Issue 36

I. Camagic et alii, Frattura ed Integrità Strutturale, 36 (2016) 1-7; DOI: 10.3221/IGF-ESIS.36.01 2 T ESTING MATERIAL oth new and exploited PM was steel A-387 Gr. B with thickness of 102 mm. Chemical composition and mechanical properties for both new and exploited PM are given in Tabs. 1 and 2. Specimen designation % max C Si Mn P S Cr Mo Cu E 0.15 0.31 0.56 0.007 0.006 0.89 0.47 0.027 N 0.13 0.23 0.46 0.009 0.006 0.85 0.51 0.035 Table 1 : Chemical composition of exploited (E) and new (N) PM specimens Specimen designation Yield stress, R p0.2 , MPa Tensile strength R m , MPa Elongation A, % Impact energy, J E 320 450 34.0 155 N 325 495 35.0 165 Table 2 : Chemical composition of exploited (E) and new (N) PM specimens. Welding of both new and exploited PM was performed in two stages, according to the following welding procedure specification:  Root pass by shielded metal arc welding, using LINCOLN S1 19G electrode, and  Filling passes by arc submerged arc welding, using LINCOLN LNS 150 wire and LINCOLN P230 flux. Chemical composition of the coated electrode LINCOLN S1 19G, and the wire LINCOLN LNS 150 according to the atest documentation is given in tab. 3, whereas their mechanical properties, also according to the atest documentation, are given in tab. 4. Filler material % mas C Si Mn P S Cr Mo LINCOLN S1 19G 0.07 0.31 0.62 0.009 0.010 1.17 0.54 LINCOLN LNS 150 0.10 0.14 0.71 0.010 0.010 1.12 0.48 Table 3 : Chemical composition of filler materials. Filler material Yield stress, R p0.2 , MPa Tensile strength R m , MPa Elongation A, % Impact energy, J, 20°C LINCOLN S1 19G 515 610 20 >60 LINCOLN LNS 150 495 605 21 >80 Table 4 : Mechanical properties of filler materials F ATIGUE CRACK GROWTH PARAMETERS EVALUATION atigue crack growth testing at room temperature was performed on three-point bending specimens, as defined by ASTM E399, [3], whereas tesitng at service temperature, 540  C, was performed on modified CT specimens, as defined by standard BS 7448 Part 1, [4]. The high-frequency resonant pulsator was used, in force control mode, with loading ratio R = 0.1 to obtain diagrams da/dN-  K for specimens with fatigue crack tip located in PM, WM and B F