Study on thermal-hydraulic response characteristics of internal compartments in the containment building under LOCA conditions

Shilei Dun , Tao Zhou , Haoyv Li , Lanyv Zhou , Yao Yao , Changhong Peng , Shuyv He
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This generates intricate dynamic structural loads, making the investigation of these non-uniform response characteristics crucial for assessing and ensuring containment integrity. Taking the Hualong One containment as the research subject, a three-dimensional computational model incorporating the main compartments and connecting passages was established. Transient numerical simulations were conducted for four accident scenarios: passive cooling system with cold-end breach closed, passive cooling system with hot-end breach closed, passive cooling system with cold-end breach open, and passive cooling system with hot-end breach open. The analysis examines the evolution of velocity fields, temperature distributions, temperatures in the breach area, pressures in the breach area, and pressure differentials between the breached compartment and adjacent compartments during the initial high-velocity jet and backflow formation. Regarding velocity, high-velocity zones primarily concentrate near the breach location, forming high-flow regions within the pressure vessel compartment and the top of the containment structure. After activating the passive cooling system, the velocity of moist air within the large upper containment space decreases, while the velocity of moist air within the pressure vessel compartment increases.Regarding water vapor, the PCCS effectively reduces the vapor content within the containment structure through wall condensation, thereby suppressing the rate of temperature rise and pressure increase. For hot-end breaches, where steam locally accumulates, the PCCS directly weakens the pressure differential driving force through immediate condensation near the breach, yielding a slightly higher suppression effect than for cold-end breaches.Regarding temperature, the side of the main pump compartment adjacent to the breach exhibits higher temperatures. Due to insufficient coolant, the pressure vessel experiences a rapid temperature rise, resulting in the highest temperatures in the central region. Temperatures decrease progressively from top to bottom within the large space. The temperature trends in the breach area are similar across the four accident scenarios: a rapid initial increase followed by relative stability. The final temperature in the hot-end breach area is higher than that in the cold-end breach. After activating the passive cooling system, temperature conditions in both cold-end and hot-end breach scenarios resemble pre-activation patterns but exhibit significantly reduced temperatures. Regarding pressure, breach zones experience rapid pressure surges within seconds, followed by minor fluctuations before the rate of increase slows. Hot-end breaches exhibit higher pressure values and faster rise rates than cold-end breaches. Activating the passive cooling system mitigates pressure growth in breach zones. Regarding inter-compartment pressure differential, the maximum pressure differential in the cold-end breach scenario peaked at 0.142 MPa within 0.25 s, while the hot-end breach scenario reached a maximum peak of 0.153 MPa at 0.31 s. After activating the passive cooling system, the pressure differential transient curve trend resembled that with the passive cooling system deactivated. However, the peak pressure differentials for both breach scenarios were effectively suppressed, resulting in a flatter curve profile. The maximum compartment pressure differential for the cold-side breach accident scenario peaked at 0.123 MPa at 0.24 s, while the maximum compartment pressure difference in the hot-end breach accident scenario peaked at 0.132 MPa at 0.26 s. Through multi-scenario computational simulations, the thermal-hydraulic response patterns of multi-compartment containment structures during LOCA accidents were obtained, leading to the following strategies: consider local structural dynamic loads for each scenario; optimize equipment layout and thermal insulation protection in high-temperature zones based on temperature field distribution; and evaluate natural circulation equipment layout in conjunction with flow field changes.</div></div>","PeriodicalId":100689,"journal":{"name":"International Journal of Advanced Nuclear Reactor Design and Technology","volume":"8 2","pages":"Pages 238-251"},"PeriodicalIF":0.0000,"publicationDate":"2026-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Advanced Nuclear Reactor Design and Technology","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2468605026000268","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2026/5/2 0:00:00","PubModel":"Epub","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

Investigating the thermal-hydraulic response characteristics of internal compartments within the containment structure during LOCA accidents holds significant scientific, engineering, and safety value for elucidating accident evolution mechanisms, evaluating compartment structural loads, and optimizing containment design. During LOCA events, high-energy fluids released through breaches create highly non-uniform velocity, Distribution of Water Vapor, temperature, and pressure distributions within the complex multi-compartment space of the containment structure. This generates intricate dynamic structural loads, making the investigation of these non-uniform response characteristics crucial for assessing and ensuring containment integrity. Taking the Hualong One containment as the research subject, a three-dimensional computational model incorporating the main compartments and connecting passages was established. Transient numerical simulations were conducted for four accident scenarios: passive cooling system with cold-end breach closed, passive cooling system with hot-end breach closed, passive cooling system with cold-end breach open, and passive cooling system with hot-end breach open. The analysis examines the evolution of velocity fields, temperature distributions, temperatures in the breach area, pressures in the breach area, and pressure differentials between the breached compartment and adjacent compartments during the initial high-velocity jet and backflow formation. Regarding velocity, high-velocity zones primarily concentrate near the breach location, forming high-flow regions within the pressure vessel compartment and the top of the containment structure. After activating the passive cooling system, the velocity of moist air within the large upper containment space decreases, while the velocity of moist air within the pressure vessel compartment increases.Regarding water vapor, the PCCS effectively reduces the vapor content within the containment structure through wall condensation, thereby suppressing the rate of temperature rise and pressure increase. For hot-end breaches, where steam locally accumulates, the PCCS directly weakens the pressure differential driving force through immediate condensation near the breach, yielding a slightly higher suppression effect than for cold-end breaches.Regarding temperature, the side of the main pump compartment adjacent to the breach exhibits higher temperatures. Due to insufficient coolant, the pressure vessel experiences a rapid temperature rise, resulting in the highest temperatures in the central region. Temperatures decrease progressively from top to bottom within the large space. The temperature trends in the breach area are similar across the four accident scenarios: a rapid initial increase followed by relative stability. The final temperature in the hot-end breach area is higher than that in the cold-end breach. After activating the passive cooling system, temperature conditions in both cold-end and hot-end breach scenarios resemble pre-activation patterns but exhibit significantly reduced temperatures. Regarding pressure, breach zones experience rapid pressure surges within seconds, followed by minor fluctuations before the rate of increase slows. Hot-end breaches exhibit higher pressure values and faster rise rates than cold-end breaches. Activating the passive cooling system mitigates pressure growth in breach zones. Regarding inter-compartment pressure differential, the maximum pressure differential in the cold-end breach scenario peaked at 0.142 MPa within 0.25 s, while the hot-end breach scenario reached a maximum peak of 0.153 MPa at 0.31 s. After activating the passive cooling system, the pressure differential transient curve trend resembled that with the passive cooling system deactivated. However, the peak pressure differentials for both breach scenarios were effectively suppressed, resulting in a flatter curve profile. The maximum compartment pressure differential for the cold-side breach accident scenario peaked at 0.123 MPa at 0.24 s, while the maximum compartment pressure difference in the hot-end breach accident scenario peaked at 0.132 MPa at 0.26 s. Through multi-scenario computational simulations, the thermal-hydraulic response patterns of multi-compartment containment structures during LOCA accidents were obtained, leading to the following strategies: consider local structural dynamic loads for each scenario; optimize equipment layout and thermal insulation protection in high-temperature zones based on temperature field distribution; and evaluate natural circulation equipment layout in conjunction with flow field changes.
LOCA条件下安全壳建筑内隔室热液响应特性研究
研究LOCA事故中安全壳结构内部隔室的热液响应特性,对于阐明事故演变机制、评估隔室结构载荷和优化安全壳设计具有重要的科学、工程和安全价值。在LOCA事件中,通过裂缝释放的高能流体在安全壳结构的复杂多室空间内产生高度不均匀的速度、水蒸气分布、温度和压力分布。这会产生复杂的动态结构载荷,因此研究这些非均匀响应特性对于评估和确保安全壳完整性至关重要。以“华龙一号”安全壳为研究对象,建立了包含主舱室和连接通道的三维计算模型。对被动冷却系统冷端裂口关闭、被动冷却系统热端裂口关闭、被动冷却系统冷端裂口打开、被动冷却系统热端裂口打开四种事故情景进行了瞬态数值模拟。分析了初始高速射流和回流形成过程中速度场、温度分布、裂口区域温度、裂口区域压力以及裂口隔室与相邻隔室之间的压差的演变。速度方面,高速区主要集中在裂口附近,形成压力容器室内和安全壳结构顶部的高流区。激活被动冷却系统后,大上部安全壳空间内的湿空气流速减小,而压力容器舱内的湿空气流速增大。对于水蒸气,PCCS通过壁面冷凝有效降低了安全壳结构内的蒸汽含量,从而抑制了温度升高和压力升高的速度。对于蒸汽局部积聚的热端裂口,PCCS通过裂口附近的立即冷凝直接削弱压差驱动力,产生的抑制效果略高于冷端裂口。在温度方面,靠近裂口的主泵室一侧温度较高。由于冷却剂不足,压力容器温度迅速上升,导致中部地区温度最高。在大空间内,温度从上到下逐渐降低。在四种事故情景中,裂口区域的温度趋势是相似的:一开始迅速上升,随后相对稳定。热端缺口区最终温度高于冷端缺口区。激活被动冷却系统后,冷端和热端裂口场景的温度条件类似于激活前的模式,但温度明显降低。关于压力,破裂区在几秒钟内经历快速的压力激增,随后在增加速度减慢之前出现轻微波动。热端裂口比冷端裂口具有更高的压力值和更快的上升速率。激活被动冷却系统可以减轻泄漏区域的压力增长。在室间压差方面,冷端裂口情景的最大压差在0.25 s内达到0.142 MPa,热端裂口情景的最大压差在0.31 s达到0.153 MPa。被动冷却系统启动后,压差瞬态曲线趋势与被动冷却系统关闭时相似。然而,两种突破情景的峰值压差都被有效抑制,导致曲线轮廓更平坦。冷端裂口事故情景的最大室压差在0.24 s时达到峰值0.123 MPa,热端裂口事故情景的最大室压差在0.26 s时达到峰值0.132 MPa。通过多场景的计算模拟,得到了多室容器结构在LOCA事故中的热液响应模式,得出了以下策略:考虑每个场景的局部结构动载荷;根据温度场分布优化高温区设备布置和保温防护;并结合流场变化对自然循环设备布置进行评价。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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