Section 4 Welding procedure tests for non-ferrous alloys
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Clasifications Register Rules and Regulations - Rules for the Manufacture, Testing and Certification of Materials, July 2022 - Chapter 12 Welding Qualifications - Section 4 Welding procedure tests for non-ferrous alloys

Section 4 Welding procedure tests for non-ferrous alloys

4.1 Requirements for aluminium alloys

4.1.1 The requirements for welding procedure qualification tests for aluminium alloys are to be in accordance with the general requirements of Ch 12, 2 Welding procedure qualification tests for steels with the following exceptions and specific requirements.

4.1.2 Non-destructive examination is to be performed in accordance with Ch 12, 2.5 Non-destructive examination (NDE) and the assessment of results is to be in accordance with Table 12.4.1 Acceptance criteria for surface imperfections of aluminium alloys and Table 12.4.2 Acceptance criteria for internal imperfections of aluminium alloys.

Table 12.4.1 Acceptance criteria for surface imperfections of aluminium alloys

Surface discontinuity Classification according to
ISO 6520-1
Acceptance criteria
Crack 100 Not permitted
Lack of fusion 401 Not permitted
Incomplete root penetration in butt joints welded from one side 4021 Not permitted
Surface pore 2017 d ≤ 0,1s or 0,1a
    max. 1,0 mm
Uniformly distributed porosity (see Note 1) 2012 ≤ 0,5% of area
Clustered porosity 2013 Not permitted
Continuous undercut 5011 Not permitted
Intermittent undercut 5012 h ≤ 0,1t or 0,5 mm (whichever is the lesser)
Excess weld metal (see Note 2) 502 h ≤ 1,5 mm + 0,1b or 6 mm (whichever is the lesser)
Excess penetration 504 h ≤ 4 mm
Root concavity (see Note 2) 515 h ≤ 0,05t or 0,5 mm (whichever is the lesser)
Linear misalignment (see Notes 3 and 4) 507 h ≤ 0,2t or 2,0 mm (whichever is the lesser)
Symbols
a = nominal throat thickness of a fillet weld
b = width of weld reinforcement
d = diameter of a gas pore
h = height or width of an imperfection
s = nominal butt weld thickness
t = wall or plate thickness (nominal size)

Note 1. To be in accordance with ISO 10042.

Note 2. A smooth transition is required.

Note 3. The limits for linear misalignment relate to deviations from the correct position. Unless otherwise specified, the correct position is to be taken when the centrelines coincide.

Note 4. Dimensional tolerances not specified in these Rules are to be mutually agreed between the manufacturer and the Surveyor.

Table 12.4.2 Acceptance criteria for internal imperfections of aluminium alloys

Internal discontinuity Classification according to
ISO 6520-1
Acceptance criteria
Crack 100 Not permitted  
Lack of fusion 401 Not permitted  
Incomplete penetration 402 Not permitted  
Single gas pore 2011 d ≤ 0,2s or 0,2a or 4 mm (whichever is the lesser)
Linear porosity (see Note 2) 2014 Not permitted  
Uniformly distributed porosity (see Note 2) 2012 0,5t to 3t ≤ 1% of area
  > 3t to 12t ≤ 2% of area
  > 12t to 30t ≤ 3% of area
  > 30t ≤ 4% of area
Clustered porosity (see Note 1) 2013 dA ≤ 15 mm or wp (whichever is the lesser)
Elongated cavity
Wormhole
2015
2016
l ≤ 0,2s or 0,2a or 3 mm (whichever is the lesser)
Oxide inclusion (see Note 2) 303 l ≤ 0,2s or 0,2a or 3 mm (whichever is the lesser)
Tungsten inclusion 3041 l ≤ 0,2s or 0,2a or 3 mm (whichever is the lesser)
Copper inclusion 3042 Not permitted  
Multiple imperfections in any cross-section The sum of the acceptable individual imperfections in any cross-section is not to exceed 0,2t or 0,2a (whichever is the lesser)
Symbols
a = nominal throat thickness of a fillet weld
d = diameter of a gas pore
h = height or width of an imperfection
s = nominal butt weld thickness
t = wall or plate thickness (nominal size), in mm
wp = width of weld or width or height of cross-sectional area
dA = diameter of area surrounding gas pores
l = length of imperfection in longitudinal direction of weld

Note 1. For this acceptance criterion, linear porosity is to be considered as three aligned gas pores in a length of 25 mm.

Note 2. Porosity is to be determined in accordance with ISO 10042. The requirements for a single gas pore are to be met by all the gas pores within this circle. Systematic clustered porosity is not permitted.

4.1.3 Acceptance of the mechanical tests is to be in accordance with Ch 11, 9 Consumables for welding aluminium alloys. Welding of the strain hardened and heat treatable aluminium alloys will generally result in a loss of tensile strength in the heat affected zone below that specified for the base materials and the tensile strength acceptance criteria to be applied is that specified for the material in the annealed or 'as fabricated' condition. Minimum values of tensile strength measured on the transverse tensile samples are given in Table 12.4.3 Tensile strength requirements by grade for aluminium alloys.

Table 12.4.3 Tensile strength requirements by grade for aluminium alloys

Parent material Grade
(alloy designation)
Minimum tensile strength
(N/mm2)
5754 190
5086 240
5083 275
5383 290
5059 330
5456 290
6005A 170
6061 170
6082 170

4.1.4 Impact tests and hardness surveys are not required for aluminium alloys.

4.1.5 Four side bend tests may be used in place of root and face bends where the test thickness exceeds 12 mm, and longitudinal bend tests may be used instead of transverse tests where the test weld is between different grades of alloy. Bend specimens are to be bent round a former in accordance with Table 11.9.1 Requirements for butt weld tests in Chapter 11, with the exception that the 6000 series alloys may be bent round a former with D/t = 7.

4.1.6 The ranges of approval to be applied to the WPS are to be as specified for steel in Ch 12, 2.15 Range of approval with the following exceptions:

  1. The welding positions approved are as detailed in Table 12.4.4 Welding procedure approval, welding positions for aluminium alloys.

  2. The aluminium alloys are grouped into three groups as follows:

    • Group A: aluminium-magnesium alloys, with Mg content ≤3,5 per cent (alloy 5754).
    • Group B: aluminium-magnesium alloys with 4 per cent ≤Mg ≤5,6 per cent (alloys 5059, 5083, 5086, 5383 and 5456).
    • Group C: aluminium-magnesium-silicon alloys (alloys 6005A, 6061 and 6082).

    For each group, the qualification made on one alloy qualifies the procedure also for the other alloys in the group, with equal or lower tensile strength after welding. The qualification made on group B alloys qualifies the procedure for Group A alloys also. Approval for the range of material grades is summarised in Table 12.4.5 Welding procedure approval, aluminium material grades approved.

  3. The qualification of a procedure carried out on a test assembly of thickness t is valid for the thickness range given in Table 12.4.6 Range of qualification for parent material thickness. In the case of butt joints between dissimilar thicknesses, t is the thickness of the thinner material. In the case of fillet joints between dissimilar thicknesses, t is the thickness of the thicker material. In addition to the requirements of Table 12.4.6 Range of qualification for parent material thickness, the range of the qualification of throat thickness of fillet welds, a, is given in Table 12.4.7 Range of qualification of throat thickness for fillet welds. Where a fillet weld is qualified by a butt weld test, the throat thickness range qualified is to be based on the thickness of the deposited weld metal.

  4. The range of shielding gas compositions approved is to be in accordance with Table 11.9.2 Shielding gas compositions in Ch 11 Approval of Welding Consumables.

  5. A change in the brand or trade name of the filler metal from that used in the test is acceptable, provided that the proposed consumable has the same or higher strength grading.

  6. A change in post-weld heat treatment or ageing is not permitted, except that for the heat treatable alloys, artificial ageing may give approval for prolonged natural ageing.

Table 12.4.4 Welding procedure approval, welding positions for aluminium alloys

Test Position Positions Approved
Downhand D D
Horizontal-vertical X D, X
Vertical up Vu D, X, Vu
Overhead O D, X, Vu and O

Note Welding in vertical down (Vd) position is not recommended.

Table 12.4.5 Welding procedure approval, aluminium material grades approved

Material used in qualification test Material Grades approved
5754 5754        
5086 5086 5754      
5083 5083 5086 5754    
5383 5383 5083 5086 5754  
5059 5059 5383 5083 5086 5754
5456 5456 5383 5083 5086 5754
6005A 6005A 6082 6061    
6082 6005A 6082 6061    
6061 6005A 6082 6061    

Note Approval includes all the different strained and tempered conditions in each case.

Table 12.4.6 Range of qualification for parent material thickness

Thickness of test assembly,
t (mm)
Range of qualification
Multi pass welds
Range of qualification
All single-run or two-run (T technique) butt welds
t ≤ 3 0,5 to 2t 0,5t to 1,1t
3 < t ≤ 20 3 to 2t 0,5t to 1,1t
t >20 ≥ 0,8t 0,5t to 1,1t

Table 12.4.7 Range of qualification of throat thickness for fillet welds

Throat thickness of test piece, a (mm) Range of qualification
a < 10 0,75 a to 1,5 a
a ≥ 10 ≥ 7,5

4.2 Requirements for copper alloys

4.2.1 The requirements for welding procedure qualification tests for copper alloys are to be in accordance with the requirements for steel as given in Ch 12, 2 Welding procedure qualification tests for steels with the following exceptions and additions.

4.2.2 Impact tests on copper alloys are not required.

4.2.3 Hardness tests are not required for seawater service.

4.2.4 For the welding of cast copper alloys for propellers, the minimum tensile strength from the transverse tensile test is to be in accordance with Table 12.4.8 Minimum transverse tensile strengths for welded copper alloy propellers .

Table 12.4.8 Minimum transverse tensile strengths for welded copper alloy propellers

Alloy designation Minimum tensile strength (N/mm2)
CU 1 370
CU 2 410
CU 3 500
CU 4 550

4.2.5 Bend tests are to be performed over a diameter of former as detailed in Table 12.4.9 Former diameters for bend testing of copper alloy welds.

Table 12.4.9 Former diameters for bend testing of copper alloy welds

Alloy designation
(see Ch 9 Copper Alloys)
Former diameter
(D/t)
Cast propellers:  
CU1 4
CU2 4
CU3 6, see Note
CU4 6, see Note
Other short freezing range castings:  
Copper-Nickel 90/10 4
Copper-Nickel 70/30 4
Aluminium bronze 6
Wrought alloys (tubes and pipes):  
Copper-phosphorus 3
Aluminium-brass 3
90/10 Copper-nickel-iron 3
70/30 Copper-nickel-iron 3

Note Where the qualification tests for these alloys are subjected to post-weld heat treatment the former diameter may be increased to D/t = 10.

4.2.6 The range of approval to be applied to the WPS is to be as specified in Ch 12, 2.15 Range of approval with the exception of the material grades which are detailed in Table 12.4.10 Range of approval for copper alloy material grades.

Table 12.4.10 Range of approval for copper alloy material grades

Category Alloy grade used in the qualification test Alloy grades approved
Propellers CU1 CU1
CU2 CU1 and CU2
CU3 CU3
CU4 CU4 see Note 1
Tubes/pipes 90/10 Copper -Nickel-Iron 90/10 Copper -Nickel-Iron
70/30 Copper -Nickel-Iron 70/30 Copper -Nickel-Iron and
  90/10 Copper -Nickel-Iron
Tubes/pipes
see Note 2
Copper-Phosphorus deoxidised - arsenical Copper-Phosphorus deoxidised - arsenical
Copper-Phosphorus deoxidised - non arsenical Copper-Phosphorus deoxidised - non arsenical
Aluminium-brass Aluminium-brass

Note 1. Where a CU3 type welding consumable has been used for the qualification test, the range of approval may also include welding of CU3.

Note 2. These grades have limited weldability and approval to weld is subject to the materials satisfying the requirements of Table 9.3.1 Chemical composition of principal elements only in Chapter 9.


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