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WELDABILITY STUDY OF AISI 1035 STEEL IN
WET TROPICAL CLIMATE USING HYDRATED
E6013-RB26 ELECTRODE
❑ Dr. Ir. Slameto Wiryolukito,
❑ Yuga Lendistanu, M.T.
Materials Science and Engineering Department, Faculty of Mechanical and Aerospace
Engineering, Institut Teknologi Bandung, Indonesia
• Water vapor absorbed into the
flux can cause hydrogen
cracking
• Higher carbon equivalent means
lower weldability
• Cheap, easy,
practical
• Commonly used
• Electrode flux
tends to absorb
water vapor
• Practical, stress
induced by self-
restraint
• Economical, samples
in small size
50
75
100
Jan Feb Mar Apr Mei Jun Jul Agt Sep Okt Nov Des
RH
(%)
Maksimum Minimum Rata-Rata
Jakarta 2015
[BMKG]
[www.twi-global.com]
[BMKG]
[AWS B4, 2016]
1st IC-DAEM & SENAMM XI 2018
Observation
Station
Yearly Average RH (%)
Source of Hydrogen in Welding Electrode
Welding
Electrode
Allowable
Moisture (%)
E6010 -
E6013 -
E70XX 0.40
E80XX 0.20
E90XX 0.15
E100XX 0.15
E110XX 0.10
Moisture in
flux
Hydrates
(·H2O)
Absorbed water
vapor
Arc Atmosphere
> 3500°C
100%
hydrogen from
hydrates exited
in weld metal
12% hydrogen
from water
vapor existed in
weld metal
Flux likely to
absorb, but easy
to release with
baking as per
manufacturer’s
recommendation
Important binder
and shield gas
former, stable up
to 1000°C
Allowable Moisture in Welding
Electrode based on AWS A5.5
[1996]
Allowable moisture for
E6013 is not specified!
[Hirai et al., 1980]
1st IC-DAEM & SENAMM XI 2018
• to acquire allowable exposure duration of the E6013-RB26 electrodes
in a wet tropical atmosphere so that no crack will occur in the AISI 1035
steel weldment
• to study cracking modes in the AISI 1035 steel weldment due to
influence of level of absorbed moisture in the E6013-RB26 electrode flux
Boundary Condition
• Base Metal : AISI 1035 Steel
• Process : SMAW, WIC Test
• Electrode : Kobe Steel RB26 Φ3.2 mm (class AWS A5.1 E6013)
• Variable : Preheat/non-preheat treatment and absorbed moisture content in the
electrode flux
• Electrode hydration and welding process was implemented in room temperature environment
• Surface crack was observed 3 days after welding
Purpose
1st IC-DAEM & SENAMM XI 2018
Work Flow Chart
1
st
IC-DAEM
&
SENAMM
XI
2018
Start
Preparation
As-Received
Characterization
AISI 1035 Steel
E6013-RB26
Electrode
• OpticalEmissionSpectrometry(OES)
• Hardness Test
• Tensile Test
• Metallography
• OES
• Weighing 100°C
• Weighing 91%RH
• Weighing 80%RH
• Weighing 68%RH
Electrode
Treatment
• Baking 100°C, 40’
• Hydration
• No preheat
• Preheat 150°C
Welding
(WIC Test)
Surface NDT
Metallography
Micro-Vickers
Hardness Test
Analysis
Conclusion
Finish
Steel Samples
ASTM 10 Grain-Sized Pearlitic Microstructures in AISI 1035 Steel As-Received
1st IC-DAEM & SENAMM XI 2018
Weld
direction
Steel Samples
1st IC-DAEM & SENAMM XI 2018
Electrode Hydration and Weighing Procedure
1] Electrode homogenization
(100°C, 40 minute) in an oven
2] Electrode
hydration using
supersaturated
salt solution agent
in air-tight
container
3] Weigh electrode in
each intended period
(0.0001 g precision),
then immediately
return the electrode to
hydration apparatus.
→ Output: absorbed
moisture mass in
electrode flux
1st IC-DAEM & SENAMM XI 2018
Electrode Mass Gain Model
8
8.3
8.6
8.9
0 60 120 180
Electrode
Covering
Gross
Weight
(g)
Baking Duration (minutes); at 100°C
Function of
Absorbed Moisture
(α) Gain in E6013-
RB26 Covering over
Exposure Duration at
91%, 80%, and 68%
Relative Humidity, at
24°C
E6013-RB26 Covering Gross
Weight over Time at 100°C
Baking Temperature; Remained
Constant after 40 Minutes
1. Baking
2. Hydration
after Baking
1st IC-DAEM & SENAMM XI 2018
Sample Coding and Treatment
Pre-Welding:
Variation in Preheat Treatment
and Absorbed Moisture Content
(α)
Welding:
Similar Heat Input
1st IC-DAEM & SENAMM XI 2018
Surface NDT Result
• Crater (≈10 mm) at the end of weldment
is neglected in crack measurement
• Crack length is measured as straight as
relative to weld length so that crack
percentage does not beyond 100%
Dye Penetrant Result
MPI Result: NP-7 (left) vs WP-0 (right)
measure
1st IC-DAEM & SENAMM XI 2018
Hardness
Hardness Test Spots [NACE MR0175]
No Preheat
634 HV =
AISI 1035
[Callister, 2014]
Preheat 150°C
• HAZ hardness was higher when
preheat was not implemented
• Even,
hardness at
some spots
were found
beyond
634 HV

martensite
phase!
1st IC-DAEM & SENAMM XI 2018
Microstructures
100 μm→
Typical Hard Microstructures with Coexistence
of Martensite, Bainite, and Pearlite Formed in
HAZ of Unpreheated Samples
Ferit Widmanstätten Formed in Both
Preheated and Unpreheated Samples
Very-Fine Pearlite and Proeutectoid Ferrite
in HAZ of Samples Preheated at 150°C
1st IC-DAEM & SENAMM XI 2018
Macrograph
NP-7: α = 7%, no preheat NP-0: α = 0%, no preheat WP-1.8: α = 1.83%, preheat 150°C,
section 45°
WP-1.4: α = 1.42%, preheat 150°C WP-0: α = 0%, preheat 150°C
14 mm
1st IC-DAEM & SENAMM XI 2018
• Crack initiated from the weld core
which is the last place of
solidification
• Intergranular crack propagated
through ferrite widmanstätten grain
boundaries up to surface
• Based on α = 0% and the crack
morphology, it was indicated as
solidification cracking
• Conclusion: it had poor
weldability when preheat was not
implemented although dry flux was
used
Cracking Modes in Sample NP-0
1st IC-DAEM & SENAMM XI 2018
Cracking Modes in Sample NP-7
• Crack initiated from HAZ, followed
by transgranular propagation
• Crack propagation turned to
intergranular in weld metal,
through the columnar structures
• Combination of hydrogen cracking
and solidification cracking
1st IC-DAEM & SENAMM XI 2018
Cracking Modes in Sample WP-1.8
Chevron cracks were characterized
by cracks that appear on both sides
of the weld metal with zigzag
patterns like stairs and 45° oriented.
Low levels of hydrogen have been
believed to cause chevron cracks.
Chevron
Surface Crack
Chevron
Subsurface
Crack
1st IC-DAEM & SENAMM XI 2018
Summary
1st IC-DAEM & SENAMM XI 2018
Welding
Recommendation
0
2
4
6
8
10
0 4 8 12 16 20 24
α,
Absorbed
Moisture
(%)
t, Duration (hours)
91%RH
80%RH
68%RH
• Crack still appeared in
WP-1.8 case
• The WP-1.4 case was
taken as a threshold
point that not generates
any crack
• Preheat at 150°C is
mandatory
1
st
IC-DAEM
&
SENAMM
XI
2018
NP-7 NP-0 WP-1.8 WP-1.4 WP-0
Conclusion
• Without preheating, 37% solidification cracking of the weld length
occurred in a sample welded with E6013-RB26 electrodes even in
the absence of absorbed moisture content in the electrode
covering.
• The addition of the absorbed moisture up to 7% created
combination of solidification cracking and hydrogen cracking with
48% surface crack.
• On the other hand, preheating at 150°C, intergranular hydrogen
chevron crack occurred when absorbed moisture reached 1.8%
with 3% surface crack.
• Crack-free weld joint has been observed on preheat at 150°C
samples with absorbed moisture 1.4% or less.
1st IC-DAEM & SENAMM XI 2018
Conclusion
• WIC test was found to be effective to study the effect of
absorbed moisture in electrode covering to the weld
soundness.
• Electrode exposure can be accurately simulated using
oversaturated salt solution as hydration agent which
gives stable relative humidity in a domestic food
container.
1st IC-DAEM & SENAMM XI 2018
Bibliography
• Lampman, S. (1997): Weld Integrity and Performance, ASM International.
• Chew, B. (1976): Moisture loss and regain by some basic flux covered electrodes, Welding Journal, AWS.
• Valencia, E. and Galeano, N. (1994): Hygroscopic behavior of certain basic‐coated electrodes in a wet tropical climate, Welding
International, 8:3, 208—213.
• American Welding Society (1996): AWS B4 Standard Methods for Mechanical Testing of Welds.
• Quincot,G.,Azenha,M.,Barros,J.,andRuiFaria(2011):UseofSaltSolutionsforAssuringConstantRelativeHumidityConditionsinContainedEnvironments,
GovernodaRepúblicaPortuguesa,Guimarães.
• Jowitt, R. and Wagstaffe, P
. (1989): The Certification of the Water Content of Microcrystalline Cellulose at 10 Water Activities, Commission of the European
Communities,Luxembourg.
• Greenspan, L. (1977): Humidity fixed points of binary saturated aqueous solutions, Journal of Research of the National Bureau of
Standards, 81A:1.
• CallisterJr.,W.danRethwisch,D.(2014):MaterialsScienceandEngineering–AnIntroduction,9thEdition,Figure10.32,Wiley,USA.(AdaptedfromEdgarC.
Bain,FunctionsoftheAlloyingElementsinSteel,1939;andR.A.Grange,C.R.Hribal,andL.F.Porter,Metall.Trans.A,Vol.8A.Reproducedbypermissionof
ASMInternational,MaterialsPark,OH.)
• Tuliani, S. (1976): A metallographic study of chevron cracks in submerged arc weld metals. Welding Research International, 6:6,
19—45.
• Mota, J. dan Apps, R. (1982): Chevron cracking – a new form of hydrogen cracking in steel weld metals. Welding Research
Council.
• Lancaster, J. (1993): Metallurgy of Welding, 5th Edition, Chapman-Hall, London, UK.
• Gedeon, S. and Eagar, T. (1990): Welding Journal, 69:7, page 264—271.
• Alipooramirabad, H., Paradowska, A., Ghoamshchi, R., Hoye, N., and Reid, M. (2016): Experimental Investigation of Welding
Stresses in MWIC Weldability Test, University of Wollongong, Australia.
1st IC-DAEM & SENAMM XI 2018
THANK YOU

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Weldability Study of AISI 1035 Steel Using Hydrated E6013 Electrode in Wet Tropical Climate

  • 1. WELDABILITY STUDY OF AISI 1035 STEEL IN WET TROPICAL CLIMATE USING HYDRATED E6013-RB26 ELECTRODE ❑ Dr. Ir. Slameto Wiryolukito, ❑ Yuga Lendistanu, M.T. Materials Science and Engineering Department, Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung, Indonesia
  • 2. • Water vapor absorbed into the flux can cause hydrogen cracking • Higher carbon equivalent means lower weldability • Cheap, easy, practical • Commonly used • Electrode flux tends to absorb water vapor • Practical, stress induced by self- restraint • Economical, samples in small size 50 75 100 Jan Feb Mar Apr Mei Jun Jul Agt Sep Okt Nov Des RH (%) Maksimum Minimum Rata-Rata Jakarta 2015 [BMKG] [www.twi-global.com] [BMKG] [AWS B4, 2016] 1st IC-DAEM & SENAMM XI 2018 Observation Station Yearly Average RH (%)
  • 3. Source of Hydrogen in Welding Electrode Welding Electrode Allowable Moisture (%) E6010 - E6013 - E70XX 0.40 E80XX 0.20 E90XX 0.15 E100XX 0.15 E110XX 0.10 Moisture in flux Hydrates (·H2O) Absorbed water vapor Arc Atmosphere > 3500°C 100% hydrogen from hydrates exited in weld metal 12% hydrogen from water vapor existed in weld metal Flux likely to absorb, but easy to release with baking as per manufacturer’s recommendation Important binder and shield gas former, stable up to 1000°C Allowable Moisture in Welding Electrode based on AWS A5.5 [1996] Allowable moisture for E6013 is not specified! [Hirai et al., 1980] 1st IC-DAEM & SENAMM XI 2018
  • 4. • to acquire allowable exposure duration of the E6013-RB26 electrodes in a wet tropical atmosphere so that no crack will occur in the AISI 1035 steel weldment • to study cracking modes in the AISI 1035 steel weldment due to influence of level of absorbed moisture in the E6013-RB26 electrode flux Boundary Condition • Base Metal : AISI 1035 Steel • Process : SMAW, WIC Test • Electrode : Kobe Steel RB26 Φ3.2 mm (class AWS A5.1 E6013) • Variable : Preheat/non-preheat treatment and absorbed moisture content in the electrode flux • Electrode hydration and welding process was implemented in room temperature environment • Surface crack was observed 3 days after welding Purpose 1st IC-DAEM & SENAMM XI 2018
  • 5. Work Flow Chart 1 st IC-DAEM & SENAMM XI 2018 Start Preparation As-Received Characterization AISI 1035 Steel E6013-RB26 Electrode • OpticalEmissionSpectrometry(OES) • Hardness Test • Tensile Test • Metallography • OES • Weighing 100°C • Weighing 91%RH • Weighing 80%RH • Weighing 68%RH Electrode Treatment • Baking 100°C, 40’ • Hydration • No preheat • Preheat 150°C Welding (WIC Test) Surface NDT Metallography Micro-Vickers Hardness Test Analysis Conclusion Finish
  • 6. Steel Samples ASTM 10 Grain-Sized Pearlitic Microstructures in AISI 1035 Steel As-Received 1st IC-DAEM & SENAMM XI 2018
  • 8. Electrode Hydration and Weighing Procedure 1] Electrode homogenization (100°C, 40 minute) in an oven 2] Electrode hydration using supersaturated salt solution agent in air-tight container 3] Weigh electrode in each intended period (0.0001 g precision), then immediately return the electrode to hydration apparatus. → Output: absorbed moisture mass in electrode flux 1st IC-DAEM & SENAMM XI 2018
  • 9. Electrode Mass Gain Model 8 8.3 8.6 8.9 0 60 120 180 Electrode Covering Gross Weight (g) Baking Duration (minutes); at 100°C Function of Absorbed Moisture (α) Gain in E6013- RB26 Covering over Exposure Duration at 91%, 80%, and 68% Relative Humidity, at 24°C E6013-RB26 Covering Gross Weight over Time at 100°C Baking Temperature; Remained Constant after 40 Minutes 1. Baking 2. Hydration after Baking 1st IC-DAEM & SENAMM XI 2018
  • 10. Sample Coding and Treatment Pre-Welding: Variation in Preheat Treatment and Absorbed Moisture Content (α) Welding: Similar Heat Input 1st IC-DAEM & SENAMM XI 2018
  • 11. Surface NDT Result • Crater (≈10 mm) at the end of weldment is neglected in crack measurement • Crack length is measured as straight as relative to weld length so that crack percentage does not beyond 100% Dye Penetrant Result MPI Result: NP-7 (left) vs WP-0 (right) measure 1st IC-DAEM & SENAMM XI 2018
  • 12. Hardness Hardness Test Spots [NACE MR0175] No Preheat 634 HV = AISI 1035 [Callister, 2014] Preheat 150°C • HAZ hardness was higher when preheat was not implemented • Even, hardness at some spots were found beyond 634 HV  martensite phase! 1st IC-DAEM & SENAMM XI 2018
  • 13. Microstructures 100 μm→ Typical Hard Microstructures with Coexistence of Martensite, Bainite, and Pearlite Formed in HAZ of Unpreheated Samples Ferit Widmanstätten Formed in Both Preheated and Unpreheated Samples Very-Fine Pearlite and Proeutectoid Ferrite in HAZ of Samples Preheated at 150°C 1st IC-DAEM & SENAMM XI 2018
  • 14. Macrograph NP-7: α = 7%, no preheat NP-0: α = 0%, no preheat WP-1.8: α = 1.83%, preheat 150°C, section 45° WP-1.4: α = 1.42%, preheat 150°C WP-0: α = 0%, preheat 150°C 14 mm 1st IC-DAEM & SENAMM XI 2018
  • 15. • Crack initiated from the weld core which is the last place of solidification • Intergranular crack propagated through ferrite widmanstätten grain boundaries up to surface • Based on α = 0% and the crack morphology, it was indicated as solidification cracking • Conclusion: it had poor weldability when preheat was not implemented although dry flux was used Cracking Modes in Sample NP-0 1st IC-DAEM & SENAMM XI 2018
  • 16. Cracking Modes in Sample NP-7 • Crack initiated from HAZ, followed by transgranular propagation • Crack propagation turned to intergranular in weld metal, through the columnar structures • Combination of hydrogen cracking and solidification cracking 1st IC-DAEM & SENAMM XI 2018
  • 17. Cracking Modes in Sample WP-1.8 Chevron cracks were characterized by cracks that appear on both sides of the weld metal with zigzag patterns like stairs and 45° oriented. Low levels of hydrogen have been believed to cause chevron cracks. Chevron Surface Crack Chevron Subsurface Crack 1st IC-DAEM & SENAMM XI 2018
  • 18. Summary 1st IC-DAEM & SENAMM XI 2018
  • 19. Welding Recommendation 0 2 4 6 8 10 0 4 8 12 16 20 24 α, Absorbed Moisture (%) t, Duration (hours) 91%RH 80%RH 68%RH • Crack still appeared in WP-1.8 case • The WP-1.4 case was taken as a threshold point that not generates any crack • Preheat at 150°C is mandatory 1 st IC-DAEM & SENAMM XI 2018 NP-7 NP-0 WP-1.8 WP-1.4 WP-0
  • 20. Conclusion • Without preheating, 37% solidification cracking of the weld length occurred in a sample welded with E6013-RB26 electrodes even in the absence of absorbed moisture content in the electrode covering. • The addition of the absorbed moisture up to 7% created combination of solidification cracking and hydrogen cracking with 48% surface crack. • On the other hand, preheating at 150°C, intergranular hydrogen chevron crack occurred when absorbed moisture reached 1.8% with 3% surface crack. • Crack-free weld joint has been observed on preheat at 150°C samples with absorbed moisture 1.4% or less. 1st IC-DAEM & SENAMM XI 2018
  • 21. Conclusion • WIC test was found to be effective to study the effect of absorbed moisture in electrode covering to the weld soundness. • Electrode exposure can be accurately simulated using oversaturated salt solution as hydration agent which gives stable relative humidity in a domestic food container. 1st IC-DAEM & SENAMM XI 2018
  • 22. Bibliography • Lampman, S. (1997): Weld Integrity and Performance, ASM International. • Chew, B. (1976): Moisture loss and regain by some basic flux covered electrodes, Welding Journal, AWS. • Valencia, E. and Galeano, N. (1994): Hygroscopic behavior of certain basic‐coated electrodes in a wet tropical climate, Welding International, 8:3, 208—213. • American Welding Society (1996): AWS B4 Standard Methods for Mechanical Testing of Welds. • Quincot,G.,Azenha,M.,Barros,J.,andRuiFaria(2011):UseofSaltSolutionsforAssuringConstantRelativeHumidityConditionsinContainedEnvironments, GovernodaRepúblicaPortuguesa,Guimarães. • Jowitt, R. and Wagstaffe, P . (1989): The Certification of the Water Content of Microcrystalline Cellulose at 10 Water Activities, Commission of the European Communities,Luxembourg. • Greenspan, L. (1977): Humidity fixed points of binary saturated aqueous solutions, Journal of Research of the National Bureau of Standards, 81A:1. • CallisterJr.,W.danRethwisch,D.(2014):MaterialsScienceandEngineering–AnIntroduction,9thEdition,Figure10.32,Wiley,USA.(AdaptedfromEdgarC. Bain,FunctionsoftheAlloyingElementsinSteel,1939;andR.A.Grange,C.R.Hribal,andL.F.Porter,Metall.Trans.A,Vol.8A.Reproducedbypermissionof ASMInternational,MaterialsPark,OH.) • Tuliani, S. (1976): A metallographic study of chevron cracks in submerged arc weld metals. Welding Research International, 6:6, 19—45. • Mota, J. dan Apps, R. (1982): Chevron cracking – a new form of hydrogen cracking in steel weld metals. Welding Research Council. • Lancaster, J. (1993): Metallurgy of Welding, 5th Edition, Chapman-Hall, London, UK. • Gedeon, S. and Eagar, T. (1990): Welding Journal, 69:7, page 264—271. • Alipooramirabad, H., Paradowska, A., Ghoamshchi, R., Hoye, N., and Reid, M. (2016): Experimental Investigation of Welding Stresses in MWIC Weldability Test, University of Wollongong, Australia. 1st IC-DAEM & SENAMM XI 2018