首页> 外文会议>International symposium on plasticity and impact mechanics >TRANSIENT DYNAMIC ANALYSIS OF 500 MWE PRESSURIZED HEAVY WATER REACTOR NUCLEAR DOUBLE CONTAINMENT FOR AIR CRAFT IMPACT LOAD
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TRANSIENT DYNAMIC ANALYSIS OF 500 MWE PRESSURIZED HEAVY WATER REACTOR NUCLEAR DOUBLE CONTAINMENT FOR AIR CRAFT IMPACT LOAD

机译:500 MWE加压重水反应堆核双粘膜的瞬态动力学分析

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Non-linear transient dynamic analysis of 500MWe Indian Pressurized Heavy water Reactor (PHWR) nuclear containment has been carried out for the aircraft impact of Boeing 707-320. The case studies include the analyses of outer containment wall (OCW) single model and the combined model with outer and inner containment wall (ICW) for impulsive loading due to aircraft impact. The impulsive load time history is generated based on the momentum transfer of the crushable aircrafts (soft missiles) of various categories such as Boeing and Airbus families on the containment structure. Initially the load is applied on OCW single model and subsequently the load is transferred to ICW after the local perforation of the OCW is noticed in the transient simulation. In the first stage of the analysis it is demonstrated that the OCW would suffer local perforation with a peak local deformation of ~117 mm without loss of the overall integrity. However, this first barrier (OCW) cannot absorb the full impulsive load. In the second stage of the analysis of the combined model, the ICW is subjected to lower impulse duration as the load is transferred after 0.19 sec due to the local perforation of OCW. This results in the local deformation of ~ 115 mm for ICW and together both the structures (OCW and ICW) are capable of absorbing the full impulsive load. The analysis methodology evolved in the present work would be useful for studying the behavior of double containment walls and multi barrier structural configurations for aircraft impact with higher energies. The present analysis illustrates that with the provision of double containments for Indian nuclear power plants, adequate reserve strength is available for the case of an extremely low probability event of missile impact due to commercial aircrafts operated in India.
机译:为波音707-320的飞机影响进行了500mWWE印度加压重水器(PHWR)核遏制的非线性瞬态动态分析。案例研究包括外壳壁(OCW)单模和与外部容纳壁(ICW)的组合模型分析,用于由于飞机的冲击而脉冲负载。基于各种类别的可抵碎飞机(软导弹)的动量转移产生脉冲负载时间历史,例如在容纳结构上的波音和空中客车家庭。最初,在OCW单一模型上施加负载,随后在瞬态仿真中注意到OCW的局部穿孔后,负载被传送到ICW。在分析的第一阶段,证明OCW将患有局部穿孔,局部局部变形〜117毫米,而不会损失整体完整性。然而,这首第一屏障(OCW)不能吸收完全冲动的载荷。在分析组合模型的第二阶段中,由于OCW的局部穿孔,ICW在0.19秒之后转移负荷后,ICW受到较低的脉冲持续时间。这导致ICW〜115mm的局部变形,并且可以一起构造(OCW和ICW)能够吸收全冲动负载。在本工作中演化的分析方法对于研究双夹持壁的行为和多屏障结构配置具有更高的能量的飞机冲击。目前的分析说明,随着印度核电站的双重遏制,由于印度运营的商业飞机,由于在印度运营的商业飞机,适当的储备强度适用于导弹影响极低的概率。

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