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March 2017

AFRICAN FUSION

15

Figure 2: A schematic view of the welded sample used in fatigue testing.

Figure 4. Drawings of the welded specimens for fatigue testing at different

conditions: W: As-welded condition; R: Repair by gouging and welding; R/UP:

Repair by gouging, welding and UP.

Figure 3: Fatigue curves of welded elements (transverse non-load carrying

attachment). 1: In the as welded condition; 2: UP was applied before fatigue

testing; 3: UP was applied after fatigue loading with the number of cycles

corresponding to 50% of expected fatigue life of samples in as-welded

condition.

Mechanical Properties

σ

y

(MPa)

σ

u

(MPa)

δ

(%)

Ψ

(%)

260

450

37.6

63

Table 1: The mechanical properties of base material.

Chemical composition (%)

C

Si

Mn

S

0.210

0.205

0.520

0.019

P

Cr

Ni

Cu

0.007

0.040

0.040

<0.010

Table 2: The data on chemical composition of base material

the mechanical properties of the material used, the type of

welded joints, the cyclic loading parameters and other factors.

For the effective application of the UP, depending on the

above-mentioned factors, a software package for optimum

application of ultrasonic peeningwas developed that is based

on an original predictive model. In the optimum application,

a maximum possible increase in fatigue life of welded ele-

ments with minimum time, labour and power consumption

is predicted [4].

Manufacturing and rehabilitation

The effectiveness of UP treatment applications to as-manu-

factured parts and in rehabilitation of parts that have already

served a considerable amount of their useful fatigue life was

studied. Rehabilitation is considered as the prevention of pos-

sible fatigue crack initiation in existing welded elements and

structures that are in service. UPwas applied to newparts and

to parts after 50% of their expected fatigue life.

Three series of large-scale welded samples imitating the

transverse non-load-carrying attachments (Figure 2) were

subjected to fatigue testing in 1: The as welded condition; 2:

After UP was applied before fatigue testing; and 3: After UP

was applied after fatigue loading with the number of cycles

corresponding to 50% of the expected fatigue life of samples

in the as-welded condition [8].

Tables 1 and 2 present themechanical and chemical prop-

erties of the materials used for preparation of the samples.

The results of the conducted fatigue testing with UP applied

to specimens in the as-welded condition and also after 50%

of expected fatigue life are presented in Figure 3.

As can be seen from Figure 3, UP caused a significant

increase in fatigue strength of the welded elements for both

series of UP treated samples. The increase in the limit stress

range at N=2×10

6

cycles of welded samples is 49% (from

119 MPa to 177 MPa) for UP treated samples before fatigue

loading; and 66% (from 119 MPa to 197 MPa) for UP treated

samples after fatigue loading – with the number of cycles cor-

responding to 50% of the expected fatigue life of the samples

in the as-welded condition.

The higher increase of fatigue life of UP treated welded

elements for fatigue curve No 3 could be explained by a more

beneficial redistribution of residual stresses and/or ‘healing’

of fatigue-damaged material by UP in comparison with the

fatigue curve No 2.

Use of UIT/UP for weld repair

UP could also be effectively used during the weld repair of

fatigue cracks [3, 5]. Figure 4 shows the drawings of large-scale

welded specimens containing non-load carrying longitudinal

attachments for fatigue testing [3]. These specimens were