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M. Gladskyi, PhD, V. Frolov, PhD, N. Zylov, A. Rubanenko
National Technical
University of Ukraine “Kyiv Polytechnic Institute”,
Institute
of Mechanical Engineering
A Method for Low-Cycle Fatigue Life Assessment of
Metallic Materials under Program Multiaxial Loading
Keywords: multiaxial
low-cycle fatigue, irregular loading, titanium alloys, damage accumulation,
limit state criteria.
Abstract. The method of
fatigue life assessment under multiaxial low-cycle block loading, which is
based on the Pysarenko-Lebedev modified criterion, the linear damage rule as
well as non-linear Manson’s approach was proposed.
The
results of low-cycle fatigue tests of titanium alloy BT9 under block are given.
The proposed approach was found to be effective and confident to take into
consideration such factors as strain state type, strain path type and loading
irregularity.
Introduction.
Construction
elements often undergo irregular multiaxial cycle loading. Though multiaxial
materials fatigue has been studied for a long time and enough of experimental
data has been accumulated, problem of including of loading irregularity in
low-cycle fatigue area is still actual. Many attempts to describe fatigue
damage process were made, which resulted in many developed models of damage
accumulation. The well known one is the conception of linear damage rule. This
approach is easy to use but it does not give adequate estimation of life in
many cases. There were many attempts to develop model based on non-linear accumulation
of fatigue damages, but most of them did not consider complex influence of such
factors as type of stress state, loading path, previous stress history on the
process of fatigue damages accumulation. Fatemi and Yang [1] give a wide survey
of the existing models and offer their classification, describe advantages and
disadvantages of each one.
In the
paper it is studied influence of sequential loading effects on the titanium
alloys BÒ9 fatigue damage and under tension-compression, torsion and 90° out-of-phase
non-proportional loading. It is proposed life estimation method both under
regular and irregular multiaxial loading. Damage model is proposed, which
considers non-proportion effects, which appear at loading regime change.
Experimental procedure.
With
the purpose of getting stress-strain state close to homogeneous were used
tubular specimens with outer diameters of 11 mm, wall thickness of 0,5 mm, test
portion length of 21 mm.
Strain
controlled tests under both proportional and non-proportional irregular loading
were carried out.
Testing
program and results are given in Table 1. The basic modes were:
tension-compression, alternating torsion and 90° out-of-phase loading. The
first stage of the programme was the block axial loading and/or torsion moment
test with given strain ranges. During this test the strain path remained
constant. The second stage of the programme was testing the specimens with
changing of the strain path. Transfer from one strain path to another was conducted
during making the
value reach the 0.5
point and then the specimen was brought to failure. At the third stage the test
with a multiple strain path change was carried out.
Proposed method.
The
Pysarenko-Lebedev modified criterion as well as the two damage rules for
assessing the BT9 titanium alloy fatigue life was chosen. In the paper the
damage accumulation hypotheses were analysed [2]: the linear hypothesis and the
Manson’s approach , according to which the damage curve is the relative fatigue
life nonlinear function and looks like this:
,
where
;
– the number of
one-level loading cycles;
– number of cycles
before failure under the given loading level;
– material constant
that is calculated from the test data under sequential double-level loading.
Table 1
Strain peak values and number of cycle to failure for BT9
titanium alloy
|
Test |
|
|
|
|
Test |
|
|
|
|
||
|
% |
cycle |
% |
cycle |
||||||||
|
a_01 |
à |
0,8 |
- |
157 |
293 |
t_01 |
t |
- |
0,8-1,0-1,2-1,0 |
50 |
601 |
|
à |
1,0 |
- |
136 |
||||||||
|
a_02 |
à |
1,0 |
- |
98 |
245 |
t_02 |
t |
- |
1,2-1,0-0,8-1,0 |
50 |
528 |
|
à |
0,8 |
- |
147 |
||||||||
|
a_03 |
à |
0,6-0,8-1,0-0,8 |
- |
50 |
519 |
at |
a |
1,0 |
- |
97 |
398 |
|
t |
- |
1,0 |
301 |
||||||||
|
a_04 |
à |
1,0-0,8-0,6-0,8 |
- |
50 |
491 |
ta |
t |
- |
1,0 |
398 |
603 |
|
a |
1,0 |
- |
205 |
||||||||
|
oatota |
- |
0,8 |
1,0 |
50 |
475 |
ao |
a |
1,0 |
- |
98 |
184 |
|
o |
1,0 |
1,0 |
86 |
||||||||
|
oa |
o |
1,0 |
1,0 |
77 |
218 |
to |
t |
- |
1,0 |
282 |
390 |
|
a |
1,0 |
- |
141 |
o |
1,0 |
1,0 |
108 |
||||
|
atat_1/5 |
a |
1,0 |
- |
40 |
423 |
ot |
o |
1,0 |
1,0 |
80 |
384 |
|
t |
- |
1,0 |
130 |
t |
- |
1,0 |
304 |
||||
|
atat_1/3 |
a |
1,0 |
- |
65 |
510 |
|
|||||
|
t |
- |
1,0 |
219 |
||||||||
Analyzing
Fig.1 and Fig.2 one can see that during the application of the
Pysarenko-Lebedev modified criterion and the linear damage accumulation
hypothesis the best correlation of the predicted and test data is obtained for
alternating torsion (path t).
|
|
|
|
Figure 1 ‒ Comparison of predicted
fatigue lives by the linear damage rule with experimental fatigue lives |
Figure 2 ‒ Comparison of predicted fatigue lives by the damage curve approach with
experimental fatigue lives |
As a
result, one can come to a conclusion about the linearity of damage accumulation
process for a given loading type. The combined application of the
Pysarenko-Lebedev modified criterion and of the Manson’s approach showed the
high level of predicted and test data correlation for all the loading programmes
except the alternating torsion. So the following modification of the Manson’s
approach is proposed:
, (1)
where
;
– strain path
orientation angle, which determines the dominating type of the strain state;
and
are fatigue strength
coefficients at finite life
for uniaxial and
torsional loadings.
So,
during the alternating torsion the damage accumulation is linear, during the
tension-compression – with the application of the Manson’s approach, and during
the biaxial proportional and non-proportional loading their linear
interpolation.
The
application of formula (1) resulted in the best correlation of the best
correlation of the predicted and test data that is shown on the Fig.3.

Figure 3 ‒ Comparison of predicted
fatigue lives by the proposed approach with experimental fatigue lives
Conclusions.
The
proposed method of fatigue life assessment under multiaxial low-cycle regular
and irregular loading, which is based on the Pysarenko-Lebedev modified
criterion, the linear damage accumulation hypothesis and the non-linear
Manson’s approach turned to be effective and allowed to take into consideration
such factors as strain state type, strain path type and loading irregularity.
References
1. Fatemi A., Yang L.
Cumulative fatigue damage and life prediction theories: a survey of the state
of the art for homogeneous materials // Int. J. Fatigue. – 1998, vol.20, No.1,
pp. 9-34.
2. Shukayev S., Zakhovayko
O., Gladskyi M., Panasovsky K. Estimation of low-cycle fatigue criteria under
multiaxial loading // Int. J. Reliability and life of machines and structures.
– 2004, vol.2, pp. 127-135.