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Ministry of Railways<br />

Government of India<br />

<strong>ASSESSMENT</strong> <strong>OF</strong> <strong>RESIDUAL</strong> <strong>LIFE</strong> <strong>OF</strong> <strong>GIRDERS</strong> <strong>OF</strong> <strong>BRIDGE</strong><br />

NO. 73 & 75 (ABANDONED), VASAI CREEK <strong>BRIDGE</strong>S ON<br />

BORIVALI – VIRAR SECTION <strong>OF</strong> WESTERN RAILWAY<br />

REPORT NO. BS –79<br />

MAY 2006<br />

RESEARCH DESIGNS AND STANDARDS ORGANISATION<br />

MANAK NAGAR LUCKNOW-226011<br />

1


PREFACE<br />

Whenever, a bridge is abandoned due to its weak substructure or some<br />

other reasons before completing its codal life, it is important to know the residual<br />

fatigue life of girders of its superstructure. If substantial life is still left, these<br />

girders can be used on other routes. If the traffic density of such routes are<br />

lower, these girders can be used for much more life span. Bridge <strong>No</strong>. 73 & 75,<br />

known as Vasai creek bridges of Mumbai Central–Virar section of Mumbai<br />

Division of W. Railway were abandoned due to their weak substructures after<br />

completing about 66 years of service life and may have still, some useful life.<br />

For estimation of the residual fatigue life of the girders by using S.N. curve<br />

Approach, apart from the of stress- cycles (S.N.) curve of the material, the<br />

stress-time history for the present day traffic passing over the girders is<br />

essential, which is not possible to be obtained in case of above bridges, as the<br />

bridges have been abandoned primarily due to weak sub–structure. For such<br />

situation, the provisions of para. 9.2&9.3 of BS code 5400 part-10 are used for<br />

assessment of residual fatigue life of these bridges. However, for more realistic<br />

results, S.N. curve has been developed by fatigue testing of some samples<br />

taken out from the existing girders. The S.N. curve, so developed, has been<br />

used for assessing the residual life of the girders, by the method using damage<br />

calculation.<br />

For this work, a test team of S/Shri Ramji lal, SRE and S.K. Awasthi,<br />

JRE-1 under the guidance of Sh. S.C.Gupta, Director/B&S/Testing was<br />

constituted. The assessment of the residual fatigue life of the girders is done by<br />

this team.<br />

Fatigue testing of the samples was conducted by the staff of Fatigue<br />

Testing Lab., under the guidance of Shri Mohan lal, SRE.<br />

Contribution of all the team members in assessment of residual life<br />

of the girders is highly appreciated. Guidance provided by Shri S.C. Gupta, to<br />

the team members was worth appreciating, and sincerely acknowledged.<br />

This report is submitted herewith for further necessary action to Executive<br />

Director ( Works), Railway Board, New Delhi.<br />

2<br />

( LALLOO SINGH )<br />

Executive Director/ B&S


INDEX<br />

S.<strong>No</strong> Contents Page no.<br />

1. Introduction 1<br />

2. Objective 1<br />

3. History of the bridge 1<br />

4. Methodology 2<br />

5. Estimation of residual fatigue life 7<br />

6 observations 10<br />

7. Conclusions<br />

TABLES<br />

11<br />

1 RU Loading: Annual traffic tonnage for standard traffic<br />

types<br />

12<br />

2 Details of fatigue testing of specimen taken out from<br />

girders of existing abandoned bridge<br />

13<br />

3 Details of past traffic passed ( GMT ) between BCT-VR<br />

14<br />

section<br />

1<br />

FIGURES<br />

Test specimen for fatigue testing 15<br />

2 S-N Curve 16<br />

3 Bar chart of traffic density between BCT-VR section during<br />

1950-96<br />

17<br />

3a Cumulative Increase in traffic density since 1950-96 17<br />

4 Histogram of computed stress cycles with different stress<br />

ranges for light traffic and traffic density of 27 GMT<br />

18<br />

5 Graph of residual life and traffic density 18<br />

ANNEXURES<br />

I Copy of the letter from Exe. Director ( Works ) Rly. Board<br />

for assessment of Residual life of Bridge <strong>No</strong>. 73<br />

( Abandoned ) near Mumbai<br />

II Calculation sheet for maximum stress range 24<br />

III References 26<br />

<strong>ASSESSMENT</strong> <strong>OF</strong> <strong>RESIDUAL</strong> <strong>LIFE</strong> <strong>OF</strong> <strong>GIRDERS</strong> <strong>OF</strong> <strong>BRIDGE</strong> NO. 73 & 75<br />

(ABANDONED), VASAI CREEK <strong>BRIDGE</strong>S ON BORIVALI – VIRAR SECTION<br />

<strong>OF</strong> WESTERN RAILWAY<br />

3<br />

19


1.0 INTRODUCTION:-<br />

Vide Executive Director ( Works) , Railway Board’s DO <strong>No</strong>. 2004/WI /WR/<br />

Girder dt. 30.04.04, Member Engineering desired that a study may be<br />

conducted to assess the residual life of the girders of the bridge <strong>No</strong>. 73 &<br />

75 (Abandoned). With a view to use them on new branch line where the<br />

traffic is going to be light in the beginning. The copy of the above letter<br />

alongwith a report prepared by Western Railway on this issue is placed at<br />

Annexure – I.<br />

2.0 OBJECTIVE:-<br />

To assess the residual life of the girders of bridge <strong>No</strong>. 73 & 75 Mumbai<br />

division of W.R.<br />

3.0 HISTORY <strong>OF</strong> THE <strong>BRIDGE</strong>S:-<br />

The bridge <strong>No</strong>. 73 & 75 (abandoned) are located on Basai Creek between<br />

Bhainder and Naigaon stations of Borivali – Virar suburban sections of<br />

Western Railway. The abandoned bridges were open to traffic on<br />

22.01.1927. There are 69 x 2 = 138 nos. of 18.3 m span steel plate<br />

girders on bridge <strong>No</strong>. 73 and 25 x 2 = 50 nos. of 18.3 m span girders in<br />

bridge <strong>No</strong>. 75. Thus, there are 188 nos. girders of 18.3 m effective span.<br />

There 8 nos. of 6.1 m span girder in bridge <strong>No</strong>. 73 & 75. The details of the<br />

girders are as follows:<br />

a) Effective Span - 18.3 m<br />

b) Overall length - 18.95 m<br />

c) Loading Standard - BG standard of 1916<br />

d) Drawing <strong>No</strong>. - CEN/57728/11-D<br />

e) Manufactured by - M/s P& W Maglellan Ltd., BB & CI. Co. -<br />

1923, Clutha Works Glasgow.<br />

The bridges were abandoned primarily due to Weak foundation and<br />

overstressed sub-structure, where stresses were found to be exceeded<br />

permissible limits, requiring heavy speed restrictions. Many CI piles were<br />

cracked and were continuing in service on clamps. there was heavy<br />

incrustation in the piles due to marine growth and same indicated<br />

extensive loss of section. But the most important and critical reason was<br />

that due to heavy sand dredging in the creek, the bed level gone down by<br />

2.45 m since 1927 and pile grip in rock was reduced to near unsafe limits<br />

in some cases.<br />

In replacements of these bridges, new bridges were constructed on well<br />

foundations at an average depth of 29 m below the mean tidal level and<br />

PSC box type girders of 1.20 m + 28 x 48.5 m spans in bridge <strong>No</strong>. 73 and<br />

4


11x 48.5 m spans in bridge <strong>No</strong>. 75 were constructed and open to traffic in<br />

the year 1993 and since than the bridges of steel plate girders have been<br />

abandoned.<br />

4.0 METHODOLOGY:<br />

For assessment of residual life of the girders of the bridges, the procedure<br />

as given in BS – 5400 part – 10 , code of practice for fatigue has been<br />

followed. The procedure given in clause 9.0 of the above code for railway<br />

bridges has been used. Two methods for fatigue assessment of railway<br />

bridges are given in clause 9.2 & 9.3 of the code. In method –1,<br />

assessment is done without damage calculation and in method –2,<br />

damage is calculated by using Miner’s summation rule. Both these<br />

methods have been used for the assessment of residual life.<br />

4.1 Method – 1: Fatigue life assessment without damage calculations:<br />

4.1.1 General:<br />

BS-5400 part 10 is a comprehensive code which is based on the concept<br />

of cumulative fatigue damage. The fatigue assessment is based on<br />

Palmgren-Miner’s damage summation model. For fatigue assessment of<br />

railway bridges, the methodology for determination of stress range has<br />

been described for different type of connections and a simplified<br />

procedure has been given for determining the limiting value of the<br />

maximum range of stress for the specified design life for two different<br />

types of standard loadings. Details of RU loading ( Ref; Table- 1) has<br />

been used for calculating the remaining fatigue life, as it is more severe<br />

than IRS MBG loading. As per code, RU loading allows for all<br />

combinations of vehicles currently running or projected to run on railways<br />

in the Continent of Europe, including the United Kingdom and is to be<br />

adopted for the design of bridges carrying main line railways of 1.4 m<br />

gauge and above. The nominal type RU loading consists of four 250 KN<br />

concentrated loads preceded and followed by a uniformly distributed load<br />

of 80 KN/m The code specifies different factor k1, k2, k3, k4 & k5 for design<br />

parameters such as design life, multiple cycle of stress loading, type of<br />

standard loading, annual GMT and multiple lane loading respectively.<br />

The code gives specific methodology and tables to calculate the factors<br />

for different design parameters.<br />

4.1.2 Limiting Stress Range, σT<br />

The constant amplitude non-propagating stress range, σ0 for the<br />

constructional detail is chosen appropriately on the basis of Table – 17 &<br />

Table 8 of the code. The limiting stress range σT is calculated for RU<br />

loading as under:<br />

5


σT = k1. k2. k3. k4. k5. σ0 ……………………………………………………..(1)<br />

Where, k1, k2, k3, k4,& k5. Are different parameters can be obtained from<br />

the code.<br />

4.1.3 Check for Design Adequacy:<br />

The design adequacy of the given detail is checked as per Clause 9.2.2.2<br />

and Clause 9.2.2.3 of the code. Where σRmax (Maximum Stress Range)<br />

should not exceed σT, i.e σRmax < σT, the detail may be considered to have a<br />

fatigue life in excess of the specified design life.<br />

4.1.4 RU Loading & IRS-MBG Loading:<br />

A comparison of EUDL values of Bending Moment as per RU loading has<br />

been made with corresponding values for IRS-MBG loading and it is found<br />

that the EUDL values as per RU loading are on higher side as compared to<br />

IRS-MBG loading. Therefore, the various factors developed for RU loading<br />

as given in BS: 5400 Part 10 have been used for fatigue life analysis of the<br />

members of the bridge subjected to MBG loading which is expected to give a<br />

fatigue life on a conservative side. But on the other hand it does not reflect<br />

exactly the loading spectrum under Indian conditions, so the reliability of<br />

results may not be as accurate.<br />

4.1.5 Fatigue life analysis:<br />

The stresses calculated during the analysis and the cross sections provided<br />

in the existing design have been used to workout the fatigue life of the<br />

girders.<br />

Following assumptions have been made during this study –<br />

a) The maximum axial stresses due to EUDL for IRS loadings have been<br />

worked out and the maximum stress range calculated as the difference of<br />

dead load stress and the maximum stress likely to come on the girder with<br />

dead load, live load with impact and occasional load. The calculation<br />

sheet for maximum stress range likely to occur on the girders is shown in<br />

Annexure-II<br />

b) The axial stresses due to load combination with occasional load have<br />

been taken into consideration to find out the maximum stress range. This<br />

combination rarely occurs in practice, therefore, the analysis is on<br />

conservative side.<br />

c) Material properties are assumed to be as per Table-8 of BS-5400 and σ0<br />

value has been taken to be corresponding to detailed classification ‘D’ of<br />

this table. This assumption may not be correct, but can be relied for rough<br />

estimation.<br />

6


d) The fatigue life of standard spans has been assessed by calculating the<br />

design life factor k1. This factor has been worked out as σRmax/(σ0 x k3)<br />

and fatigue life calculations have been done by inversion, using the<br />

equations given in Clause 9.2.3 of BS-5400 Pt.-10 by taking fatigue life as<br />

minimum of the following:<br />

Fatigue Life<br />

or<br />

<br />

120<br />

…………………………………………………………..(2)<br />

m<br />

k1<br />

Fatigue Life <br />

120<br />

…………………………………………………………(3)<br />

2<br />

k<br />

m<br />

1<br />

Where m = 3.0 taken from Table-8 for detailed Class ‘D’.<br />

e) Value of RU loading factor k3 has been taken from Table-4 of the code<br />

considering the case of heavy traffic loading, corresponding to the base<br />

length (L) of the influence line diagram for the girder.<br />

f) Value of GMT factor, k4 is assumed as 1.0 for GMT of 18 to 27 million<br />

tonnes. Actual GMT data suggests that this assumption is very much on<br />

conservative side.<br />

g) For single lane loading value of lane factor, k5 is taken as 1.0.<br />

4.2 Method-2: Fatigue life assessment with damage calculations :<br />

4.2.1 General : This method involves a calculation of Miner’s summation<br />

and may be used for any detail for which S-N relationship is known for any<br />

known load or stress spectrum. This method may be used as a more precise<br />

alternative to the simplified procedure as described in para. 4.1of this report.<br />

The essential information which is required to assess the fatigue life of a<br />

structure is the pattern of stresses likely to be observed in it, during the<br />

passage of normal traffic and the relationship between the applied stress<br />

cycles and the number of times these can be withstood by the material of the<br />

structure. This can be achieved by subjecting the representative samples<br />

not only to varying constant amplitude cycles or stresses but also to<br />

complete stress spectrum. Using test results and curve fitting technique, S-N<br />

relationship can be obtained. Under normal service conditions, Railway<br />

bridge structures are subjected to spectrum of varying stress – amplitude<br />

and therefore, a process of damage accumulation continues. The fatigue<br />

damage depends on the combined effect of the frequencies of different<br />

stress ranges, likely to be observed by the structure under service loading.<br />

Referring to Palm-gren Miner’s theory of linear damage accumulation , the total<br />

damage to the structure is given by D= ∑ ni/Ni.<br />

Where , ni = Observed number of stress cycles for different stress<br />

ranges<br />

7


Ni = Theoretical number of stress cycles corresponding to<br />

observed stress ranges from S-N curve.<br />

i = 1,2,3 …. Upto n stress ranges<br />

When the damage ( D) become equal to 1, the specimen fails and so the failure<br />

occurs when D= ∑ ni/Ni. = 1<br />

Many researchers have not been able to find good credence to this hypothesis.<br />

The main reason is that a stress cycles causes different extent of damage<br />

depending on its application on the material during its life. Research carried out<br />

by ORE, under question D-128, has suggested that under assumption of normal<br />

distribution of fatigue test data, the probability of failure by fatigue is considerably<br />

low when the life is evaluated at two Standard deviations below 50 % probability<br />

curve. To achieve this, the cumulative damage factor in the above equation is<br />

taken as 0.3, where N is taken from mean S-N curve. Therefore, in our study<br />

the criterion for fatigue failure is taken as D= ∑ ni / Ni = 0.3<br />

4.2.2 S.N. Curve: The relationship between constant amplitude stress range<br />

(Sre) applied to the specimen and number of cycles upto its failure (N) is called<br />

SN Curve. Generally it is plotted on log-log scale with number of cycles in<br />

millions on abscissa and stress range in N/mm 2 on ordinates. The slopping line<br />

represents the finite fatigue life of the material. Mathematically SN curves are<br />

defined in log-log form by the following equations:<br />

Log N = Log a –M.Log Sre<br />

Where, log a is the intercept on x-axis and M is the reciprocal of the slope of<br />

the finite life portion of the SN curve. In normal form N is represented by the<br />

following equation:<br />

N = a / (Sre) m<br />

4.2.3 Fatigue testing: Instead of using the S-N curve from the code for class<br />

‘D’, Twelve numbers of specimen ( Six numbers each from top and web plate ) taken for<br />

fatigue testing from the abandoned bridge <strong>No</strong> 73 girders for getting the actual fatigue<br />

behavior of the material. The result of the fatigue testing can be used for bridge <strong>No</strong>. 75 as<br />

the bridges are made up of similar material and are in operation on the similar times with<br />

similar traffic. The specimens were tested for fatigue life in RDSO laboratory. The<br />

specimen without holes were fabricated by welding end plates on either side of the<br />

specimen as shown in fig.1. and subjected to fatigue test as per program of loading as<br />

shown in table -2. The number of cycles at which the samples tested/failed is also shown<br />

in the table. Sample designated as W-1 and B-1 were tested up to 10 million<br />

cycles at the stress range 40 N/mm2 and did not fail even after completing 10<br />

million cycles. Other samples were tested up to 2 million cycles due to some<br />

higher load ranges and some of them failed before reaching 2 million cycles. The<br />

higher values of load ranges are selected, so that the values of stress ranges<br />

cover almost all the parts of the anticipated SN curve. The minimum load for<br />

fatigue testing is taken as 30 KN for all the samples. It has been observed that<br />

generally fatigue crack appears near the welding of end plates and propagates<br />

8


slowly before failure, which shows the ductile nature of the material. The actual<br />

values of cycles at failure with their corresponding stress ranges are plotted on<br />

log-log scale. The best fit line, representing maximum number of points is drawn.<br />

This line represents the SN curve for the material of the girder. The samples<br />

which have completed 10 million cycles without failing are not considered for<br />

plotting the best fit line as the samples were tested below the endurance limit.<br />

SN relationship so obtained is shown in fig. 2 is used for calculating the residual<br />

life of the girders. The values of constant a and M of the curve, calculated are<br />

3.51 x 10 15 and 4.61 respectively. Therefore the equation of the curve is:<br />

N = 3.51 x 10 15<br />

(Sre) 4.61<br />

or Log N = Log 3.51 x 10 15 - 4.61 log (Sre)<br />

4.2.4 Stress spectrum: The number of different stress ranges are computed based<br />

on maximum stress experienced by the girders as per MBG loading i.e., 96.25<br />

N/mm 2 (Annexure-II) and reducing it proportionately up to the lowest range of<br />

fatigue testing of the specimen taken out from of the existing girders. Although, it<br />

is a plate girder bridge and stress range – cycle data of such bridges are not<br />

available and hence to simulate with Indian railway conditions, the frequency of<br />

the cycles are taken from the results obtained from the analysis of the stress-<br />

time records of residual life estimation of Ganga bridge <strong>No</strong>. 110 up, an open web<br />

girder near Kanpur, Lucknow division of N.R. As the observed stress range of<br />

girders of the same bridge on down line is higher than the value of calculated<br />

maximum stress range of this bridge, hence not considered for the residual life<br />

calculations. Since the annual traffic density of this section is about 10 GMT at<br />

the time of testing of the bridge and hence these values of stress cycles are<br />

augmented by 2.7 times as at the time of closure of traffic on these bridges the<br />

annual traffic density of this section was approximately 27GMT. The calculated<br />

values of anticipated stress cycles for different stress ranges are shown below:<br />

S <strong>No</strong>. Stress range in N/mm 2<br />

9<br />

<strong>No</strong>. of stress cycles<br />

1 96.625-86.625 32<br />

2 86.625-77.000 0<br />

3 77.000-67.375 0<br />

4 67.375-57.750 62<br />

5 57.750-48.125 0<br />

6 48.125-38.500 0<br />

7 38.500-28.875 38<br />

A stress histogram of the above different stress ranges and number of cycles<br />

has been prepared and shown in Fig.-3.<br />

4.2.5 Traffic Density and Speed:


Since the residual life calculations as per Miner’s summation rule are based on<br />

the damage caused per day by the present day traffic and fatigue test conducted<br />

on the specimen which have undergone different load cycles in the past, hence<br />

the traffic passed in the past will not affect the residual life calculations. The<br />

residual life calculations in this report for this methodology are based on annual<br />

density of 27 GMT and hence, the traffic density increases/decrease in future,<br />

the residual life will decrease/increase on prorata basis and will effect the<br />

calculations. The details of traffic passed in GMT on the bridge during 1950-51 to<br />

1995-96 is shown in table-3, fig.4 & 4a. On perusal of the table and figures , it is<br />

seen that the traffic density which was 9.95 GMT in the year 1950-51, increases<br />

to 27.15 GMT in the year 1992-93, the year in which the bridge was abandoned.<br />

However, the maximum traffic density prior to 1976-77 was about 18 GMT and<br />

increases thereafter up to about 27 GMT. Speed of the train also affect the<br />

residual life of the girders, hence for calculation of maximum stress likely to be<br />

observed on the girders, the impact factor has also been considered.<br />

5 ESTIMATION <strong>OF</strong> <strong>RESIDUAL</strong> <strong>LIFE</strong>:<br />

5.1 Assessment of residual life without Damage Calculation:<br />

Following values of different parameters are considered for estimation of<br />

residual life.<br />

i) detailed class considered = D (from table 17 of code)<br />

ii) Maximum stress range ( σT ) = 96.25 N/mm 2 (calculated)<br />

iii) Constant amplitude stress (σ0) = 53 N/mm 2 (from table 8 of code)<br />

iv) m = 3 (from table 8 of code)<br />

v) k 2 = 1.0 by considering one stress range only<br />

vi) k 3 = 1.92 (Heavy traffic) from table 4 of code<br />

= 2.19 (Medium traffic)from table 4 of code<br />

= 2.74 (Light traffic) “ “<br />

vii) k 4 = 0.89 (42 to 27 GMT) from table 5 of code<br />

= 1.0 (27 to 18 GMT) “ “<br />

= 1.13 (18 to 12 GMT) “ “<br />

vii) k 5 = 1.0 (for single lane loading) from table 6 of the code<br />

Value of design life factor (k1) is calculated by the formula<br />

σ T<br />

k 1 = -------------------------------------------<br />

k 2 . k 3 . k 4 . k 5 . σ0<br />

5.1.1 For Heavy Traffic:<br />

a) Traffic density 42 – 27 GMT<br />

96.25<br />

10


k1 = ------------------------------------------- = 1.063<br />

1.92 x 0.89 x 53<br />

Life = 120 / k1 m+2 = 88 years<br />

Remaining Life = 88 – 66 = 22 years<br />

b) Traffic density 27 - 18 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.946<br />

1.92 x 1.0 x 53<br />

Life = 120 / k1 m = 142 years<br />

Remaining Life = 142 – 66 = 76 years<br />

c) Traffic density 18 - 12 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.837<br />

1.92 x 1.13 x 53<br />

Life = 120 / k1 m = 205 years<br />

Remaining Life = 205 – 66 = 139 years<br />

5.1.2 For Medium Traffic:<br />

a) Traffic density 42 – 27 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.932<br />

2.19 x 0.89 x 53<br />

Life = 120 / k1 m = 148 years<br />

Remaining Life = 148 – 66 = 82 years<br />

b) Traffic density 27 - 18 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.829<br />

2.19 x 1.0 x 53<br />

11


Life = 120 / k1 m = 211 years<br />

Remaining Life = 211 – 66 = 145 years<br />

c) Traffic density 18 - 12 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.734<br />

2.19 x 1.13 x 53<br />

Life = 120 / k1 m = 304 years<br />

Remaining Life = 304 – 66 = 238 years<br />

5.1.3 For Light Traffic:<br />

a) Traffic density 42 – 27 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.745<br />

2.74 x 0.89 x 53<br />

Life = 120 / k1 m = 291 years<br />

Remaining Life = 291 – 66 = 225 years<br />

b) Traffic density 27 - 18 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.663<br />

2.74 x 1.0 x 53<br />

Life = 120 / k1 m = 412 years<br />

Remaining Life = 412 – 66 = 346 years<br />

c) Traffic density 18 - 12 GMT<br />

96.25<br />

k1 = ------------------------------------------- = 0.587<br />

2.74 x 1.13 x 53<br />

12


Life = 120 / k1 m = 594 years<br />

Remaining Life = 594 – 66 = 528 years<br />

Calculated Residual Life of girders in different conditions are shown below:<br />

S Traffic Type Residual Life in years for Traffic Density<br />

.<strong>No</strong>.<br />

42 – 27 GMT 27 – 18 GMT 18 – 12 GMT<br />

1 Heavy Traffic 22 76 139<br />

2 Medium Traffic 82 145 238<br />

3 Light Traffic 225 412 528<br />

5.2 Assessment of residual life with damage calculation: . It may be used as a<br />

more precise alternative to the simplified procedure as described in para.5.1<br />

above. This method involves a calculation based on Miner’s summation rule.<br />

S.N. curve developed for limited number of fatigue testing of specimen taken out<br />

from the existing girders and stress cycles are computed from the data as shown<br />

in para 4.2.4 of this report. The calculation of residual life of the girders based on<br />

the loading spectrum of the Ganga bridge for traffic density of 27 GMT, is shown<br />

below:<br />

Stress range in<br />

N/mm 2<br />

Mean Stress<br />

Range in<br />

N/mm 2<br />

13<br />

<strong>No</strong>. of cycles<br />

per day<br />

<strong>No</strong>. of cycles as<br />

per SN curve X<br />

10 6<br />

96.250-86.625 91.4375 32 3.19<br />

67.375-57.750 62.5625 62 18.16<br />

38.500-28.875 33.6875 38 315.06<br />

Damage per Year (D) =∑ (ni/Ni)<br />

=[(32/3.19)+(62/18.16)+(38/315.06)]x10 -6<br />

=0.005<br />

Residual Life = 0 .3/D<br />

= 60 years<br />

6.0 Observations:<br />

It is observed from the method of assessment of residual fatigue life, without<br />

damage calculation that residual life of the girders is more conservative as the<br />

minimum residual life calculated is 22 years for heavy traffic (42-27GMT) and the<br />

maximum residual life is 528 years for light traffic (18-12GMT). However, based<br />

on load spectrum as per Indian Rly’s traffic pattern the residual life as per<br />

damage calculation method is 60 years for traffic density of 27 GMT. It seems to<br />

be more realistic. The residual life, for lighter traffic conditions. By considering<br />

the fact that the residual life varies inversely with the traffic density, the<br />

relationship between residual life and traffic density can be drawn on log-log


scale ( fig.-5) and residual life for the actual operational traffic density of the<br />

section, where these girders are likely to be used, can be obtained with the use<br />

of this graph. Although, it is observed from the report prepared by the Railway<br />

(Annexure-I) that many girders are having corrosion particularly in top flange<br />

plates, but this factor is not considered in this study. Hence, it is advised that the<br />

corroded parts of the girders should be replaced before their reuse.<br />

7.0 Conclusions:<br />

The girders of both the abandoned bridges can be used for traffic density of<br />

27GMT for a period of about 60 years. With replacement of corroded parts, the<br />

remaining life span of the girders can be extended further, if traffic density is less<br />

than 27 GMT and good maintenance practices are being followed.<br />

--------<br />

14


15<br />

Table –1<br />

RU Loading : Annual traffic tonnage for standard traffic types<br />

S<br />

<strong>No</strong><br />

.<br />

Traffic<br />

Type<br />

Train Type Train<br />

Weight<br />

(t)<br />

<strong>No</strong>. of<br />

Trains per<br />

annum<br />

Total<br />

Tonnage<br />

GMT<br />

1 Heavy Heavy Freight 1120 4821 5.40<br />

Heavy Freight 1120 7232 8.10<br />

Mixed Freight 852 15845 13.50<br />

Total 27.00<br />

2 Medium Diesel Hauled Pass. Train 600 22500 13.50<br />

Heavy Freight 1120 2411 2.70<br />

Heavy Freight 1120 6027 6.75<br />

Steel Train 1794 2257 4.05<br />

Total 27.00<br />

3 Light Steel Train 1794 752 1.35<br />

Electric Multiple Unit 372 14516 5.40<br />

Suburban trains 344 23546 8.10<br />

Suburban Trains 172 47093 8.10<br />

Diesel Hauled Pass. Train 600 4500 2.70<br />

Electric Hauled Pass. Train 572 2360 1.35<br />

Total 27.00<br />

Table –2<br />

Details of fatigue testing of specimen taken out from girders of<br />

existing abandoned bridge no 73


Sl.<br />

<strong>No</strong><br />

Specimen<br />

designation<br />

Stress<br />

range in<br />

KN<br />

Load range in<br />

KN<br />

Min Max.<br />

16<br />

Frequency<br />

In Htz<br />

1. W-1 40 13.20 30.80 Between<br />

10-15<br />

<strong>No</strong>. of<br />

cycles in<br />

million to be<br />

tested<br />

10 or failure<br />

which ever<br />

<strong>No</strong>. of<br />

cycles in<br />

millions<br />

tested upto<br />

10 *<br />

2. W-2 70 13.20 44.00 ----do----is<br />

earlier.<br />

2 or failure<br />

which ever<br />

is earlier<br />

1.03<br />

3. W-3 100 12.87 55.57 ----do----- -do- 2.12*<br />

4. W-4 130 13.20 70.40 ----do----- -do- 0.25<br />

5. W-5 160 13.20 83.60 ----do----- -do- 0.62<br />

6. W-6 220 12.87 107.25 ----do----- -do- 0.03<br />

7. B-1 40 18.24 42.56 ----do----- 10 or failure<br />

which ever<br />

is earlier.<br />

10*<br />

8. B-2 70 19.20 64.00 ----do----- 2 or failure<br />

which ever<br />

is earlier<br />

0.84<br />

9. B-3 100 19.20 83.20 ----do----- -do- 1.79<br />

10. B-4 130 19.20 102.40 ----do----- -do- 1.18<br />

11. B-5 160 19.20 121.60 ----do----- -do- 0.31<br />

12. B-6 190 18.72 137.28 ----do----- -do- 0.11<br />

* Samples not failed<br />

Table - 3<br />

Details of past traffic passed (GMT) between BCT– VR Section<br />

UP DN


Year GMT during the GMT Cum. GMT during the GMT Cum.<br />

Year<br />

Year<br />

50-51 9.95 9.95 9.95 9.95<br />

51-52 5.96 15.91 5.96 15.91<br />

52-53 6.03 21.94 5.03 21.94<br />

53-54 6.23 28.17 6.23 28.17<br />

54-55 6.33 34.5 6.33 34.5<br />

55-56 7.16 41.66 7.16 41.66<br />

56-57 8.15 49.81 8.15 49.81<br />

57-58 8.62 58.43 8.62 58.43<br />

58-59 8.63 67.06 8.63 67.06<br />

59-60 8.64 75.7 8.64 75.7<br />

60-61 9.59 85.29 9.59 85.29<br />

61-62 9.27 94.56 9.27 94.56<br />

62-63 9.8 104.36 9.8 104.36<br />

63-64 10.14 114.5 10.14 114.5<br />

64-65 11.21 125.71 11.21 125.71<br />

65-66 12.08 137.79 11.78 137.79<br />

66-67 12.9 150.69 12.1 149.59<br />

67-68 13 163.69 12.3 161.89<br />

68-69 11 174.69 11.5 173.39<br />

69-70 11.7 186.39 11.49 184.88<br />

70-71 10.92 197.31 10.54 195.42<br />

71-72 12.13 209.44 11.83 207.25<br />

72-73 18.72 228.16 18.1 225.35<br />

73-74 18.34 246.5 17.86 243.21<br />

74-75 16.49 262.99 16.71 259.92<br />

75-76 18.39 281.38 17.64 277.56<br />

76-77 19.06 300.44 17.31 294.87<br />

77-78 23.81 324.25 25.1 319.97<br />

78-79 25.69 349.94 25.05 345.02<br />

79-80 23.55 373.49 23.17 368.19<br />

80-81 23.38 396.87 22.25 390.44<br />

81-82 22.8 419.67 21 411.44<br />

82-83 22.43 442.1 21.7 433.14<br />

83-84 22.92 465.02 22.43 455.57<br />

84-85 22.66 487.68 20.87 476.24<br />

85-86 23.53 511.21 20 496.24<br />

86-87 24.32 535.53 23.27 519.51<br />

87-88 27.17 562.7 26.14 545.65<br />

88-89 28.14 590.84 28.3 573.95<br />

89-90 24.43 615.27 22 595.95<br />

90-91 25.42 640.69 23.51 619.46<br />

91-92 27 667.69 25.88 645.34<br />

92-93 27.85 695.54 27.15 672.49<br />

93-94 28.22 723.76 27.2 699.69<br />

94-95 28.65 752.41 28.76 728.45<br />

95-96 28.69 781.1 29.52 757.97<br />

Specimen for fatigue testing<br />

17


All dimensions are in mm<br />

18<br />

Fig – 1


Stress range in N per sq mm<br />

1000<br />

100<br />

Stress Range Vs <strong>No</strong>. of cycles<br />

S-N Curve<br />

10<br />

0.100 1.000 10.000<br />

<strong>No</strong>. of cycles in millions<br />

19<br />

Br. 73 DN<br />

Fig. - 2<br />

Traffic passed (GMT) between BCT– VR Section during 1950-96


Cummulative Traffic in GMT<br />

Traffic in GMT<br />

35<br />

30<br />

25<br />

20<br />

15<br />

10<br />

5<br />

0<br />

900<br />

800<br />

700<br />

600<br />

500<br />

400<br />

300<br />

200<br />

100<br />

0<br />

50-51<br />

50-51<br />

53-54<br />

53-54<br />

56-57<br />

59-60<br />

Traffic in GMT passed in the past<br />

62-63<br />

65-66<br />

Cummulative traffic in passed in the past<br />

56-57<br />

59-60<br />

62-63<br />

65-66<br />

68-69<br />

71-72<br />

68-69<br />

71-72<br />

Years<br />

74-75<br />

Years<br />

20<br />

77-78<br />

80-81<br />

83-84<br />

86-87<br />

89-90<br />

92-93<br />

95-96<br />

Fig – 3<br />

Fig – 3a<br />

Computed stress cycles with different stress ranges for traffic<br />

density of 27 GMT<br />

74-75<br />

77-78<br />

80-81<br />

83-84<br />

86-87<br />

89-90<br />

92-93<br />

95-96<br />

UP<br />

DN<br />

UP<br />

DN


<strong>No</strong>. of cycles<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

0<br />

Traffic density in GMT<br />

P.K. SANGHI<br />

100<br />

96.625-<br />

86.625<br />

10<br />

86.625-<br />

77.000<br />

77.000-<br />

67.375<br />

21<br />

67.375-<br />

57.750<br />

57.750-<br />

48.125<br />

Stress Range in N/Sq mm<br />

Life Vs GMT<br />

48.125-<br />

38.500<br />

38.500-<br />

28.875<br />

1<br />

1 10 100 1000<br />

Residual life in years<br />

Fig – 4<br />

Fig – 5<br />

Annexure – I


EXEC. DIRECTOR (WORKS)<br />

D.O. <strong>No</strong>. 2004/WI/WR/Girder New Delhi – dt. 30.04.2004<br />

Dear Shri R. K. Gupta,<br />

Sub: Alternate use of released steel girders of Vasai Creek bridges on<br />

Borivali – Virar section of Western Railway.<br />

On Borivali – Virar section of Western Railway, Bridge <strong>No</strong>. 73 & 75 across<br />

Vasai Creek have been newly constructed. The old bridges built in 1916 have<br />

been abandoned.<br />

Member Engineering , has desired that a study may be conducted on the<br />

residual life of the released girders of the old bridges and also the extent of<br />

strengthening required with a view to use them on new branch lines where the<br />

traffic is going to be light in the beginning. A report prepared by Western Railway<br />

on this issue is enclosed herewith for considerations.<br />

In view of the above, I would request you to take up the study and submit<br />

report including cost of strengthening and loading standard permissible for these<br />

released girders for further consideration of the Board.<br />

With regards,<br />

Shri R. K. Gupta,<br />

Executive Director/B&S,<br />

RDSO,<br />

Lucknow.<br />

22<br />

Yours sincerely<br />

Sd/-<br />

(P. K. SANGHI)<br />

Annexure<br />

ABANDONED STEEL <strong>BRIDGE</strong> ON VASAI CREEK IN CCG – VR SECTION <strong>OF</strong><br />

MUMBAI SUBURBAN.


1. The Vasai Creek is spanned by bridge nos. 73 & 75 in CCG – VR section<br />

of Mumbai Division on Western Railway. The Creek is in tidal zone, experiencing<br />

rise and fall in water level but the riverbed is never dry.<br />

2. HISTORY:<br />

The abandoned bridge in question, which was in fact the second bridge,<br />

was opened for traffic on 22.01.1927. The bridge was built 122 feet (36.5 m)<br />

East of the first bridge. The bridge was designed to BG standard of loading<br />

1916. The piers consisted of 6 nos. piles at 9 feet c/c spacing with 3 feet and 2.5<br />

feet dia piles and had provision for future quadrupling . The substructure consists<br />

of fish bellied plate girders of 60 feet (18.3 m) span. There were 69 spans in<br />

south creek and 25 spans in north creek. There were 6.1 m span at either<br />

approach of the two bridges.<br />

The bridge was studied by RDSO in 1969 and was found to be weak in<br />

foundation and the CI piles and bolts were found to be overstressed .<br />

Subsequently, extensive field trials were conducted in association with IIT<br />

Bombay and based on same construction of new bridge was included in railway<br />

budget of 1981-82.<br />

The reasons for abandoning the bridge were as follows:<br />

a) The bridge being located on Bombay-Delhi Rajdhani trunk route, where<br />

double heading of locomotive was essential, the bridge was not found to<br />

be fit for normal speed. Even for the existing load, the foundation and the<br />

substructure stresses were found to be exceeded permissible limits<br />

requiring heavy speed restrictions.<br />

b) A number of CI piles were cracked and were continuing in service of<br />

clamps.<br />

c) Due to standing water at all times at the bridge location, the foundation<br />

could not be inspected thoroughly. There was heavy incrustation in the<br />

piles due to marine growth and the same indicated extensive loss of<br />

section.<br />

d) The most important and critical reason was that due to heavy sand<br />

dredging in the creek which was the most important source of sand for<br />

Bombay peninsula, the bed level from 1927 had gone down by 8 feet<br />

(2.45 m) and the pile grip in rock was reduced to near unsafe limits in<br />

some cases.<br />

In replacement of the bridge, new bridge was constructed on well<br />

foundations at an average depth of 29 m below the mean tidal level and<br />

PSC box type girders 65.10 m east of the second bridge and consisted of<br />

1 x 20 m + 28 x 48.5 m PSC Box spans in bridge <strong>No</strong>. 73 and 11 x 48.5 m<br />

PSC box spans in bridge <strong>No</strong>. 75. The bridge was opened to traffic in year<br />

May 1993.<br />

23


3. CONDITION <strong>OF</strong> STEEL <strong>GIRDERS</strong> <strong>OF</strong> BR.NO. 73 &75 (OLD)<br />

3.1 The bridge <strong>No</strong>. 73 & 75 ( abandoned ) are located on Vasai Creek<br />

between Bhainder and Naigaon stations of CCG – VR suburban<br />

section. The old is located on the west most side of the existing bridge.<br />

There are 69 x 2 = 138 nos. of 18.3 m span girders on bridge <strong>No</strong>. 73 and<br />

25 x 2 = 50 nos. of 18.3 m span girders in bridge <strong>No</strong>. 75. Thus, there are<br />

188 nos. girders of 18.3 m effective span. There 8 nos. of 6.1 m span<br />

girder in bridge <strong>No</strong>. 73 & 75 which can not be reused since these have<br />

already completed their fatigue life.<br />

3.2 The details of girders are as follows:<br />

a) Effective Span - 18.3 m<br />

b) Overall length - 18.95 m<br />

c) Height at end - 1.87 m<br />

d) Height at center - 1.91 m<br />

e) Flange width - 430 mm<br />

f) C/C of girder leaves - 1.88 m<br />

g) Loading Standard - BG standard of 1916<br />

h) Drawing <strong>No</strong>. - CEN/57728/11-D<br />

i) Manufactured by - M/s P& W Maglellan Ltd., BB & CI. Co. -<br />

1923, Clutha Works Glasgow.<br />

3.3 The girders of the bridge were inspected visually by Dy. CE (Br.) BL and<br />

the following points were brought out:<br />

The girders in the bridge can be classified into two broad categories<br />

based on visual inspections:<br />

a) Type I : The type I girders are having:<br />

i) Corrosion in top flange plates upto 7 mm at sleeper seat locations i.e.<br />

at every 65 cms spacing.<br />

ii) 80 % gussets are having corrosion by minimum 4 mm, out of total 8<br />

mm thickness. Many gussets are perforated.<br />

iii) 30-35 % rivets have lost more than 50 % head due to corrosion in top<br />

flange.<br />

iv) Bracings are generally in satisfactory condition, except the end cross<br />

frame top lateral angles, which are corroded and reduced in thickness.<br />

v) There is slight corrosion in the bottom angle of main girder and the<br />

same is generally OK.<br />

vi) There is corrosion of upto 1 mm at the junction of the web plate with<br />

bottom main angle.<br />

24


vii) The girders are having sliding bearings i.e. girders are directly resting<br />

on the bed plates with slotted holes in bottom flange having holding<br />

down bolt through the same.<br />

viii) All girders require painting.<br />

b) Type II : The type II girders are having:<br />

i) Corrosion in top flange plates upto 4 mm at sleeper seat locations i.e.<br />

at every 65 cms spacing.<br />

ii) 50 % gussets are having corrosion by minimum 4 mm, out of total 8<br />

mm thickness. Many gussets are perforated.<br />

iii) 15-20 % rivets have lost more than 50 % head due to corrosion in top<br />

flange.<br />

iv) Bracings are generally in satisfactory condition, except the end cross<br />

frame top lateral angles, which are corroded and reduced in thickness.<br />

v) There is slight corrosion in the bottom angle of main girder and the<br />

same is generally OK.<br />

vi) There is corrosion of upto 1 mm at the junction of the web plate with<br />

bottom main angle.<br />

vii) The girders are having sliding bearings i.e. girders are directly resting<br />

on the bed plates with slotted holes in bottom flange having holding<br />

down bolt through the same.<br />

viii) All girders require painting.<br />

3.4 Based on inspection, the girders pertaining to different spans have been<br />

grouped as under:<br />

I<br />

II<br />

Type Bridge <strong>No</strong>. Span <strong>No</strong>. Remarks<br />

73<br />

1 to 26 UP/DN, 31-33 UP/DN, 40 UP/DN, 41<br />

UP, 42-43 UP/DN, 44 UP, 49 UP, 50 UP/DN,<br />

51 DN, 52 UP, 55 UP/DN, 58 UP, 60 UP/DN,<br />

62-64 UP, 65 UP/DN, 66 UP, 67 UP/DN, 68<br />

UP, 69 DN, TOTAL : 88 <strong>GIRDERS</strong><br />

25<br />

1. Span 14 UP has top flange<br />

corrosion up to 10 mm &<br />

perforation at places.<br />

2. End cross frame bottom<br />

lateral angle is perforated in<br />

span 56 UP & 68 UP requiring<br />

replacement.<br />

75 2-18 UP, 20-25 UP, TOTAL : 23 <strong>GIRDERS</strong> -<br />

27-30 UP/DN, 34-39 UP/DN, 41 DN, 44 DN, -<br />

73<br />

45-48 UP/DN, 49DN, 51 UP, 52 DN, 53-54<br />

UP/DN, 56-57 UP/DN, 58 DN, 59 UP/DN, 61<br />

UP/DN, 62-64 DN, 66 DN, 68 DN, 69 DN<br />

TOTAL : 50 <strong>GIRDERS</strong><br />

75 1-25 DN, 1 UP, 19 UP, TOTAL : 27<br />

DN line sleeper seat could not<br />

<strong>GIRDERS</strong><br />

inspected due to track.<br />

3.5 The recommendations based on inspections are :


a) The type I girders require replacement of top flange plate, all gussets and<br />

corroded bracings along with provision of centralized bearings and<br />

stiffening plates before use. All girders are require to be painted.<br />

b) The type II girders require replacement of corroded gussets and rivets<br />

and need based replacement of top flange at critical locations and<br />

provision of centralized bearings and stiffening plates before use. All<br />

girders are require to be painted.<br />

3.6 The girders require the following prerequisites before the same can be<br />

released for use elsewhere.<br />

a) There is a water pipe line on bridge <strong>No</strong>. 75 provided on bracing between<br />

girders of UP line and DN line for the inhabitants of the island between<br />

bridges <strong>No</strong>. 73 and 75.<br />

b) There is an H.T. electric line on bridge <strong>No</strong>. 75 provide bracing between<br />

girders of UP line and DN line for the inhabitants of the island between<br />

bridges <strong>No</strong>. 73 and 75.<br />

c) The girders have lived part of the useful life in the period between 1927<br />

and 1993 and the balance fatigue life is to be assessed for the section<br />

where the girders are to be used.<br />

-------------<br />

26


WEIGHT CALCULATION<br />

Calculation sheet for maximum stress range<br />

27<br />

Annexure-II<br />

S.<br />

<strong>No</strong><br />

Description<br />

of Member<br />

Size Sectional<br />

Area<br />

. mm<br />

mm cm 2<br />

Unit<br />

Weight<br />

Kg/m/cm 2<br />

Length of<br />

Member<br />

Required<br />

number<br />

m<br />

Weight<br />

Kg<br />

1 2 3 4 5 6 7<br />

1 STIFFNER<br />

2’=609.6 mm<br />

2’7’’=787.4mm<br />

3’8’’=1117.6mm<br />

2 Stiffner Angle<br />

5’=1524 mm<br />

3 T-BAR<br />

5’=1524mm<br />

5’=1524mm<br />

4 Stiffner Angle<br />

5’=1524 mm<br />

T-Bar<br />

5’=1524 mm<br />

5’=1524 mm<br />

Main Angles<br />

5 Top Flange<br />

Angles<br />

30’=9144mm<br />

6 Bottom Flange<br />

Angles<br />

30’=9144mm<br />

7 WEB PLATE<br />

30’=9144mm<br />

deduction due to<br />

fish valley shape<br />

Rectangular<br />

shape<br />

3’x1’5’’<br />

Triangular shape<br />

3’x4’7’’<br />

8 Top Flange<br />

Cover Plate<br />

I st Top Plate<br />

L=30’=9144mm<br />

2 nd Top Plate<br />

L=17’6’’=5334m<br />

90x909x12<br />

90x909x12<br />

90x909x12<br />

75x75x10<br />

150x75x10<br />

150x75x10<br />

75x75x10<br />

150x75x10<br />

150x75x10<br />

115x115x10<br />

115x115x10<br />

12.7x1524<br />

12.7x914.4<br />

1/2x12.7x914.5<br />

508x15.8<br />

457x15.8<br />

20.19<br />

20.19<br />

20.19<br />

14.02<br />

19.96<br />

19.96<br />

14.02<br />

19.96<br />

19.96<br />

22<br />

22<br />

193.54<br />

-116.12<br />

-58.06<br />

80.26<br />

72.23<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.7854<br />

0.6096<br />

0.6096<br />

1.1176<br />

1.524<br />

1.524<br />

1.524<br />

1.524<br />

1.524<br />

1.524<br />

9.144<br />

9.144<br />

9.144<br />

0.4318<br />

1.397<br />

9.144<br />

5.334<br />

4<br />

2<br />

2<br />

4<br />

2<br />

2<br />

2<br />

2<br />

1<br />

2<br />

2<br />

1<br />

1<br />

1<br />

1<br />

1<br />

38.67<br />

19.33<br />

35.44<br />

67.12<br />

47.78<br />

47.78<br />

33.56<br />

47.78<br />

23.89<br />

361.35<br />

315.99<br />

315.99<br />

1389.95<br />

-39.38<br />

-63.7<br />

576.4<br />

302.59<br />

9 Top Flange<br />

Cover Plate<br />

I st Top Plate<br />

L=30’=9144mm<br />

2 nd Top Plate<br />

508x15.8 80.26 0.7854 9.144 1 576.4<br />

L=18’6’’=5638m 457x15.8 72.23 0.7854 5.638 1 319.84<br />

10 Web Splice 304.8x8 24.38 0.7854 1.295 3 74.39<br />

4129.82<br />

say 4130 Kg<br />

Weight of 30 Feet Span = 4130.0 Kg<br />

Weight of 60 Feet Span (single) 2x4130 = 8260.0 Kg


Weight of 60 Feet Span (double) 2x8260 = 16520.0 Kg<br />

Add 2% for rivetting = 330.4 Kg<br />

Total = 16850.4 Kg<br />

Say = 17 t<br />

Add 5% = 0.85 t<br />

(4% for bearing and 1% for any missed member)<br />

Total = 17.85 t<br />

Say = 18 t<br />

Track wt. 0.4 t/m = 7.58 t<br />

Total = 25.58 t<br />

Total Area = 503.35 cm 2<br />

Deduction for rivets 4x2.54x1.0 = 10.16 cm 2<br />

Net Area = 493.19 cm 2<br />

Ixx = 1/12 x (508 x32 3 + 457 x 32 3 ) + 508 x 32 x (794 -16) 2<br />

+ 457 x 32 x (794 -16) 2 + 1/12 x 10 x 1524 3 + 4 x { 2800000 + 2200<br />

x (1524/2 - 33.2) 2 }<br />

Ixx = 26328791605 mm 4<br />

Ixx = 2.63287 x 10 10 mm 4<br />

Ixx = 2.63287 x 10 6 mm 4<br />

Y’ = 794 mm = 79.4 cm<br />

Dead Load = 25.58 t<br />

= 255.8 KN<br />

DL+LL+IL = 2984.8 KN<br />

B.M(DL) = WL/16 = 255.80 x 1000 x 1830/16 2.92571 x 10 7 Ncm<br />

B.M(DL+LL+IL) = WL/16 = 2984.80 X 1000 X 1830/16 3.41386 X 10 8 Ncm<br />

Stress(min) = BM(DL) x Y’/Ixx = 8822.33 N/cm 2 = 8.8233 N/mm 2<br />

Stress(max) =BM(DL+LL+IL) x Y’/Ixx =10295.53 N/cm 2 = 102.9553 N/mm 2<br />

Stress(T) = Stress(max) x A gross/A net =102.95 x 503.35 / 483.16 = 105.07 N/mm 2<br />

Stress range = Stress(T) – Stress(min) = 105.07 – 8.82 = 96.25 N/mm 2<br />

Effective length L’ = 18.3 m<br />

28


REFERENCES:<br />

29<br />

Annexure – III<br />

1. Estimation of the residual life of floor system of Ganga Bridge near<br />

Balawali ( Civil Engineering Report <strong>No</strong>. 175 )<br />

2. Investigations on the assessment of residual life of early steel/wrought<br />

iron girder bridges ( Civil Engineering Report <strong>No</strong>. 245 )<br />

3. Assessment of fatigue life of early steel/wrought iron girder bridges<br />

( Report <strong>No</strong>. BS-5 )<br />

4. Guidelines for assessment of residual life of early steel/wrought iron girder<br />

bridges ( Report <strong>No</strong>. BS-39 )<br />

5. Statistical distribution of axle loads and stresses in railway bridges<br />

( ORE Report <strong>No</strong>.1 Question D-128 )<br />

6. Fatigue life of riveted railway bridges by Bjorn Akesson, Chalmers<br />

university of technology, Sweden .<br />

7. Condition monitoring and life assessment of railway bridge 449/3/34 over<br />

river Tapti near Bhusaval by Department of civil engineering IIT, Mumbai<br />

8. Assessment of residual fatigue life of Ganga bridge near Kanpur, N. Rly.<br />

( Report <strong>No</strong>. BS- 70 & 75 )<br />

9. Code of practice for fatigue ( BS-5400: Part 10 )

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