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Journal of Materials Processing Technology 210 (2010) 279–287 Contents lists available at ScienceDirect Journal of Materials Processing Technology journal homepage: www.elsevier.com/locate/jmatprotec Selective Laser Melting of thin wall parts using pulse shaping K.A. Mumtaz , N. Hopkinson Rapid Manufacturing Research Group, Loughborough University, Leicestershire, LE11 3TU, UK article info Article history: Received 22 May 2009 Received in revised form 3 September 2009 Accepted 10 September 2009 Keywords: Selective Laser Melting Inconel Pulse shaping Surface roughness abstract Pulse shaping is a technique used to temporally distribute energy within a single laser pulse. This provides the user an added degree of control over the heat delivered to the laser material interaction zone. Pulses that induce a gradual heating or a prolonged cooling effect can be generated with peak power/pulse energy combinations specifically tailored to control melt pool properties and eventual part formation. This investigation used a pulsed 550 W Nd:YAG laser to produce thin wall Inconel 625 ® parts using pulse shapes that delivered a variety of different energy distributions. Parts built with and without pulse shape control were measured for width, top and side surface roughness. The efficacy of pulse shaping control is discussed including potential benefits for use within the Selective Laser Melting process. Pulse shaping was shown to reduce spatter ejection during processing, improve the top surface roughness of parts and minimise melt pool width. © 2009 Elsevier B.V. All rights reserved. 1. Introduction Industry is becoming increasingly interested in Solid Freeform Fabrication (SFF) technologies to produce fully functional metal parts. This family of processes involves a layer-wise shaping and consolidation of material (e.g., powder and wire) allowing parts to be produced with a high geometric freedom directly from a CAD model. The use of SFF has also the potential to drastically reduce the time period between the initial conceptual design of a part and its actual fabrication. A group of SFF technologies known as Direct Metal Laser Fabrication (DMLF) utilize lasers to consolidate metal. One such DMLF process known as Selective Laser Melting (SLM) builds metal parts by melting powder from a powder bed using a laser. 1.1. Selective Laser Melting SLM is a powder bed process that begins with the deposition of a thin layer of powder onto a substrate. A high power laser raster scans the surface of the powder, the heat generated causes powder particles to melt and form a melt pool which solidifies as a consoli- dated layer of material (Santos et al., 2004). Once the layer has been scanned another layer of powder is deposited and is again melted by the laser and solidifies to form the next layer of the part. Fig. 1 shows a schematic of this process. Powder particles that are not melted remain loose and are removed once the component is complete. Supports are required to anchor down certain unsupported features Corresponding author. Tel.: +44 (0) 1509 227 564. E-mail address: [email protected] (K.A. Mumtaz). due to shrinkage and curling of solidifying material. This restricts the process geometric freedom and incurs further post-processing operations to remove supports. The main advantage of SFF processes such as SLM is the capabil- ity to build complex geometries that would otherwise be difficult or impossible to produce using conventional manufacturing pro- cesses. This is due to the versatility, accuracy and small spot size of a laser beam. The possibility to build thin wall parts to a high resolu- tion complements the technology’s main advantage and extends its manufacturing capabilities. However the production of metal parts via SLM has many difficulties. Many processing issues arise due to the use of a high power laser to fully liquefy material from a powder bed. High heat input often causes an increase in material vapourisa- tion and spatter generation during processing. Surface roughness is another SLM issue that is influenced by particle melting, melt pool stability and re-solidifying mechanisms. 1.2. Surface roughness and part resolution The surface roughness of a part is critical in many applications with some applications requiring a surface roughness of 0.8 m or better to avoid premature failure from surface initiated cracking (Dalgarno, 2007). Commercial powder bed machines such as MTT’s Realizer and EOS M270 often require post-processing operations such as surface machining, polishing and shot peening to attain final part surface finish. The top surface roughness of a solidified melt pool can be affected by a rippling effect that occurs due to surface tension forces exerting a shear force on the liquid surface. This is primarily due to a surface temperature difference between the laser beam and the solidifying zone caused by the motion of the laser beam. As 0924-0136/$ – see front matter © 2009 Elsevier B.V. All rights reserved. doi:10.1016/j.jmatprotec.2009.09.011

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Journal of Materials Processing Technology 210 (2010) 279–287

Contents lists available at ScienceDirect

Journal of Materials Processing Technology

journa l homepage: www.e lsev ier .com/ locate / jmatprotec

elective Laser Melting of thin wall parts using pulse shaping

.A. Mumtaz ∗, N. Hopkinsonapid Manufacturing Research Group, Loughborough University, Leicestershire, LE11 3TU, UK

r t i c l e i n f o

rticle history:eceived 22 May 2009eceived in revised form 3 September 2009ccepted 10 September 2009

a b s t r a c t

Pulse shaping is a technique used to temporally distribute energy within a single laser pulse. This providesthe user an added degree of control over the heat delivered to the laser material interaction zone. Pulsesthat induce a gradual heating or a prolonged cooling effect can be generated with peak power/pulse

eywords:elective Laser Meltingnconelulse shaping

energy combinations specifically tailored to control melt pool properties and eventual part formation.This investigation used a pulsed 550 W Nd:YAG laser to produce thin wall Inconel 625® parts using pulseshapes that delivered a variety of different energy distributions. Parts built with and without pulse shapecontrol were measured for width, top and side surface roughness. The efficacy of pulse shaping control isdiscussed including potential benefits for use within the Selective Laser Melting process. Pulse shapingwas shown to reduce spatter ejection during processing, improve the top surface roughness of parts and

h.

urface roughness minimise melt pool widt

. Introduction

Industry is becoming increasingly interested in Solid Freeformabrication (SFF) technologies to produce fully functional metalarts. This family of processes involves a layer-wise shaping andonsolidation of material (e.g., powder and wire) allowing parts toe produced with a high geometric freedom directly from a CADodel. The use of SFF has also the potential to drastically reduce

he time period between the initial conceptual design of a part andts actual fabrication. A group of SFF technologies known as Direct

etal Laser Fabrication (DMLF) utilize lasers to consolidate metal.ne such DMLF process known as Selective Laser Melting (SLM)uilds metal parts by melting powder from a powder bed using a

aser.

.1. Selective Laser Melting

SLM is a powder bed process that begins with the deposition ofthin layer of powder onto a substrate. A high power laser raster

cans the surface of the powder, the heat generated causes powderarticles to melt and form a melt pool which solidifies as a consoli-ated layer of material (Santos et al., 2004). Once the layer has beencanned another layer of powder is deposited and is again melted by

he laser and solidifies to form the next layer of the part. Fig. 1 showsschematic of this process. Powder particles that are not melted

emain loose and are removed once the component is complete.upports are required to anchor down certain unsupported features

∗ Corresponding author. Tel.: +44 (0) 1509 227 564.E-mail address: [email protected] (K.A. Mumtaz).

924-0136/$ – see front matter © 2009 Elsevier B.V. All rights reserved.oi:10.1016/j.jmatprotec.2009.09.011

© 2009 Elsevier B.V. All rights reserved.

due to shrinkage and curling of solidifying material. This restrictsthe process geometric freedom and incurs further post-processingoperations to remove supports.

The main advantage of SFF processes such as SLM is the capabil-ity to build complex geometries that would otherwise be difficultor impossible to produce using conventional manufacturing pro-cesses. This is due to the versatility, accuracy and small spot size ofa laser beam. The possibility to build thin wall parts to a high resolu-tion complements the technology’s main advantage and extends itsmanufacturing capabilities. However the production of metal partsvia SLM has many difficulties. Many processing issues arise due tothe use of a high power laser to fully liquefy material from a powderbed. High heat input often causes an increase in material vapourisa-tion and spatter generation during processing. Surface roughness isanother SLM issue that is influenced by particle melting, melt poolstability and re-solidifying mechanisms.

1.2. Surface roughness and part resolution

The surface roughness of a part is critical in many applicationswith some applications requiring a surface roughness of 0.8 �m orbetter to avoid premature failure from surface initiated cracking(Dalgarno, 2007). Commercial powder bed machines such as MTT’sRealizer and EOS M270 often require post-processing operationssuch as surface machining, polishing and shot peening to attainfinal part surface finish.

The top surface roughness of a solidified melt pool can beaffected by a rippling effect that occurs due to surface tension forcesexerting a shear force on the liquid surface. This is primarily dueto a surface temperature difference between the laser beam andthe solidifying zone caused by the motion of the laser beam. As

280 K.A. Mumtaz, N. Hopkinson / Journal of Materials Processing Technology 210 (2010) 279–287

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Fig. 1. Selective Laser Melting process.

he thermal gradients reduce, gravity and surface curvature coun-eract the external shear force and eventually restores the surfaceeight of the melt pool to the free level (Ramos et al., 2003). How-ver, viscous forces delay this relaxation process and quick meltool solidification time often ensures that complete relaxation isot fully achieved.

The roughness of a part can also be affected by a phenomenonnown as balling. Balling is the breakup of the melt pool into smallpheres. It occurs when molten material does not wet well to thenderlying substrate due to high surface tension differences gener-ted as a result of variations in thermal properties across the meltool (Fuh et al., 1995; Kruth et al., 2003; Morgan et al., 2004). Ther-al gradients cause a thermocapillary flow of a fluid within theelt pool from regions with low surface tension to regions with

igh surface tension, known as Marangoni convection (Romboutst al., 2006). The breaking up of the melt pool into smaller enti-ies reduces the variation in melt pool surface tension. Balling canncrease with the generation of excessive molten material or if vis-osity within a melt pool is too low (Agarwala et al., 1995). Krutht al. (2004) stated that when the total surface of a molten poolecomes larger than that of a sphere with the same volume, thealling effect takes place. Balling is a severe impediment on inter-

ayer connection, it decreases part density and increases top/sideurface roughness. The side roughness of a part can also increaseue to partially melted, entrained powder particles that stick andgglomerate to the outer edge of the solidified melt pool known

s “satellite formation” or “hillocks” (Tolochko et al., 2004; Elsen,007). Satellite formation mainly occurs when powder particles areot given enough time or heat to penetrate the melt pool beforeelt pool solidification.

Fig. 3. Laser input demand (a

Fig. 2. Pulse shape generation.

The minimum achievable feature size (resolution) has greatinfluence on part accuracy. Dimensional tolerances and repeatabil-ity are key factors with any DMLF technology. Minimum resolutionis of high importance in the design of functional parts, e.g., for thinwalls or open cell structures in medical applications. Thin walls arean example for so-called positive minimum feature size (smallestsolid part possible) while open cells are an example for negativeminimum feature size (smallest gap size possible) (Rehme andEmmelmann, 2005).

Surface roughness and part resolution are all heavily dependenton laser processing parameters and melt pool control. A techniqueknown as pulse shaping has been shown to extend the degree ofcontrol over a laser’s energy distribution and therefore has thepotential to improve the control over melt pool formation, stabilityand eventual part properties (Fig. 2).

1.3. Pulse shaping

A pulsed laser emits bursts of energy that consist of a fixedamount of energy for a specified duration. Pulse shaping is a tech-nique used to temporally distribute energy within a single laserpulse. It can also be defined as a variation in power supplied toa laser to change the shape of the output pulse and subsequentlythe heat distribution within the pulse (Kanzler, 2006). Changing theenergy distribution within a pulse can completely change the melt-ing behaviour of a material. Pulse shaping can be accomplished bydividing the pulse’s current used to excite a laser flash lamp into

as many as 20 individual sectors and specifying the duration andpeak power of each sector. The current supplied causes the flash-lamps to emit light that is absorbed and amplified by the Nd:YAGcrystal (only for Nd:YAG laser). This amplified light is emitted in

) and laser output (b).

K.A. Mumtaz, N. Hopkinson / Journal of Materials Processing Technology 210 (2010) 279–287 281

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2.1. System setup

The SLM system used within this investigation included a GSILumonics JK701H Nd:YAG laser. The laser has a TEM00 Gaussian

Fig. 4. Ramp Up (a), Ramp Dow

hort bursts/pulses through various focusing lenses and eventuallynto a work piece as shown in Fig. 3. The electric current supplieds therefore one of the main factors that dictate the characteris-ics of the laser pulse. This allows the user to specifically tailor thenergy distribution to the nearest 0.5 ms within a single laser pulse.he electric current supply is set using a Hgt control ranging from% to 100%, 0% indicates no current and 100% indicates maximumurrent. Fig. 3(a) shows an example of a standard pulse’s demandrofile. This is known as a Rectangular pulse shape or “top hat”ulse shape with power densities remaining nominally constanthroughout the pulse. Rectangular pulse shapes are the simplestnd most extensively used laser pulse shape within academia andndustry containing only one energy sector. This pulse shape ised to the flashlamps but due to the filter effect a more realisticutput profile of the laser is represented in Fig. 3(b). With mostolid state lasers such as the Nd:YAG, the use of a Rectangularulse shape input creates an overshoot that can be between 75%nd 100% over the allocated average peak power (Ppav) for the first.7–1.1 ms and comprises of 2–5% of the pulse energy (Bransch etl., 1994). The extent of the overshoot varies according to the laserarameters. This overshoot can be beneficial in regard to increasedenetration in laser drilling (Cheng et al., 2000), however an oversage of energy within a very short space of time can increaseaterial spattering (Petrov et al., 1992). After the overshoot the

aser power delivery normalises to its steady state value for theajority of the pulses duration. This is then followed by an abrupt

oss of power that results in rapid cooling of the processed mate-ial. The standard pulse shape’s laser output will characteristicallyemain the same even with use of varied pulse durations and pulsenergies.

Pulse shaping research has mainly focused on the use of twoulse shapes, Ramp Up and Ramp Down. Fig. 4(a) and (b) showshe demand input and output of a Ramp Up and Ramp Down pulsehape. As the names suggest these pulses either emit the major-ty of their power early or late within the pulse. This equates toither a gradual heating or gradual cooling of material. Howeverulse shapes can be adjusted such that a very complex heatingistribution is applied, as shown in Fig. 4(c). The range of useableeak power/pulse energy combinations at a fixed pulse durationan be extended allowing a further improved control over laserrocessing.

Within the laser welding of metal sheet studies have shown thatltering the laser current input demand and producing alterativeulse shapes are beneficial in reducing spatter generation, porosityormation, hot cracking and improvement of weld surface finishWeedon, 1987; Badawi et al., 1989; Petrov et al., 1992; Katayamat al., 1993; Bransch et al., 1994).

Very limited work to date has been conducted using pulse shap-ng techniques to laser process metal powder. Sparks et al. (2006)

sed a 1 kW CO2 diode laser to melt powder fed H13 tool steel.rom preliminary studies it was found that varying the duration ofRamp Down pulse shape influenced microstructure grain growthnd could potentially improve properties such as part hardness oratigue strength.

and complex (c) pulse shapes.

2. Experimental methodology and testing

A variety of Ramp Up and Ramp Down pulses were generatedwhen producing thin wall parts measuring 25 mm in length fromfour 100 �m powder layers. Parts were built on a 10 mm thick steelsubstrate. The pulse shapes employed were progressively increasedin duration and overall energy. The effects of pulse shaping on parttop/side arithmetic average surface roughness (Ra) and width weretested. Sample surface Ra was measured three times for each sam-ple using a Talysurf CLI 2000. The Talysurf evaluated 12.5 mm of thesamples surface with a cut-off length of 2.5 mm. Fig. 5 illustratesthe surfaces of the thin wall part that were measured for rough-ness. Sample width was measured using digital callipers along threesegments of the sample’s length.

The most effective pulse shapes were identified and used to pro-duce larger thin wall test parts 25 mm in length built from 80 �mto 100 �m powder layers. These were tested for Ra in multipledirections (including vertical side Ra). Laser repetition rate andscan speeds remained fixed at 40 Hz and 400 mm/min, respectivelythroughout all experimentation. These were based upon parame-ters developed by Mumtaz and Hopkinson (2008) when optimisinglaser process parameters in producing thin wall Inconel 625® withlow top/side Ra using non-pulse shaping techniques.

The degree of plasma plume generated during processing wasalso measured during processing. A plasma plume is ionised metalvapour that can exert a recoil pressure on the melt pool. Increases inplasma plume intensity are directly related to increases in spatterejection (Park and Rhee, 1999) leading to powder bed contamina-tion and obstruction of powder depositor/leveller. Plasma plumeheight was measured using a fixed digital video camera and com-puter software ImageTool to identify a link between the use ofcertain pulse shapes and the amount of spatter generated duringprocessing.

Fig. 5. Top/side Ra measurement of thin wall part.

282 K.A. Mumtaz, N. Hopkinson / Journal of Materials Processing Technology 210 (2010) 279–287

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Fig. 6. Optimised thin wall sample and stan

rofile, a spot size of 0.8 mm and a maximum power output of50 W. The pulses of laser energy generated by the flash lamps areed through a Ø1 mm silica optical fibre delivery cable to the laseread and are deflected through 90◦ by a reflecting mirror onto a

ocusing optic. The light is focused and passes through the laserozzle onto the powder bed. Powder is deposited onto a steel sub-trate that is itself placed on a processing table that is driven by a-axis CNC controlled machine. The laser head remains static dur-

ng processing but can move along the z-axis prior to processing.rgon gas was fed through the laser nozzle onto the processing areat a rate of 10 ml/s to protect the parts from the effects of oxidis-tion. Pulse shape monitoring was undertaken using an externallytted digital storage PC oscilloscope (PicoScope 3205) to measurend analyse voltage waveforms.

.2. Material characterisation

Inconel 625® powder (Sandvik Osprey, UK) was supplied sizedo 53 ± 25 �m. The exact particle size distribution was measured toe a D(v, 0.1) of 22.51 �m (10% of the volume distribution is belowhis value), D(v, 0.5) of 45.48 �m (volume median diameter, 50% ofhe distribution is above and 50% is below this value) and a D(v, 0.9)f 58.59 �m (90% of the volume distribution is below this value).

. Experimentation

Ramp Up and Ramp Down pulse shapes were used to producehin wall parts. A total of 56 parts were produced, tested andompared to the properties of parts produced using a standardectangular pulse shape (non-shaped) developed in other workMumtaz and Hopkinson, 2009). It was envisioned that the use ofulse shaping would offer a more precise and tailored control overhe heat input and would allow a refining and improvement overhe use of standard Rectangular pulses.

.1. Standard Rectangular pulse (non-pulse shaped)

Fig. 6 shows the standard Rectangular pulse shape used in pro-ucing a thin wall part (0.49 mm in width) with low top (9 �m) and

able 1amp Up/Down pulse shape processing range.

Pulse shape Pulse width (ms) Pulse energy (J)

Ramp Up 1.7–10 0.6–2.2Ramp Down 1–10 0.5–2.5

Rectangular pulse shape input and output.

side Ra (10 �m) developed in other work (Mumtaz and Hopkinson,2008). This pulse was produced without the use of pulse shapingand was used for comparison with parts produced using pulse shap-ing techniques. An image of the central portion of the top surfaceof the thin wall part is also displayed within the figure. The averagepeak power of this pulse was 1.4 kW, however the maximum peakpower as a result of overshoot was 1.8 kW. It was observed thatovershoot not only occurred with the pulse’s power but also withthe pulse’s duration. Instead of being set at a minimum 0.5 ms induration the pulse extends to 0.7 ms, this extension increases theheating time and potentially the volume of liquid produced andwidth of the part. During processing a plasma plume of approxi-mately 5 mm in height was produced from the processing area.

3.2. Ramp Up and Ramp Down pulse shapes results

A variety of Ramp Up and Ramp Down pulse shapes were gen-erated and used to process four layers of Inconel 625®, each with alayer thickness of 100 �m. The Ramp Up pulses varied from 1.7 msto 10 ms and contained pulse energies and peak powers rangingfrom 0.6 J to 2.2 J and 0.7 kW to 1 kW, respectively. Note, it was notpossible to produce Ramp Up pulses shorter than 1.7 ms in dura-tion due to the nature of pulsed laser generation creating an initialspike at the beginning of the pulse. This needed to be eliminatedin order to allow gradual Ramp Up power delivery. This was onlyachieved with extension of the pulse duration above 1.7 ms. RampDown pulses were easier to generate and varied between 1 ms and10 ms and contained pulse energies and peak powers ranging from0.5 J to 2.5 J and 1.3 kW to 2 kW, respectively. The ranges of RampUp and Ramp Down parameters are shown in Table 1.

Due to the energy distribution within a Ramped Up pulse shape,melt pool generation is more likely to occur at the end of the pulsewhen peak power is at its highest. Leading up to the main peakpower the gradual increase in laser energy heats up the mate-

rial and reduces its reflectivity, allowing energy to be more easilyabsorbed. As a result of this energy distribution the peak powerrequired to melt Inconel 625® was on average 0.8 kW less than thatused within the Ramped Down pulse shapes. This ramping up ofenergy can therefore be viewed as a preheating of material, reduc-

Repetition rate (Hz) Power (W) Scan speed (mm/min)

40 24–88 40040 20–100 400

K.A. Mumtaz, N. Hopkinson / Journal of Materials

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ig. 7. Surface Ra , width and plasma plume of thin walled part produced using Rampp and Ramp Down pulse shapes.

ng the thermal energy required to achieve full melting and also themount of plasma plume/spatter generated during processing dueo a less aggressive heating regime.

Fig. 7 displays top/side Ra, width and plasma plume height ofhin walled parts created using the variety of Ramp Up and Rampown pulses. Trends reveal that top Ra does not vary consider-bly (9–15 �m) with the use of Ramp Up pulse shapes rangingrom 1.7 ms to 10 ms in duration. Within laser processing of metalowders a lot of energy is required to initiate a melt pool dueo high reflectivity. Once the melt pool has been initiated theatent heat of fusion has been overcome, the material’s reflectiv-ty drops and subsequently requires less energy to remain molten.he late melt pool formation followed by rapid solidification doesot allow surface profile variations to reduce through relaxationechanisms (movement of fluid due to gravity). This in combina-

ion with the use of low peak powers (less recoil pressure) resultsn top Ra values that do not considerably vary. Ramp Up part sidea (14–42 �m) varied more than top Ra and degraded as pulseuration increased. This may be attributed to more liquid beingroduced with the use of longer pulse durations causing the melt

ool width to expand and cause larger thermal variations acrosshe melt pool, possibly promoting balling perpendicular to the meltool.

However this increase in side Ra is more likely to be a result ofartially melted powder particles outside the melt pool agglomer-

Processing Technology 210 (2010) 279–287 283

ating and balling up into small spherical entities, attaching to theedges of the main melt pool, otherwise known as satellite forma-tion. A larger melt pool will have a greater thermal mass to transferinto surrounding powder particles resulting in an increase in par-tially melted powder particles (satellites) that attach to the edge ofthe melt pool. Due to the use of generally low peak powers withRamp Up pulses, lower recoil pressures are exerted on the meltpool, possibly allowing this satellite formation to settle and attachto the edge of the melt pool. Larger recoil pressures generated asa result of higher peak powers could have improved the melt poolwetting behaviour to the substrate and potentially reduced side Ra

as satellites may have been forcefully detached from the extrem-ities of the melt pool onto the powder bed. The lowest combinedtop/side Ra (10 �m and 23 �m, respectively) was achieved witha 1.7 ms Ramp Up pulse shape using a pulse energy of 0.7 J and apeak power of 0.8 kW (marked with “RU1” in Fig. 7 with actual pulseshape and sample produced shown in Fig. 8 (b)). Due to the low peakpower with the Ramp Up energy distribution a minimum level ofplasma plume/spatter was generated during processing (1 mm inheight). As a result of low plasma plume height the negative effectsassociated with spatter generation during SLM processing would bereduced. This Ramp Up pulse shape is examined further in Section3.3.

The use of Ramp Down pulse shapes appears to have a pos-itive effect on top/side Ra with the use of shorter pulse durations(1–2 ms). Fig. 7 shows that lowest top Ra of 6 �m was achieved witha 1.5 ms Ramp Down pulse with 1.1 J of pulse energy (marked with“RD1” in Fig. 7 with the actual pulse shape and sample producedshown in Fig. 8(c)). This pulse is further examined in Section 3.3.Ramp Down energy distributions promote an early melt pool for-mation due to the use of high peak power early within the pulse.This causes the melt pool to be more prone to expansion as fur-ther energy is used to increase the volume of liquid within themelt pool. This promotes further satellite formation as heat is givenmore time to dissipate from the solidifying melt pool into the pow-der bed forming partially melted powder particles, causing sideRa to increase. This is reflected in Fig. 7 with Ramp Down side Ra

being generally higher than that of Ramp Up pulses at similar pulsedurations. As with Ramp Up pulses, increases in Ramp Down pulseduration increases side Ra.

During Ramp Down pulse shape generation an unexpected pulseshape was generated. A 1 ms pulse was split into two sectors, thefirst sector was set to 39 Hgt and the second sector to 0 Hgt. It wasexpected that the pulse would follow the same energy distribu-tion as that of the optimised 0.5 ms Rectangular pulse (reaching0.7 ms in duration) as the power would essentially only be presentwithin the first 0.5 ms sector. However the result was unexpectedwith the pulse’s total duration being Suppressed down to 0.5 ms(marked with “S1” in Fig. 7 with actual pulse shape and sampleproduced shown in Fig. 8(d)). By inserting a second sector with ademand of 0 Hgt the pulse duration is effectively reduced in orderto achieve zero power between 0.5 ms and 1 ms (second sector).The Suppressed pulse shown in Fig. 8(d) had the same peak poweras the standard optimised Rectangular pulse (1.8 kW) but with 0.3 Jless energy and shorter duration (0.2 ms shorter). This resulted in asample measuring 0.42 mm in width (Suppressed pulse and sam-ple are shown in Fig. 8(d)). The width of the sample was reducedcompared to the Rectangular pulsed sample due to reduced pulseduration and pulse energy as in Fig. 8(a). A shorter laser on-timerestricted the melt pool width as heat had less time to conduct radi-ally from the centre of the melt pool inhibited satellite formation at

the edges of the melt pool. Lower pulse energy reduces the volumeof liquid produced within the melt pool. The high peak power atthe beginning of the pulse is sufficient to generate a melt pool thatvery rapidly solidified. The low pulse energy caused plasma plumeto be restricted to 3 mm. The combination of low melt pool width

284 K.A. Mumtaz, N. Hopkinson / Journal of Materials Processing Technology 210 (2010) 279–287

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Fig. 8. Standard Rectangular pulse shape

nd sufficiently high peak power allowed the sample to possess aow top/side Ra of 10 �m.

.3. Test part validation

Initial pulse shape experimentation in Section 3.2 had identifiedhree pulse shapes that potentially held advantages over the usef the standard non-shaped Rectangular pulse. These advantagesnclude improvements to part properties such as surface rough-ess, part width and reduction in plasma plume/spatter generationuring processing. In order to validate and test the effectiveness ofhese pulse shapes, taller thin wall parts were built. These thin wallarts were 25 mm in length and consisted of 80 �m and 100 �mowder layers. Three test parts were built for each of the four dif-

erent pulse shapes. The test parts were measured for top Ra andide Ra in horizontal and vertical directions. The results for the testarts produced using a standard Rectangular pulse and the threeffective pulse shapes are shown in Fig. 9.

Fig. 9. Thin wall part surface roughness and width.

hree effective pulse shapes and samples.

3.3.1. Results and discussionFig. 9 shows the results of surface Ra and width of the thin wall

structures made using the different pulse shapes. Fig. 10 shows theside view of some of the thin wall parts produced.

3.3.1.1. Rectangular pulse. The Rectangular pulse as expected pro-duced thin walls (0.62 ± 0.04 mm in width) with a top Ra values(9 ± 2 �m) lower than that of side Ra (13 ± 4 �m horizontal and15 ± 5 �m vertical). It was discovered that the side Ra in the verti-cal direction was higher than that of the side Ra in the horizontaldirection. This could be a result of interlayer connections betweenmelted layers of powder increasing Ra in this direction. Measuringside Ra along the horizontal axis will only take into considerationone layer. Measuring in the vertical axis measures across mul-tiple layers, a melted interlayer connection has the potential toincrease side Ra. The thickness of the thin walled structure mea-sured 0.62 ± 0.04 mm with a standard deviation of 0.03. Using thesame laser parameters a thin walled part produced from four layersmeasured lower at 0.49 mm (Section 3.2). This variation in mea-sured wall thickness could be related to the multiple reheatingcycles and heat build-up when producing tall parts. Four 0.1 mmlayer will produce a thin wall not more than 0.4 mm in height,there would not be a larger degree of heat buildup as the substratewould very quickly conduct heat away from the thin wall structure(Morgan et al., 2001). The processing of further layers (80 layers inthis case) will cause the average width of the wall to increase dueto multiple reheating cycles and build up of heat within the bulk ofthe processed Inconel structure. More heat buildup will cause themelt pool to expand as more heat is available for powder particlesto melt. This expansion of the melt pool with taller specimens mayalso be a reason why the side Ra in the horizontal direction for the

test parts are higher than those produced from four 0.1 mm lay-ers. Fig. 10 shows the side view of the thin wall structure producedusing a Rectangular pulse. The top and edge profile for the structureis flat and consistent. This indicates that the heat input deliveredto the material was sufficient in creating flat consistent melt pool

K.A. Mumtaz, N. Hopkinson / Journal of Materials Processing Technology 210 (2010) 279–287 285

arts p

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Fig. 10. Side view of thin wall test p

hat did not suffer from part distortion as a result of excessive heatnput. The height of plasma plume generated during processingsing the Rectangular pulse was approximately 5 mm, the sameesult measured in early experiments employing the same pulsehape.

.3.1.2. Ramp Up pulse. Section 3.2 had identified that a Rampp pulse had been particularly useful in minimising plasmalume/spatter generation during processing. This pulse used theame pulse energy as that of the Rectangular pulse but insteadpread the energy over a period of 1.5 ms (as opposed to 0.7 ms)nd operated at a lower peak power of just 0.8 kW (as shown inig. 8(b)). Compared to the other three pulse shapes, the Ramp Upulse was the most successful in its reduction of spatter gener-tion producing only 1 mm of plasma plume. This observation ofower spatter ejection during processing is consistent with otheresearches that have employed Ramp Up pulse shapes to laser weldetal sheets (Katayama et al., 1993; Fujinaga et al., 2000; Gower et

l., 2005; Pan et al., 2005). As expected the side Ra (17 ± 8 �m hor-zontal and 22 ± 5 �m vertical) of parts processed using this pulseegraded as a result of increasing pulse duration due to satelliteormation. Late melt pool generation and rapid melt pool solidifi-ation occurred as a result of the Ramp Up energy distribution, thisroduced a lower volume of liquid present within the melt poolnd subsequently a smaller part width (0.6 ± 0.02 mm with a stan-ard deviation of 0.01). Fig. 10 shows the side view of the thin walltructure produced using the Ramp Up pulse. The top edge profilef the structure is not completely flat and consistent. It is possiblehat the use of low peak powers caused bulges on the top surfaceo appear. Low peak powers exert lower recoil pressures on a melt

ool. The recoil pressure contributes to reshaping of the melt poolrom a spherical structure to a flatter wider profile. Generally thehape of the melt pool is dominated by surface tension forces whichre affected by melt pool temperature variations. If inconsistenciesxist within the melt pool and powder bed, recoil pressures can

roduced using various pulse shapes.

then assist the melt pool in acquiring a more uniform consistentshape (due to a mechanical force compacting the surface of themelting pool). If lower recoil pressures are present then the incon-sistencies that form during melt pool solidification will be moreheavily influenced by thermocapillary flows and surface tensioncaused by thermal temperature variations. The low heat input andlow HAZ produced as a result of the Ramp Up energy distributionmay alleviate processing issues associated with shrinkage, residualstress build-up and cracking.

3.3.1.3. Ramp Down pulse. The Ramp Down pulse had been identi-fied in Section 3.2 as the pulse that would produce parts with thelowest top Ra. This pulse had the same peak power as the Rectan-gular pulse but contained a higher pulse energy of 1.1 J spread overa longer duration. Fig. 9 shows the result of this pulse, the top Ra

and side Ra (horizontal and vertical) were measured to be 8 ± 3 �m,26 ± 5 �m and 28 ± 7 �m, respectively. The top Ra of the parts waslower than any of the other parts produced with other pulse shapes.The high temperature generated using this pulse increased themelt pools viscosity, this combined with the increased melt poolsolidification time assisted the movement and spreading of moltenmaterial reducing variations in overlapping melt pools. As expectedthe side Ra values were the highest out of all the effective pulseshapes. This was because the pulse contained the largest pulseenergy of 1.1 J. This combined with longer pulse durations (1.6 msactual) causes a larger volume of liquid to be produced and a sub-sequent widening of the melt pool. The majority of the heat fromwithin the melt pool is drawn away from the edge of the melt poolinto surrounding material and environment, causing large ther-mal gradients between the centre and extremities of the melt pool.

Satellite formation increased as more energy and time was givenfor partially melted particles to agglomerate and attach to the edgeof the melt pool, subsequently increasing side Ra. The wall thick-ness was 0.79mm ± 0.08 with a standard deviation of 0.06, this wasthe largest wall thickness out of all the samples due to the higher

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ulse energy used during processing. Fig. 10 shows the side viewf the thin wall part produced using the Ramp Down pulse. The topdge profile is not flat and dips towards the centre. This is possibly aesult of too large a heat input causing large amounts of powder tonter the melt pool. As more powder enters the melt pool there isess material available for the laser to process in the direction of thecan causing a reduction in melt pool widths and height. During therst series of pulses, molten pools are created, which attract pow-er particles lying next to it under capillary action (Song, 1997).his leaves areas deficient in powder at the position of the secondet of pulses and after solidification a depression is formed there.ue to the Ramp Down pulses higher energy and stronger heatingffect the plasma plume/spatter generation during processing wasigher as a result of 6 mm plasma plumes. The larger spatter gen-ration with the use of Ramp Down pulses has also been observeduring the laser welding of metal sheets (Tzeng, 2000; Gower et al.,005).

.3.1.4. Suppressed pulse. The Suppressed pulse was able to min-mise the laser on-time down to 0.5 ms. The pulse was also designedo contain a high peak power, low energy and short duration.esults indicate that the thin wall structure produced had a lowop and side Ra (10 ± 2 �m top, 12 ± 3 �m horizontal and 15 ± 6 �mertical) that were very similar to those produced with the Rect-ngular pulse. As expected the melt pool width remained lowroducing an average wall width of 0.56 ± 0.04 mm with a stan-ard deviation of 0.02. This was 0.06 mm thinner than the thin wallart produced using the Rectangular pulse. In addition the part wasrocessed using a lower pulse energy of 0.42 J, this could assist ineducing part distortion due to a lower heat build-up. Due to theelt pool width remaining relatively small, the melt pool solidi-

ed at a faster rate than that of a larger melt pool. This reducedolidification time restricts the time available for melt pool insta-ilities to develop and satellite formation. The low energy withinhe pulse reduced the plasma plume height to 3 mm such that spat-er generation during processing was minimal. It should be notedhat a reduction in plasma plume height may indicate a reduction inhe magnitude of recoil pressure exerted on the melt pool. Fig. 10hows the side view of the thin wall part created using the Sup-ressed pulse. This structure has sharp edge profiles and a level topurface, similar to that produced using the Rectangular pulse. Thisndicates that a correct level of material heating occurred such thatnconel successfully melted without causing too much part distor-ion or slumping of parts due to insufficient powder. However theottom right corner of the thin wall part did not fully bond/attacho the steel substrate. Warping caused the Inconel 625® wall tourl away from the substrate. The low energy and short pulse dura-ion may not have provided a sufficient enough bond between thenconel and steel substrate. However this lack of bonding was onlybserved in one of three thin wall parts with the other two appear-ng to have fully bonded. This sharp edge profile is possibly due tohe thin melt pools produced and relatively quick melting and cool-ng of the melt pools. Commercial systems such as MTT SLM processmit their laser output in short burst in order to minimise the HAZnd reduce part distortion. However short bursts are not able toully simulate that of a Suppressed pulse due to the continuousave output not generating high peak powers as those achievedith a pulsed wave laser.

. Conclusions

Ramp Up pulse shapes generally operated at lower peak powerss compared to standard and Ramp Down pulses. This is because thenergy distribution induces a gradual heating of powder particles.he materials’ reflectivity reduces as its temperature increased,

Processing Technology 210 (2010) 279–287

this reduced the peak power required to induce full melting. Thegradual heating could be viewed as preheating reducing spattergeneration during processing. Ramping up was not effective inreducing top/side Ra due to late melt pool generation and use oflow peak powers. However due to low heat input, Ramp Up pulsesmay be effective in reducing distortion due to shrinkage and thusimprove the accuracy of parts and help to alleviate mechanicalstresses. Ramp Down pulse shapes were able to minimise top Ra dueto early melt pool generation, increased pulse duration, increasedenergy, reduced melt pool viscosity and more time being availablefor capillary and thermocapillary flows to rearrange liquid withinthe melt pool. The external mechanical force applied by recoil pres-sures was also a factor in flattening and smoothing the top surfaceprofile of the melt. However due to the increased heating the vol-ume of liquid present within the melt pool increased causing themelt pool to expand in width. This gave more time for heat to con-duct from the melt pool into the surrounding powder, partially meltpowder it and forming a small agglomerated molten spheres thatattached to the edge of the melt pool, subsequently increasing sideRa.

A Suppressed pulse shape that consisted of a high peak power,low energy and short time duration proved to be the most effec-tive pulse shape. It enabled an aggressive rapid melting and rapidcooling of material including the generation of high recoil pres-sures exerting an external force on the melt pool. This improvedthe wetting of the melt pool onto the substrate within a shortspace of time and flattened out the top surface profile of the meltpool. The high recoil pressure may assist in detaching any satelliteformation from solidifying on the edge of the melt pool, result-ing in a lower side surface roughness. As a result of the shortlaser on-time and low pulse energy the width of the melt poolwas reduced due to less energy and less time for heat to diffusesideways causing a narrowing of the melt region and inhibitingsatellite formation. The added degree of control available throughpulse shaping improved certain part properties producing supe-rior high resolution parts with combined low top and side surfaceroughness.

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