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TRISO-fuel element thermo-mechanical performance modeling for the hybrid LIFE engine with Pu fuel blanket

机译:带Pu燃料层的混合式LIFE发动机的TRISO燃料元件热机械性能建模

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摘要

A TRISO-coated fuel thermo-mechanical performance study is performed for the fusion-fission hybrid Laser Inertial Fusion Engine (LIFE) to test the viability of TRISO particles to achieve ultra-high burn-up of Pu or transuranic spent nuclear fuel blankets. Our methodology includes full elastic anisotropy, time and temperature varying material properties, and multilayer capabilities. In order to achieve fast fluences up to 30 × 10~(25) n m ~(-2) (E > 0.18 MeV), judicious extrapolations across several orders of magnitude of existing material databases have been carried out. The results of our study indicate that failure of the pyrolytic carbon (PyC) layers occurs within the first 2 years of operation. The particles then behave as a single-SiC-layer particle and the SiC layer maintains reasonably-low tensile stresses until the end-of-life. It is also found that the PyC creep constant, K, has a striking influence on the fuel performance of TRISO-coated particles, whose stresses scale almost inversely proportional to K. Conversely, varying the geometry of the TRISO-coated fuel particles results in little differences in terms of fuel performance.
机译:对聚变裂变混合激光惯性聚变引擎(LIFE)进行了TRISO涂层的燃料热机械性能研究,以测试TRISO粒子的可行性,以实现Pu或超铀废核燃料毯的超高燃烧。我们的方法包括完全弹性各向异性,随时间和温度变化的材料特性以及多层功能。为了获得高达30×10〜(25)n m〜(-2)(E> 0.18 MeV)的快速通量,已经对现有材料数据库的几个数量级进行了明智的推断。我们的研究结果表明,热解碳(PyC)层的失效发生在运行的前两年内。然后,这些颗粒表现为单SiC层颗粒,并且SiC层保持合理低的拉伸应力,直到使用寿命终止。还发现PyC蠕变常数K对TRISO涂层的颗粒的燃料性能有显着影响,其应力比例几乎与K成反比。相反,改变TRISO涂层的燃料颗粒的几何形状几乎没有燃油性能方面的差异。

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