Issue 24

Yu. G. Matvienko, Frattura ed Integrità Strutturale, 24 (2013) 119-126 ; DOI: 10.3221/IGF-ESIS.24.13 121 Figure 1 : Hydrogen distribution H C through the thickness for the hydrogen-charged specimen at the distance of 30 m  from the crack tip ( max 20 K  m MPa ). H YDROGEN CHARGING CONDITIONS he problem of the effect of hydrogen charging conditions on the character of the hydrogen distribution in the specimen with a crack has been analysed. For this reason, the fatigue pre-cracked CT specimens were hydrogen charged in the same solution as the main set of the specimens at different values of the current density over a period of 2 hours under constant static load corresponding to two applied (constant) stress intensity factor values 10 K (Tab. 2). 10 K ( m MPa ) Current density (A/dm 2 ) 0 / C C H 30 6 10 2.9 3.0 50 6 10 3.8 3.8 Table 2 : The effect of hydrogen charging conditions on the hydrogen distribution ahead of the crack tip on crack extension line. The distribution of hydrogen ahead of the crack tip was measured by the same procedure as for the specimens after the fatigue test [12]. The values of the ratio of the maximum local concentration H C of hydrogen ahead of the crack tip to the volume concentration 0 C of hydrogen in the specimen were estimated. The results clearly show that the variation of the cathodic current density in these ranges does not influence on the 0 / H C C ratio which is determined only by the value of the applied stress intensity factor 10 K . T HE EFFECT OF HYDROGEN ON FATIGUE CRACK BEHAVIOUR negligible crack tip plastic zone is created due to the hydrogen embrittlement, mechanical properties of the high- strength steel and a low applied stress. It means that a linear elastic fracture mechanics methodology can be used to quantify the fracture toughness and fatigue crack growth behaviour. It follows that the maximum stress intensity factor must have an influence on fatigue damage evolution and the hydrogen distribution in the vicinity of the crack tip and, as a result, the physical growth of the fatigue crack. T A

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