Page 10 - Handbook of Materials Failure Analysis
P. 10

2      CHAPTER 1 Progressive failures of components




                         technical/economic activity offering significant potential in problem-solving viable
                         growth.
                            Metal components exhibit lower service life when operated at elevated temper-
                         atures. Depending on the particular environmental and loading conditions, the most
                         common causes of elevated-temperature failures can be classified as creep-
                         originated, environmentally induced fractures, high-temperature fatigue, and ther-
                         mal fatigue [2]. Creep is realized through the nucleation and growth of transgranular
                         or intergranular voids depended on the applied operating conditions, that is, stress
                         and temperature [3]. Creep is a progressive time-dependent deformation which leads
                         to final rupture with potential catastrophic consequence and implications to health,
                         safety, and environment. Remaining life-assessment techniques are a valuable asset
                         in failure prevention and cost minimization of high-temperature working equipment.
                         Methods using the Larson-Miller parameter (LMP), expressed in Equation 1.1, life
                         fraction rules, and damage accumulation conditions are very popular in remaining
                         life prediction [4,5], along with finite-element analysis (FEA) modeling presented
                         in the relevant literature [6]


                                                   LMP ¼ T   23 + logtÞ                  (1.1)
                                                           ð
                         where T is the operating temperature (K) and t is the service time (h).
                            Larson-Miller creep rupture curves present the stress variation as a function of
                         LMP. Knowledge of stress and temperature conditions could therefore lead to the
                         determination of the estimated creep life with at a certain statistical confidence level.
                         Life fraction is used for the estimation of remaining life of structural elements
                         exposed at high temperatures, according to Equation 1.2:

                                                      t op  t test
                                                         +   ¼ 1                         (1.2)
                                                      T op  T test
                         where t op is the operating time, T op is the total operating time at service conditions,
                         t test is the time for rupture at the test under accelerating conditions, and T test is the
                         time for rupture of fresh component under accelerating conditions.
                            The commonly referred eight forms of corrosion were addressed in the classical
                         corrosion literature [7]. The issue of stress corrosion cracking (SCC) of stainless
                         steels is a critical research field due to the extensive use of such materials in special
                         applications and the associated risks (unexpected failure without warning, severe
                         impact to human safety and environment). It is a dominant failure mechanism for
                         metallic components in unit operations industries that embrace many types of phys-
                         ical and chemical processes, under elevated temperatures, high pressures, and chem-
                         ically reactive environments. SCC of a stainless steel spiral heat exchanger in a
                         distillation column has been attributed to the action of chloride ions in the cooling
                         water, compromising the integrity of the protective oxide layer, producing corrosion
                         pits and facilitating crack formation [8]. SCC was also attributed to the detrimental
                         effect of chloride ions as reported in the case of failure of an AISI 304 styrene
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