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Safety assessment of Generation Ⅲ nuclear power plant buildings subjected to commercial aircraft crash Part I: FE model establishment and validations

机译:遭受商用飞机坠毁的第三代核电站建筑物的安全评估第一部分:有限元模型的建立和验证

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Investigations of the commercial aircraft impact effect on nuclear island infrastructures have been drawing extensive attention, and this paper aims to perform the safety assessment of Generation Ⅲ nuclear power plant (NPP) buildings subjected to typical commercial aircrafts crash. At present Part I, finite element (FE) models establishment and validations for both the aircrafts and NPP buildings are performed. (i) Airbus A320 and A380 aircrafts are selected as the representative medium and large commercial aircrafts, and the corresponding fine FE models including the skin, beam, fuel and etc. are established. By comparing the numerically derived impact force time-histories with the existing published literatures, the rationality of aircrafts models is verified. (ii) Fine FE model of the Chinese Zhejiang Sanao NPP buildings is established, including the detailed structures and reinforcing arrangement of both the containment and auxiliary buildings. (iii) By numerically reproducing the existing 1/7.5 scaled aircraft model impact tests on steel plate reinforced concrete (SC) panels and assessing the impact process and velocity time-history of aircraft model, as well as the damage and the maximum deflection of SC panels, the applicability of the existing three concrete constitutive models (i.e., K&C, Winfrith and CSC) are evaluated and the superiority of Winfrith model for SC panels under deformable missile impact is verified. The present work can provide beneficial reference for the integral aircraft crash analyses and structural damage assessment in the following two parts of this paper.
机译:对商用飞机对核岛基础设施的影响的研究一直受到广泛关注,本文旨在对遭受典型商用飞机坠毁的第三代核电厂(NPP)建筑物进行安全评估。目前,第一部分进行了飞机和NPP建筑物的有限元(FE)模型的建立和验证。 (i)选择空中客车A320和A380飞机作为代表性的中型和大型商用飞机,并建立了相应的精细FE模型,包括蒙皮,横梁,燃料等。通过将数值推导的冲击力时间历程与现有的公开文献进行比较,验证了飞机模型的合理性。 (ii)建立了中国浙江三ao核电厂建筑物的精细有限元模型,包括安全壳和辅助建筑物的详细结构和加固布置。 (iii)通过数值复制现有的1 / 7.5比例飞机模型在钢板增强混凝土(SC)板上的冲击试验,并评估飞机模型的冲击过程和速度时程,以及SC的损坏和最大挠度评估了现有三种混凝土本构模型(即K&C,Winfrith和CSC)的适用性,并验证了Winfrith模型在可变形导弹撞击下对SC面板的优越性。本文的工作为以下两个部分的飞行器整体碰撞分析和结构损伤评估提供有益的参考。

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