第二代FeCrAl合金辐照后断裂韧性表征

Xiang Chen, K. Field, Dalong Zhang, C. Massey, J. Robertson, K. Linton, A. Nelson
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引用次数: 3

摘要

FeCrAl合金在高温蒸汽环境中具有优异的抗氧化性能,是耐事故燃料(ATF)包层应用的有前途的候选材料。目前,有限的断裂韧性数据可用于FeCrAl合金,包括美国能源部先进燃料运动(AFC)计划下橡树岭国家实验室(ORNL)新开发的FeCrAl合金。本研究将C06M (81.8Fe-10Cr-6Al-0.03Y-2Mo-0.2Si)和C36M (78.8Fe-13Cr-6Al-0.03Y-2Mo-0.2Si)两种第二代候选FeCrAl合金在ORNL的高通量同位素反应堆(HFIR)中辐照,评估这两种合金在中子辐照后的断裂特征。在HFIR中辐照6只兔胶囊,目标温度分别为200°C、330°C和500°C,目标损伤剂量分别为8位移/原子(dpa)和16 dpa。辐照后断裂韧性测试按照ASTM E1921标准中的主曲线法进行。主要研究结果如下:1)C06M和C36M合金在辐照硬化和脆化方面表现出相似的辐照响应。2)辐照温度对C06M和C36M的辐照硬化和辐照脆化作用不同:在166℃~ 204℃辐照后,两种材料均表现出明显的辐照硬化和辐照脆化;在315℃~ 343℃辐照后,两种材料均表现出较小的辐照硬化,无辐照脆化。在501℃~ 507℃之间辐照后,两种材料均出现了辐照软化现象,但未出现辐照脆化现象。3)对比中子辐照前后C06M和C36M钢的显微硬度和主曲线参考温度T0q,我们没有观察到这两个参数之间的线性相关。这主要是由于主曲线参考温度T0q在166-204℃和315-343℃范围内对辐照的平缓响应所致。4)C06M在未辐照条件下比C36M表现出更低的T0q,这意味着韧性更好,即使在中子辐照后也保持这种趋势,但在166-204℃辐照后,两种材料的T0q相似。5)在硬化脆化方面,辐照剂量为7 dpa时,C06M和C36M的辐照效应均趋于饱和。
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Post-Irradiation Fracture Toughness Characterization of Generation II FeCrAl Alloys
FeCrAl alloys are promising candidate materials for the accident tolerant fuel (ATF) cladding application due to their exceptional resistance to oxidation in elevated temperature steam environments. Currently, limited fracture toughness data are available for the FeCrAl alloys, including the FeCrAl alloys newly developed at Oak Ridge National Laboratory (ORNL) under the U.S. Department of Energy’s Advanced Fuels Campaign (AFC) program. In this study, two Generation II candidate FeCrAl alloys, i.e., C06M (81.8Fe-10Cr-6Al-0.03Y-2Mo-0.2Si) and C36M (78.8Fe-13Cr-6Al-0.03Y-2Mo-0.2Si), were irradiated in the High Flux Isotope Reactor (HFIR) at ORNL to assess the fracture characteristics of these alloys after neutron irradiation. A total of six rabbit capsules were irradiated in HFIR at target temperatures of 200°C, 330°C, and 500°C up to target damage doses of 8 displacements per atom (dpa) and 16 dpa. Post-irradiation fracture toughness testing was performed following the Master Curve method in the ASTM E1921 standard. The main findings of this study are: 1) Both the C06M and C36M alloys exhibited a similar response to irradiation concerning irradiation hardening and embrittlement. 2) The irradiation temperature played different roles in terms of irradiation hardening and embrittlement for both C06M and C36M: after irradiation between 166°C and 204°C, both materials exhibited significant irradiation hardening and embrittlement; after irradiation between 315°C and 343°C, both materials showed small irradiation hardening without irradiation embrittlement. After irradiation between 501°C and 507°C, however, the irradiation softening without irradiation embrittlement was observed in both materials. 3) Comparing the microhardness and Master Curve reference temperature T0q before and after neutron irradiation, we did not observe a linear correlation between the two parameters for both C06M and C36M steels. This should be mainly due to a flat response of the Master Curve reference temperature T0q to the irradiations at 166–204°C and 315–343°C ranges 4) C06M showed a lower T0q, meaning better toughness, than C36M at the unirradiated condition, and such trend was kept even after neutron irradiation except for the 166–204°C irradiation after which both materials had similar T0q. 5) In terms of hardening and embrittlement, the irradiation effect on both C06M and C36M appeared to saturate after an irradiation dose of 7 dpa.
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