Visible Light Emissions during Gas Tungsten Arc Welding and Its Application to Weld Image Improvement Spectral windows where external sensors will have the least radiance disturbance were established, providing for the possibility of an improved weld pool image BY E. VV. KIM, C. ALLEMAND AND T. VV. EAGAR ABSTRACT. An experimental study was carried out to map the light emissions from a gas tungsten arc using 24 combinations of weld parameters. Data were collected with a computer-interfaced double monochromatic imaging system which has a rejection ratio of 106. The intensity scale was calibrated throughout the wavelength range from 4880 A to 7300 A, using a spectral radiance standard lamp which is traceable to NBS standards. Lines were identified by element and wavelength with 0.65 A wavelength resolution. The effect of intensity calibration was found to be very important in terms of comparing spectral maps and intensities. The emissions were found to be dramatically different with different shielding gases, welding current and base metals. Spectral windows, where the external sensors will have the least disturbance from welding arc emission, were also determined. An improved image of the weld pool can be obtained by operating within these spectral windows. Twodimensional distributions of major elements in an arc plasma are also presented, and the anode spot on the molten weld surface was observed. Introduction Improvement of automated welding will require development of new sensor systems. As the welding arc is a harsh environment, noncontacting sensor devices are preferred, since they do not disturb the process and do not require extra equipment in the welding setup. A number of investigators have developed methods for viewing the weld pool in order to control joint tracking and weld E W. KIM, C ALLEMAND and T. W. EAGAR are with the Massachusetts Institute of Technology, Cambridge, Mass. bead width; however, each of these systems must exclude the arc light in order to obtain a clear image of the weld pool (Refs. 1-4). Since the arc is a spectral radiator, and this spectra is influenced strongly by the metal vapors emitted from different base metals, it would be desirable to map the spectra on a variety of base plates in order to select the windows in the spectrum which are relatively free of arc light. Arc light emissions also have potential as a welding information source. The emission changes with weld parameters and responds well into the kilohertz range (Ref. 5). Unfortunately, spectral data on arcs are currently available under only a few combinations of weld parameters and wavelengths. Furthermore, in most cases, the intensities from different investigations and even from the same investigation are not comparable because of a failure to calibrate the measurement systems (Refs. 5-8). Most of the work has been done to determine the feasibility of using the arc light as a sensor or to investigate the characteristics of arc emissions. It can be seen from a review of these papers that few studies have been devoted to mapping the spectra and determining windows which are relatively free of arc light. KEY WORDS GTAW Light Emissions Emission Intensity Intensity Calibration Monochromatic Image Image Improvement Anode Spot Motion Spectral Data System Arc Plasma Elements Arc Current Effects Shielding Gas Effect Some researchers have applied spectra for weld monitors or sensor systems (Refs. 9-15). In these studies, it was shown that the emission spectra can be used to detect changes in the welding arc, due to such phenomena as reduction in shielding gas flow rate, loss of flux in flux cored welding wire or the presence of hydrogen. Another study incorporated welding spectra to enhance the image quality of the weld pool (Ref. 4). The major purpose of the present work is to spectrally map light emissions in the range of 4880 A to 7300 A during gas tungsten arc welding, and to correlate changes in the spectra to changes in the welding parameters. The intensities are calibrated with reference to a standard lamp, the radiance of which is traceable to NBS standards. In this way, all intensities are measured on the same scale. Mapping the emission with various combinations of weld parameters provides comparison of the emission characteristics. Further, this mapping defines spectrally blind regions (of minimum spectral intensity). These regions can be a basis from which to choose windows in the spectra where external sensors will have the least disturbance from welding arc emissions. The spectral distribution of the major spectral lines were also photographed based on the results of this spectral mapping. Experimental W o r k Equipment The spectra obtained in this study were made with the equipment schematically shown in Fig. 1. Direct current electrode negative (DCEN) polarity was supplied by a commercial welding power supply followed by a current regulator, which gives control over the welding current to within 1% of the set value. Light from the arc was reflected by a WELDING RESEARCH SUPPLEMENT 1369-s 0- C u r r e n t to Double Strip Chart Filter 25 Hz Recorder Voltage Monochromator Scan L o w Pass Converter ADC Control PDP 11/23 Computer Tektronix VT 105 Plotter Graphic ADC : A n a l o g u e to D i g i t a l C o n v e r t e r Fig. 1 — Schematic arrangement Lens of spectral Disk Monitor data analysis PM Storage : Photomultiplier system Grating Mirror Collimator 1 Actual subtractive configuration Light Source is shown here as an additive entrance Slit one for clarity purpose. Rotation of the grating was controlled by a stepping motor. The number of stepping pulses and the pulse rates were also used as data-sampling trigger pulses for a data collecting computer. Calculated spectral band pass and measured values are compared in Table 1. The spectral resolution used is 0.65 A with a 20% maximum error in determining the peak intensity. The rejection ratio of the monochromator as a band pass filter was also measured to be better than 106. The half-band widths at which the 1 0 - 3 peak intensity was transmitted are tabulated in Table 2. The intensities were calibrated by comparison with a lamp whose radiance is traceable to NBS standards. This lamp was used as the light source at the position of the arc source, and output intensities were taken through the entire opto-electronic system. The ratio of this output to the lamp radiance was used as an intensity calibration factor. This factor Grating Mirror Collimating and focusing are accomplished I by the same mirror labeled collimator PM : Photomultiplier Fig. 2 — Light path in the flat mirror and was focused onto the entrance slit of the imaging doublemonochromator (Ref. 16). The arc was viewed at 75 deg from the arc column axis to imitate a realistic position for an arc sensor. The image comprised the molten surface, the arc column and the cathode tip. The image center was aligned with the center of the slit to provide a symmetrical image. The imaging double-monochromator used in this study has a 500-mm focal length and a reflection grating of 1180 grooves/mm. A schematic drawing of this instrument in Fig. 2 shows the light path through the instrument. A photomultiplier (PM) was attached just after the exit slit in order to monitor the spectral intensity. It is also possible to use a beam splitter to monitor the monochromatic image and intensity simultaneously. Spectral data were collected at the exit slit without using the beam splitter in order to obtain better signal intensity. The image was used only to check the position of the arc and to take pictures of the two-dimensional monochromatic light distribution. double-monochromator 438.0 Q LLI I— < 328.0 — CH Table 1—Band Pass of Imaging Double Monochromator cn H _l 240.0 — = < Measured 160.0 — s >- Slit Width (micron) Calculated 500 250 100 50 40 30 20 7.63 3.81 1.53 0.76 0.61 0.46 0.31 H CO Ld 0.0 H . 1 00 Amp. A 1 1 S000.0 [ ' 5500.0 I WAVELENGTH Fig. 3 — Effect of current on 4880 A-7300 370-s I DECEMBER 1987 ' I 6000.0 A spectra 6500.0 7008.0 FWHI<a> N e l<b> (A) 6929.5 Ne l<b> 5400.6 3.46 1.40 0.74 3.33 1.43 0.78 CA) of He arc on copper FWHI< a (A) at (a) F W H I - f u i ! w i d t h at half intensity. (b) Ne I—Ne neutral line. 0.56 — 0.55 Table 2—Half-Band Width at 1/1000 Peak Transmission Table 3—Measured Wavelength Deviation Z" Wavelength (A) Slit Width (micron) Single Side Band 1000 750 500 242 14.4 10.3 (A) Element From Table Difference (A) 4917.87 4931.21 5016.30 5105.54 5153.18 5218.25 5292.27 5700.44 5782.19 5875.44 6678.24 7065.39 4918.37 4931.56 5016.61 5105.30 5153.24 5218.20 5292.52 5700.24 5782.13 5875.62 6678.15 7065.12 -0.50 +0.29 +0.31 -0.24 +0.06 -0.05 +0.25 -0.20 -0.06 +0.18 -0.09 -0.27 Q. Cu W Cu Cu Cu Cu Cu Cu Cu He He He 7.1 3.7 w a s used t o normalize the intensity o v e r t h e entire w a v e l e n g t h range studied; h o w e v e r , since b o t h the e n t r a n c e slit size and t h e s o u r c e position m a y b e c h a n g e d d u r i n g the m e a s u r e m e n t t o o b t a i n the best signal c o n d i t i o n f r o m t h e w e l d i n g arc, t h e calibrated spectral intensities are o n l y relative. Nevertheless, t h e relative intensities at any t w o w a v e l e n g t h s are linearly p r o p o r t i o n a l . UJ Measured II I I I I I I I I I I T y p e AISI 304 stainless steel, Ti-6Al-4V alloy, 5083 a l u m i n u m alloy a n d c o p p e r plate w e r e used as base metals. Three d i f f e r e n t w e l d i n g currents, 100, 150 and 200 A , w e r e u s e d w i t h e l e c t r o d e negative polarity (DCEN). The 3 / 3 2 - i n . (2.4m m ) diameter E W T h 2 e l e c t r o d e was used w i t h an 8 - m m (0.3-in.) arc length. T h e arc v o l t a g e w a s 12 V f o r a r g o n shielding and 22 V f o r helium shielding. T h e arc w a s r u n o n a specimen plate b a c k e d by a w a t e r - c o o l e d c o p p e r block. W e l d i n g grade a r g o n and helium w e r e used as shielding gases at f l o w rates of 20 c f h (9.4 L/min) f o r Ar a n d 25 c f h (11.8 L / m i n ) f o r H e . Spectra w e r e t a k e n at each o f these 24 e x p e r i m e n t a l c o m b i n a tions. Results and Discussion LU o o cc < LU C/> LU CC o _l LU 320.0 — 240.8 — > a LC H —I UJ > a. 400. 0 a < Welding Conditions o X o -J < o cc < I 60.0 UI (/) 80.0 2 UJ h2 Z ^^.20Q.Amp^ CO LU 0- o . 100 Amp. 0.0 H 1 5000.0 ' I ' 5500.0 I 6000.0 WAVELENGTH Fig. 2 _ 1 SO Amp.. ' _i LU I 6500.0 7080.0 CAD > X o < 4- Effect of current on 4880 A-7300 A spectra of Ar arc on copper LU rated the u p p e r limit of t h e data collecting system are m a r k e d w i t h u p w a r d a r r o w s . T h e relative intensities in t h e w a v e l e n g t h tables are s o m e w h a t different f r o m those of t h e e x p e r i m e n t a l results. By a n d large, s t r o n g t a b u l a t e d lines m a t c h t h e test results, b u t differences o f t e n o c c u r w h e n t h e intensity level of a spectral line is l o w . This m a y be d u e t o t h e interaction effects of each element in the arc. As e x p e c t e d , dramatically different arc Spectral Map (/) Ul DC LU a. o_ i UJ V e r y s t r o n g lines f r o m shielding gas usually a p p e a r e d in each spectral m a p , e v e n w i t h d i f f e r e n t arc c u r r e n t levels. These lines w e r e used as a r e f e r e n c e f o r w a v e l e n g t h calibration b y assigning the characteristic w a v e n u m b e r t o the c o r r e s p o n d i n g data p o i n t in a data file (Ref. 20). T o check the accuracy in d e t e r m i n i n g wavelengths, a comparison was made f o r t h e case of a 200-A helium (He) arc o n a c o p p e r plate. T h e results are listed in Table 3, w h i c h s h o w s v e r y g o o d accurac y w i t h i n 0.7 A . M e a s u r e d values w e r e referenced to standard wavelength tables (Refs. 1 7 - 1 9 ) . T h e spectral m a p s f o r the case o f the entire 24 c o m b i n a t i o n s of w e l d p a r a m e ters are s h o w n in Figs. 3 - 1 0 . The spectra at w a v e l e n g t h s longer than 6 9 0 0 A usually consist only of s t r o n g a r g o n (Ar) lines, namely Ar I 6 9 6 5 . 4 3 , 7 0 6 7 . 2 3 , 7147.04 a n d 7270.94. These w e r e o m i t t e d f r o m the spectral m a p . S o m e lines w h i c h satu- > Ul Q 400.0 Cl LJ h- < ~v 1 X CJ CC 328.0 < — UJ (/> cr CQ H -J UJ 248.0 cc z — < Ul a. O 160.0 > > H CO Ul a Ld •a-x X 0.0 o tr < H 5800.0 5500.0 6808.0 WAVELENGTH 6500.0 7000.0 CA5 Fig- 5 - Effect of current on 4880 A -7300 A spectra of He arc on AISI 304 stainless steel WELDING RESEARCH SUPPLEMENT 1371-s LU 400.0 f\ Q UJ h- 320.8 < CC in H . _ —, _ 240.0 j < CJ> \y 160. 8 > FH CO LU I— — - 88.0 ~ 0.0 r ^ i H 5088.0 i i ! 5500.0 i 6000.0 ' i 6508.8 ' r 7808. WAVELENGTH CAD Fig. 6 —Effect of current on 4880 A-7300 A spectra of Ar arc on AISI 304 stainless steel 400.0 Q LJ I— < 320.0 — 240.0 — cr m < a 160.0 >H CO 80.0 Ld 5000.0 5500.0 6080.0 6500.0 7000.0 WAVELENGTH CAD Fig. 7-Effect of current on 4880 A-7300 A spectra of He arc on AA 5083 spectra were obtained with different base plates. This is due to the different metal vapor species which evaporate from the weld pool. Since these metal vapor species may dominate the temperature profile and the electrical properties of the arc, it can be seen that a change in the composition of the workpiece can dramatically change the nature of the welding arc (Refs. 8, 21-23). As shown in Figs. 3 and 4, the major lines from the He arc on a water-cooled copper plate are Cu I and He I. In the case of the Ar arc, Ar I and Ar II lines are dominant. With argon shielding, copper lines appeared only at the 200-A current. The greater intensity of the Cu lines in the He arc is due to the melting of the plate. This is due to the fact that He gas liberates more heat than Ar gas. This can be explained by the fact that the arc voltage of He shielding is about 10 V higher than that of Ar shielding, due to the higher ionization potential of He. This trend was consistent with each experiment performed. Figures 5 and 6 show the results on AISI 304 stainless steel. The major metallic lines observed were Cr I and Fe I. In Figs. 7 and 8, the dominant metallic lines from the 5083 aluminum alloy experiment are shown to be Mg I and Al II. Magnesium lines saturated the upper limit of the data collecting system. Figures 9 and 10 show the results of the Ti-6AI-4V alloy experiment. The major lines from this experiment are Ti, Ti I and Al II. Thermodynamic calculations made by Block-Bolten, Eagar and Cobine, ef al, are consistent with these observations (Refs. 24-26). The data can also be presented in finer detail, as shown in Figs. 11 and 12. An atlas of calibrated light emission intensities during gas tungsten arc welding with 24 combinations of welding parameters has been produced (Ref. 20). Effect of Intensity Calibration 480. 0 r\ O LU I— < cr CQ H 328.8 — 240.0 _ ] < CJ I 60.0 — > lH CO 80.0 Ld 0.0 H 5000.0 5500.0 6000.8 WAVELENGTH 6500.0 CAD Fig. 8 - Effect of current on 4880 A -7300 A spectra of Ar arc on AA 5083 372-s I DECEMBER 1987 7000. A comparison between a spectral map with calibrated intensities and one without calibration is shown in Fig. 13. It is seen that the uncalibrated intensity ratio between t w o lines, compared with the calibrated ratio, can be in error by as much as 15 times. This strong effect of calibration on relative intensities explains some of the difficulty in comparing other spectra that have been presented in the literature. The light transmission characteristics through the entire optical system depends upon the optical components used. The sensitivity and noise of the electrical data collecting and processing equipment also affect the characteristics of the system. It is important to take both factors into account in an integrated manner, as is done in this work, in order to obtain consistent results. Effects of Welding Parameters It is clear that most of the lines appear at all current levels on the same material but with quite different relative intensities. Some of the relative intensity changes are quantified in Figs. 14, 15 and 16. The intensities from neutral lines increase with Ar shielding but decrease after reaching a maximum with He shielding. On the contrary, the intensity of singly ionized lines in Fig. 16 shows a consistent decrease. This may be due to a transition from a singly ionized Fe ion changing to a secondary ion emitting light at a wavelength which is not within the range concerned in this research. Essentially, the plasma may become more optically thick at this wavelength as the current is increased (Ref. 27). It is also seen that the intensity of the tungsten line from the electrode increases with current when using He shielding. It was also found that the background intensity with Ar shielding at 200 A is approximately 20 times higher than that with He shielding. One possible explanation for this higher background intensity is the higher electrical conductivity and the lower thermal conductivity of the Ar plasma compared to the He plasma (Ref. 8). Another possible explanation may be the free-to-bound electron transition of the singly ionized Ar atoms, due to their lower ionization potential compared to that of He. Although the background is lower, the peaks are higher with He for any line which appears in both shielding gases. This may be due to the higher arc power of the He gas shielding caused by the higher total arc potential drop, or it may be due to the fact that He is optically thinner than Ar. The base metal also affects the intensities of some lines. For example, as shown in Figs. 3, 5, 7 and 9, the intensities of the same line, 5875.62 He I, differs greatly according to the composition of the base metal. This probably results from the interactions of each vapor or ion species in the arc plasma, again confirming the fact that the metal vapor can dominate the properties of the arc. The property change of the plasma due to the presence of metal vapors requires a more rigorous study in the future. Spectral Window The spectrally blind regions where external sensors will have the least disturbance from welding arc emissions were determined easily in the figures presented in this work. Four spectra from four different base materials are superimposed in one graph on a coarse wavelength scale in Fig. 17. It was found that windows on the coarse wavelength scale are present at 5790-5870 A, 5890-6010 A, and 6440-6630 A for these four base metals with He and Ar shielding gas. 400.8 —a 320.0 — 240.0 — a Ld I— < cr CQ H _l a. o _i ui < > I 60.0 > X o cc < H CO Ul V) LU Ld Z H 8.0 cr T 5000.0 5500.0 6000.0 6500.0 7088.0 WAVELENGTH CAD oa. Fig. 9-Effect of current on 4880 A-7300 A spectra of He arc on TI-6AI-4V > ui a x 400 0 Ld I— cc < ui tn ui 320 0 oc < OC CD H _l CJ , r\ Q _ , 240 0 Q- < O \y O I 60 0 -J Ul ~ > > • FH 88 0 CO , X o zLd I— cc 0 < fa / -1 H 5008.0 I I I 5500.0 I I 6000.0 I r 6500.8 WAVELENGTH 7000.0 Ul tn ui cc CAD Fig- 10-Effect of current on 4880 A-7300 A spectra of Ar arc on TI-6AI-4V CL o > LU a r*\ Sa" X CJ 150.0 —a cr < n LJ 1— < <X m H _J < a </ >I— H CO 120.0 — ui tn 98.0 — ux S Q- 60.0 — o _l LU > 30.0 — 1— 0.0 — UJ Q xJxx^jti-^^ zLd AAII . „100 Amp,, X ~l H 5160.0 . 11 5190.0 \ ^V^JVX_^XXA_J1U ' 1 5220.0 ' 1 r 5250.8 WAVELENGTH CAD Fig. 11 — Effect of current on spectra of He arc on AISI 304 stainless steel, 5183 A -5268 A WELDINC RESEARCH SUPPLEMENT | 373-s X CJ oc < Ul <n ui oc 70.0 < CY CC CALIBRATED INTENSITY H _! < /X'Wv-V-a-'' CO Z LU _luw. I4.0 200 Amp. ^.•XxyA-^ 1 00 Amp. 0.0 H Q UJ | —i i SI 60.0 N < i | t 5220.0 T 52S0.0 W A V E L E N G T H CA5 Fig. 12 —Effect of current on spectra of Ar arc on AISI 304 stainless steel, 5183 A-5268A UNCALIBRATED INTENSITY tr a | S190.0 S Cr I 5204.52 + F. I 5204.58 A Cr I 5286.64 IM LJ I— 384 STAINLESS STEEL Ar GAS <5 Cr I 5206.44 + F» I 5206.60 < CY CQ WAVELENGTH CA5 Fig. 13 — Effect of intensity calibration on spectra of 200-A He arc on copper < Fig. 14 — Effect of shielding gas and current on emission intensity of Cr I and Cr I + Fe I lines from AISI 304 stainless steel I2B.0 I 53.B 1S0.0 CURRENT CAMP) -8A1-4V Ar GAS Q Ld I— < cr CO < CO Fig. 15—Effect of shielding gas and current on emission intensity of Ti I line from TI-6AI-4V z Ld 90.0 120.0 150.0 1S CURRENT CAMP) Fig. 16—Effect of shielding gas and current on emission intensity of Fe II, Fe I, W lines from AISI 304 stainless steel OL 304 STAINLESS STEEL H . SAS Ar GAS _ Q A © e i— < cr cc r. H F« I U F* II H _l < L_ I- :z H I 90.0 374-s | DECEMBER 1987 120.0 1 150.0 CURRENT CAMP5 1 180.0 4923.92 4957.6! 5B15.32 5616.44 Ld I- < CY CO H _l Cr O 240.0 — < _ i LU > 160.0 — LU Q H CO CJ Fig. 17—Spectral window for Ar and He shielding LU I— z H cr < LU CO LU cr 5500.0 6000.0 6500.0 WAVELENGTH CAD Cr O Windows for fine wavelength scales can also be found in the same manner from graphs similar to Figs. 11 and 12 (Ref. 20). LU Monochromatic Photography X CJ To see the effect of the spectral windows^ photographs were taken with a 6520-A interference band pass filter, as proposed in the previous section. These are compared with the photographs taken with neutral density (ND)_ filters. The interference filter has a 100-A band pass FWHI. As shown in Figs. 18 and 19, better images of molten surfaces were obtained with the narrow band filter than with the ND filter. As stated previously, Ar shielding has a higher continuum emission than He; hence, the arc light is still present in Fig. 18A. This emission is concentrated in the vicinity of the tungsten electrode. Figures 20 and 21 are images from a video monitor screen made with the double monochromator, using its 14-A band pass FWHI. These photographs show the distribution of Cr4-Fe and Mn, respectively. These are heavily concentrated just above the molten pool. This observation _i > Ul Q cr < LU tn LU cr z LU 0- o > LU Q CJ cr < LU <n ui cr Fig. 18 - Image of Ar arc on 304 stainless steel. Fig. 19- Image of He arc on 304 stainless steel. A — 652 ± 5 nm interference filter; B — neutral A — 652 ± 5 nm interference filter; B - neutral density filter density filter o. o _i ui > X CJ cc < Ul tn UJ oc a. O _i ui > Ul O X O < UJ CO Fig. 20 — Distribution of the Cr+ Fe line on 304 stainless steel at 520.6 ±1.4 nm. A—Ar arc; B — He arc WELDING RESEARCH SUPPLEMENT 1375-s Fig. 21 — Distribution of a Mn line on 304 stainless steel at 601.6 ± 1.4 nm. A-Ar arc; B-He arc Fig. 22 —Anode spot mode on 304 stainless steel at Cr + Fe 520.6 1.4 nm. A -Spot mode, 150 A, Ar shielding; B-ring mode, 200 A, Ar/2H2 shielding is in accordance with the results of population density measurements in an arc plasma (Ref. 28). Metallic elements are also observed to be more concentrated at the center of the molten surface, as seen in Fig. 21. Figure 22A also shows a spot at the center. This picture was taken with a reduced exposure to improve the image of the spot. This bright spot is believed to be an anode spot where the current density and temperature is higher than other locations on the weld pool surface. It was found that the shape of the anode spot changes from a spot to a ring with increasing current. Figure 22B shows this. The center ring is believed to be the locus of the anode spot, and the inverted cone is the reflected image of the arc column. The fusion boundary is marked with a white curve. The transition occurs at around 150 A. The ring shape is believed to be related to the depressed molten anode surface (Ref. 29). At high 376-s I DECEMBER 1987 currents, above 150 A, the anode spot is thought to move around the ridge of the depressed pool surface with a nonrandom motion. The video observation showed a rotating motion of the ring. This will affect the distribution of the metallic elements in an arc plasma, and thus the heat input mode to the workpiece. A ring-shaped heat input model should be considered, and the electromagnetically driven convection flow in the weld pool will be changed in comparison with typical mathematical models of arc welding (Refs. 30-32). The rotating spot along the ridge may drag the molten metal and work as an asymmetric driving force for the weld pool circulation. Conclusion Spectral maps for 24 combinations of weld parameters were made in the wavelength range from 4880 A to 7300 A using a calibrated intensity scale with 0.65-A wavelength resolution. Lines can be identified by species and wavelengths within this resolution. The effect of intensity calibration was found to be very important in comparing different spectral maps and intensities, as the uncalibrated ratio between t w o lines could be in error by as much as 15 times. The major metallic lines identified were Cr I and Fe I for AISI 304 stainless steel, Cu I for copper, Ti, Ti I, and Al II for Ti-6AI-4V alloy, and Mg I and Al II for 5083 aluminum alloy. The lines from the shielding gases were always very strong. Argon gas shielding at 200-A arc current showed approximately 20 times higher background emission level compared to the He gas shielding, but the peak intensities were generally higher with He gas shielding than with the Ar gas shielding. The intensity changes at different current levels were compared graphically and numerically. The characteristics of these changes were found to vary from element to element and were also found t o b e a f f e c t e d b y t h e shielding gas. Spectral w i n d o w s w e r e d e t e r m i n e d f o r b o t h the Ar a n d He shielding gases f o r a n u m b e r o f d i f f e r e n t base plate c o m p o sitions. It w a s f o u n d that w i n d o w s are present at 5 7 9 0 : 5 8 7 0 A , 5 8 9 0 - 6 0 1 0 A , a n d 6 4 4 0 - 6 6 3 0 A. By i n c o r p o r a t i n g these spectral w i n d o w s , a clearer image of a w e l d p o o l is possible. By means of m o n o c h r o m a t i c p h o t o g r a p h y , the a n o d e spot w a s o b s e r v e d t o change its shape f r o m a spot t o a ring w i t h increasing c u r r e n t . It is b e l i e v e d that this m a y b e d u e t o m o v e m e n t o f t h e a n o d e spot a r o u n d the o u t e r ridge of the depressed w e l d p o o l surface. H e n c e , it is seen that a n o d e s p o t m o t i o n o n m o l t e n w e l d pools at high w e l d i n g current ( a b o v e 150 A) is n o n - r a n d o m . This c o u l d h a v e an i m p o r t a n t e f f e c t b o t h o n the heat distribution o f non-planar m o l t e n w e l d pools a n d o n the e l e c t r o m a g n e t i c a l ly d r i v e n c o n v e c t i o n w i t h i n t h e w e l d pool. It is r e c o m m e n d e d that this w o r k be e x t e n d e d t o the case of a m o v i n g arc. A study o n t h e t e m p o r a l change o f an arc emission will also help lead t o an u n d e r standing of the w e l d i n g arc plasma. Acknowledgments T h e authors appreciate t h e s u p p o r t f o r this w o r k f r o m t h e O f f i c e o f Naval Research, u n d e r C o n t r a c t N 0 0 0 1 4 - 8 0 - C 0 3 8 4 , and t h e D e p a r t m e n t o f Energy, u n d e r C o n t r a c t DE-FG02-85ER13331. References 1. Bolstad, |. O. 1985. 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Temperature fields produced by traveling distributed heat sources. Welding Journal 62(12):346-s to 355-s. 31. Goldak, )., Chakravarti, A., and Bibby, M. 1984. A new finite element model for welding heat sources. Met. Trans. 15B(6):299305. 32. Christensen, N., Davies, V. de L., and Gjermundsen, K. 1965. Distributions of temperatures in arc welding. British Welding Journal, Vol.12, pp.54-75. Weldability of Steels— Fourth Edition By Prof. R. D. Stout This w e l l - k n o w n b o o k on t h e w e l d i n g m e t a l l u r g y of steels has been extensively revised by Prof. S t o u t , Dean E m e r i t u s of t h e G r a d u a t e S c h o o l , Lehigh University. T h e fully i n d e x e d , 4 5 0 - p a g e , c l o t h - b o u n d v o l u m e , w h i c h c o n t a i n s n u m e r o u s i l l u s t r a t i o n s a n d t a b l e s , w a s p u b l i s h e d in A p r i l 1 9 8 7 . T h e p r i c e o f Weldability of Steels—Fourth Edition is $ 4 0 . 0 0 p e r c o p y , p l u s $ 5 . 0 0 f o r p o s t a g e a n d h a n d l i n g . O r d e r s s h o u l d b e s e n t w i t h p a y m e n t t o t h e W e l d i n g R e s e a r c h C o u n c i l , S u i t e 1 3 0 1 , 3 4 5 E. 4 7 t h St., N e w York, NY 1 0 0 1 7 . W E L D I N G RESEARCH S U P P L E M E N T 1377-s
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