Page 76 - Handbook of Materials Failure Analysis
P. 76

70     CHAPTER 4 Creep damage of high alloyed reformer tubes




                         This reaction proceeds at a temperature range of 850-900 °C and under pressure of
                         3-3.5 MPa, according to kinetics that depends on process parameters, catalyst, and
                         tube size [2].
                            Reforming tubes are very critical components being exposed to severe conditions
                         for long time during service. Each tube is formed by two or three pieces, produced by
                         centrifugal casting, machined, and butt welded. Tubes have usually inside diameter
                         of 60-200 mm, wall thickness in the range 10-25 mm, and total length of 10-15 m
                         and are designed for a nominal life of 100,000 h in service with a diameter straining
                         of about 3%, at temperatures and internal pressures, respectively, up to 980 °C and
                         35 bar [3]. The operating temperatures, together with the hoop stress due to internal
                         pressure, give rise to typical creep conditions: stress around 30 MPa and deformation
                                      s .
                         rate of  10  10  1
                            At a first analysis, failure mechanism of the alloys utilized for reforming tubes can
                         be summarized as nucleation of cavities and their evolution into microcracks and final
                         cracks, which are qualitatively shown on a typical strain-time curve, together with the
                         applicability fields of inspecting methods (Figure 4.1).
                            Although reformer tubes have a design life over than 10 years, premature failures
                         are often observed. Their life is primarily limited by creep damage, driven by a com-
                         bination of high service temperatures and hoop stresses that can evolve also into cat-
                         astrophic failure [4].





                                                                                     Macro-
                                Primary creep           Tertiary creep
                                                                                     cracks

                                                                                    Micro-
                                                                                    cracks
                             Strain

                                       Secondary creep                            Aligned
                                                                                  cavities


                                                                               Isolated
                                                                               cavities


                                                    Time                  Radiography
                                                                         Ultrasound
                                                                         Eddy current
                                                         LOTIS
                         FIGURE 4.1
                         Typical creep curve and applicability fields of inspecting methods.
   71   72   73   74   75   76   77   78   79   80   81