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ASSESSMENT OF RESIDUAL LIFE OF GIRDERS OF BRIDGE No

ASSESSMENT OF RESIDUAL LIFE OF GIRDERS OF BRIDGE No

ASSESSMENT OF RESIDUAL LIFE OF GIRDERS OF BRIDGE No

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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

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