Fatigue Damage Estimation in Existing Railway Steel Bridges by Detailed Loading History Analysis
Alessio Pipinato,^{1}Carlo Pellegrino,^{1} and Claudio Modena^{1}
^{1}Department of Structural and Transportation Engineering, University of Padova, Via Marzolo 9, 35131 Padova, Italy
Academic Editor: Z. Li
Received06 Feb 2012
Accepted02 Apr 2012
Published24 Jul 2012
Abstract
Fatigue life estimation of metal historical bridges is a key issue for managing cost-effective decisions regarding rehabilitation or replacement of existing infrastructure. Because of increasing service loads and speeds, this type of assessment method is becoming relevant. Hence there is a need to estimate how long these structures could remain in service. In this paper a method to estimate fatigue damage in existing steel railway bridges by detailed loading history analysis is presented. The procedure is based on the assumption that failure probability is a function of the number of predicted future trains and the probability of failure is related to the probability of reaching the critical crack length.
1. Introduction
A relevant amount of the bridges in the European railway networks are metal made and have been built during the last 100 years. The increasing volume of traffic and axle weight of trains means that the current loads are much higher than those envisaged when the bridge was designed. In this context, issues as maintenance, assessment, rehabilitation, and strengthening of existing bridges assume a significant importance [1, 2]. The authors have developed some works concerning assessment and fatigue behavior of metal railway bridges by means of full-scale experimental testing. In particular in Pipinato et al. [3, 4] full-scale tests on dismantled steel bridges have been developed, whereas assessment of existing bridges and estimation of their remaining fatigue life are shown in Pipinato and Modena [5] and Pipinato et al. [6]. Moreover, a comprehensive method to assess the reliability of existing bridges taking fatigue into account has been recently published [7]. Among historical metal bridges, riveted structures are the most common; the role of riveted connections in the fatigue assessment is documented by several researches, such as, in Bruhwiler et al. [8], Kulak [9], Akesson and Edlund [10], Di Battista et al. [11], Bursi et al. [12], Matar and Greiner [13], Boulent et al. [14], Albrecht and Lenwari [15], Kühn et al. [16], Albrecht and Lenwari [17], and Brühwiler et al. [18]. Fatigue is one of the most common causes of failure in riveted bridges, as highlighted by the ASCE Committee on Fatigue and Fracture Reliability [19] and confirmed by Byers et al. [20]. Increasing loads on existing riveted bridges and the fact that these bridges were not explicitly designed against fatigue-raised questions regarding their remaining fatigue life. As a consequence, a better knowledge of the loading history is needed, having a relevant role in the fatigue damage assessment. The fatigue damage mainly depends on the following three main parameters: the stress range amplitude due to traffic load; the geometry of the construction details; the number of stress cycles due to the past traffic which directly influences the remaining fatigue life of a structure. In the context of structural reliability assessment, a comprehensive examination of fatigue safety and remaining service life of railway bridges is based on these three main parameters. The main objective of this paper is to estimate the fatigue damage in existing railway metal bridges and at the same time to determine the remaining fatigue life according to a step-by-step procedure referring to the LEFM (Linear Elastic Fracture Mechanics) theory by means of detailed loading history analysis. The method is then applied to a real case study, the Meschio railway bridge briefly described in the following paragraph.
2. Case Study
The Meschio bridge, a short span riveted flanged railway bridge built in 1918, was taken out of service in 2005 (Figure 1). It has been used in the line Mestre-Cormons, which is located in the North-eastern part of Italy. The net span of the bridge was 12.40 m. The main horizontal structure was made of two couples of twinned riveted composite flange beams. Wooden beams were located between the coupled beams, with a net distance of 565 mm from web to web of the beams, while the beam height was 838 mm. In this open-deck riveted railway bridge, transversal short shear diaphragms are riveted with double angles to both webs carried the rails. Each twinned beam supported the wooden elements of a single rail. The thickness of the main beam plates was 11 mm. The web was reinforced by 1 m spaced shear stiffeners, whereas the flanges were reinforced with 10 mm thick plates. The plate thickness increased from the abutment to the midspan. Each pair of twinned beams was linked to the corresponding pair with transverse bracing frames. The characteristics of the materials and more details on the geometry are described in Pipinato et al. [3, 4], while a typical cross section has been reported in Figure 2. Because the examined bridge was characterized by a simple structure, that is, a statically determinate bridge, it was rather easy to evaluate the nominal stress on members and connections of the bridge. In order to check these results, a stress analysis has been performed with a simplified FEM model, calibrated with observed strains derived from real scale testing results [3, 4].
2.1. Load History Assumption
Railway traffic estimation has been based on International Union of Railways, UIC [21] and on real data observed in the railway network from 1900 to 1990. A quadratic polynomial regression based on these data was performed and used for future traffic estimation (Figure 3). The maximum traffic capacity of the railway line in which the bridge is included has been assumed equal to 235 trains/day, following to the maximum capacity of the main national railway lines. According to these assumptions, the adopted traffic model are shown in Figures 3 and 4: the past real traffic and its growth tendency by adopting the UIC regression is shown in Figure 3, while the capacity of the line is developed in Figure 4 according to different traffic trend evolution, until a maximum of 235 trains/day. Figure 4 shows the traffic estimation from 1900 to 2020, with increasings of 1%, 2%, 3% and the UIC regression tendency (percentage increasing versus time) to estimate the number of trains passed on the bridge. UIC traffic data have been considered for the past, whereas some assumptions have been proposed for the future. The method described in the following is based on the aforementioned traffic estimation, and this scenario is also in accordance with CER [23]: in fact for the period 1995–2004, CER traffic increase is of 16%, just like UIC traffic increase. The past traffic has been assumed with a rate of 50% of passengers and 50% of freight trains [24]. Traffic assumption includes train type and convoy numbers: from 1900 to 1990 these data are presented in Table 1, while from 1991–2000 traffic was estimated according to Instruction 44/F [25], as described in Table 2. As a matter of fact, load models have been implemented as they were coded in the different historical periods analyzed:(i)the historical loadings have been assumed according to UIC 779-1 [21];(ii)from 1991 to 2000, the traffic spectrum has been based on the Instruction 44/F [25];(iii) from 2001 up to now, loads refers to LM71 (Figure 5; [22]) load model (method A) or to Instruction 44/F (method B) [25].
Period
Train/day
Type
UIC ref.
Train type [%]
Train/day for type
1900–1908
34,3
Tot.
17,2
Passenger
A03
100%
17,2
17,2
Freight
A04
100%
17,2
1909–1923
47,2
Tot.
23,6
Passenger
A05
60%
14,1
A06
40%
9,4
23,6
Freight
A07
100%
23,6
1924–1938
60,0
Tot.
30,0
Passenger
A08
60%
18,0
A09
40%
12,0
30,0
Freight
A07
60%
18,0
A10
40%
12,0
1939–1953
55,7
Tot.
27,8
Passenger
A11
50%
13,9
A12
50%
13,9
27,8
Freight
A10
60%
16,7
A13
40%
11,1
1954–1968
72,8
Tot.
36,4
Passenger
A14
25%
9,1
A15
17%
6,2
A17
33%
12,0
A18
25%
9,1
36,4
Freight
A16
40%
14,6
A20
60%
21,9
1969–1983
102,8
Tot.
51,4
Passenger
A14
28%
14,4
A18
36%
18,5
A19
36%
18,5
51,4
Freight
A20
40%
20,6
A21
60%
30,9
1984–1990
120,0
Tot.
60,0
Passenger
S01
56%
33,6
S02
44%
26,4
60,0
Freight
S03
37%
22,2
S04
37%
22,2
S05
13%
7,8
S06
13%
7,8
Train type
Name
Train/day
Axle/day
Locomotive (L) and carriages (Ci)
t/axle
Wagon number
Wagon type
Axle spacing [m]
1
IC
20
960
L
20,25
1
2.6-6.4-2.6
Intercity
C1
15
5
2.56-16.44-2.56
C2
12,75
6
2.56-16.44-2.56
2
EC
10
340
L
20
1
2.85-2.35-2.85-2.35-2.85
Eurocity
C1
14,25
2
2.56-16.44-2.56
C2
12
5
2.56-16.44-2.56
3
EXPR
15
990
L
20
1
2.85-2.35-2.85-2.35-2.85
Express
C1
14,25
10
2.56-16.44-2.56
C2
12
5
2.56-16.44-2.56
4
DIR
30
1380
L
18,6
1
2.85-2.35-2.85-2.35-2.85
Direct
C1
10,675
10
2.4-16.6-2.4
5
ETR
10
480
L
20
2
3-9-3
Eurostar
C1
11,6
10
3-17.3-3
6
TEC
15
990
L
18,7
1
2.85-2.35-2.85-2.35-2.85
Container freight
C1
20
15
1.8-12.8-1.8
7
Merci acciaio
10
720
L
18,7
2
2.85-2.35-2.85-2.35-2.85
Steel freight
C1
20
15
1.8-13.06-1.8
8
Treno merci tipo D4
5
380
L
20
2
2.85-2.35-2.85-2.35-2.85
D4 freight
C1
22,5
16
1.8-4.65-1.8
9
Treno merci misto
5
270
L
18,7
1
2.85-2.35-2.85-2.35-2.85
Mixed freight
C1
16
24
9
For historical trains and for Instruction 44/F trains, dynamic amplification factor φ is calculated according to EN 1991-2 [22]:
where:
where is the train speed (m/s) and is the determinant length (m). For LM71 load model (method A), the dynamic amplification factor has been calculated according to EN 1991-2 [22]
assuming , and = determinant length. All the dynamic amplification factors applied have been reported in Table 3.
Period
Train type
Train name
Speed [km/h]
D.A.F. [dynamic amplification factor]
Code ref.
1900–1983
Passenger/freight
A03/A21
100
1,135
UIC
1984–1990
Passenger
S01
125
1,168
UIC
Passenger
S02
140
1,190
UIC
Freight
S03
80
1,111
UIC
Freight
S04
80
1,111
UIC
Freight
S05
80
1,111
UIC
Freight
S06
80
1,111
UIC
1991–2000
Passenger
IC
200
1,290
Instr.44/f
Passenger
EC
160
1,221
Instr.44/f
Passenger
EXPR
150
1,205
Instr.44/f
Passenger
DIR
140
1,190
Instr.44/f
Passenger
ETR
250
1,391
Instr.44/f
Freight
TEC
120
1,161
Instr.44/f
Freight
Merci
100
1,135
Instr.44/f
Freight
Treno merci
100
1,135
Instr.44/f
Freight
Treno merci
120
1,161
Instr.44/f
2001–:
Fatigue load
LM 71
—
1,380
EN1991-2
2.2. Assessment Procedure
The assessment method is based on a probabilistic evaluation of the reliability margin defined in the form:
where is the structural resistance and represents action effects. The probability of failure is defined as:
Assuming statistical independence of and , the probability of failure can be defined as:
where is the cumulative function distribution of structural resistance , expresses probability occurrence of action effects in the near of the point
As a consequence, the probability of failure could be expressed as:
and the reliability index could be expressed as [26]:
The aforementioned procedure could be specified to the bridge case study, where the calculated probability of fatigue fracture to obtain the probability of failure could be estimated as:
where is failure probability; is probability of fatigue fracture; is probability of crack detection that is considered zero () since structural health monitoring system has been used on the bridge [27, 28]. The probability of failure can also be expressed with the reliability index according to the normal standard distribution. Finally the reliability of a structural element is compared to the target value:
where is reliability index with respect to failure; is target reliability index. This model implies the use of the fatigue action effect (the required nominal fatigue strength) as “required operational load factor ” which is obtained by dividing the required nominal fatigue strength by the action effect of the fatigue load:
where is the required nominal fatigue strength; is the required operational load factor; -stress range due to the load model adopted at worst position (), considering the dynamic amplification (, e.g., maximizing the fatigue stress amplitude). For a simplified probabilistic approach, a relation between mean value of required operational load factor and number of future train passages has been introduced [28]. The mean of the required operational load factor is then read for fatigue category chosen (expressed as , number of load cycles corresponding to the constant-amplitude fatigue limit) starting from a number of future trains (as from 2005); this relation could be used for any influence lengths [28], commissioning time, and freight traffic fraction. According to the same model, a value of 0.04 may be taken as standard deviation of the required operational load factors, resulting from the assumed fuzziness of the traffic model [28]. Adopting the following notation and assumption:
where is the standard deviation of the required fatigue strength; is the reliability index; is the mean of the fatigue strength ( relating to 2 × 10^{6} cycles); is the mean of the required fatigue strength as a function of the number of future trains ; is the standard deviation of the fatigue strength where is the slope of the curve, and is the standard deviation of test results; is the standard deviation of the fatigue strength. It should be observed that the variability in curve is only on life and not on stress range and that the variability of stress for a given life is not statistically related to variability of life for a given stress. Specific values of are recommended for a determinate remaining service life, according to ISO/CD 13822 [29]: for the assessment of existing structures and the fatigue limit state, reference indexes should be for not visible detail and for visible detail. The reliability model herein presented has been related to the aforementioned traffic spectra and loadings.
2.3. Damage Accumulation
Due to the inherent disadvantage of the curve approach, which cannot incorporate information on crack size, an alternative approach based on LEFM concepts [30, 31] is considered in this study. The LEFM approach is based on crack propagation theory [32–35]. The Paris law [36], the most common LEFM-based crack growth model, is used since it retains the simplicity of the fatigue evaluation process. This can be described as:
where is the crack size, is the number of stress cycles, and are material constants and is the stress intensity range. According to LEFM theory [31], can be estimated as:
where is the tensile stress range, is the geometry function to take into account stress concentrations [37], such as, the stress concentration coefficient and the dimensions of the specimen under consideration. It is not completely clear how the stress cycles below a constant amplitude fatigue limit affect the fatigue life [38]. Stress cycles due to live loads could be lower than the fatigue limit [39] and in these particular cases, according to Miner’s rule [40] and to damage verifications based on Eurocodes (e.g., [41]), they should not produce any damage. The damage model developed in this paper considers the damage due to stress cycles below the cut-off limit which causes a damage in term of crack propagation according to LEFM principles [42]. The adopted damage model implies that stress ranges are damage effective only if is exceeded, where is the damage limit and is the fatigue limit for constant amplitude stress ranges at the number of cycles , defined by [30] and taking as the initial crack size, the could be expressed as:
That could be written as
being
Combining (15) and (16), with = constant,
and taking
Equation (22) can be written as
in which is the depth of the crack at a number of cycles equal to . According to Kunz [30] the initial size of the crack mm. According to Bremen [43], (15) could be also written as:
And according to (16),
It follows that
And being constant
It follows that
The single damage increases, taking as the cut-off limit and as the category detail at the number of cycles , according to Kunz [30] is represented by:
where = applied stress range, curve slope, = total damage.
Failure will occur when the accumulated damage , according to Miner [40]. In the case study analyzed, the bridge has been built in 1918 and dismantled in 2005. Table 4 shows that damage accumulation starts with A05 UIC train (1909–1923), and all the following trains contribute to the damage as reported. For every train type contributing to damage, the number of cycles of the detail category (), the damage increasing (), the axles number passed at the end of the period () are reported. Category for bending detail and for shear detail has been assumed, as suggested by EN 1993-1-9 [41]: the category detail reference has been made according to Eurocode indications. Load models are described by concentrated characteristic axle load that implies cycle fluctuation in the structural components: stress variations have been counted as per ASTM [44]. Basing on real scale structural tests [45] a linear correlation between axle load () and stress variations, without dynamic amplification factor, has been reported in Figures 6 and 7. Moreover, Table 5 reports the cycle counting model adopted, while in Table 6 a damage calculation example making reference to a single train, UIC A03 from 1900–1908 is reported.
Nc
Train A03 (1900–1908)
0,000E + 00
2,0E + 06
0,0000000097
0,0E + 00
0,000
0,000E + 00
2,0E + 06
0,0000000097
0,0E + 00
0,000
0,000E + 00
2,0E + 06
0,0000000097
0,0E + 00
0,000
Train A04 (1900–1908)
0,000E + 00
2,0E + 06
0,0000001823
0,0E + 00
0,000
0,000E + 00
2,0E + 06
0,0000001823
0,0E + 00
0,000
0,000E + 00
2,0E + 06
0,0000001823
0,0E + 00
0,000
Train A05 (1909–1923)
0,000E + 00
2,0E + 06
0,0000003146
6,2E + 04
0,019
1,950E − 02
2,0E + 06
0,0000003193
6,2E + 04
0,020
3,928E − 02
2,0E + 06
0,0000003235
1,2E + 05
0,040
7,938E − 02
2,0E + 06
0,0000003305
1,9E + 05
0,061
1,408E − 01
2,0E + 06
0,0000003385
2,8E + 05
0,094
Train A06 (1909–1923)
2,352E − 01
2,0E + 06
0,0000004895
4,1E + 04
0,020
2,554E − 01
2,0E + 06
0,0000004896
4,1E + 04
0,020
2,757E − 01
2,0E + 06
0,0000004896
2,1E + 04
0,010
2,858E − 01
2,0E + 06
0,0000004897
2,1E + 04
0,010
2,959E − 01
2,0E + 06
0,0000004897
4,1E + 04
0,020
3,161E − 01
2,0E + 06
0,0000004897
5,0E + 05
0,243
Period
Train
Train/day
Tractor (L) carriage (Ci)
kN/axle
axles
carriage
Axles/day
[kN]
Axles/year
17,2
L
140,00
3
1
51,5
420
1,9E + 04
17,2
L
120,00
2
1
34,3
240
1,3E + 04
1900–1908
A03
17,2
L
100,00
1
1
17,2
100
6,3E + 03
17,2
C1
50,00
3
6
308,9
900
1,1E + 05
Tot.
411,8
1660
1,5E + 05
62,0
1,245
77,19
3
73,70
100
0,00E + 00
2,0E + 06
3,62E − 08
1,7E + 05
0,006
60,0
1,245
74,70
3
73,70
100
6,12E − 03
2,0E + 06
1,38E − 08
1,1E + 05
0,002
22,0
1,245
27,45
3
73,55
100
7,67E − 03
2,0E + 06
0,00E + 00
5,6E + 04
0,000
11,0
1,245
13,72
3
73,51
100
7,67E − 03
2,0E + 06
0,00E + 00
1,0E + 06
0,000
2.4. Calculation of Reliability Index
The reliability analysis of detail 1 and 2 (Figures 8, 9, and 10) has been performed assuming the methodology described above and by adopting the aforementioned load models, applied to the hot-spot details: the midspan bottom flange and the riveted connection of the short shear diaphragm transverse connecting the principle beams. Table 7 reports the analysis from 2005-future for detail 1 and load method A, while Table 8 for load method B. Table 9 reports the analysis from 2005-future for detail 2 and load method A, Table 10 for load method B: as could be observed, these tables illustrate the increasing number of future trains , the value of and , the decreasing value of , and the bridge status according to this analysis; moreover, the precise value of the out of service year is reported at the end of the bridge damage lifecycle. According to these values, the reliability index trends are plotted (Figures 11, 12, 13, and 14). Moreover, the hypothesis to repair the detail 2 has been analyzed: the precise time interval has been identified in the average value (Figure 15). Results have highlighted that the detail 1, assuming the load model A, will reach the out of service in 2043, while the same detail loaded with the model B terminates in 2049; the detail 2, the hot spot of this structure, based on the load model A will be the out of service in 2021, while the same detail loaded with the model B goes out of service in 2027: by repairing the more damaged detail 2, it is possible to increase the service life of the bridge of about 12 years.
Year
Status
2005
2,09E + 05
3,1
2,3
2,71
In service
2010
5,36E + 05
3,1
2,3
2,65
In service
2015
8,76E + 05
3,1
2,3
2,59
In service
2020
1,23E + 06
3,1
2,3
2,54
In service
2025
1,59E + 06
3,1
2,3
2,48
In service
2030
1,96E + 06
3,1
2,3
2,42
In service
2035
2,35E + 06
3,1
2,3
2,37
In service
2040
2,74E + 06
3,1
2,3
2,32
In service
2045
3,14E + 06
3,1
2,3
2,26
Out of service in 2043
Year
Status
2005
2,09E + 05
3,1
2,3
2,57
In service
2010
5,36E + 05
3,1
2,3
2,48
In service
2015
8,76E + 05
3,1
2,3
2,41
In service
2020
1,23E + 06
3,1
2,3
2,36
In service
2025
1,59E + 06
3,1
2,3
2,34
In service
2030
1,96E + 06
3,1
2,3
2,34
In service
2035
2,35E + 06
3,1
2,3
2,34
In service
2040
2,74E + 06
3,1
2,3
2,34
In service
2045
3,14E + 06
3,1
2,3
2,32
In service
2050
3,55E + 06
3,1
2,3
2,29
Out of service in 2049
Year
Status
2005
2,09E + 05
3,1
2,3
2,80
In service
2010
5,36E + 05
3,1
2,3
2,63
In service
2015
8,76E + 05
3,1
2,3
2,46
In service
2020
1,23E + 06
3,1
2,3
2,31
In service
2025
1,59E + 06
3,1
2,3
2,17
Out of service in 2021
Year
Status
2005
2,09E + 05
3,1
2,3
2,65
In service
2010
5,36E + 05
3,1
2,3
2,52
In service
2015
8,76E + 05
3,1
2,3
2,43
In service
2020
1,23E + 06
3,1
2,3
2,36
In service
2025
1,59E + 06
3,1
2,3
2,32
In service
2030
1,96E + 06
3,1
2,3
2,28
Out of service in 2027
(a)
(b)
(a)
(b)
3. Conclusions
This work deals with the estimation of the fatigue damage in existing railway metal bridges and the remaining fatigue life according to a detailed loading history analysis. The method is then applied to a real case study. In terms of loadings, a detailed loading history analysis has been performed by adopting two different load methods, A and B: the historical loadings have been assumed according to UIC 779-1 [21]; from 1991 to 2000, the traffic spectrum has been based on the Instruction 44/F [25]; from 2001 up to now, loads refer to LM71 load model (method A) or to Instruction 44/F (method B). It was confirmed that the critical fatigue detail of the bridge is located in the riveted connection of the short-shear diaphragm connecting principle beams as shown in previous mentioned studies. Moreover, different results according to different load methods related to the future traffic (i.e., load A and load B) should influence the expected fatigue life; in particular, a more realistic fatigue load model (load A) could lead to an extension of the fatigue life of the investigated bridge; on the contrary, an assessment based on conservative and approximate code load model could lead to a shorter lifetime prediction. The method described in this work enables a better understanding of the damage level in steel bridges, and could help to maintain in service existing bridges, adopting detailed loading history analysis. As a matter of fact, managing authorities should be aware of the possibility to correctly estimate residual life of existing infrastructure, for example, by implementing maintenance program based on advanced analytical assessment.
Acknowledgment
The authors wish to thank Mr. M. Gueli for contributing to some numerical analyses developed during the thesis. The research conclusions are only the views of the authors.
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