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reliability assessment of offshore jacket structures in niger delta

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eliability <strong>of</strong> the group brac<strong>in</strong>gs was estimated and presented <strong>in</strong> Table 2. The completebrac<strong>in</strong>g member <strong>reliability</strong> and <strong>jacket</strong> legs <strong>reliability</strong> were also established <strong>in</strong> Table 3 and4 respectively. The overall <strong>reliability</strong> <strong>of</strong> the <strong>jacket</strong> structural systems and <strong>reliability</strong> factorwere also estimated and presented <strong>in</strong> Table-5.The data gathered dur<strong>in</strong>g the platform survey <strong>in</strong>cludes anodes percentage utilization.The survey revealed that anodes located <strong>in</strong> the splash zone are depleted faster than the oneplaced <strong>in</strong> the other tidal zones along the <strong>jacket</strong> length. A <strong>jacket</strong> structural member wasflooded due to pitt<strong>in</strong>g corrosion <strong>in</strong> the jo<strong>in</strong>t welds.The entire <strong>jacket</strong> was found to be covered with uniform rust<strong>in</strong>g. The member corrosionlosses range from 0% to 17% compared with members as built thickness. The rate <strong>of</strong>corrosion is found to be higher <strong>in</strong> the splash zone than any other tidal zones due toaccelerated corrosion process <strong>in</strong> the area.In this paper, the failure mode <strong>of</strong> <strong>jacket</strong> <strong>structures</strong> was <strong>in</strong>terpreted as either series orparallel systems and depends on member arrangement and correlation. The brac<strong>in</strong>g membersare <strong>in</strong> parallel systems failure mode and majority <strong>of</strong> brac<strong>in</strong>gs yield for failure before thestructure collapse mode is wholly developed. The failure mode <strong>of</strong> a <strong>jacket</strong> platform legs isassociated with series system and if any one <strong>of</strong> the legs develop failures mode the wholeplatform is considered to has failed and recommended for abandonment.The <strong>reliability</strong> <strong>assessment</strong> method developed <strong>in</strong> this study is most appropriate s<strong>in</strong>cethe technique elim<strong>in</strong>ate the rigorous exercises associated us<strong>in</strong>g 3D computer s<strong>of</strong>tware forexist<strong>in</strong>g platform <strong>assessment</strong> due to member corrosion losses. The method is a handy tool tomonitor structural safety with regards to structural member thickness corrosion loss andit can be accomplished with pocket calculator or Micros<strong>of</strong>t excel-s<strong>of</strong>tware. ReliabilityFactor (FR) is proposed <strong>in</strong> the study to establish <strong>jacket</strong> <strong>structures</strong> safety as the platformis age<strong>in</strong>g.3.1 Reliability FactorThe <strong>reliability</strong> <strong>of</strong> a newly <strong>in</strong>stalled <strong>jacket</strong> is 1 or 100%, s<strong>in</strong>ce the structural membersare corrosion free. A factor (RF) is hereby established between an <strong>in</strong>tact and corroded<strong>jacket</strong> structural system <strong>reliability</strong> to determ<strong>in</strong><strong>in</strong>g the rate <strong>of</strong> structural system <strong>reliability</strong>decreases.The proposed factor can be represented mathematically as:1RF = (17)R nM.A. Salau, D.E. Esezobor, M. F. Omotoso/Petroleum & Coal 53 (4) 291-301, 2011 297R n – Jacket structural system <strong>reliability</strong>Accord<strong>in</strong>gly, <strong>jacket</strong> <strong>reliability</strong> prediction for the year 2008 is estimated and presented<strong>in</strong> Table 5. The factor is essential to determ<strong>in</strong>e <strong>jacket</strong> safety dur<strong>in</strong>g the operat<strong>in</strong>g lifecycleas the factor shows <strong>jacket</strong> <strong>reliability</strong> reduction rates. The value is suggested to be 1.0 to1.25 s<strong>in</strong>ce load factor <strong>of</strong> safety is about 1.25 depend<strong>in</strong>g on the load under consideration.However, this factor may be fixed by <strong>in</strong>dividual operator <strong>of</strong> the platforms based on herbest eng<strong>in</strong>eer<strong>in</strong>g practice.Table 5 System Reliability & Reliability Factor EstimationS/N Period 1985 20081 Duration 0 yrs 23 yrs2 Support Legs (R SL ) 1 0.99953 Jacket Brac<strong>in</strong>g (R SG ) 1 0.85784 Reliability (R SJ ) (1.0 x1.0) =1.0 (0.9995 x 0.8578) = 0.85775 Reliability Factor (RF) (1.0/1.0) =1.0 (1.0/0.8577) = 1.1664. ConclusionsTime-variant formulation for <strong>reliability</strong> <strong>assessment</strong> <strong>of</strong> an exist<strong>in</strong>g <strong>of</strong>fshore <strong>jacket</strong><strong>structures</strong> was derived and presented taken <strong>in</strong>to account structural component damage dueto corrosion loss. Application <strong>of</strong> series and parallel <strong>reliability</strong> theories was applied for theestimation <strong>of</strong> <strong>jacket</strong> structural system <strong>reliability</strong>, with regards to member corrosion wastage.The technique was proposed for <strong>of</strong>fshore <strong>jacket</strong> structural <strong>assessment</strong> procedures.The advantage <strong>of</strong> this <strong>assessment</strong> method over manual structural member capacitycheck and 3D computer model due to corrosion loss <strong>in</strong>cludes provision <strong>of</strong> structural <strong>reliability</strong>values for <strong>in</strong>dividual member and as well as for the whole <strong>jacket</strong> structural system. This

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