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Chapter 23Basics of structural Reliability                            425




                                                         First excursion from safe
                                                         domain to failure domain


                                                                             \





                                  LSF: g(x(t))=xl -x2(t)



                                                                         Time  t

                            Figure 23.5  Time Variant Reliability


                     P/ (t) = 1 - P[N(~) o n g(x(o)) > 01                           (23.31)
                                    =


                                                                                    (23.32)
                 where, N(t) is the number of out-crossing in the interval [O,t].  Out crossings are the excursions
                 from safe domain to failure domain.
                 For marine structural analysis, stochastic load processes are often replaced by time-invariant
                 random variables to represent the lifetime loads. This also applies to cases of simultaneous
                 random loads. The combined extreme load  needs to be determined appropriately since the
                 respective  maximum  values  of  different  load  processes  do  not  necessarily  occur
                 simultaneously. This  depends  upon  the  application  of  methods  of  load  combination as
                 described in the above subsection.


                 23.8  Reliability Updating
                 Reliability  methodology  can  be  used  as  a  tool  to  reassess  structural  integrity.  Such
                 reassessment is required, e.g. when the inspection results are available or design conditions are
                changed. New measures of structural reliability are achieved based on new information. The
                 information can be grouped in two classes
                   Sampling of quantities
                   Observations
                To demonstrate the reliability updating, a component with load S and strength R is taken as an
                example. The failure probability is
                                     m
                     PI  = P[R - S I =   (.)A (sb                                   (23.33)
                                 01
                                     -m
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