In addition to advanced generation/reception, true depth
or volume-corrected S-scans are popular due to their apparent coverage
and imaging. Figure 1 shows an example of an S-scan with easy discontinuity
location analysis. Discontinuities located on the B0 (half skip) horizontal
line are on the inner diameter, and those on the T1 line (full skip)
are on the outer diameter. Signals in between B0 and T1 are midwall.
While S-scans, as Figure 1 shows, give apparent coverage, it is not
fully clear that all sections of the weld are actually tested, or how
many S-scans are required for full coverage. This is the purpose of
this paper.

Figure 1 — S-scan of a weld with inner and outer diameter
discontinuities located.
S-SCAN COVERAGES AND BEVEL INCIDENCE ANGLES
Coverage for manual testing using S-scans is not an issue,
as procedures normally require the operator to raster scan over the
full weld (this is the same as conventional manual testing). However,
for encoded linear scans using S-scans, coverage is important. In order
to get the benefits of faster scanning with smaller instruments, a limited
number of S-scans is desired. Clearly, S-scans may cover the whole weld,
if the wall is thin. For thicker walls, multiple scans are obviously
needed: either a single pass with a suitably long array, or multiple
passes.
The situation is complicated by the requirements to be
close to the bevel incidence angle (ASME, 2007), or to use "appropriate"
angles. How close is close enough? Theoretical work (Charlesworth and
Temple, 1989) showed that an incidence within 5° of the bevel could
be considered close enough, while at 10°, off-incidence angle signal
amplitudes start to drop off significantly. Effectively, there is no
consensus at the practical level.
In addition, monocrystal probes normally only come at
fixed angles such as 45, 60 and 70°. If the designer (legitimately)
mandated a weld bevel angle of 37.5°, it would never be possible
to test within ±5° of bevel incidence angle. Overall, it
appears that there is no uniformity of practice here.
Modeling of the bevel incidence angle was performed with
a basic graphic design program that provides angular information on
a simple butt weld. The results are shown in Figure 2. Depending on
the bevel incidence angles required, either two S-scans (for ±10°)
or three (for ±5°) will provide "appropriate" angles
(ASME, 2007). This work did not define "coverage," particularly
for thin-walled components.

Figure 2 — Model of bevel incidence angle: (a) ±5°
bevel incidence angle coverage (requires three S-scans for coverage);
(b) ±10° bevel incidence angle coverage (requires two S-scans
for coverage); (c) ±10° coverage on thicker wall (still requires
only two S-scans for coverage).
CODES
Inspection codes generally accept new technologies like
phased arrays. This applies specifically to the three main North American
codes: ASME (2007), API (1996) and AWS (2006). However, the techniques
and technologies need approval. All these codes have methodologies for
adopting new technologies and techniques.
The general conditions to be met for any weld examination
in ASME include "an appropriate angle" and "full volume
coverage" (ASME, 2007).
MODELING PROCEDURES
This work used simple computer modeling to determine coverage
of various weld profiles and thicknesses to show whether full coverage
is obtained or not. The software used does not calculate bevel incident
angles commercially yet, but readily shows coverage using S-scans. The
program is simple to use, and fulfills the ASME scan plan requirements.
It is typical of the type of simple ray tracing programs that are, or
should be, available on standard phased array instruments to evaluate
ASME and other code scan plans.
Modeling was performed on three basic welds: butt welds,
T-welds and K-welds. The assumption is that the T-welds and K-welds
are reasonably thick, while butt welds can be any thickness. The array
was moved to optimize the test, on the basis that all operators will
generate a scan plan and follow it during testing.
The software uses standard commercial arrays and wedges,
which can be selected as appropriate. These probes are then placed on
the modeled component, including the weld profile, to view the beam
patterns. Using S-scan parameters (for example, angular range), S-scan
coverage can be immediately visualized. Moving the probe around or changing
the setup parameters allows the operator to optimize the test, and print
the results for a scan plan and auditable report. Multiple S-scans and
multiple arrays can be modeled, as well as more complex components.
The dotted lines beside the ray trace fan are the 6 dB drop-off points
- that is, what is normally considered adequate coverage by code.
A prototype software version has bevel incidence angle
calculated, as shown in Figure 3. Here, selected angles on a 25 mm (1
in.) pipe wall with a single S-scan are shown; interestingly, essentially
full coverage is obtained, while bevel incident angles are only just
above 10° at worst.

Figure 3 — Ray tracing using advanced software with sample
bevel incidence angles (arrowed) calculated on 25 mm (1 in.) wall double-V
weld.
MODELING RESULTS
Single V Weld
This weld configuration is typical of shielded metal arc
welding prep: it has a 2 mm (0.08 in.) land, 60° included angle
and a 2 mm (0.08 in.) gap. The probe/wedge combination for thin wall
examples has been selected to minimize the dimension to the nose of
the wedge (Figure 4a). This is necessary to ensure optimum approach
for the root region. The modeling was performed on walls from 5 to 25
mm (0.2 to 1 in.). The 5 MHz array modeled used a 16 element, 10 mm
(0.4 in.) aperture. Figure 4b shows the dimensions of the 5 MHz 64 element
array used for thicker walls.

Figure 4 — Dimensions of: (a) probe/wedge used for thin wall
examples; (b) larger 64 element array and wedge.
Thin wall sections will be problematic in that the root
regions may not be accessible, even with a 70° refracted angle on
the half skip. Coverage using a half skip may be possible with wedge
modification. Figures 5a to 5d show a series of welds from 5 to 9 mm
(0.2 to 0.35 in.) wall, all covered by a single S-scan. Figure 5a shows
the coverage on 5 mm (0.2 in.) with a single skip. Depending on the
geometry and parameters, it may be possible to obtain volume coverage
using a 1.5 skip technique, as shown in Figure 5b.

Figure 5 — Modeling results with single S-scan on thin walled
butt welds: (a) 5 mm (0.2 in.) wall using standard 45 to 70° refracted
shear wave S-scan; (b) 5 mm (0.2 in.) wall using 1.5 skip 50 to 65°
refracted shear wave S-scan; (c) 7 mm (0.28 in.) wall using standard
45 to 70° refracted shear wave S-scan; (d) 9 mm (0.35 in.) wall
using standard 45 to 70° refracted shear wave S-scan; (e) 9 mm
(0.35 in.) wall using standard 45 to 70° refracted shear wave
S-scan with increased standoff.
As thickness increases the traditional approach using
a 45 to 70° S-scan sweep is feasible, even with a relatively wide
cap. In both cases (5 and 7 mm [0.2 and 0.28 in.]) the angles of approach
for the root rely on corner reflections and the skip up to the upper
weld bevel provides reasonable angle approach, albeit slightly more
than 10° off the bevel angle at the upper extreme (Figure 5c). However,
at the upper extreme (cap region) the corner effect will again ensure
high probability of detection especially at the 45 to 50° refracted
range.
Of course the gap is critical at this juncture. If the
gap gets too wide, the 1.5 skip option would need to be used to ensure
suitable root coverage. By the time the wall thickness reaches 9 mm
(0.35 in.), the coverage of the root-region by a refracted 65 to 70°
angle can be reasonably assured for most conditions of cap geometry
(Figure 5d). However, at this point the cap region could suffer a reduced
coverage in the heat affected zone of the probe side of the weld. If
the gap is not excessive, this can be adapted to by a slight increase
in standoff (Figure 5e).
The minimum angle could be extended to 40 from 45°
and still achieve the volume coverage (if calibratable at this range).
However, the assumption that the root is properly addressed assumes
that the gap is not varying and the center of the weld cap can be used
as a guide to adequately assure the probe position for alignment. Both
of these assumptions cannot be guaranteed to be true.
In addition, this is a 30° weld bevel; other weld
bevels and component geometries are possible, so the best solution is
modeling on the specific weld bevel to produce a scan plan. These modeling
results can only be regarded as a guideline.
At thicknesses over 9 mm (0.35 in.), single V bevels should
be tested using a minimum of two S-scans with two different standoffs
from each side of the weld. This may be achieved by two passes or, if
the probe/wedge design is suitable, it may be possible to leave the
probe in one position and generate two sets of S-scans per side. Results
from 10 mm (0.4 in.) and up are shown in Figures 6a and 6b. The amount
of standoff difference will depend on the configuration, and is typically
0.5 to 1.5 aperture dimension. The illustrations in Figure 6 use a 10
mm (0.4 in.) aperture (16 elements with 0.6 mm [0.02 in.] pitch).

Figure 6 — Modeling results for walls 10 mm (0.4 in.) and
up: (a) 10 mm (0.4 in.) wall using standard 45 to 70° refracted
shear wave S-scans with two standoffs (b) 25 mm (1 in.) wall using
standard 45 to 70° refracted shear wave S-scan with two standoffs.
For thicker sections, the ratios remain the same; however,
the probability exists that the volume of concern extends to greater
dimensions due to the heat affected zone. Two standoff positions not
only ensure required volume coverage, but also provide increased probability
of detection by providing a second angle of approach on the bevel face.
These results were essentially established in earlier
modeling and experimental work (Moles and Zhang, 2005). Here, the concern
was more about the bevel incidence angle than coverage; however, the
conclusions are similar. For thin walls, enough ultrasound was "showered"
back to the probe for detection with a single pass. For thick walls,
multiple S-scans were required for "appropriate" angles. Note
that two smaller probes were used here, though a single larger array
should be technically feasible.
One last point about the modeling images: while the software
may not give direct measurements of the bevel incident angle yet, the
images show clearly that in some cases the angles are not "appropriate."
This does not apply so much on the near bevel, but Figures 5 and 6 show
that angles on the far side weld bevel are clearly inappropriate. The
codes generally require testing from both sides, which is supported
here. Though angles may be inappropriate, coverage may be adequate on
the far bevels.
Double V
Double V weld preparations are typically used where wall
thickness increases and access is available from the two sides. One
purpose of double V weld preparations is to reduce the weld volume that
could result from the wide openings that could occur if the single V
was continued. The angles used will be greatly dependent on the welding
process and access. Since no single preparation geometry exists, the
one used for illustration here will consider a relatively wide opening
with symmetrical geometry left and right and inside and out.
The probe/wedge combination for heavier wall examples
need not be as concerned with the approach restrictions of cap dimensions,
and can be larger than those required for thin walls. A typical off-the-shelf
5 MHz 64 element probe can be used for most applications. Dimensions
of such a probe are shown in Figure 4b.
The likely scenario for increased thickness would be to
use larger apertures, so this has been increased to 20 elements, or
approximately 12 mm (0.47 in.). Figures 7a to 7c show the modeled results.
Because of the shorter height from the root to the near and far surfaces,
the openings at the surfaces are smaller than was the case for the single
V. This means that a single 45 to 70° S-scan could be used to cover
the volume of interest. This is seen in the blue S-scan in Figure 7a.
However, in order to better address the possibility of incomplete root
penetration (midwall on this illustration) a second S-scan is presented
that covers the root region with a direct soundpath.

Figure 7 — Modeling results for symmetrical double V welds:
(a) 25 mm (1 in.) wall using standard 45 to 70° refracted shear
wave S-scans with second standoff for root; (b) 50 mm (2 in.) wall
using standard 45 to 70° refracted shear wave S-scans with second
standoff for root, showing lack of coverage; (c) 50 mm (2 in.) wall
using standard 45 to 70° refracted shear wave S-scans with three
standoffs.
Although the "volume" can in some cases be fully
addressed by a single focal law, the added coverage of a second S-scan
(from both sides of the weld) should be a requirement, which it is in
ASME (2007). In Figure 7a, the apertures are 20 elements, with the first
start element at #7 and the second aperture starting at #40. Hence,
almost two aperture dimensions separate the focal laws. This distance
will vary depending on the weld dimensions.
The ability to address both the weld outer edges at the
heat affected zone and still provide direct approach to the root area
cannot extend continuously and will be limited by the probe dimensions.
As an example, using the same design of bevel and probe/wedge combination
on a 50 mm (2 in.) wall, the coverage cannot be maintained (Figure 7b).
This would require a third S-scan and a repositioning of the probe/wedge,
as shown in Figure 7c.
Sometimes asymmetry of the weld bevel is used to overcome
welding approach difficulties. Bevel angles may then be reduced in some
cases, but the relative root position and weld openings must be considered.
For thicker sections this will in most cases require more than two S-scan
standoffs. Figures 8a to 8c illustrate some examples of asymmetric welds
and possible testing solutions using S-scans. In Figure 8a, the weld
is well covered using three S-scans. In Figure 8b, the (interior) root
is poorly addressed as a result of only two S-scans. Note that Figure
8b also shows a less than ideal angle approach to the weld prep at about
1/3 to 1/2T depth. This can be improved by using a hybrid triple S-scan,
as shown in Figure 8c. (Figure 8c still shows a less than ideal angle
approach to the weld prep at about 1/2T depth with this setup. The region
between the green and the red shows that a small portion is not covered
with a direct first half-skip approach.)

Figure 8 — Modeling results for asymmetrical double V welds:
50 mm (2 in.) wall using standard 45 to 70° refracted shear wave
S-scans with three standoffs for asymmetric bevel; (b) 50 mm (2 in.)
wall using standard 45 to 70° refracted shear wave S-scans with
two standoffs for asymmetric bevel, but now inverted; (c) possible
hybrid triple S-scan approach for testing double V welds with asymmetric
profiles.
Other Weld Configurations — T-welds
Examination of welds is not always as simple as that presented
for butt welds. Curved surfaces or angled intersections can provide
other considerations. Also, access is always a consideration since some
surfaces are often unavailable for testing.
The general rule for ultrasonic testing is to inspect
the weld from the surface on which the bevel is made. For T-welds, this
will be dependent on the preparation type. As with butt welds, the preparation
can be single or double-sided. Similar considerations must be given
for access (probe size) and volume coverage, as was done for butt welds.
Access to the vertical face (unbeveled) may be limited or the wall thickness
may be such that no practical skip effect can be used to approach the
weld from those surfaces. Fusion faces provide a major concern for weld
quality and the vertical land at the root is again given extra coverage
where possible. This will usually involve two standoff positions when
using S-scans (T-connections are not likely encountered in thinner wall
plate, such as less than 10 mm [0.4 in.]). Figures 9a and 9b show two
sample T-weld profiles and testing strategies.

Figure 9 — T-weld profiles and testing strategies: (a) 20
mm (0.8 in.) beveled T-weld using standard 45 to 70° refracted
shear wave S-scans with two standoffs; (b) 20 mm (0.8 in.) beveled
plate on 20 mm (0.8 in.) plate using standard 45 to 70° refracted
shear wave S-scans.
Although a single fusion-face is well-approached from
the plate via a skip, and a single standoff may suffice, little useful
information is gained and weld surface geometry may present limitations
for access and cause mode conversions.
When access is possible from the opposite wall, the ideal
access is made to view the longest fusion face and also provide access
to angle beams to assess the beveled faces. Where concern exists for
toe cracking on the unbeveled plate, a second set of S-scans (or E-scans)
can be made (Figures 10a and 10b). In Figure 10a, a normal incidence
is all that is required for the flat fusion line of the member the probe
is on. The beveled fusion lines would normally be covered by the angular
approach from the lower member.

Figure 10 — Scanning from the opposite wall: (a) 20 mm (0.8
in.) plates using 0° E-scan, and 0 to 35° S-scans at two standoffs
with another two standoffs for 0 to –35° S-scans using refracted
compression mode; (b) 20 mm (0.8 in.) plates using two compression
mode S-scans 25 to 45° and –25 to –45° for toe
cracking.
DISCUSSION
One question that has been asked is whether we really
need to perform two S-scans on thin plates to get coverage. The modeling
shows clearly that on butt welds of less than 10 mm (0.4 in.), coverage
can be achieved in a single S-scan. However, not all bevel incidence
angles will be optimum. Will we miss discontinuities? The answer, based
on previous modeling (Moles and Zhang, 2005), is probably no for thin
plates, as the probe aperture is relatively large in comparison with
the wall, and should collect reflected ultrasound well.
However, this is not the case with all welds. Above 10
mm (0.4 in.), two S-scans are definitely required for coverage. In addition,
two S-scans are required for appropriate angles. As the wall gets thicker,
more than two S-scans may be required. For complex weld configurations,
no predictions are possible. However, it is generally straightforward
to model the component, and then determine what the optimum S-scan positions
are, and whether coverage is possible. A future version of the software
will have bevel incidence angles, so both coverage and appropriate angles
can be determined with a simple program.
Codes typically require some knowledge of "coverage,"
so this trend of using modeling should continue, primarily for encoded
linear scans. Note that coverage and appropriate angles are not the
same; one can have coverage but inappropriate angles. In such a case,
little may be detected.
CONCLUSION
Simple ray tracing programs can show coverage of welds
using S-scans for linear encoded scan plans. To answer the question
of whether more than one S-scan is required for thin walls, the modeling
shows that a single S-scan can obtain coverage for a butt weld up to
around 10 mm (0.4 in.). For codes such as ASME Section V (2006) that
require scan plans for linear encoded scanning, simple modeling appears
to be the best solution to show coverage and appropriate angles. Realistically,
it is not possible to give rules from this modeling due to the wide
configuration variations in welds (and probes); these results should
be treated as guidelines only.
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AchAPI, Recommended Practice
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Fabrication and Qualification of Technicians, third edition,
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ASME, ASME Boiler and
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Ultrasonic Examination, per Article 4, Section V, New York, American
Society of Mechanical Engineers, 2006.
ASME, ASME Boiler and
Pressure Vessel Code, New York, American Society of Mechanical
Engineers, 2007.
AWS, D1:1 2006, Structural
Welding Code - Steel, Miami, Florida, American Welding Society,
2006.
Charlesworth, J.P. and J.A.G.
Temple, Ultrasonic Time of Flight Diffraction, Hertfordshire,
England, Research Studies Press, 1989.
Moles, M. and J. Zhang, "Construction
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