influence of surface depression and convection on arc weld geometry

8
8/12/2019 Influence of Surface Depression and Convection on Arc Weld Geometry http://slidepdf.com/reader/full/influence-of-surface-depression-and-convection-on-arc-weld-geometry 1/8 INFLUENCE OF SURF CE DEPRESSION ND CONVECTION ON RC WELD POOL GEOMETRY M L Lin and T W Eagar Materials Processing Center Massachusetts Institute of Technology Cambridge, Massachusetts ABSTRACT The relative importance of surface d e p re ssion and convection in determining the depth of w e l ~ penetra tion in sta tionary GTA welds has been studied. The results in d i ca t e that a deep crater de p r ession forms on the surface of a stee l weld poo l at currents in excess of 250 amperes. During the transition from shallow to deep penetration, the depression grows from one millimete r or l ess to four or five mil l imeters with an increase of only twen ty amperes. Such a dram at i c c hange cannot be explained due to th e plasma jet momen tum alone . It is propose d that the major cause of the deep penetration at these current l eve ls is a vortex which is created by circumferential rotation of the weld pool. Some evidence suggests that the deep vo rtex is self-stabilizing a nd that t h is creates a h ysteresis i n the weld penetrat io n as t he current is ramped upward a nd downwa rd through the trans ition fr o m s h allow to deep penetration. I t is bel iev ed that this vortex depression is the major cause of finger penetration in GM welding as w ell . Tr avelling GTA we lds were also made to investigate t he effects of deep surface depressio n on weld defect formatio n. High speed cinemapho t ography was used to show the flow behavior from the front to th e back of th e weld pool . In s t eels, and in t i t anium allo ys , this flow is most likely driven by s urface tension gradients. It was f ound that the deep vortex penetra tion and the rearward fluid f l ow can ex p lain h ~ p e bead, undercutting and tunnel bead defects. It is bel ieved t hat a Sim ila r mechanism is responsible for hol low bead defects in stove pi pe welding. INTRODUCTION In o rd er to improve produ ctivity mo r e use is being made of a u tomated welding; however, as a result a nu mber of problems arise which seldom occur in manua l welding . Two of the most fundame n ta l concerns are sea m tracking and control of weld bead geometry , both of which must be cont r olled if a reliable weld is to be produced. In this paper several of the factors controlling weld be a d geomet ry wil l be discussed. One of the diffic ulti es en c oun tered in a pr ior i p redic ti on of weld shape is th at many parameters must be taken into accou nt because a ll a r e found to have more or less influence on the weld pool geometry. If the welding process i s to be automated with c l os e d l oop contro l of the we l d zone size, it is desirable to more fully und erstand the mechanisms w hich influence heat and fluid flow in th e molten weld pool so that the influence of th ese process parameters can be understood. Most o f the fundamen t al research work on gas tungsten arc welding has been limited to low current ranges, i . e . less than ab o ut 200 amperes due to instabilities in the liquid pool and to the pr esence of defects such as humping and undercutti ng at higher currents. l{hile good 63 agreement has been found between empirical data and the predicted values of weld pool geometry at low cur re n ts when the current is increased to higher ranges , e . g. mor e than 250 ampe r es more scatter is obtained. It is be l ieve d t hat surface depression a nd convec ti ve fl o w in the weld pool may begin to play important roles in these higher current regimes. Rosenthal [1,2) fi rst used point and line heat so ur c es moving at a constant speed to calculate pure co n du c tion heat transport in plates of semi - infinit e thickness . Tsai [3 ) found th a t the in c onsistency between the expe rimental weld poo l sh a pe and the predicted va lu e based on the simp le point source theory can be reduced to a large extent by assuming a dis tributed heat source on the weld surface. It was found that the intr oduction of the distributed heat so u rce ca n match the predicted values of weld geometry reasonab l y well wi t h the empirical data at low c ur rents At high c ur rents, m u ch l arger errors ar e fou nd, which suggest that effects other than thermal conduction and the distributed heat source may be important . Generally, depression of t he weld pool surface has re ceive d l it tl e attention. Ishizaki [4 ) s tu died depressio n in gas me t al arc welds but no extensive study of su r face depression in gas tungsten a rc welding has be e n fo u nd in the literature. Mos t invest i gators believe that s urface depression r esults from the impinging pl asma jet . Such jets have been studied in steelmaking [5), however, these results can hardly be app  ed to the weld pool due to the large differences in dimension involved and to the fact th at the eq uations derived are based up on emp irical re s ul ts i n which t he pa rameters are different f r om thos e in in gas tungste n arcs. Numerous studies [6-12) have shown that the co n ve c t ive pattern in the weld pool influences heat flow and weld bead size. t is believed that the mo t ive forces for fluid f low i n t he weld po ol are (1) the elect r omagnetic force (Lorent z force) , 2) t he b uoyancy force (thermal convect io n) , (3) the s urfac e tension force, and (4) the impinging gas jet force. The re is t t le agreement as to which of these forces dominate unde r specified we l d ing conditions; however, most autho r s agree that increasing the weld i ng curren t is expecte d t o increase the intensity of convective fluid f low - because hi g h er cu r re n t density and he at flux wi l l enhance t h e driving forces for fluid flow, which in turn will influence the penetration pr o file. Fluid flow and surface depress i on are also responsible for the formation of weld defects such as humping and undercutting of the weld bead. Humping and und e rcutting are common in high tra vel s peed and high c urr ent GTAH we ld in g . The mech anisms of f ormation of these defects have been discussed by several researchers [7,13,14]; however, no satisfacto r y explanations have been proposed . Su rfa ce tension and arc force we r e m e n t ~ o n e as the forces which produce these defects , but the mechanisms a re s ti ll poo rly

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Page 1: Influence of Surface Depression and Convection on Arc Weld Geometry

8/12/2019 Influence of Surface Depression and Convection on Arc Weld Geometry

http://slidepdf.com/reader/full/influence-of-surface-depression-and-convection-on-arc-weld-geometry 1/8

INFLUENCE OF SURF CE DEPRESSION ND CONVECTION ON

RC WELD POOL GEOMETRY

M L Lin and T W Eagar

Materials Processing Center

Massachusetts Institute of Technology

Cambridge, Massachusetts

ABSTRACT

The relat ive importance of surface depre ssion and

convection in determining the depth of w e l ~ penetration in s ta t ionary GTA welds has been studied. Theresul ts ind i ca t e that a deep cra ter depr ession forms

on the surface of a stee l weld poo l a t currents inexcess of 250 amperes. During the t ransi t ion fromshallow to deep penetration, the depression grows from

one millimete r or l ess to four or f ive mil l imeters with

an increase of only twenty amperes. Such a drama t i cchange cannot be explained due to th e plasma j e t momentum alone . I t i s proposed that the major cause of the

deep penetration a t these current l evel s i s a vortexwhich i s created by circumferential rotation of theweld pool. Some evidence suggests that the deep vo r tex

i s se l f -s tabi l iz ing and that t h i s creates a hysteresisi n the weld penetratio n as t he current i s ramped upwardand downward through the trans i t ion fr om sh allow todeep penetration. I t is believed that th is vortex

depression is the major cause of f inger penetrationin GM welding as we l l .

Tr avelling GTA we lds were also made to investigatet he effects of deep surface depression on weld defectformation. High speed cinemapho t ography was used toshow the flow behavior from the front to th e back of

th e weld pool . In s t eels, and in t i t anium allo ys ,this flow i s most l ike ly driven by surface tensiongradients. I t was f ound that the deep vortex penetra

tion and the rearward f lu id f l ow can explain h ~ p ebead, undercutting and tunnel bead defects. I t i s

bel ieved t hat a Sim i la r mechanism i s responsible for

hol low bead defects in stovepipe welding.

INTRODUCTION

In o rd er to improve product ivi ty mo r e use i s

being made of au tomated welding; however, as a resul t

a number of problems ar ise which seldom occur in manua lwelding . Two of the most fundamenta l concerns are seamtracking and control of weld bead geometry , both of

which must be cont r olled i f a rel iable weld is to be

produced. In this paper several of the factorscontroll ing weld be ad geomet ry wil l be discussed. One

of the diff icul t i es en coun tered in a pr io r i predic t i on

of weld shape is th a t many parameters must be takeninto account because al l a r e found to have more or lessinfluence on the weld pool geometry. I f the welding

process i s to be automated with cl os ed l oop contro l ofthe we ld zone size, i t i s desirable to more fullyunderstand the mechanisms which influence heat and

fluid flow in th e molten weld pool so that the influence

of th ese process parameters can be understood. Mostof the fundament a l research work on gas tungsten arcwelding has been l imited to low current ranges, i . e .

less than ab out 200 amperes due to ins tabi l i t ies in thel iquid pool and to the pr esence of defects such as

humping and undercutti ng at higher currents. l{hile good

63

agreement has been found between empirical data and thepredicted values of weld pool geometry a t low curre n ts

when the current i s increased to higher ranges , e . g .

more than 250 amper es more scat ter i s obtained. I t is

be l ieved t hat surface depression and convect ive fl o win the weld pool may begin to play important roles inthese higher current regimes.

Rosenthal [1,2) f i rs t used point and l ine heat

so ur ces moving at a constant speed to calculate pure

conduc t ion heat transport in pla tes of semi- i n f in i te

thickness . Tsai [3 ) found th a t the in consistency

between the experimental weld pool sh ape and thepredicted va lu e based on the simple point source theorycan be reduced to a large extent by assuming a dis

tr ibuted heat source on the weld surface. I t was found

that the in t roduction of the distributed heat source

can match the predicted values of weld geometry

reasonab l y well wi t h the empirical data a t low cur rents

At high currents, mu ch l arger errors are found, which

suggest that effects other than thermal conduction andthe distributed heat source may be important .

Generally, depression of t he weld pool surface has

re ceived l i t t l e at tent ion. Ishizaki [4 ) s tu died

depression in gas me t a l arc welds but no extensive

study of sur face depression in gas tungsten arcwelding has be en fo und in the l i t e ra ture . Mos t invest i gators believe that s urface depression r esults from the

impinging plasma j e t . Such j e t s have been studied in

steelmaking [5), however, these resul ts can hardly beapp   ed to the weld pool due to the large differencesin dimension involved and to the fac t th at the eq uationsderived are based upon emp i r ical re sul ts i n which t he

parameters are dif ferent f r om those in in gas tungstenarcs.

Numerous s tudies [6-12) have shown that the conve c t ive pattern in the weld pool influences heat flow

and weld bead size. t is believed tha t the mo t ive

forces for f lu id f low i n t he weld pool are (1) theelect r omagnetic force (Lorentz force) , 2) t he buoyancy

force (thermal convectio n) , (3) the s urface tensionforce, and (4) the impinging gas j e t force. There is

t t le agreement as to which of these forces dominate

under specified we ld ing condit ions; however, most

author s agree that increasing the weldi ng curren t i s

expected t o increase the in tensi ty of convective fluid

f low -because h igher cu rre n t density and hea t flux wi l lenhance t he driving forces for fluid flow, which inturn wil l influence the penetration pr of i le .

Fluid flow and surface depress i on are alsoresponsible for the formation of weld defects such as

humping and undercutt ing of the weld bead. Humping and

unde rcut t ing are common in high travel speed and highcurrent GTAH we ld in g . The mechanisms of f ormation of

these defects have been discussed by severalresearchers [7,13,14]; however, no sa t isfacto r yexplanations have been proposed . Surface tension and

arc force we r e m e n t ~ o n e as the forces which produce

these defects , but the mechanisms are s t i l l poo r ly

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understood. The pur pose of the present paper is toass ess the val idi ty of previously explained mechanisms

and t o quantify the relative importance of surfacedepression and convection in determining the shape of

arc weld pools.

EXPERUIENTAL PROCEDURES

A series of stationary and t ravelling bead-on-plate

welds wer e made with var ying currents, voltage andelectrode t ip ang l es . All the samples were cut from as ingle 304 s ta in less s tee l pl ate of 13 mm thickness.

In stationa ry arc welding, measurements were made after

a dwe l l time of 3 seconds so as not to overheat the

plate . This time is long enough to approxima t e the heatinpu t used in travelling arc welds. In order to seethe in f l uence of l onger dwell time on the spo t welding

penetration profi l e , spots up to 24 seconds were a l so

used. In travelling welds , a wide range of travellingve l ocity was us ed in order to investigate the effect of

speed on the formation of weld defects and on the pene

tration mechanisms . Pure argon was used wit h t he flow

ra te set a t 1 mo hr + 10% El ectrodes wi th 30, 60, 90, 120 degree cones were

used . l ~ e l i n g cu r rent varied from 200 amperes to 350amperes arc voltage was set at three different

values;lOV

,2V

and lSV. In several tests weldingcur re nt was ups l oped and downsloped in order to see at ransi t ion from shallow t o deep penetration.

High speed photography was also used to investigatethe f l uid f low on the top surface of th e liquid pool and

to pr ovide a clearer view of the sequence of formation

of we l d defects .

RESULTS

Stat ionary Arc WeldsAs shown in Figures 1 and 2, a sma  increase of

welding curren t can increase the surfa ce depression of

a spot weld by a large amount . The deep surface depres

si on in high current ranges produces a finger - type penet ra t ion profile as shown in Figure 2. A cone- shaped

a)

Fig 1 a) Surface depress i on and penetrat i on profi le at

235 amperes of a stat ionary arc weld on 304s ta i nl ess steel after t hree seconds .

cavi ty i s often fo und at the bottom of these deep pene

tration profiles. For electrodes with larger t ip angles

such as 90 and 120 degree s , the t ransi t ion current from negligible to significan t surface depression depth

i s i ncreased to slightly higher current s . This might

suggest that plasma j e t s play an important role since

such j e t s are stronge r at low t ip angles; however, th is

64

matter wil l be discussed subsequently .

b)

Fig . 1(b)

(a )

Fig . 2 a) Surface dep ress ion and penetration profi l e a t285 amperes of a stationa r y a r c we l d on 304stai n less stee l after three seconds .

b)

Fig . 2 b)

As shown in Fi gure 3, no increase of weld pool

depth was found when we l ding t ime was increased from3 seconds to 24 seconds; however, both the width andthe area of the weld pool were found t o in c rease with

time.

Travelling Helds

Humping beads were found at high currents and a thig h travelling speed as s hown in Figure 4. lfuen the

trave l speed of the arc i s l ess than 2 mm/sec . , nohumping i s found and th e weld pool shape does not

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volume of l iqu id f i l l s t he cavity fo rmed by the de ep

surface depre s s ion .

DISCUSS ION

I t w ll be s hown that previo us models of weld con

vection are not capable of explaining the behavior noted

above. In this paper a new model wil l be presented

which utay explain the ob served behavior. Th e f i r s tproblem to be considered i s the abrupt t ransi t ion from

sh a l low to de ep pene t ra t ion as seen in Fi gures 1 and 2.

Compound Vor t ex

Usually the plasma j e t fo rce i s mentioned as the

cause of deep surface depression; how ever , i f this istru e , one would not expec t an abrupt i ncre as e in depress io n within th e t r ans i t ion current range as shown inFigure 6 , since the plasma je t force in crea ses in asmooth manner as t he squa r e of the a rc current 15].In addition, a simple analysis indicates that t he plasma

j e t only has sufficient f o rce to depre ss the pool by1 a t 300 amperes see th e Appendix). A possible

mechanism whi ch may explain the ob se rved sudden incr ease

of s ur face depres s i on and the depth of the depression

i s a compound vor tex as shown in Figure 7. Such a vor

tex can be developed a t high weldi ng cu rrent s due to a

Free Vortex

D

Forc ed

Vor tex

Fr ee Vortex

Fig . 7 Str u ct u re of the compound vortex. Assum in g

no t ransit ion region between the forced

and f ree vortex .

ci r cumferent i al rota tion of t he l iquid. A compoundvor tex consi s ts of a fo rc ed vor tex in t he central zone

of the l i qu id pool t ogethe r with a free vortex in the

regions far ther away f r om the centra l zone. The depth

produced by a fo rced vor tex i n an infini te la rge l iquid

pool is

2 2wf y

D = 2g

with t he or igin referred t o point A i n Figure 7 and the

depth pr oduce d by the free vortex i n a s im i l a r pool i s

D

with the o rigin refe r red to point B in Fi gure 7 where

wf is the f orc ed angula r ve lo c i ty in the forced vor tex

region, R0

is the radius of the forced vor t ex region

and g i s the accelera t ion of gravi t y.

66

Fi gures 8 and 9 show the calculated surface depression

fo r d i fferen t values of R0 and Wf. I t can be seen that

as the forced angular velocity Wf increases, th e maximum surface depression depth inc r eases sharply and t heshap e is similar to the obse r ved f i nger- type depress io n .In addit ion , as R0 increases, the dep t h of finger- t ype

surface depr ession a lso increases . This means thatwider , higher current we l ds are more s usceptible toforma tion of deep surface depres s ion since Ra i s g r eater .In addit ion, i t wi l l be no t ed that t he vor tex depression

does not depend on t he density of the metal whe r easme ta l densi t y has a direct influence on surface depress ion caused by plasma j e t fo rces. In pr ac t i ce , thedeep dep ression i s fo und t o be no greater in a lumi numthan in s te e l . This agrees wi th the vortex model of

depr es s i o n wh ereas the plasma j e t model pred i cts two tothree times greater penetrat ion in a luminum th an in

s t ee l .

o co

-0 . 20

ia.-o .eec

c

o.ee

I0 . 0 l. O 2 .0 3 . 0

I : 10 Rov / ce c2: 20 Rov / sec

3: 30 Rov/c . ,c

Ro =0.5 mm

...Rad ia l dJs lan co mm

6 u

Fig . 8 Depth induced by compound vo r tex wi th a small

forced vo r t ex reg i on R0 = 0 .5 mm .

One might quest ion the source of the c i rcumferent i a l f l ow which produces the vortex; however t he cause

of this c ircumfe r entia l flow has been discussed by

Millere e t a l . 16 ] . In essence , an arc perfectlyal igne d along t he axis of symmetry cannot pr oduc e aci r cumferenti a l flow, but any perturbation f r om the

central axis is unstable and wil l grow unt i l a circumferent ial flow is produced....

I.e

-2 .0

3   8

E

e_•·•

: :; s .uQ.

0a a.a -

  1 . 0

-a .a

... l.O 2.0

Ra d i a l

I : 1 0R .v/o:cc2• 20 R .v /   oc3 : 30 Rov / .-ec

Ro a l .5 mm

3 .0 0 '·d iG l on c  . mm

e.e

Fi g . 9 Dep th induced by compound vo r tex i t h a large

forced vor t ex re g io n R0

= 1. 5 mm .

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When the current is low, the plasma je t force is

believed co be the dominant factor in determi ning thesurface depression. s current increases, the vortex

intensity increases. In the t ransition current ranges,in addition to the plasma j e t force, the vortex may be

strong enough co cause finger- type surface depression

of the l iquid puddle.

Heat Distribution in Arc Column at High Currents

In i g u r ~ 3   i t i s shown that the area and the

width of weld increases with time while the depth ofweld is nearly con stan t . This implies that the deep

surface depression of the weld pool a t high current smay greatly modify heat flow and current flow in the arc

column, since the central region of the weld pool

receives l i t t le hea t from the arc column at high currents.

In the low current range, the gas-liquid interfaceis essentia l ly plana r and heat distr ibution in the arccan be approximated by a Gaussian distribution. How-ever, in the high current range, a Gaussian distr ibution

may no longer represent the true heat distribution.This maldis t r ibution is caused by the deep surface de

pression of the anode surface, most of the current wil lflow to the side surfaces of the crater instead of being

Fig. 1 Schematic repres entat ion of the eq uipotentiall in es and the current f low paths when a deep

c rate r fo rms .

distributed evenly over the crater s urface . This arisesfrom the fact that both the ca th ode and the anode s ur faces have constant e l ectr ic potentia ls , therefore, the

deep surface crater wil l make the equi- potential l inesdenser on the s ide surface than at the bottom of t he

cra ter . Thus, maldis t r ibution of current f low i s

expected. Since 80 percent of the heat in the arccolumn is transported by the current, there is almost

no he a t transferred to the bot t om of the crate r andthe depth does not increase with time. Once the crater

i s formed   most of the current i s deflected to th e sidewalls of th e crater   and i t therefore requires le sscurrent to sustain the crater than i s required to formthe cra ter originally; thus a hysteresis loop in the

penetration depth versus current graph occurs as shownin Figure 11.

The lack of heat t ransfer d irec t ly to the bottom

of the crater has been observed in high speed cinemaphotography and by metallographic sectioning   both of

which show dry sol id metal a t the bottom of the cra ter .This a lso provides indirect confirma t ion of the vor tex

67

theory, since a vortex and surface tens ion can extract

a l l liquid from the bottom of the cavity whereas t he

plasma j e t momentum would probably leave behind a thickfi lm of l iquid.

Defect Formation

Some of the mechanisms of defect f ormation at h igh

currents can also be explained by deep surface depression and fluid flow in the liquid pool. s shown inFigure 12, at high welding cur rents , a deep surface

cra ter is formed. s current enters the l quid metal ,t wil l diverge. This divergence of current path causes

a pressure gradient which i nduces f luid flow . Since

the solid metal has higher elec tr ic conductivity than

the liquid metal, most of the cur rent entering t he pool

wil l flow to the front pa r t of the arc, while less current passes th rough the elongated weld pool behind the

arc as shown in Figure 12 b) . The unbalanced dis t r ibut ion of current flow in the crater wil l usuall y push

liquid me t a l forward as seen in Figure 12 b). Howeversurface tension forces push the l iquid me t a l backward

because the temperature in the front part of the arc i shigher than behind the arc. Thus, in th e in i t i a l stageof formation of humped we ld beads, surface tension

forces and electromagnetic forces compete to drive the

liquid metal. In l a te r stages   the l iquid me t a l behind

the arc becomes swollen , bringing i t closer to the

e lectrode and attracting more of the current to theliquid metal behind the arc. Finally, mos t of the current wil l flow to th e humped weld bead behind the arcan d the electromagnetic force wil l push the l iq uid metalbackward in the same direct ion as surface tension fo rces .Thus, both the electromagnetic force and the metal i s

comp le tely removed from beneath the arc. This unsteady

motion can explain formation of humped we ld beads .

E

e

•cC>

••

5

3

240 280

Cur rent  mperes

Fig. 11 Variation of penetration depth wi th current

Undercutting may also ar ise f rom convec tion in the

we ld pool . The eddy flows behind th e arc will drivethe l iquid metal from the s ide su r f aces of the groove

by th e travelling arc, to the centerline of the weld

pool behind the arc. f the t ravel s peed i s greatenough and hence the sol id i f ica t ion ra te is rapid

enough   the l iquid metal close to the center l ine of thewe ld pool wil l solidify be fo re th is wave has time toref lec t back toward the edges of th e pool where t he

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liquid metal is depleted. The concen tra t ion of so l id i -

f i ed met al along the centerline of the weld coupledwith a deplet ion a long th e edges re su lt s in undercu t-

t ing .

WELDING DIRECTION

a)

(b)

Fi g. 12 Schematic representat ion of the fo rmat ion ofhum pi ng by ma ld i s t r ibu t ed current in theli quid poo l which produces unbalance del ec t romag ne t i c forces.

Finally, t i s be l i eved t hat the strong eddymot ion behind th e arc , as shown in Figure 12 (b) , is

responsible for t he t unne l bead defec t s s hown inFigure 6. The eddy fo rms at the top of th e pl ate wit ha depressed f inger pene t ra t ing deeply into the metal.The circumferential eddy motion prevents metal f r omf i l l in g the bottom of the depression re su l t ing i n tu n-nel porosi t y a l ong the base of t he we l d bead . I t i sbelieved that s imi l a r mot io n may accoun t for th e hollm•

bead defec t noted i n stovepip e weld i ng . I n t h is case,a deep depres s ion or key hole is fo rmed by t he expanding

gases produced by decomposition of the el ec t rode

coating. A c i r cumfe r en t i al f l ow may be i nduce d whichinhibi ts meta l from s inking to the ro o t of the weld

bead in a manne r s imi l a r to th a t described above for

the tunnel porosity.

CONCLUSIONS

Whe n the welding current i s i nc r eased to a specif ict ransi t ion range, th e depth of surface de pr ession

increases s harply i n a mann er that cannot be expla in edby plasma j e t momentum alo ne . The formation of avortex on t he surface of the l iquid poo l may helpexplain bot h the magnitude and the form of t his t r ans i -t i on f rom shallow to deep penetra tion.

Deep surface depression and f lu id f l ow may a lso

explai n tne forma t ion of a num be r of defects such as

hum ped beads , und ercutting and hollow beads . I t is

hoped tha t the grea t er understanding of the fo rc es

68

desc rib ed in this paper and the res ul tin g convect ion

in the weld pool may lead to improved methods of

avoiding th es e problems i n welded construction.

ACKNOWLEDGDIENTS

Th e au t ho rs are grateful f or s uppor t of th is workby the Office of Naval Resea rch und er Con trac tN00014-C-80-0384.

APPENDIX

Two approaches, a force balance and calculus ofvariation of th e pool sh ape, were used to s tudy the

in f luence of plasma j e t fo r ce on t he depth of s urface

depression. The force balance in the case of an in f in i-

t e l y large l i qui d pool i s

p

h

0p

arc

dens i ty of liquid metal

dep t h of surface depression with r espect tothe highest po int of depress io n curve

two prin cipa l radi i of curvature of th esurface a t the center l in e

surface te ns ionar c pr ess ure

Us ing arc pressure da t a measured by Osaka Trans

former Co . [17], one e st imates a sur face depress iondepth of 1 a t 300 amperes and 90 deg re e e lec t rodet ip angle f or values of 1300 dyne/em.

Th e shape of the sur face depression which posses-ses the minimum energy given a constraint of a cons t antvolume of t he l i quid met a l can be calculated us ingca lcul us of variation . Us ing a comp uter t o num er ic al ly

solve t hi s problem, i t was found t ha t , f or a 90 degree

e lectrode t ip angle and pure a rgon sh ie lding gas at300 ampe r es , the max imum depth of surface depres s i onis less th an 1 [1 8] . Thus , bo th approaches showthat plasma j e t force cannot to ta l ly expla i n the mag-nitude of the s urface depr ess ion nor ca n i t explainthe s udd en i ncrease of depre ss ion i n the trans i t ion

current ra nge.

REFERENCES

1 . Rosentha l , D., Hathematica l Theory of Heat Dis t -ribut ion During l ~ e l d i n g an d Cut ting   , Held. J . ,

20(5) , 1941 , pp . 220s .

2. Rosenthal, D., Theory of Hoving Sources of Hea tand I t s Appl i ca t ion to Metal Treatments   , ASHE,

Vol. 68, No . 8, 1946, pp. 849 .

3. Toai , N. S. , Ph.D. Thes i s , Department of Hate r ialsScience and Engineering, Mass . I ns t . of Techno logy,

Cambr idge, Nass. , 1983.

4.

5.

6 .

I s hizaki , K. , A New Ap pr oa ch to the He chanism ofPenet r a t ion , Pool Chemi s t ry and Neta l lurgy,

The Welding Inst i tute Int ern a tional Conference,

London, April 1980, pp. 65.

Brads haw, A. V. and ~ a k e l i D., in Heat an d Hass

Transfer in Process Heta l lurg y  , The Inst i t ut io nof Nining and Netal lurgy, London, 1967.

Apps , R. L., N lner, D. R. , A Note on th e Behavio r

Page 7: Influence of Surface Depression and Convection on Arc Weld Geometry

8/12/2019 Influence of Surface Depression and Convection on Arc Weld Geometry

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7.

of Liquid Metal Under the Arc   , Brit . Weld. J . ,

Vol. 10, July 1963, pp. 348.

Bradstreet, B J . , Effect of Surface Tension andHetal Flow on Weld Bead Format ion , Weld. J . ,

Vol. July 1968, pp. 314s.

8. Shercliff , J . F., Fluid Notions Due to an ElectricCurrent Source , J . of Fluid Hechanics, Part 2,

Vol. 40, 1970, pp. 241 .

9. Woods, R A , Milner, D R. , Notion in the loleldPool in Arc Welding , lo/eld. J . , Vol. 50, April1971, pp. 163s .

10. Lawson, W H S. , Ker r, H. W., Fluid Notion inGTA Weld Pool. Part 1, Flow Patterns and lo/eld

Pool Homogeneity , lo/elding Research Int 1. , 6 (5 ) ,

1976, pp. 63.

11. Bukarov, V A. , e t a l . , The Effect of Convection

of Metal in the lole l d Pool on Penetration , We ld ingProduction, Vol. 25, No 11, 1978, pp . 5.

12. Heiple, C R., Roper, J . R., Hechanicsm for Hinor

Element Effect on GTA Fusion Zone Geometry , Weld .

Vol. 61, April 1982 , pp. 97s.

13. Paton, B E., e t al . , Certain Special Features

of the Formation of lo/elds Hade at High Speeds ,

Auto . Welding, Vol. 24 , No . 8 , 1971, pp. 1.

14 . Savage, W F. , et a l . , Ef fect of Arc Force onDefect Formation in GTA Welding , Weld. J . ,Vol. 58, J uly 1979, pp. 212s .

15. Burleigh, T. D. and Eagar, T. W., Heasurements

of the Force Exerted by a Welding Arc , Met. Trans. ,14A(6), J une 1983, pp. 1223-1224.

16. Hillere , R. P. , Sharamkin, V I . , and Scherbinin,

E. V , Effect of a Longitudinal Magnet ic Field onElectrica l ly Driven Rotational Flow i n a Cylindri

cal Vessel , Hagnetohydrodynamics, 16(1), 1980,pp. 66.

17. Unpublished technical report, Osaka Transformer

Co. , Osaka, Japan, 1980 .

18. L. Lin, unpublished re s earch , 1983 .

69

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