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Weld metal and heat affected zone (HAZ) properties of tanker hull structures

TWI Bulletin, September/October 2002

 

Jack Still
Jack Still

Jack Still worked in the steel industry as a metallurgist, which involved advising customers on welding of clad steels. He transferred to the fabrication industry and worked for Motherwell Bridge, Babcock and Wilcox and eventually Redpath Dorman Long. During this period he was involved with the fabrication of pressure vessels, tanks, boilers, offshore structures and modules. In 1978 he joined the offshore oil and gas industry and during the last 24 years worked for Britoil/BP, Shell Expro and eventually Amerada Hess on projects involving jacket and production modules, construction of an FPSO and refrubishment of mature structures.



Julian Speck
Julian Speck

Julian Speck joined TWI in 1998 with a BSc Eng in Materials Engineering from the University of Cape Town. He now undertakes a variety of structural integrity and risk-based assessment projects in the oil, gas and power industries. He is involved in the development of TWI's fitness-for-service (FFS) assessment and risk-based inspection programmes.

With the introduction of floating, production, storage and offloading vessels (FPSOs) for processing hydrocarbons from remote subsea wellheads, concerns have been highlighted regarding the integrity of tanker hull structures for FPSO applications. Although construction of hull structures are in accordance with class rules, FPSOs are intended to remain on location during their field life without having to dry-dock for inspection or repair. Jack Still and Julian Speck provide an overview of a test programme conducted to assure the fracture resistance of a recently completed Afromax tanker hull destined for conversion to an FPSO.


It is common practice for the ship builder to specify the hull materials in accordance with the classification society rules. The materials normally selected for an Afromax tanker consist of Grades A and AH32 carbon-manganese steel. Owing to the anticipated service conditions of the vessel, the outer hull materials were changed to Grades D and DH32. In addition, the thickness of the deck and the bottom of the hull, in Grade DH32, was increased by 3mm.

This upgrade in material was intended to provide improved resistance against fracture, ie resistance to the initiation of brittle cracks (fracture toughness) and crack arrest properties. Specific details of the composition and properties of hull steels are summarised in Tables 1 and 2, respectively. Figure 1 illustrates the location of the material grades within the hull structure.

Table 1: Chemical properties and product analysis

Grade Chemical analysis
  C Si S P Mn Ni Cr Mo V Ti Cu Nb Al
Soluble
N
  Chemical composition (All values quoted are maximum unless otherwise stated)
D 0.21 0.10/0.35 0.035 0.035 0.60min See Note 1  
  See
Note 1
     
DH32 0.18 0.10/
0.50
0.035 0.035 0.90/
1.60
0.4 0.2 0.08 0.05/
0.10
0.02 0.035 0.02/
0.05
0.015min  
  Typical product analysis
D 0.14 0.26 0.004 0.02 1.27 0.02 0.003 Tr - - 0.01 - - -
DH32 0.14 0.39 0.008 0.014 1.22 0.02 0.03 Tr - - 0.02 0.02 0.039 -
Note 1. When Ni, Cr, Mo and Cu to be reported.
When the amount does not exceed 0.02% these elements to be reported as <0.02%

Table 2: Mechanical properties for hull materials

  Mechanical properties Charpy impact properties
Grade Thickness,
mm
UTS Min,
N/mm 2
Yield min,
N/mm 2
Elongation,
Min %
Test
temperature, °C
Longitudinal,
joules
Transverse,
joules
Specification
D <50 400 235 22 -20 27 20
DH32 <50 440 315 22 -20 34 24
Typical product
mechanical properties
D 17.5 461 318 28 -20 210
DH32 19.5 541 449 25 -20 206
Fig.1. FPSO Hull materials
Fig.1. FPSO Hull materials
Location ABS base material Thickness, mm
A (Deck) Gr. DH32 19.5
B Gr. DH32 19.5
C (Side shell) Gr. D 17.5
D Gr. DH32 19.5
E (Bottom) Gr. DH32 19.5

Selection of welding consumables

The selection of welding consumables, was based on the weld metal Charpy impact toughness requirements matching the minimum Charpy impact toughness levels specified for the hull materials. Ship classification societies in this instance specify either Grade 2Y or 3Y consumables for welding Grades D and DH32 steels. The Charpy impact toughness requirements for 2Y consumables is 34J at 0°C which also meets the requirements for Grades A and AH32 steels. Grade 3Y consumables specify Charpy impact toughness requirements of 34J at -20°C, which satisfy the toughness requirements for Grade D and Grade DH32 steels.

Welding procedure test programme of work

Gas shielded flux cored arc (GSFCAW) and electro-gas (EGW) are the two main welding processes used during the construction of a tanker hull structure. Ceramic backing tiles are extensively used in conjuction with the above processes to enable single-sided welds to be produced, reducing the fabrication time. Figure 2 outlines the areas where GSFCAW and EGW are applied. Based on the use of the welding processes during construction of the hull structure, the weld test programme involved both Grades D and DH32 steels. The test plates included two GSFCAW consumables (AWS A5.29 E80T1-K2 1 from two consumable manufacturers (hereafter referred to as consumables A and B), and one EGW consumable, ie consumable C (AWS A5.26 EG70T-2 2).

Fig.2. Welding processes used for block assembly and erection
Fig.2. Welding processes used for block assembly and erection
Location Welding process Application Position 
A (Deck) GSFCAW (Root) Semi-automatic 1G (Ceramic backing)
GSFCAW Automatic 1G
B GSFCAW Semi-automatic 1G (Ceramic backing)
GSFCAW Semi-automatic 1G (Ceramic backing)
GSFCAW Semi-automatic 3G (Ceramic backing)
C (Side shell) GSFCAW Automatic 3G (Ceramic backing)
D GSFCAW Semi-automatic 3G (Ceramic backing)
E (Bottom) GSFCAW (Root) Semi-automatic 1G (Ceramic backing)
GSFCAW Automatic 1G
GSFCAW Semi-automatic 1G (Ceramic backing)

The welding procedure test plates were welded as single-sided welds in the vertical position, using a ceramic backing strip. Examples of the welding parameters recorded for both GSFCAW and EGW are presented in Table 3. No preheat was applied, ie material temperature was recorded as ambient. The maximum interpass temperatures recorded were 88 and 21°C, for the GSFCAW and EGW, respectively. Typical weldment macro-sections for both welding processes are shown in Fig.3.

Table 3: Electro gas welding and gas shield flux cored arc welding procedures

EGW joint preparation
GSFCA run sequence and joint preparation
Bead Diameter
mm
Polarity Amps Volts Weld
speed,
cm/
min
Heat
input,
KJ/
cm
Bead
5 layers
Diameter 
mm
Polarity Amps Volts Weld
speed,
cm/
min
Heat
input,
KJ/
cm
1 1.6 DCRP 410 38 9.6 97.4 1 1.2 DCRP 210 27 11.6 29.3
              2 1.2 DCRP 210 29 19.6 18.6
              3 1.2 DCRP 220 32 14.8 28.5
              4 1.2 DCRP 200 27 15.7 20.6
              5 1.2 DCRP 190 27 13.2 23.3
Electro gas welding (EGW)
shielding gas

Shielding gas flow rate 25 litres/min using 99% CO 2
Gas shield flux cored arc welding (GSFCAW)
shielding gas

Shielding gas flow rate 25 litres/min using 99% CO 2

Fig.3a) Typical gas-shield flux-cored arc weld (GSFCAW)
Fig.3a) Typical gas-shield flux-cored arc weld (GSFCAW)
Fig.3b) Typical electro-gas weld (EGW)
Fig.3b) Typical electro-gas weld (EGW)

Chemical analyses of plate materials and weld metals

The base metal and weld metal chemical analysis results are presented in Table 4. The GSFCAW welds contained additions of nickel, titanium, and boron. Both the nickel and the boron elements were in sufficient quantities to improve fracture toughness. The titanium is available for the dual purpose of promoting fracture toughness, while also acting as a sacrificial element to combine with nitrogen and thereby protect the boron addition. The weld metal chemical analysis of the EGW contained a relatively high manganese and molybdenum content.

Table 4: Weld material and parent material chemical analysis

Plate
No
C Si S P Mn Ni Cr Mo V Cu Nb Ti Al B
Weld
metal
1 (A)

0.06

0.37

0.012

0.015

1.27

1.41

0.03

<0.005

0.02

0.04

0.011

0.044

0.005

0.0062
2 (A) 0.06 0.42 0.009 0.015 1.20 1.45 0.03 0.005 0.01 0.005 0.009 0.041 <0.0003 0.0037
3 (B) 0.05 0.46 0.008 0.015 1.29 1.42 0.03 0.005 0.02 0.005 0.010 0.041 <0.0003 0.0039
4 (B) 0.05 0.34 0.013 0.014 1.22 1.45 0.03 <0.005 0.02 0.04 0.010 0.036 0.004 0.0053
5 (C) 0.07 0.48 0.008 0.019 1.82 0.02 0.03 0.19 <0.002 0.01 <0.002 0.017 0.013 0.0014
Plate
mate-
rial
1

0.15

0.18

0.003

0.023

0.74

0.01

0.03

<0.005

0.005

0.005

<0.002

<0.002

0.026

<0.0003
2 0.15 0.18 0.003 0.023 0.74 0.01 0.03 <0.005 0.005 0.005 <0.002 <0.002 0.024 <0.0003
3 0.16 0.27 0.003 0.016 0.99 0.01 0.04 <0.005 0.005 0.005 <0.002 <0.002 0.022 <0.0003
4 0.16 0.27 0.005 0.016 0.99 0.01 0.04 <0.005 0.005 0.005 <0.002 <0.002 0.023 <0.0003
5 0.15 0.18 0.003 0.021 0.74 0.01 0.02 <0.005 0.005 0.005 <0.002 <0.002 0.025 <0.0003
(A) GSFCAW - Electrode A, (B) GSFCAW - Electrode B, (C) EGW Electrode C

Mechanical properties of the test plate weldments

The mechanical properties of the test plate weldments are presented in Table 5. The Charpy impact toughness values of the weld metal for both welding processes and material grades were found to satisfy the minimum requirements of the classification society. Weld (HAZ) Charpy impact tests on specimens notched one millimetre from the fusion boundary, measured impact energy values well above the minimum specification requirements for the base material. The lowest HAZ Charpy impact toughness results were recorded in test plate No.3, in the Grade DH32 steel. The reason for the low value was not specifically investigated. (It was noted that the recorded welding parameters for this test plate were similar to that of the other test plate welds while the parent material composition showed no irregularities). The HAZ properties of the EGW welds measured comparatively higher values of impact toughness.

Table 5: Weld metal mechanical properties

Plate
No.
All weld metal tensiles Charpy impact tests
(Test temperature -20°C)
  Hardness test
(load 10kg)
 
RP 0.2%,
N/mm 2
Max
stress,
N/mm 2
Weld,
Joules
HAZ,
Joules
Parent
material
HAZ Weld
metal
HAZ Parent
material
1 (A) 475 633 80-80-75 168-165-177 137 156 206 147 134
2 (A) 548 671 96-93-102 228-236-243 157 150 213 154 142
3 (B) 512 638 105-102-103 81-86-94 153 171 222 172 150
4 (B) 420 609 89-101-102 150-214-151 150 176 217 160 148
5 (C) 473 677 63-90-56 43-107-126 156 162 203 157 152
(A) GSFCAW - Electrode A, (B) GSFCAW - Electrode B, (C) EGW Electrode C

All weld metal tensile tests recorded 0.2% proof strengths of between 420 to 512N/mm 2, while the parent material tensile properties ranged from 304 to 383N/mm 2. A Vickers hardness survey carried out on weldments recorded hardness values of between 212-240, and 169-181, in the weld metal and HAZ respectively.

CTOD fracture toughness

Crack-tip opening displacement (CTOD) fracture toughness tests were performed for use in a fracture mechanics-based engineering critical assessment (ECA). [3] The results of the ECA were subsequently used to identify the maximum flaw (fatigue crack) size that the fatigue sensitive hull welds could tolerate, prior to failure by fracture.

Weld metal and weld HAZ CTOD tests were manufactured from all procedure test panels and tested in accordance with BS 7448. [4,5] The range and the appropriate value ( δ mat) of CTOD fracture toughness test results (at -10°C), for each of the test panels, are presented in Table 6. In general, the accuracy of a sample depends on its size and on the variability of the property measured. If a material is microstructurally homogeneous, the sample size can be small. If it is non-homogenous, eg weld HAZ, the sample size must be large to be representative of the material.

Table 6: Summary of measured CTOD values at -10°C

Description Region δ min, mm δ mat, mm δ mat, mm*
ABS Grade D Parent material 1.570 1.613 1.570
ABS Grade DH32 Parent material 0.702 0.778 0.721
Gr. D, FCAW, E80T1-K2 (1) HAZ
Weld material
1.050
0.265
1.231
0.594
1.105
0.325
Gr. D, FCAW, E80T1-K2 (2) HAZ
Weld material
0.332
0.189
1.281
0.651
1.056
0.225
Gr. DH32, FCAW, E80T1-K2 (1) HAZ
Weld material
0.427
0.160
0.558
0.709
0.443
0.226
Gr. DH32, FCAW, E80T1-K2 (2) HAZ
Weld material
1.018
0.404
1.330
0.603
1.018
0.421
Gr. D, EGW, E70T-2 HAZ
Weld material
0.098
0.131
1.487
0.408
0.578
0.214
* δ mat is the second lowest CTOD value in a set of six specimens

Sets of six CTOD specimens were therefore tested for each weldment region. The 'appropriate' value of CTOD fracture toughness ( δ mat), for use in an ECA for failure by fracture, is subsequently defined as the second lowest result from the set. [6]

δ mat for all of the test panels was above 0.100mm. The highest were measured in the parent materials, ie δ mat > 0.500mm. Both parent materials exhibited fully plastic (ductile) behaviour during testing. The failures of the weld HAZ specimens were also ductile, except for a few results from the HAZ of a FCAW panel (Grade D, E80T1-K2 (B), δ min = 0.332mm) and the EGW panel (Grade D, E70T-2, δ min = 0.098mm). Post-test examinations revealed that the fracture event of the lowest HAZ CTOD result in the FCAW panel exhibited no tearing. The lowest HAZ CTOD in the EGW panel was found to be due to a significant pop-in, ie the arrest of a crack after it rapidly extends across a brittle microstructural region.

Weld metal and weld HAZ metallography

The weld metal and weld HAZ were metallographically examined from all of the test panels, ranging from 50 to 100X magnification. Examples of these microstructures are shown in Figure 4 (test plate No. 3, 19.5mm thickness, Grade DH32) and Figure 5 (test plate No.4, 17.5mm thickness, Grade D) and comprised the following phases:

Fig.4a) GSFCAW weld metal 100x
Fig.4a) GSFCAW weld metal 100x
Fig.4b) FSFCAW HAZ 100x
Fig.4b) FSFCAW HAZ 100x
Fig.5a) EGN weld metal 100x
Fig.5a) EGN weld metal 100x
Fig.5b) EGN HAZ 50x
Fig.5b) EGN HAZ 50x

Fig.4a. As-deposited and refined weld metal microstructure between two successive passes. The varying microstructural features are typical of multi-pass fusion welds, depending on the location within the weld.

Fig.4b. Weld HAZ, fusion line and weld metal microstructure comprising re-crystallised, transformed and tempered zones within the HAZ.

Fig.5a. As deposited microstructure at the outer edge of the weld, towards the fusion line. These large islands increase in size with increasing peak temperature and increasing residence time.

Fig.5b. Weld metal, fusion line and weld (HAZ). The HAZ microstructure exhibits enlarged areas of polygonal ferrite, a distinguishing feature of this comparatively high heat input process.

Ensuring quality of FPSO welds

The results of the materials test and inspection programs, over and above the class requirements introduced by the operator during construction, [6] were used in a fracture mechanics-based assessment to determine the maximum flaw size tolerable in the hull under in-service loading. Although this test programme was applied to a hull structure intended for conversion to an FPSO vessel, the principles could be applied to any vessel particularly tanker hull structures designed to operate in severe operating conditions.

Acknowledgements

The authors acknowledge the guidance of Dr R Razmjoo (Manager, Advanced Materials Structures, TWI) and Dr M Dawes (Principal Consultant, Fracture Testing, TWI) in preparation of this paper. The authors also thank Mr D Ellin, Chief Metallurgist, at The Test House, Cambridge, for undertaking the metallographic examinations.


References

Author Title
1 E80T1-K2, ANSI/AWS A5.29: 'Specification for low alloy steel electrodes for flux cored arc welding', American Welding Society, Miami, 1998.
2 EG70T-2, ANSI/AWS A5.26: 'Specification for carbon and low alloy steel electrodes for electrogas welding', American Welding Society, Miami, 1997.
3 BS PD 6493: 'Guidance on methods for assessing the acceptability of flaws in fusion welded structures', British Standards Institute, London, 1991. Return to text
4 BS 7448 - Part 1: 'Fracture mechanics toughness tests - Method for the determination of K lc, critical CTOD and critical J values of metallic materials', British Standards Institute, London, 1991. Return to text
5 BS 7448 - Part 2: 'Fracture mechanics toughness tests - Method for the determination of K lc, critical CTOD and critical J values of welds in metallic materials', British Standards Institute, London, 1997.
6 Still J R and Speck J B Hull: Weld quality for offshore oil production vessels; AWS, Welding Journal, August 2000, 33-38.