Structural Health Monitoring for Reinforced Concrete Containment Using Inner Electrical Resistivity Method

Mostafa H. Hassaan, M. Elmasry, Nabil Hassan EL Ashkar
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引用次数: 1

Abstract

Nuclear power plants (NPPs) are considered as the main source for generating electricity nowadays in some countries. The effect of impact of heavy fully loaded aeroplane such as (Boeing 747-200c) causes leakage of the radiation through the cracks generated on the external RC containment of NPPs, and this leads to severe damage for humans and cities. In this research paper, external RC containment is modeled using ANSYS and hit by Boeing 747-200c which is the heavier aeroplane compared to other jets and causes severe damage for external RC containment. In addition, the impact location for Boeing 747-200c is considered at 30 m vertical height. RC containment response was studied after the impact of an aeroplane and a proposed structural health monitoring technique is applied using embedded sensors in order to detect and locate the embedded cracks that is generated due to the effect of impact of heavy aeroplane. It was concluded that RC containment is intact except for the impact region which is damaged. An experimental program was applied on a part of the element in ANSYS which is away from the impact region. Four specimens were cast using heavy weight concrete in laboratory. Three cracked specimens consist of different lengths of vertical cracks which represent different times of impact in order to replicate crack propagation as in ANSYS. The cracks are simulated inside laboratory specimens using failure criteria. The parameters used in detecting the cracks for specimens are the percentage change in electrical resistivity and Decimal Logarithm Resistivity Anisotropy (DLRA) at which they give a good indication for the presence of the crack.
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用内电阻率法监测钢筋混凝土安全壳结构健康
目前在一些国家,核电站被认为是发电的主要来源。满载的重型飞机(如波音747-200c)的撞击效应导致辐射通过核电站外部RC安全壳上产生的裂缝泄漏,这对人类和城市造成严重损害。在本研究中,使用ANSYS对RC外围护层进行建模,并与波音747-200c飞机进行碰撞,波音747-200c飞机相对于其他喷气式飞机更重,对RC外围护层造成了严重的破坏。此外,波音747-200c的撞击位置考虑为垂直高度30米。研究了飞机撞击后混凝土结构的安全壳响应,提出了一种基于嵌入式传感器的结构健康监测技术,用于检测和定位由于大型飞机撞击而产生的嵌入式裂缝。结果表明,除冲击区受损外,RC安全壳是完整的。在ANSYS中对远离冲击区域的部分元件进行了实验研究。4个试件在实验室采用重混凝土浇筑。三个裂纹试件由不同长度的垂直裂纹组成,代表不同的冲击时间,以复制ANSYS中裂纹的扩展。利用破坏准则模拟了实验室试样内部的裂纹。用于检测试样裂纹的参数是电阻率的百分比变化和十进制对数电阻率各向异性(DLRA),它们可以很好地指示裂纹的存在。
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