtothemovementaxes utilised.Theresolution is dependentonthewavelengthoftheSAWs.Onlyasinglevaluefor stepsizeisgivenwhichindicatesthath=hx=hywithnoz-axisstep sizepresent.Thescanswereabletogathernearsubsurface informa-tion−thesubsurfacesensitivitydepthisrelatedtothewavelength ofthecreatedSAW,approximately24m.
Firstly,acoarsescanwasconductedtoobtainapproximate sur-facelayerinformation. Thedefined minimumdefect, Dmin, was
Fig.3.(a)schematicoftheSRASsystem,(b)opticalimageand(c)acousticimageobtainedfromSRASscanonAMsamplefrompublishedwork[21].
Fig.4. StepsofmanufacturewithNDEinstrumentation:(a)thedesignofthepart;(b)slicingoftheparttocreatemachinecode;(c)manufactureofthepartonalayerper layerbasisand(d)analysisalsoonalayerperlayerbasis.
Table1
SRASscanningparametersutilisedforSLMsamplemeasurements.AfterSmithetal.[21].
Example Description
MinimumDefect,
Dmin(m)
LayerSize(m) StepSize,
h(m)
Resolution,r
(m)
MinimumCluster Size,Clmin
Numberofdata points,N
tscan(s)+tlatency
(s)
SRAScoarse 50 X:10000
Y:10000
25 100 4 160000 0.0008
SRASfine 20 X:10000
Y:10000
5 100 3 4000000 0.0008
Thesamplemanufacturingtimeofthetestspecimen (dimen-sions:10×10×10mm)wascalculatedtobe2072s,arisingfrom ahatchspacingof75m,beamspeedof600mms−1,layer thick-nessof30mandrecoatingtimeof4s.Usingthisinformation,the temporalpenalty(perlayer)forthecoarseandfinescansusingEq. (4)werecalculatedtobe59and1442,respectively.UsingEq.(6), theresultingspatialcapabilitiesareequalto67and100forthe coarseandfinescan,respectively.Furthermore,dataabout sub-surfacedefectsisalsoavailableusingSRAS−thespatialcapability forsubsurfaceinformationwascalculatedtobe69and21forthe coarseandfinescan,respectively.
Fromthepresenteddata,itcanbeseenthatthespatial capa-bilityoftheSRASinstrumentcanbeconsideredsuitableforboth scanenvironmentsinthisrequirementdefinition(discussed fur-therinthesimulateddatacasestudy).Iftheuserrequiresasmaller Dmin,thespatialcapabilitywouldneedtobechangedaccordingly
− this in turnwill affect thetemporal penalty of the measur-inginstrument.Specifically,forSRASintegrationeffortsintoSLM manufacture,thetemporalpenaltymaycurrentlybeprohibitive. Therefore,furtherworkisstillrequiredtooptimisetheSRASdata
acquisitionspeed withoutcompromisingonaccuracy.However, sinceSRASisascalablesystem,thespatialcapabilityandits tem-poralpenalty can beadjusted to suit theapplication of in-situ monitoringinAM.
4.2. Casestudy2:OCTforSLS
OCThasbeenshowntobeaviablecandidateforSLSpart inter-rogation[8].Thiscasestudyfocussesonhowanend usercould obtaininformationofhowcapablethisinspectionmethodis,with freelyavailableinformation.ThetwocommerciallyavailableOCT systemschosenaretheCirrusHD-OCT5000(referredtoasOCT1) andtheTopcon3DOCT2000(OCT2).AssumingaSLStestspecimen wasproducedwithdimensionsof(10×10×10)mmwithalayer thicknessof100m,meltinglaserscanningspeedof2500mms−1
Fig.5. ProbabilityofDetectionofdefects.Thenumberofporesdetectedreducesdrasticallywithareductioninthespatialcapabilityoftheinstrumentwhilsttherelative densityofporesincreasestoapproach100%density(bulkdensity).Theinsetsshowa3Dinterpolationofthesimulatedscandata.
Table2
ExamplesofOCTscanparametersforNDEcapabilitycalculation.
Example Description
MinimumDefect,
Dmin(m)
LayerSize (m)
StepSize,h(m) Resolution,r
(m)
MinimumCluster Size,Clmin
Numberofdata points,N
tscan(s)+tlatency
(s)
OCT1 30 X:10000
Y:10000
15 5 4 1332000 3.7×10−5
OCT2 30 X:10000
Y:10000
46 6 4 355550 2×10−5
Fig.6.Histogramsrepresentingtheporeareadeterminedbypixelcountingat dif-ferentspatialcapabilities.Theabsolutenumberofdeterminedporesisreduced alteringthedistribution.
Table2.Onlyasinglevalueforstepsizeisgivenwhichindicates thath=hx=hywithnoz-axisstepsizepresent.
Fromtheabovepresenteddata,boththespatialcapabilityand temporalpenalty(forx−y)canbecalculated.Intheliterature,it hasbeenoutlinedthatOCTcanreturnasubsurfacedataset[8]but thematerial-specificinformationisnotavailablethroughthedata sheets.FortheOCT1example,thetemporalpenaltyperlayerwas foundtobe8.5;thespatialcapabilitywasfoundtobe2.5.This indicatesthat,whilsttheinterrogationwouldconsiderablyextend themanufacturingtimeofthesamplecubes,thedatathatcould beobtainedfromtheNDEinstrumentwouldbesufficientforthe
requirements.Incontrast,theOCT2exampleyieldedatemporal penaltyof5.4 perlayerandspatialcapability of0.97. Thetime penaltyforutilisingthisscanningsystemwouldbelower,butthe dataobtainedwouldbeinsufficientfortherequirementsstated above.
Inaddition,theseOCTscanstrategy exampleshelp in deter-miningthebestapproachforintegrationofOCTsystemsforSLS applicationsbasedonuserrequirements.InthecaseofOCT1,the spatialcapabilityissufficientbuteffortscouldbefocussedon opti-misingtheinterrogationtimeperlayer.Inthecase ofOCT,the spatialcapabilitycouldbedeemedinsufficient,soaredesignofthe opticalsystemcouldberecommendedinordertomeet specifica-tions.
4.3. Simulateddefectstudy
Thissectionoutlinestheeffectsofnon-idealspatialcapabilities ofmeasurementinstrumentation,withafocusondetectabilityof defects,aswouldbeobservedinAM.Astatisticalporeanalysisis conductedonthesimulatedsurfaceinformationthatwascreated asdescribedinSection3.1.Thedatamimicsthat,whichcouldbe obtainedfromanAMmanufacturingprocesssuchasSLM.The pro-cessingstepsofsuchamanufacturingmethodareshowninFig.4.A commondesign-to-partsequenceconsistsofthemodellingofthe partinCAD(Fig.4(a)),slicingoftheparttocreatethemachinecode forproduction(Fig.4(b)),manufactureofthepart(Fig.4(c)),and analysis(Fig.4(d)),wherethelattertwostepsoccuronalayerper layerbasis,asisdiscussedpreviously.
Throughthedesignof thespatialcapabilityformula, avalue between0<Cs<1indicatesanon-optimisedscanenvironment.A
Csvalueof1,bydefinition,showsthattheNDEprocessis
Fig.7.Histogramsof(a)circularityand(b)aspectratioofdetectedporesinthesimulateddatasets.TheshapedescriptorsaredefinedaccordingtoEqs.(7)and(8).
hastohavebeensetaccordingtothemicrostructuralrequirements ofthepartinproduction.Forthepurposesofthisstudy,the sim-ulatedscandatawasresizedtoyieldnon-idealspatialcapability valuesandarecomparedtoanidealcasescenario.Theminimum defectsizewasdefinedas100mandminimumclustersizeis2×2 pixels,foralldiscriminationchanges.Therelativedensityofpores presentversusbulkmaterialareapresentwascalculatedthrough pixelcountingasametricdescribingtherelationshipofapparent poresobservedandabulkdensityofthesimulatedpart(100%dense inanidealcasescenario).
WhenthespatialcapabilityofanNDEmethodisinsufficient,the numberofdetectabledefectsreducesdramatically.Thisisshown withtheprobabilityofdetectiondatapresentedinFig.5,wherea spatialcapabilityof0.5(discriminationof50m/pxinthiscase) onlyallowsforthedetectionofapproximately73%ofthepores presentin thedata set.Witha furtherreduction in discrimina-tion,thenumberofdetectableporesapproacheszero.Thisisshown withtherelativepartdensitymeasurementonthesecondordinate inFig.5,whereareductionindiscriminationyieldsameasured volumetricdensityapproaching100%,untilnomoredefectsare detectable.ThisanalysisalignswithworkbyMaskeryetal.who characterisedandquantifiedporosityofAl-Si10-Mgsamplecubes
producedwithSLM[18].Intheirstudy,therelativedensityofthe test cubes,analysed withXCT,closely resemblesthebehaviour observedinthesimulateddataataspatialcapabilityof1.Theinsets inFig.5,a3Dinterpolationofthelayerscandata,showhowthe decreaseinspatialcapabilityaffectstheavailablepixeldata.Aclear visualreductioninpores(portrayedingrey)canbeobserved.
Inordertooutlinehowthedegradingavailabilityofdataaffects measurementofdefects,distributionhistogramsoftheporeareas areshowninFig.6.Aclearreductioninabsolutenumberofpores detectedcanbeobservedforthereducingspatialcapabilities.As soonasthedatasetisresizedtoanon-idealcapability,the dis-tributionbehaviourbecomeserraticandnotrepresentativeofthe defectspresentinthesimulateddata.Itmustbementionedthatthe simulatedpores,similarlytorealdefectsobservedinSLM manu-facture,arenon-perfectspheres.This,hence,warrantstheneedfor investigatinghowporeshapedescriptorsdeviatewiththe alter-ationindiscrimination.
Fig.7 shows the circularityand theaspect ratiohistograms forthesimulatedscandata.Trendstowardsamorecircularpore shape(Fig.7(a))canbeobserved.Again,theabsolutenumberof detectableporesisreflectedbuttheresultsareskewedtowardsan fcircvalueof1,whichismostprominentataspatialcapabilityof
0.2andabove.Theaspectratio,faspect,showninFig.7(b)outlines abroadrangewithfewporesperfectlyround.Thisisalsotobe expectedinarealscenario.Withthespatialcapabilityofthe sim-ulateddatareducing,however,therandomnatureoftheporesis notrepresentedanymore,indicatingapredictablebehaviour.The shapedescriptorsalongsidetheporeareadistributionare essen-tialindefiningshapegeometriesanditcanbeclearlyseenthata reductioninspatialcapabilityhindersthis.
Theabovediscussedsimulateddataoutlinestheeffectswhen thespatialcapabilityisbelow 1.AssumingtheNDEinstrument scanparametershavebeenadaptedappropriately,tocorrelatewith theminimumdefectsize,thecapabilityshouldbeaminimumof 1toavoid lossofdata.However,it mustbepointedout thata spatialcapabilityabove1maynotbeidealbecauseitisclosely linkedwiththescantime.Itshouldbeconsideredwhetherthere isatrade-offthatenablesanincreaseinscanningtimewhilstnot losinginformation.
5. Conclusions
ThecurrentdrivetoutiliseAMtechnologiesforhighvalue appli-cationsisaleadingfactorindevelopingin-situintegrationofNDE methods.Currently,theapplicabilityoftheseprocessesforlayer perlayerscanninghasnotbeenrigorouslyassessed.Inorderto quantitativelyassessthecapabilityofaNDEmethodinanin-situ oronlineintegrationwithanAMprocess,aspatialcapabilityand temporalpenaltymeasureneedtobedeveloped.Thespatial capa-bilitydescribestherelationshipbetweentheminimumdefectsizes, inAMproduction,and scanparametersthattheNDEmethodis requiredtoresolveaccurately.Specifically,someparametersmay not beuniformin alldirections whichis accommodatedin the model.Thespatialcapabilityisdefinedby
Cs=rDmin/Clmin(hX,hY,hZ).
Thetemporalpenaltyassessesthechangeintimefor manu-facturewithandwithoutNDEinstrumentation.Thisrelationship accommodatessequentialprocessingaswellasparallelprocessing inthatthescanlatencytimeoftheNDEprocesscanbedisregarded. Inthiscaseatimepenaltyof1istheresult.Utilisingtheapproachof measuringfortemporalpenaltycanaidinoptimisingthescanning regimeforallowableextratimeintheAMprocess.Thetemporal penaltyisdefinedby
Pt=N
tscan+tlatency
defectsreducesdrasticallybutalsotheshapedescriptorsusedfor characterisingdefectsyieldfalsifieddata.
WithutilisingthisNDEcapabilityapproach,optimisationofthe manufacturingandinterrogationenvironmentcanoccurthrough aquantifiedcomparativeanalysis.
Acknowledgements
This work was supported by “UK Research Centre in Non-destructiveEvaluation”(EPSRCGrantNo.EP/L022125/1), “Metrol-ogyforPrecisionandAdditiveManufacturing”(EPSRCGrantNo. EP/M008983/1)and “In-situMonitoringofComponentIntegrity DuringAdditiveManufacturingUsingOpticalCoherence Tomog-raphy”(EPSRCGrantNo.EP/L01713X/1).
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