Section
4 Welding procedure tests for non-ferrous alloys
4.1 Requirements for aluminium alloys
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:
-
The welding positions
approved are as detailed in Table 12.4.4 Welding procedure approval,
welding positions for aluminium alloys.
-
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.
-
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.
-
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.
-
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.
-
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
4.2.2 Impact tests
on copper alloys are not required.
4.2.3 Hardness
tests are not required for seawater service.
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.
|
|