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Structural analysis of a metal spent-fuel storage cask in an aircraft crash for risk assessment

机译:飞机失事中金属乏燃料存储桶的结构分析,以进行风险评估

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摘要

Evaluations of the impact resistance of a dry storage cask under mechanical impact loadings resulting from a large commercial aircraft crash have become an important issue for designers and evaluators, in order to promote interim dry storage activities and to evaluate design safety margins. This study presents a method to evaluate the structural integrity of a generic metal cask subjected to various mechanical loading conditions, which represent aircraft engine impacts, on different locations of the cask body. Thirty representative impact conditions are analyzed to provide a comprehensive evaluation of cask damage response. The applied engine impact load time functions were carefully re-derived by utilizing CRIEPI's proposed curve through Riera's approach for six impact velocities, and applied to five locations on a freestanding cask: lateral impacts on the lower half, center of gravity, and upper half of the cask body, corner impact on the lid closure, and vertical impact on the center of the lid closure. A nonlinear dynamic finite element analysis is performed to evaluate the dynamic response of the cask lid closure system and to calculate the lid gaps. The release fractions from the cask to the environment for each impact condition are preliminarily estimated by referring to a proposed methodology from literature. It is believed that this paper presents a systematic process to connect the mechanical analysis of a cask response at the moment of aircraft engine impact with its radiological consequence analysis. (C) 2016 Elsevier B.V. All rights reserved.
机译:为了促进临时干燥存储活动并评估设计安全裕度,对于大型商用飞机坠机造成的机械冲击载荷下的干燥存储桶的抗冲击性评估已成为设计人员和评估人员的重要问题。这项研究提出了一种方法来评估通用金属酒桶在酒桶体不同位置承受各种机械载荷条件(代表飞机发动机撞击)的结构完整性。分析了三十种代表性冲击条件,以提供对桶损伤反应的全面评估。通过Riera的方法利用CRIEPI的建议曲线对六种冲击速度进行仔细地重新推导了所应用的发动机冲击载荷时间函数,并将其应用于独立桶的五个位置:对下半部,重心和上半部的侧向冲击桶身,拐角撞击盖子盖,垂直撞击盖子盖的中心。进行非线性动态有限元分析,以评估桶盖封闭系统的动态响应并计算盖间隙。通过参考文献中提出的方法,可以初步估算每种撞击条件下从木桶到环境的释放比例。可以相信,本文提出了一个系统的过程,将飞机发动机撞击时桶反应的力学分析与其放射学后果分析联系起来。 (C)2016 Elsevier B.V.保留所有权利。

著录项

  • 来源
    《Nuclear Engineering and Design》 |2016年第11期|60-72|共13页
  • 作者单位

    Korea Adv Inst Sci & Technol, Dept Nucl & Quantum Engn, 291 Daehak Ro, Daejeon 305701, South Korea;

    Keimyung Univ, Dept Mech & Automot Engn, Dalgubeol Daero 1095, Daegu, South Korea;

    Korea Adv Inst Sci & Technol, Dept Nucl & Quantum Engn, 291 Daehak Ro, Daejeon 305701, South Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
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