基于荷载时程分析法的商用飞机撞击钢板混凝土结构安全壳的有限元分析

朱秀云;潘 蓉;林 皋;李 亮

振动与冲击 ›› 2015, Vol. 34 ›› Issue (1) : 1-5.

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振动与冲击 ›› 2015, Vol. 34 ›› Issue (1) : 1-5.
论文

基于荷载时程分析法的商用飞机撞击钢板混凝土结构安全壳的有限元分析

  • 朱秀云1,2,潘 蓉2,林 皋1 ,李 亮2
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FEM Analysis of Steel Plate Concrete Containment against Commercial Aircraft ImpactBased on Force Time-History Analysis Method

  • ZHU Xiu-yun1, 2, PAN Rong2, LIN Gao1, LI Liang2
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摘要

由于钢板混凝土墙背部钢板能够有效地约束混凝土在撞击方向上的运动以及限制混凝土碎片的飞溅,为了抵御商用飞机撞击,新型核电机组的核岛厂房外墙通常设计为钢板混凝土结构(SC)。本文基于荷载时程分析法,运用经典的显式非线性动力分析软件ANSYS/LS-DYNA,进行了波音707-320型号商用飞机撞击某钢板混凝土结构安全壳的响应分析。计算结果表明,即使在安全壳筒身最不利撞击部位冲击作用下,像波音707-320型号的商用飞机对该安全壳的影响是较小的,且增大钢板的厚度能够有效的减小冲击作用下结构的响应。

Abstract

Due to the rear-face steel plate of the steel plate concrete wall is very effective in preventing the perforation and scabbing of concrete, in order to resist the impact of commercial aircraft crash, Steel plate concrete (SC) structures are selected to be used in the design of external walls of nuclear island buildings for the new type nuclear power plant. In this paper, the FEM code ANSYS/LS-DYNA was used to simulate the re-sponse analysis of a Boeing 707-320 aircraft impact on a steel plate concrete (SC) containment based on the force time-history analysis method. The results show that even though in the condition of the Boeing 707-320 commercial aircraft impact load applied on the most adverse impact position of the cylinder containment, the response of the SC containment is small, in the other word, the SC containment can resist the impact. Fur-thermore, the increase of the thickness of the steel plate can effectively reduce the structural response to the impact.

关键词

荷载时程分析法 / 飞机撞击 / 钢板混凝土结构安全壳

Key words

Force Time-History Analysis Method / Aircraft Impact / Steel Plate Concrete Containment

引用本文

导出引用
朱秀云;潘 蓉;林 皋;李 亮. 基于荷载时程分析法的商用飞机撞击钢板混凝土结构安全壳的有限元分析[J]. 振动与冲击, 2015, 34(1): 1-5
ZHU Xiu-yun;;PAN Rong;LIN Gao;LI Liang. FEM Analysis of Steel Plate Concrete Containment against Commercial Aircraft ImpactBased on Force Time-History Analysis Method[J]. Journal of Vibration and Shock, 2015, 34(1): 1-5

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