1 School of Materials Science and Engineering, Anhui University of Technology, Maanshan 243002, China 2 State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing, Beijing 100083, China 3 School of Metallurgical Engineering, Anhui University of Technology, Maanshan 243002, China
Cite this article:
Yongqiang WANG,Bin YANG,Na LI,Suhua LIN,Li SUN. EMBRITTLEMENT OF σ PHASE IN STAINLESS STEEL FOR PRIMARY COOLANT PIPES OF NUCLEAR POWER PLANT. Acta Metall Sin, 2016, 52(1): 17-24.
Cast austenite stainless steel (CASS) possesses excellent mechanical properties, good workability and high resistance to localized corrosion in chloride environments due to the dual phase microstructure in which the island a-ferrite phase distributes in the g-austenite matrix. So they are widely used in the primary coolant pipes of nuclear power plants. However, undesirable s phase can precipitate in these steels when they are welded or heat treated and it severely decreases the toughness of stainless steels. Although some works have been done to investigate the effect of s phase on mechanical properties of CASS, the mechanism of embrittlement was still lacking. In this work, the effect of s phase on toughness of Z3CN20.09M CASS was investigated, and the embrittlement mechanism of s phase in CASS was discussed by using in situ tensile test, microhardness technology and fracture analysis. It was found that the impact energy of specimens aged at 750 ℃ decreased severely due to the presence of s phases. The (s+g2) structure formed by the eutectoid decomposition of a phase is very hard and its hardness is much higher than that of austenite. This makes the deformation between (s+g2) structure and austenite incoordinate in aged specimens. The precipitation of s phase brought more s/g2 and a/s/g2 high energy non-coherent boundaries. These boundaries hindered dislocation movements and brought stress concentrations. So cracks initiated at the s/g2 or a/s/g2 boundaries preferentially and propagated rapidly when the aged specimen bearded impact stress. The much potential cracking sites (s/g2 and a/s/g2 boundaries) in the (s+g2) structure is the main reason of embrittlement of aged Z3CN20.09M CASS with low toughness.
Fund: Supported by National Natural Science Foundation of China (No.51501001), National High Technology Research and Development Program of China (No.2012AA03A507) and Natural Science Foundation of Anhui Province (No.1508085QE102)
Fig.1 Geometry of specimens used for in situ tensile tests (unit: mm)
Fig.2 SEM images of Z3CN20.09M specimens as solution state (a) and aged at 750 ℃ for 50 h (b), 100 h (c), 200 h (d)
Fig.3 TEM image of Z3CN20.09M specimen aged at 750 ℃ for 200 h and its SAED patters (insets)
Fig.4 Impact energy (a) and volume fraction of s phase (b) of Z3CN20.09M specimens aged for 24 and 100 h at different temperatures (RT—room temperature)
Fig.5 Impact energy of Z3CN20.09M specimens aged at 750 ℃ for different times (Inset shows the variation of impact energy of specimens with aging time less than 4 h)
Fig.6 Farcture surfaces of Z3CN20.09M specimen unaged (a) and aged at 750 ℃ for 50 h (b), 100 h (c), 200 h (d), and EDS results in the regions marked by circle in Figs.6b~d (e~g)
Fig.7 Schematic of the longitudinal section near fracture surface of specimens (a), and SEM images of longitudinal section near fracture surface of Z3CN20.09M specimens unaged (b) and aged at 750 ℃ for 50 h (c), 200 h (d)
Fig.8 Microhardness of ferrite and austenite in specimens unaged and aged at 750 ℃ for 200 h
Fig.9 Measuring point of microhardness of ferrite and austenite in specimens unaged (a) and aged at 750 ℃ for 200 h (b)
Fig.10 SEM images of specimen aged at 750 ℃ for 200 h during in situ tensile test under loads of 0 N (a), 390 N (b), 730 N (c), 860 N (d), 960 N (e) and high magnification image of the region marked by square in Fig.10e (f) (Inset in Fig.10d shows the high magnification image of the region marked by square)
Fig.11 In situ tensile fracture surfaces of Z3CN20.09M specimens unaged (a) and aged at 750 ℃ for 200 h after tensile tests (b)