Hydrogen Cracking of Ferritic-Austenitic Stainless Steel Weld Metal
Manuscript Number: P2058
By: A J Leonard (Project Leader, TWI, UK)
R N Gunn (Plant Assessment Manager, Plant Integrity, UK)
T G Gooch (Technology Manager, TWI, UK)
Presented at 'Stainless Steel World Duplex America
2000' conference, 29 February - 1 March 2000
Abstract
Ferritic-austenitic stainless steels are normally regarded as
readily weldable by common arc processes. However, cases of weld
metal hydrogen cracking have been reported, principally at joints
produced using shielded metal arc welding (SMA); the present study
was carried out to examine conditions under which the problem was
likely to occur.
First, a procedure was derived for hydrogen analysis of
ferritic-austenitic SMA weld metals, based on the vacuum hot
extraction method. Second, self-retrained single run and multipass
weld cracking tests were performed, with consumables varying in
deposit hydrogen potential and phase balance. Weld metal cracking
was found to occur only at high ferrite contents and hydrogen
levels. The results were correlated with other published
information, and a diagram was produced relating cracking to the
consumable hydrogen content determined under standard conditions
and the deposit phase balance. From this correlation, the risk of
hydrogen cracking in practice is expected to be low, given adoption
of normal welding procedure guidelines.
1. Introduction
To achieve optimum mechanical and corrosion resistance properties,
welding procedures for ferritic-austenitic stainless steels must be
carefully controlled to ensure that a satisfactory phase balance is
achieved in the weld area with negligible formation of
intermetallic phases. With such control, the alloys are normally
regarded as readily weldable by common arc processes, in the sense
of producing defect-free joints. However, cases of weld metal
hydrogen cracking under production conditions have been reported to
TWI, principally at joints produced using shielded metal arc
welding (SMA). In practice, the problem is particularly associated
with fairly high hydrogen levels and ferrite contents. Several
workers have investigated the problem using various experimental
methods
[1-7] , but quantitative
limits have not been well defined for either duplex or superduplex
grades.
Conventionally, hydrogen cracking risk with transformable
ferritic steels is dependent upon the diffusible hydrogen content
at normal ambient temperature, and this can be determined using a
standard procedure with collection over mercury [8] . With duplex stainless steels, overall
diffusion rates are slow because of the presence of austenite [5] , although local diffusion in
ferrite may well be as rapid as with carbon-manganese steels. Thus,
collection of diffusible hydrogen at room temperature is
impractical, and a number of studies have recommended extraction at
elevated temperatures [1-7,] [9, 10] . However, there remains a need
for definition and standardisation of a suitable analysis
temperature and time.
The present work was in two phases. First, a procedure was
derived for hydrogen analysis of ferritic-austenitic SMA weld
metals based on the vacuum hot extraction method (VHE) [11] . Not all laboratories have access to
VHE equipment for measuring hydrogen in a production situation.
Therefore, weld metal hydrogen levels were also measured using
vacuum encapsulation of a sample in quartz glass [3] followed by heating for hydrogen
extraction and analysis by a commercial gas chromatography
instrument. The aim was to identify an extraction temperature that
would give consistent and complete hydrogen totals within a
reasonable time period, i.e. less than 24 hours, which would allow
rapid quality control of electrode batches. Second, self-restrained
weld metal cracking tests were carried out, involving both single
run and multipass assemblies, to examine the conditions of hydrogen
content and deposit microstructure under which the problem was
likely to occur.
2. Experimental Procedure
2.1 Materials
The compositions of the base materials and consumables used in the
study are shown in
Table 1. In Phase I, in order to
produce a range of weld metal ferrite levels, three parent
material/consumable combinations were explored. Most of the
hydrogen analyses were performed on 25%Cr deposits on 316L-type
base plate, which were chosen to approach 80% austenite on the
basis that this would cover the range of practical concern and
would indicate the maximum evolution time necessary for different
production batches of consumables. Further deposits were produced
to study the effect of lower austenite contents (i.e. 60%) on
hydrogen evolution from 22% and 25%Cr materials. Deposits were then
produced to assess the reliability of the analysis method for
different hydrogen levels associated with varying coating type and
welding process.
Table 2 lists the
materials employed and welding conditions used for the Phase I
deposits.
Table 1 Compositions of materials employed in the study
Material
Code |
Thickness,
mm |
Phase |
Element, wt% |
| C |
Si |
Mn |
Cr |
Ni |
Mo |
N |
Other |
| Base Plates |
| 316L |
12mm |
I |
0.013 |
0.42 |
1.35 |
17.05 |
10.3 |
2.11 |
0.045 |
- |
| S31803/1 |
12mm |
I |
0.020 |
0.45 |
1.65 |
22.0 |
5.8 |
3.03 |
0.165 |
- |
| S31803/2 |
20mm |
II |
0.019 |
0.48 |
1.74 |
21.8 |
5.8 |
2.73 |
- |
- |
| S31803/3 |
12mm |
II |
0.020 |
0.45 |
1.63 |
22.3 |
5.8 |
1.97 |
0.166 |
- |
| S32750 |
12mm |
I |
0.017 |
0.39 |
0.37 |
25.0 |
7.7 |
4.09 |
0.275 |
- |
| Electrodes |
| 22.9.3.LR*(a) |
|
I |
0.025 |
1.0 |
0.80 |
22.0 |
9.0 |
3.0 |
0.12 |
- |
| 25.10.4.LR |
|
I |
0.031 |
0.54 |
0.74 |
25.3 |
10.4 |
3.8 |
0.242 |
- |
| 25Mar |
|
I |
0.021 |
1.05 |
0.78 |
24.5 |
8.9 |
3.0 |
0.20 |
- |
| 25Mb |
|
I |
0.032 |
0.65 |
0.97 |
25.4 |
9.9 |
4.12 |
0.23 |
- |
| 22Mb |
|
I |
0.032 |
0.42 |
0.95 |
23.2 |
9.22 |
3.07 |
0.16 |
- |
| 22MbL |
|
I |
0.031 |
0.39 |
0.91 |
23.1 |
9.2 |
3.05 |
0.16 |
- |
| 22Mbr |
|
I |
0.024 |
0.4 |
0.8 |
23.5 |
8.7 |
3.1 |
0.22 |
- |
| W1 |
|
II |
0.045 |
0.33 |
1.12 |
24.8 |
8.0 |
3.17 |
0.19 |
1.74Cu |
| W3 |
|
II |
0.040 |
1.07 |
0.55 |
22.3 |
5.3 |
3.01 |
0.22 |
- |
| 22.9.3.LR(b) |
|
II |
0.025 |
1.0 |
0.8 |
22.5 |
9.5 |
3.2 |
0.16 |
- |
| 85% ferrite |
|
II |
- |
- |
- |
- |
- |
- |
- |
- |
| Submerged arc |
| 22S |
|
I |
0.009 |
0.47 |
1.59 |
22.4 |
8.7 |
3.14 |
0.14 |
- |
| 25S |
|
I |
0.016 |
0.33 |
0.78 |
25.2 |
9.2 |
3.66 |
0.23 |
0.64Cu, 0.58W |
| Flux cored |
| 22F (W2) |
|
I, II |
0.017 |
0.69 |
1.35 |
22.6 |
9.6 |
3.11 |
0.16 |
0.05Cu |
| *R = rutile, ar = acid rutile, b = basic, br =
basic rutile |
Duplex stainless steel plate, grade UNS S31803, was used for
both single and multipass welds in Phase II. Plates of 12 and 20mm
thickness were used for the single pass and multipass deposits
respectively. The single pass welds utilised two SMA consumables. A
standard 22%Cr duplex consumable was employed, together with an
experimental electrode, designed to produce high weld metal ferrite
levels (~85%). Both consumables were 3.2mm in diameter and had a
rutile flux coating. The multipass welds studied in Phase II
utilised three consumables. Two SMA consumables were used, viz a
commercial 25%Cr electrode, and an experimental 22%Cr electrode
with only 5.3%Ni to give a high ferrite level (62-85%), while a
third weld was produced using a commercial 22%Cr flux cored
wire.
2.2 Derivation of Hydrogen Analysis Procedure
Hydrogen evolution behaviour was evaluated at different
temperatures. For this purpose, each weld consisted of a single
pass bead-on-plate deposit of 100mm length following the guidance
of ISO 3690: Part 2
[8] . Stainless
steel base metal blanks were not degassed to maximise hydrogen
content, although each electrode was baked at 350°C for 1 hour
prior to welding. The welding conditions employed for each deposit
type are given in
Table 2, with electrodes being deposited
using automatic equipment. The end pieces were removed and the
ferrite/austenite content determined by point counting
(Section 2.4) .
Table 2 Materials employed and welding conditions used for
Phase I deposits.
(a) Evaluating hydrogen behaviour.
Deposit
code |
Base
plate |
Electrode
type |
Electrode
diameter,
mm |
Voltage,
V |
Current,
A |
Travel
speed
mm/min |
Arc energy,
kJ/mm |
| 25/80 |
316L |
25Mar |
4.0 |
30 |
132 |
224 |
1.1 |
| 22/60 |
S31803 |
22.9.3.LR |
4.0 |
28 |
147 |
224 |
1.1 |
| 25/60 |
S32750 |
25.10.4.LR |
3.25 |
22 |
103 |
150 |
0.9 |
(b) Varying consumable type and welding process.
Weld
code |
Drying
conditions |
Humidity*
g/m 3
|
Voltage,
V |
Current,
A |
Travel speed
mm/min |
Arc energy,
kJ/mm |
| SMAW |
| 25Mar |
From sealed packet |
10.8 |
30 |
130 |
205 |
1.1 |
| 25Mar350 |
350°C/2hrs |
7.7 |
30 |
131 |
214 |
1.1 |
| 25Mb |
From sealed packet |
5.0 |
23 |
111 |
171 |
0.9 |
| 22Mb |
From sealed packet |
7.7 |
23 |
110 |
188 |
0.8 |
| 22MbL |
From sealed packet |
5.0, 7.7 |
23 |
111 |
182 |
0.9 |
| 22Mbr |
From sealed packet |
7.7 |
23 |
133 |
200 |
0.9 |
| SAW |
| 22Sab |
As-received wire & flux |
4.8, 8.6 |
30 |
485 |
293 |
3.0 |
| 25Sab |
As-received wire & flux |
8.6 |
26 |
339 |
188 |
2.8 |
| 22Sab350 |
350°C/2hrs |
8.6 |
30 |
491 |
293 |
3.0 |
| 22Sab350 |
350°C/2hrs |
4.8 |
26 |
354 |
194 |
2.9 |
| FCAW |
| 22F |
From sealed packet |
5.8 |
31 |
187 |
439 |
0.8 |
| * Humidity in grammes of water per m 3
of dry air. |
On completion, most of the test pieces were stored in liquid
nitrogen until analysis was performed. However, one sample of a
triplicate set was left under ambient conditions for four days, to
study the need for liquid nitrogen storage. The hydrogen evolution
behaviour of each deposit, in terms of ml/H 2
/STP/100g deposited weld metal, was determined against time by the
VHE method at different temperatures. This was generally based on
individual deposits, although duplicate or triplicate analyses were
carried out on selected samples to investigate the level of
repeatability in the VHE analysis. If extraction required longer
than six hours, the specimens were allowed to cool and then
reheated under vacuum the next day. The high austenite deposit
25/80 ( Table 2) was first analysed at extraction
temperatures over the range 400°C to 950°C, and the time
required for hydrogen evolution was noted. Once the temperature
that would lead to hydrogen analysis results in less than one day
was identified, the evolution behaviour of two duplex deposits
(i.e. 22/60 and 25/60 in Table 2) was explored. Analysis
was then carried out using other SMA electrodes and submerged arc
and cored wire welding, as in Tables 1 and 2,
using triplicate samples.
Comparison between VHE and encapsulation methods of hydrogen
analysis was made using three commercially available 22Cr duplex
stainless steel consumables, the analyses of which are included in
Table 1. All of the consumables were deposited on type
S31803 plate. VHE was carried out on each of the deposits at a
temperature of 700°C for 3.5 hours. Vacuum encapsulated samples
were heated in a furnace at 400°C for 72 hours to allow for
hydrogen evolution: the hydrogen content was then determined by gas
chromatography (GC) at ambient temperature by breaking the capsule
in a flow of Ar carrier gas using a Yanaco G-1006 instrument. In
the event, the results obtained indicated that complete extraction
into the capsule was not being achieved. Accordingly, an additional
test was undertaken with titanium powder added to the capsule to
getter any hydrogen evolved from the sample.
2.3 Hydrogen Cracking Tests
2.3.1 Single Run Welds
The single run tests were based on the Y-groove approach, to induce
weld metal cracking as encountered in practice. Test plates were
machined in accordance with JIS standard Z3158 (1993)
[12] . In order to obtain a high ferrite
(~85%) level in Y-groove test runs, two panel assemblies were
buttered with the high ferrite consumable prior to machining, the
electrodes having been baked at 350°C for 2 hours prior to use.
Welding conditions were set to provide an arc energy of 1kJ/mm. The
root gap in the Y-groove was machined to 1.6±0.2mm. Anchor
welds, either side of the Y-groove, were made by electron beam
welding.
To obtain different hydrogen levels, test electrodes of each
type were placed in a humidity cabinet, at 28.5°C and 74%
humidity, for 24 hours, or baked at 350°C for 2 hours prior to
welding. Single run, Y-groove test welds were deposited using each
electrode type and hydrogen potential. Welding was carried out at
22°C and 46% relative humidity. A total of four test welds was
deposited, the welding conditions again being chosen to give an aim
arc energy of 1kJ/mm ( Table 3).
Table 3 Welding conditions used in the Phase II Y-groove
cracking tests
| Weld |
Consumable |
Current, A |
Voltage, V |
Arc energy,
kJ/mm |
| W4 |
85% ferrite |
111 |
28 |
0.9 |
| W5 |
85% ferrite |
111 |
28 |
0.9 |
| W6 |
22.9.3.CR(b) |
111 |
30 |
1.0 |
| W7 |
22.9.3.CR(b) |
111 |
29 |
0.9 |
Hydrogen analysis test blocks were machined from the same test
plate as the Y-groove samples in accordance with BS 6693 [13] . Triplicate sets of blocks were
machined for each electrode and aim hydrogen level. Test electrodes
were either baked or humidified as described above. Test weld beads
were deposited at the same time as the Y-groove test runs to ensure
similar testing conditions. All test runs were deposited with arc
energies of ~1kJ/mm. After welding, the test blocks were cleaned to
remove the slag and were stored in liquid nitrogen. The hydrogen
content was then determined by VHE at 950°C for 1.5 hours.
On completion of welding, the Y-groove samples were left for 1
week prior to examination. After this time, the weld caps were
examined for evidence of any surface cracks. In addition, each test
weld was sectioned as detailed in JIS Z3158 [12] , which requires a total of five
transverse sections to be taken through the weld bead at equal
distances apart, and examined for evidence of cracking.
2.3.2 Cracking in Multipass Welds
The test plate was cut into portions of 400mm length x 150mm width,
a 30° bevel edge preparation was applied, and the root was seal
welded using superduplex consumables. The first 100mm from the stop
and start of each preparation was filled, again using superduplex
consumables. The test welds were then deposited in the resultant
groove using the conditions given in
Table 4.
Table 4 Summary of Phase II - Multipass welding conditions
Weld
code |
Consumable |
Diameter |
Humidity*,
g/m 3
|
No. of
passes |
Current,
A |
Voltage,
V |
Travel
speed,
mm/min |
Arc energy,
kJ/mm |
Interpass
temperature,
°C |
| W1 |
25%Cr SMA |
5mm |
10.8 |
10 |
168-202 |
25 |
170-203 |
1.4-1.9 |
<200 |
| W2 |
22F |
1.2mm |
11.0-11.5 |
9 |
192-198 |
31 |
320-400 |
0.9-1.2 |
<150 |
| W3 |
22%Cr SMA |
3.25mm |
11.8-13.0 |
21 |
100-110 |
26 |
170-260 |
0.6-0.9 |
<150 |
| * Humidity in grammes of water per m 3
of dry air. |
As soon as each panel cooled from welding, it was inspected
using 45° and 70° angled compression wave probes, from all
three orthogonal directions, including the weld root. The equipment
employed was a Force Institute P-scan system with a sensitivity set
using a 3mm diameter side drilled hole in a duplex test block,
following BS 3923 part 1 [14] .
This system takes ultrasonic (UT) signals and probe positions to
produce a three view image of the weld volume with a detection
limit of about 0.5mm. Subsequent UT inspection of each panel took
place after 1, 2, 4, 8, 16 and 30 days, and then monthly, until at
least six months had expired. For comparison, dye penetrant
inspection was undertaken, as was radiography using 400keV X-ray
equipment viewed from the cap side.
2.4 Metallography
Metallographic sections through each Phase I weld deposit and
Y-groove test run were prepared in order to determine the phase
balance. This was performed by manual point counting, using a 25
point (5x5) grid at X1400 magnification; a total of 16 fields was
measured. Phase identification was aided by staining the ferrite
phase, either by electrolytic etching in 20%KOH, or by using a
'magnetic etch' treatment, which involved immersion in a
magnetic iron oxide colloidal solution, 1%Fe
3 O
4 in a hydrocarbon base. On
the multipass welds in Phase II, the cap pass of each panel was
ground flat and the Ferrite Number (FN) determined using a
Ferritscope.
3. Results
3.1 Derivation of Hydrogen Analysis Procedure
3.1.1 Hydrogen Evolution
The hydrogen evolution behaviour of deposit 25/80 at different VHE
temperatures is shown in
Fig.1. The rate of hydrogen
extraction was dependent on the temperature, with higher
temperatures accelerating extraction. For instance at 950°C,
extraction was almost complete after about 100 minutes, whereas
over 50 hours were required for complete removal at 400°C. The
temperature of extraction did not significantly affect the final
level of hydrogen evolved over the range studied.
Comparison of the evolution behaviour at 700°C for different
deposits and base materials is given in Fig.2
Fig.1 Hydrogen evolved against time for a range of temperature
(deposit 25/80)
|
. The austenite content of each deposit is shown in
Table
5. Deposit 25/80 appeared to take slightly longer to reach a
plateau than the other deposits, consistent with the high austenite
content (81%,
Table 5) reducing the hydrogen diffusion
rate. Evolution was substantially complete for all deposits after
about 3
1 /
2
hours.
Table 5 Austenite content of Phase I weld deposits
Fig.2 Evolution behaviour of different deposits at
700°C
|
Results of the analyses on a range of deposits are given in
Table 6
| Material code |
Austenite content, % |
| 25/80 |
81.2 (2.5) |
| 22/60 |
59.3 (4.9) |
| 25/60 |
60.8 (3.8) |
| Figures in parentheses are ± 95% confidence
limits |
. It will be noted that the different sample types displayed a
range of hydrogen content, from about 5-20ml/100g deposited metal,
with good repeatability in all cases.
Table 6 Hydrogen contents of commercial consumables
The sample stored under ambient conditions prior to analysis gave a
result of 19.3ml of H 2
| Sample Code |
VHE results, ml H 2/STP/100g |
Variation from
Average, % |
| 1 |
2 |
3 |
Average |
| SMAW |
| 25Mar |
19.8 |
18.8 |
19.3# |
19.3 |
±2.6 |
| 25Mar350 |
16.4 |
16.6 |
17.2 |
16.7 |
±3.0 |
| 25Mb |
4.5 |
5.4 |
5.9 |
5.2 |
±13.5 |
| 22Mb |
9.0 |
9.0 |
9.2 |
9.1 |
±1.1 |
| 22MbL |
8.6 |
8.3 |
9.7 |
8.9 |
±9.0 |
| 22Mbr |
4.8 |
5.6 |
5.1 |
5.2 |
±7.7 |
| W1* |
23.7 |
21.9 |
25.8 |
23.8 |
±8.4 |
| W3* |
23.2 |
- |
- |
23.2 |
- |
| SAW |
| 22S |
5.3 |
5.4 |
5.5 |
5.4 |
±1.9 |
| 25S |
3.7 |
3.8 |
4.0 |
3.8 |
±5.3 |
| 22Sab |
11.7 |
13.8 |
12.6 |
12.7 |
±8.7 |
| 25Sab |
11.1 |
10.2 |
11.1 |
10.8 |
±5.6 |
| 22Sab350 |
6.7 |
6.4 |
7.4 |
6.9 |
±6.8 |
| 25Sab350 |
5.8 |
6.5 |
4.3 |
5.6 |
±23.2 |
| FCAW |
| 22F (used in W2*) |
15.4 |
15.5 |
14.9 |
15.3 |
±2.6 |
- Not analysed/not applicable
* Employed in Phase II
# Sample left under ambient conditions prior to analysis. All
other samples were stored in liquid nitrogen. |
compared with 18.8 and 19.8ml for the comparable samples stored at
-196°C. Thus, there appeared to be no effect of storage
conditions on the consequent hydrogen levels.
3.1.2 Comparison between VHE and encapsulation techniques
The results of VHE and encapsulation methods are presented in
Table 7. The encapsulation technique consistently produced
lower results than VHE in the deposits analysed. Therefore,
selected samples, which had been encapsulated and heated, were
re-analysed by the VHE method. This exercise showed that
significant levels of hydrogen remained in the sample after
encapsulation, while the sums of the two analyses were similar to
single analysis by VHE at 700°C for 3.5 hours (
Table
7). The sample encapsulated with titanium powder showed low
hydrogen content on analysis, indicating complete hydrogen
evolution and pickup by the titanium.
Table 7 Summary of results for different hydrogen analysis
techniques and sample types
3.2 Hydrogen Cracking Tests
Deposit
code |
Sample
code |
Humidity
g/m 3
|
Preparation |
Analysis
technique |
Extraction
Conditions |
Results,
mlH 2/STP/100g |
| 22Mb |
1-3 |
7.7 |
- |
VHE |
700°C/3.5hrs |
9.0, 9.0, 9.2 |
| 4,5 |
7.7 |
Sealed in glass, 400°C/72hrs |
GC |
RT* |
3.4, 3.6 |
| 4 |
- |
Re-analysis of no.4 |
VHE |
950°C/1.5hrs |
+6.5 |
| 22Mbr |
6-8 |
7.7 |
- |
VHE |
700°C/3.5hrs |
4.8, 5.1, 5.6 |
| 9-11 |
7.7 |
Sealed in quartz, 400°C/72hrs |
GC |
RT |
1.1, 1.3, 2.0 |
| 9 |
- |
Re-analysis of no.9 |
VHE |
950°C/1.5hrs |
+4.7 |
| 12-14 |
7.7 |
Sealed in quartz, 400°C/72hrs |
GC |
RT |
1.2, 1.8, 3.2 |
| 15,16 |
7.4 |
Sealed in quartz with 6g of Ti,
400°C/72hrs |
VHE |
950°C/1.5hrs |
0.86, 0.93 |
| 17,18 |
7.4 |
Sealed in quartz, while heated to 200°C/2 hrs,
400°C/72hrs |
GC |
RT |
1.15, 0.95 |
| 17,18 |
- |
Re-analysis of no.17, no.18 |
VHE |
950°C/1.5hrs |
+4.3, +3.7 |
| 22F |
24-26 |
5.8 |
- |
VHE |
700°C/3.5hrs |
14.9, 15.4, 15.5 |
| 27, 28 |
13.8 |
Sealed in quartz, 400°C/72hrs |
GC |
RT |
7.5, 8.5 |
| 27 |
- |
Re-analysis of no.27 |
VHE |
950°C/1.5hrs |
+9.6 |
| 29-31 |
13.8 |
Sealed in quartz, 400°C/72hrs |
GC |
RT |
9.6, 9.8, 10.2 |
| *RT - normal ambient temperature. |
3.2.1 Y-Groove Tests
Table 8 shows the weld metal hydrogen levels achieved with
each of the consumables. The ferrite content and results of the
hydrogen cracking tests are shown in
Table 9. Both of the
high ferrite weld beads (W4 and W5) cracked. The high hydrogen test
bead (W5, 17.5ml/100g) cracked within a few hours of welding, while
the low hydrogen bead (W4, 11.4ml/100g) cracked in less than three
days.
Table 8 Weld metal hydrogen results - Y-groove cracking test
samples.
| Weld |
Hydrogen level, ml/H 2/STP/100g weld
metal |
| 1 |
2 |
3 |
Average |
| W4 |
11.18 |
11.76 |
11.22 |
11.4 |
| W5 |
17.23 |
18.23 |
17.07 |
17.5 |
| W6 |
15.00 |
14.36 |
15.88 |
15.1 |
| W7 |
18.17 |
19.28 |
18.43 |
18.6 |
Table 9 Weld metal ferrite content and Y-groove cracking test
results.
The weld metal microstructures were typical of duplex stainless
steel deposits. The high ferrite welds contained some grain
boundary and isolated intragranular austenite. Cracking in each of
the high ferrite welds was transgranular in nature and propagated
through the ferrite phase, Fig.3
| Weld |
Volume fraction
of ferrite, % |
Result of Y-groove test |
| W4 |
83 (5) |
Cracked |
| W5 |
82 (4) |
Cracked |
| W6 |
57 (6) |
Not cracked |
| W7 |
56 (4) |
Not cracked |
| Figures in parentheses are ±95% confidence
limits. |
. Some cracks arrested at ferrite-austenite boundaries. The crack
morphology was typical of that observed in practical problems of
hydrogen cracking in duplex weld deposits.
3.2.2 Multipass Welds
Fig.3 Cracking in weld W4
|
The ferrite and hydrogen contents of the multipass welds are shown
in
Table 10. Panel W1 showed two root indications on the
initial UT scan within one hour of welding. The nature of these
indications did not change during the subsequent 9.5 months
inspection, nor did any other indications appear. No flaws were
detailed in panel W2 at any time during a six month inspection. Two
indications were found in panel W3 directly after welding; no
changes occurred in these indications after five months inspection,
nor did any flaws appear. No evidence of cracking was detected by
either dye penetrant inspection or radiography. Sectioning of each
of the panels after inspection was completed did not reveal any
cracking, although porosity was found in panel W2, which had not
been detected by UT.
Table 10 Multipass weld metal ferrite and hydrogen
content.
4. Discussion
| Weld |
Ferrite content, FN |
Hydrogen level, ml/H 2/STP/100g weld
metal |
| 1 |
2 |
3 |
Average |
| W1 |
59 |
23.7 |
21.9 |
25.8 |
23.8 |
| W2 |
55 |
15.4 |
15.5 |
14.9 |
15.3 |
| W3 |
90.5 |
23.2 |
- |
- |
23.2 |
4.1 Hydrogen Analysis Procedure
The objective of Phase I was to derive a hydrogen analysis
procedure with particular emphasis on the extraction temperature
that would lead to total hydrogen analysis results to be obtained
within a 24 hour period.
Table 11 lists the key results of
this work, showing the recommended times at a range of extraction
temperatures for VHE. The use of an extraction temperature of
700°C allows for welding and analysis within 24 hours, meeting
the perceived practical aim, even for electrode batches giving high
austenite contents. Nevertheless, it is within the capability of
VHE to extract hydrogen at 950°C, which only takes 1
1 /
2 hours and allows for
triplicate analyses in one working day. Further, the work indicates
that samples do not need to be stored in liquid nitrogen prior to
analysis. This allows samples to be stored under ambient conditions
without jeopardising results.
Table 11 Recommended minimum extraction times for VHE.
Table 6
| Extraction temperature, °C |
Recommended minimum
extraction time |
| 400 |
7 days |
| 500 |
36 hours |
| 600 |
16 hours |
| 700 |
3 1 / 2 hours |
| 950 |
1 1 / 2 hours |
illustrates that the VHE method with extraction at 700°C is
applicable to a range of consumable types, welding processes and
associated hydrogen levels. As would be anticipated, the greatest
variations in results from triplicate analyses was observed for low
hydrogen contents, about 5ml/100g deposited metal. At higher
hydrogen levels, the repeatability is consistently less than 10% of
content. This behaviour is similar to conventional analysis of
ferritic steel deposits, and, in the general case, is as expected
for analysis of any element present at the ppm level.
The results of this work clearly indicate that the encapsulation
method gives lower readings than obtained by VHE. Subsequent
measurement by VHE showed that hydrogen was retained in the steel
using the encapsulation method. The most likely explanation for
this is that, during hydrogen evolution at 400°C in the
capsule, a positive hydrogen partial pressure is developed,
hindering further liberation from the weld deposit: this is
consistent with the apparent complete evolution in the sample
encapsulated with a titanium getter. This observation has also been
made by other workers [16] . On the
other hand, Kaçar [17],
performed repeat analyses on duplex weld deposits using the
encapsulation technique, and did not report any further hydrogen
evolution on reheating. Clearly, further work is required in this
area before the generally more convenient encapsulation/gas
chromatography approach can be accepted for routine hydrogen
analysis.
4.2 Hydrogen Cracking Tests
4.2.1 General Comments
The current work has demonstrated the adverse effect of high levels
of weld metal ferrite on the risk of fabrication hydrogen cracking
in duplex stainless steels.
Figure 4 shows the results
together with previous data generated at TWI from Y-groove SMA
tests on 22%Cr duplex stainless steel
[5] .
The programme sought to generate cracking data for SMA welds, in
22%Cr duplex stainless steel, for which the consumable hydrogen
level had been determined using the VHE method. Cracking occurred
in welds containing ~83% ferrite and hydrogen levels of 11.4 and
17.5ml/H 2
Fig.4 Results of TWI hydrogen cracking tests
|
/STP/100g deposited metal. The welds containing 'normal'
volume fractions of ferrite did not crack. In addition, three
multipass welds were made, none of which cracked.
4.2.2 Comparison With Other Work
Several workers have investigated fabrication hydrogen cracking in
duplex and superduplex stainless steels using a variety of
experimental methods
[1-7], [9,10] . Comparison of the current results
with other published work is problematic, in that other workers
used a variety of welding techniques, cracking tests and hydrogen
analysis procedures. The choice of welding process may affect the
weld metal hydrogen content and also microstructure in the sense of
inclusion levels, which may influence cracking behaviour
[15] . The current work primarily examined
SMA welding, as this is of particular practical significance in
terms of fabrication hydrogen cracking. Data exist for gas tungsten
arc welding (GTAW)
[1,2], [7], but, because hydrogen was added via the
shielding gas, they cannot be readily converted to a deposit
hydrogen content for comparative purposes.
Figure 5 shows
the results of the current work, together with published data from
other workers who used the Y-groove test to evaluate the cracking
of SMA deposits. The axes of
Fig.5 are deposited hydrogen
content and weld metal ferrite volume fraction. The former may be
determined by appropriate consumable analysis and the latter may be
obtained by phase balance checks on weld procedure qualification
samples: hence, both parameters can be readily employed by a
welding engineer, to assess the risk of a problem arising in
practice.
Lundin et al carried out Y-groove cracking tests using both duplex
and superduplex stainless steels, with SMA weld deposits [4,5]
Fig.5 Y-groove and other test results. Closed symbols indicate
that welds cracked
|
. The hydrogen content of the deposited metal was determined using
a quartz encapsulation method. The current work, supported by van
der Mee et al
[16] , has shown that
the encapsulation method of measuring hydrogen may underestimate
the true level, and thus the data points from Lundin's work may
be raised from their position in
Figure 5. The degree by
which each of the points should be raised is not known, but it is
unlikely that Lundin's actual hydrogen levels were considerably
higher than the reported analyses. It should be noted that Lundin
recorded ferrite number (FN) and not % ferrite in his work.
However, reasonable correlations exist between FN and % ferrite,
[18], for both 22Cr
[6], [19,20], and 25Cr alloys
[21]. The results in
Fig.5 are
presented in terms of % ferrite, with Lundin's data having been
converted using relationships derived at TWI, namely:
% ferrite = 0.57FN + 8.82 (for 22Cr duplex stainless steel, [20];
% ferrite = 0.82FN + 3.6 (for 25Cr superduplex stainless steel, [21] .
The current work agrees well with the results of Lundin et al,
accepting that the reported hydrogen levels of the welds are
probably lower than actual.
Walker and Gooch [5] used a
similar experimental approach to the present investigation, and
carried out Y-groove cracking tests on 22%Cr duplex stainless steel
with commercial SMA consumables. The deposited metal hydrogen
content was determined by VHE. Welds containing ~60% ferrite and
12-16ml/H 2 /STP/100g deposited metal did not
crack. These results compare favourably with the current work.
It is possible to include in Fig.5 a boundary curve,
separating cracking and no cracking conditions for SMA deposits in
duplex stainless steel. It should be noted that there exists some
degree of uncertainty as to the shape of the curve in
Fig.5 at ferrite volume fractions between 65 and 85%
because of a lack of data, and further study is desirable.
4.2.3 Practical Implications
In the current comparison of results, both microstructure, in terms
of ferrite volume fraction, and hydrogen content, in terms of
deposited metal, are accounted for. The graph (
Fig.5)
provides a guide to prevent fabrication hydrogen cracking in SMA
welded ferritic-austenitic stainless steels. To illustrate the
point, the work of Beeson
[22]
represents an in-service failure of SMA welded UNS S31803 duplex
stainless steel. It was reported that cracks appeared to start at a
highly ferritic (over 90% ferrite) cap pass, and that the welds
contained 24ppm hydrogen. This behaviour would clearly be expected
from
Fig.5. The present results show that fabrication
hydrogen cracking may be avoided by maintaining a weld metal phase
balance of less than 60% ferrite and a deposited hydrogen content
of less than 18ml/H
2 /STP/100g: this is
consistent with practical experience. Whilst the majority of the
data presented was generated using single pass welds, it is
believed that the graph does present a basis for predicting the
likelihood of cracking in multipass production welds.
5. Conclusions
- The VHE method of hydrogen analysis is applicable to duplex
stainless steel weld metals. Table 11 presents guidance as
to the minimum time required to extract hydrogen using VHE
equipment in the 400 to 950°C temperature range.
- Fabrication hydrogen cracking in SMA 22%Cr duplex stainless
steel weld deposits may be avoided by maintaining a weld metal
phase balance of less than 60% ferrite and a deposit hydrogen
content of less than 18ml/H 2 /STP/100g.
- A predictive diagram has been generated, using the results of
the current work and other published data, to aid the prevention of
fabrication hydrogen cracking in practice.
6. Acknowledgements
The authors thank their colleagues at TWI for advice and assistance
throughout the programme. Grateful acknowledgement is made also to
members of two Group Sponsored Projects at TWI for guidance during
the programme of work, and for permission to publish this paper,
viz: Chevron UK Ltd, ESAB AB, Lincoln Smitweld BV, AB Sandvik Steel
and Shell U.K. Exploration and Production.
7. References
Copyright by TWI, 1999
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| 8 |
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|
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| 13 |
|
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| 14 |
|
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| 15 |
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| 16 |
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| 18 |
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| 20 |
Walker R A, |
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| 21 |
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