Investigation of the probabilistic low cycle fatigue design curves at stress cycling.

Bazaras, Z. ; Cesnavicius, R. ; Ilgakojyte-Bazariene, J. 等

1. Introduction

In working conditions some equipment's components are affected by high loads, which results in elastic plastic cyclic deformation. These type of loads may cause fatigue damage over time and results in crack propagation and fracture of the equipment. Due cyclic overloads, the cyclic varying stresses exceeds the proportional limit of the materials and after thousands cycles the fatigue crack appears which will result in part's failure with hardly predictable corollary [1, 2].

Aiming to improve the reliability and safety of the structures, the probabilistic methods for low cycle fatigue data, are applied in many manuscripts [3, 4]. These methods are based on statistically collected cyclic loading data and their probabilistic characteristics.

Probabilistic methods have been used for the assessment of statistical and fatigue damage properties [5].

Considerable contribution to the investigation of probabilistic methods, probabilistic substantiation of allowable stresses and strength safety and proposed calculation in the static and cyclic strength are used by many investigators [6-8].

The aim of this paper is to design the probabilistic estimation curves of low cycle fatigue. Also, a comparison of the probabilistic curves with the experimental data have been made [9].

2. Experimental setup for monotonic and low cycle loading

Experimental setup consists of 50kN testing machine YMM-5 and an electronic part, which is designed to record the stress-strain diagrams, cycles and contol the gear reversal. The 4 mm/min speed of deformation was used for tensile experiments. The cycle frequency of 4-10 cycles/min and 20 mm/min speed of deformation were used for low cycle tension-compression testing. The force and deformation meassurement range warries not more than [+ or -] 5%. GOST 25.502-79 standard was used for metal fatigue tests, whereas GOST 22015-76 - for probabilistic calculation of matallic parts. All the testing set-up with mechanical and electrical schemes is described in literature [10].

Experimental monotonic tension and low cycle tension-compression were carried out under ambient temperature. The specimens were tested under symmetric loading (R = -1) and experimental data was registered up to of the crack initiation.

The specimens of circular cross-section with d = 10 mm were used for low cycle fatigue tension-compression experiments. The specimens were made of grade steel 15Cr2MoVA and 45 rods according the dimensions presented in the Fig. 1.

For determination of mechanical properties the material for monotinic tension specimens was taken from the part of cyclic test specimens which has not been subjected to plastic deformation. The specimens of circular cross-section with d = 5 mm and length 5d were used for these tests.

[FIGURE 1 OMITTED]

In this paper, the low cycle fatigue tests were carried out under stress limited loading with two materials: cyclically softening steel 15Cr2MoVA (Fig. 2, a) and cyclically stable steel 45 (Fig. 2, b). The chemical composition and mechanical properties of the tested materials are presented in Table 1 and Table 2. As it seen from the Table 2, the materials are very ductile, especially 15Cr2MoVA ([psi] = 80%) [7-9]. The monotonous tension curve has plasticity of yielding, whereas 15Cr2MoVA doesn't have [9].

Three stress levels at stress cycling are evenly distributed over the range. Number of the tested specimens at each loading level are presented in the Table 3. In the middle levels number of the specimens were increased because the increased scatter was observed in the intermediate zone.

[FIGURE 2 OMITTED]

3. Mathematical analysis of probabilistic low cycle fatigue design curves

The purpose of stress limited tests is to define material fracture characteristics at elastic-plastic cyclic loading. For the assessment of a material strength the analytical relation between the static damage and accumulative plastic deformation was introduced in the Eq. (1) [1]:

[sigma.sub.a][N.sup.m.sub.p] = [sigma.sub.u][N.sup.m.sub.u]=const, (1)

where [sigma.sub.a] is stress amplitude; [N.sub.p] is fatigue durability; [N.sub.u] is number of cycles to fracture; m is a constant.

For analytical calculation, the fatigue curve of stress limited loading can be expressed as follow [11]:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)

where [e.sub.0] - initial strain; [m.sub.[sigma] - a constant dependent of mechanical properties of the material.

Under stress limited loading the part fractures due to quasi-static damage [d.sub.K], caused by the accumulated plastic strain [e.sub.pk], and due to fatigue damage dN, resulted by the cyclic plastic strain, which is characterized by the hysteresis loop's width [TEXT NOT REPRODUCIBLE IN ASCII]. The total damage d may be written (up to fracture, d= 1) [10]:

d = [d.sup.q.sub.K] + [d.sup.l.sub.N] (3)

where [d.sup.q.sub.K], [d.sup.l.sub.N] - quasi-static and fatigue damage; q and l - material constants [9-10].

Fatigue damage is calculated using the following Eq. (4):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (4)

where [FORMULA NOT REPRODUCIBLE IN ASCII] - fatigue damage accumulated during k loading semi-cycles, [FORMULA NOT REPRODUCIBLE IN ASCII] - fatigue damage accumulated up to crack initiation (when [d.sub.K] = 0).

Quasi-static damage is calculated using the following Eq. (5):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (5)

where [TEXT NOT REPRODUCIBLE IN ASCII] - accumulated plastic strain after k loading semi-cycles; [FORMULA NOT REPRODUCIBLE IN ASCII] - maximum uniform strain under monotonic loading which corresponds [sigma.sub.u].

The accumulated plastic strain after k loading semi-cycles, can be expressed as follows:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (6)

for cyclically softening and stable materials the accumulated plastic strain can be expressed as follows:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)

where [A.sub.1], [A.sub.2], [beta], [alpha] are material constants.

For strain cycling, the Eq. 4 can be written as:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (8)

For k loading semi-cycles the Eq. 4 can be expressed as:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (9)

where [TEXT NOT REPRODUCIBLE IN ASCII] - width of the hysteresis loop of initial semi-cycle.

When k = [k.sub.0]) the accumulated fatigue damage is equal [d.sub.N] = 1.

Durability of low cycle stress limited loading till the fatigue fracture can be expressed:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (10)

Quasi-static damage can be calculated applying Eq. 5 and for quasi-static and intermediate mode [d.sub.K] < 1. For quasi-static mode [d.sub.N] << [d.sub.K] and for practical calculations it is assumed that [d.sub.K] = 1, then:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (11)

For the intermediate mode quasi-static and fatigue damages can be calculated from Eqs. (3)-(5):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (12)

for tested materials it is assumed that q = l.

Calculated curve of low cycle stress limited loading only fatigue damage is evaluated then can be written:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (13)

where [FORMULA NOT REPRODUCIBLE IN ASCII] - accumulated fatigue damage till crack initiation which is characterized by the hysteresis loop's width [FORMULA NOT REPRODUCIBLE IN ASCII] - accumulated fatigue damage till crack initiation which is characterized by the hysteresis loop's width [FORMULA NOT REPRODUCIBLE IN ASCII], etc.

The fatigue curve in logarithmic coordinates [FORMULA NOT REPRODUCIBLE IN ASCII] has a shape of the straight line, then:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (14)

where [FORMULA NOT REPRODUCIBLE IN ASCII] then:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (15)

where [FORMULA NOT REPRODUCIBLE IN ASCII] - average value of the hysteresis loop's width; [k.sub.0] - semi-cycle of initial loading; [alpha.sub.2] and [C.sub.2] - material constants.

If the expressions [FORMULA NOT REPRODUCIBLE IN ASCII], [FORMULA NOT REPRODUCIBLE IN ASCII] are used, where [FORMULA NOT REPRODUCIBLE IN ASCII], then:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (16)

Substituting Eq. (16) into (15) it is obtained [MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]

By introducing the [FORMULA NOT REPRODUCIBLE IN ASCII], the dependence can be written:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (17)

The analytical curves as only fatigue damage were calculated applying the following Eq. (18):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (18)

For calculation of the monotonous tension, the linear or step-function approximation can be applied. Using the step-function approximation, the Eq. (18) will look:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (19)

where [FORMULA NOT REPRODUCIBLE IN ASCII]; [m.sub.0] - material intensification coefficient for step-function approximation.

For cyclically hardening, softening and stable materials:

F (k) = exp [beta] (k - 1); (20)

F (k) = 1/[k.sub.0] (21)

F (k) = 1 (22)

where [alpha] = [beta] = 0.

For cyclically stable materials:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (23)

Then sum of relative cyclic deformations (Eq. 13) can be replaced by sum of relative durability, then:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (24)

Then [FORMULA NOT REPRODUCIBLE IN ASCII] and substituting into Eqs. (14), (24) becomes:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (25)

or

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (26)

For the step-function approximation using Eq. 26 it can be:

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (27)

4. Verification of low cycle fatigue design curves

The probabilistic low cycle design curves were calculated for steel 15Cr2MoVA and 45 using the Eqs. (19) and (27). The parameters for calculation of these curves are presented in Table 4.

The probabilistic constants of the low cycle strain limited loading of steel 15Cr2MoVA and 45 were used for calculation are shown in Table 5.

Probabilistic constants of [C.sub.2] and [alpha.2] were determined using logarithmic coordinates [FORMULA NOT REPRODUCIBLE IN ASCII] (Fig. 3). Width of the hysteresis loop was calculated using Eq. (28):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (28)

The probabilistic curves of low cycle stress limited loading for steel 15Cr2MoVA was calculated using Eq. (19) and for steel 45--using Eq. (27). The parameter of cyclical deformation was determined by Eq. (29):

[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (29)

[FIGURE 3 OMITTED]

Fig. 4, a shows the probabilistic curves of stress limited loading where curve of 99% probability shows lowest lifetime, whereas 1% - highest. This is due to high reduction of [e.sub.pr] , which was used in this type of calculation and also high reduction of deformation parameters compare to reduction of the area of cross-section [psi]. This type of calculation showed contrariety with experimental data. To eliminate this type of discrepancy, mean arithmetic parameters of cyclic deformation was used for the next step.

For determination of the probabilistic curves, the probabilistic coefficients' [C.sub.2], [C.sub.3], [alpha.sub.3] values were used (Table 5). Using this type of calculation methodology, the low cycle curves got appropriate order, i. e. curve of 1% showed lowest lifetime, whereas 99% - highest (Fig. 4, b).

The probabilistic calculation of low cycle stress limited curves for steel 15Cr2MoVA is shown in Fig. 4, a, whereas for steel 45 in Fig. 5, a. The comparison of calculation and experimental data of these graphs is shown in Fig. 4, b, and Fig. 5, b, respectively.

Low cycle stress limited calculation for anisotropic materials showed a satisfactory agreement with experimental data when loading level is [FORMULA NOT REPRODUCIBLE IN ASCII]. When loading level [FORMULA NOT REPRODUCIBLE IN ASCII], the calculation is not adequate, because of quasi-static damage which gives error, but doesn't count to fatigue lifetime calculation.

[FIGURE 4 OMITTED]

[FIGURE 5 OMITTED]

5. Conclusions

The following conclusions can be drawn from this study:

1. Design curves of fracture probability for steels 15Cr2MoVA and 45 at low cycle stress limited loading were calculated and the probabilistic curves were compared with experimental ones.

2. Low cycle stress limited calculation for anisotropic materials showed a satisfactory agreement with experimental data when loading level is [FORMULA NOT REPRODUCIBLE IN ASCII]. When loading level [FORMULA NOT REPRODUCIBLE IN ASCII], the calculation is not adequate, because of quasi-static damage which gives error, but doesn't count to fatigue lifetime calculation.

References

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(2.) Iida, K., Inoue, H. 1973. Life distribution and design curve in low cycle fatigue, Papers of Ship Research Institute, Tokyo, No. 45, 39 p.

(3.) Beretta, S., Foletti, S. 2014. A simple format for failure probability under LCF and its application to a complex component, 20th European Conference on Fracture (ECF20), Procedia Materials Science 3: 2098-2103.

(4.) Zhu, S.-P.; Huang, H.-Z.; Ontiveros, V.; He, L.-P.; Modarres, M. 2012. Probabilistic low cycle fatigue life prediction using an energy-based damage parameter and accounting for model uncertainty, International Journal of Damage Mechanics 21: 1128-1153. http://dx.doi.org/10.1177/1056789511429836.

(5.) Schmitz, S.; Seibel, T.; Beck, T.; Rollmann, G.; Krause, R.; Gottschalk, H. 2013. A probabilistic model for LCF, Computational Materials Science 79: 584-590.

(6.) Haldar, A.; Mahadevan, S. 2000. Probability, Reliability and Statistical Methods in Engineering Design, New York, John Wiley & Sons, 305 p.

(7.) Mahutov, N.A. 2005. Structural durability, resource and tech. safety, Novosibirsk: Nauka, Vol. 1, 494 p. (in Russian).

(8.) Mahutov, N.A. 2005. Structural Durability, Resource and Tech. Safety, Novosibirsk: Nauka, Vol. 2, 610 p. (in Russian).

(9.) Bazaras, Z. 2005. Analysis of probabilistic low cycle fatigue design curves at strain cycling, Indian Journal of Engineering & Material Sciences 2: 411-418.

(10.) Daunys, M. 2005. Cycle Strength and Durability of Structures, Kaunas: Technologija, 286 p. (in Lithuanian).

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INVESTIGATION OF THE PROBABILISTIC LOW CYCLE FATIGUE DESIGN CURVES AT STRESS CYCLING

Received March 10, 2016

Accepted April 14, 2017

Z. Bazaras, R. Cesnavicius, J. Ilgakojyte-Bazariene, R. Kersys

(*) Kaunas University of Technology, Studenty 56, 51424 Kaunas, Lithuania, E-mail: [email protected]

(**) Kaunas University of Technology, Studenty 56, 51424 Kaunas, Lithuania, E-mail: [email protected]

(***) Kaunas University of Technology, Studenty 56, 51424 Kaunas, Lithuania, E-mail: [email protected]

(****) Kaunas University of Technology, Studenty 56, 51424 Kaunas, Lithuania, E-mail: [email protected] Table 1 Chemical compositions of tested materials C Si Mn Cr Ni Mo Steel 0.18 0.27 0.43 2.7 0.17 0.67 15Cr2MoVA V S P Mg Cu Al 0.30 0.019 0.013 - - - C Si Mn Cr Ni Mo Steel 45 0.46 0.28 0.63 0.18 0.22 - V S P Mg Cu Al - 0.038 0.035 - - - Table 2 Mechanical properties of tested materials Grade [sigma.sub.pr] [sigma.sub.0.2] [sigma.sub.u] MPa % Steel 15Cr2MoVA 280 400 580 Steel 45 340 340 800 Grade [S.sub.k] [e.sub.pr] [PSI] MPa % Steel 15Cr2MoVA 1560 0.2 80 Steel 45 1150 0.26 39 Table 3 Statistical low cycle testing program Stress limited loading Grade Loading level Number of specimen 1.00 20 Steel 15Cr2MoVA 1.12 40 1.25 20 1.00 20 Steel 45 1.25 40 1.50 20 Table 4 Probabilistic values of the cyclic characteristics Parameters Probability, % 1 10 30 50 70 90 99 Steel 15Cr2MoVA [A.sub.1] 0.23 0.87 1.32 1.60 1.94 2.40 3.04 [A.sub.2] 0.30 0.94 1.34 1.64 2.00 2.43 3.06 [S.SUB.T] 1.15 1.20 1.25 1.28 1.30 1.35 1.40 [m.sub.0] 0.15 0.17 0.19 0.21 0.23 0.26 0.30 [beta]X1[0.sub.-3] 0.04 0.16 0.42 0.85 1.80 4.80 19.0 C X 1[0.sub.-4] 1.10 3.00 4.80 7.40 11.0 21.0 50.0 Steel 45 [A.sub.1] 0.60 0.76 0.87 0.95 1.04 1.15 1.29 [A.sub.2] 0.64 0.80 0.89 0.96 1.05 1.16 1.30 [S.SUB.T] 0.92 1.02 1.07 1.11 1.15 1.21 1.29 [m.sub.0] 0.14 0.16 0.18 0.19 0.20 0.22 0.25 Table 5 Probabilistic constants Parameters Probability, % 1 10 30 50 70 90 99 Steel 15Cr2 MoVA [C.sub.1] 205 215 235 240 260 285 350 [alpha.sub.1] 0.48 0.49 0.49 0.50 0.50 0.50 0.50 [C.sub.2] 500 535 590 630 680 790 940 [alpha.sub.2] 0.53 0.53 0.53 0.54 0.54 0.54 0.54 [C.sub.3] 286 302 330 339 368 403 494 [alpha.sub.3] 0.98 0.96 0.96 0.92 0.92 0.92 0.92 Steel 45 [C.sub.2] 7.60 12.0 19.8 27.5 37.0 67.0 230 [alpha.sub.2] 0.24 0.25 0.28 0.31 0.32 0.38 0.52