WJ_1988_04_s88

Embed Size (px)

Citation preview

  • 8/12/2019 WJ_1988_04_s88

    1/7

    The Effects of Heat Input and WeldProcess on Hot Cracking in Stainless Steel

    The Sigmajig test was used to quantify the hot-crackingresponse of Type 316 stainless steel welded with the

    GTA W EBW and LBW processes

    BY G . M . G O O D W I N

    ABSTRACT. The Sigmajig cracking response of a single heat of 0.010-in.-thick(0.25-mm) Type 316 stainless steel wasdetermin ed as a funct ion of we lding p rocess and parameter variations within aprocess. It was found that changes inwelding parameters resulted in changesin cracking response, even when grossenergy input was maintained constant.Higher travel speeds and elongated we ldpool shapes increased the crackingresponse, as did increased heat input.Cracking responses for all three weldingprocesses, gas tungsten arc (CTA), electron beam (EB), and pulsed solid-statelaser beam (LB), were found to follow acommon relat ionship with net heat input .Both EB and LB we lds sh ow ed highercracking resistance than GTA welds.

    In t roduc t ion

    The initial application of the Sigmajigtest (Ref. 1) used a standard set of w e l ding parameters with the CTA process toevaluate the dependence of crackingsensitivity on heat-to-heat compositional

    K E Y W O R D S

    Sigmajig Test316 Stainless SteelHot Cracking ResponseHeat InputElectron Beam WeldingPulsed Laser WeldingGTA Weld ingCracking ResistanceThreshold StressArgon Shielding

    G M. GOODWIN is a mem ber of the Metalsand Ceramics Division, Oak Ridge NationalLaboratory, Oak Ridge, Tenn.

    Paper presented at the 68th A nnual AWSMeeting, held March 22-27, 1987. in C hicago,III.

    effects in stainless steels. In this work, aspecific, relatively crack-sensitive heat ofType 316 stainless steel was used tostudy the effect of heat input variationson cracking sensitivity using three welding processes: gas tungsten arc, electronbeam, and pulsed solid-state laser.

    There are numerous examples in theliterature documenting the effects of heatinput on hot cracking. Typically, anincrease in heat input increases crackingsensitivity, but often, there are also complicating factors to be considered, including changes in solidification mode (Refs.2-4) or compositional effects (Refs. 5-7).Solidif icat ion growth morphology hasalso been shown to be an importantfactor (Refs. 8, 9). Few studies haveattempted to isolate the effect of individual parameters (Ref. 10), and fewer yet

    have addressed process-to-process variations (Ref. 11). In this study, w e hav eintentionally selected a single crack-sensitive heat of material known to solidify asprimary austenite for the processes andparameters investigated. The variations inresponse are thus attributable as nearly aspossible to changes in stress at the trailingedge of the weld pool , which are determined by heat input, heat flow, thermalgradients , and weld pool geometry.

    Experimental Conditions

    A single heat of 0.010-in.-thick (0.25-mm) Type 316 stainless steel was usedthrougho ut the experiment . Its com position is given in Table 1. Previous w or k(Ref. 1) established a threshold crackingstress 1 o f 18 ksi (124 MPa), as comparedwith other commercial heats rangingfrom 15 to 53 ksi (103 to 365 MPa). It hasa reasonably high P 4- S content (0.042wt- ), a Cr-N i ratio of 1.47 (Ref. 12), apredicted ferrite number (FN) of 0 (Ref.13), and, as typified in Fig. 1, invariablysolidifies as primary austenite with a smallamount of residual eutectic ferrite.

    Gas tungsten arc welds were produced under argon w ith a constant arclength of 0.035 in. (0.88 mm). UsingDCEN and a 1/16-in. (1.6 mm) diameter

    thoriated tungsten electrode with a 45-deg included angle and a 0.010-in. t runcat ion, arc current and travel speed weresystematically varied above and belowthe standard conditions of 20 A and 35ipm (14.8 mm/s) (Ref. 1). Five specimenswere run at each combinat ion of param-

    1 Threshold cracking stress, a m in, is defined inRef. 1 as the ap plied stress above whichcracking first occurs.

    I .aa

    y : ~~y^

    Fig. 1 Typicalmicrostructure of gastungsten arc w eld inType 316 stainlesssteel. Heat 828013.Solidification mode isprimary austenite witha small amoun t ofeutectic ferrite.Murakam i s e tch

    88-S | APRIL 1988

  • 8/12/2019 WJ_1988_04_s88

    2/7

  • 8/12/2019 WJ_1988_04_s88

    3/7

    100

    80

    6

    g 4

    2 0

    HEAT 828013207MPa (30ksi)TRAVEL SPEED = 14.8 mm/s (35in./min)AVERAGE OF FIVE TESTS 1 er

    18 20 22I (amps)

    28

    Fig. 3-

    a?

    o