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Conceptual design for a re-entrant type fuel channel for supercritical water-cooled nuclear reactors.

机译:超临界水冷核反应堆折返式燃料通道的概念设计。

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摘要

Current CANDU-type nuclear reactors use a once-through fuel-channel with an annulus gas insulating it from the moderator. The current reference design for a CANDU-type SuperCritical Water-Cooled Reactor (SCWR) is to eliminate the annulus gap and use a ceramic insert to insulate the coolant from the moderator. While such a design may work, alternative fuel-channel design concepts are under development to explore the optimum efficiency of SCWRs. One such alternative approach is called the Re-Entrant fuel-channel.;A numerical model was developed and MATLAB was used to calculate the heat loss from the insulated Re-Entrant fuel-channel along with the temperature profiles and the heat transfer coefficients for a given set of flow, pressure, temperature and power boundary conditions. Thermophysical properties were obtained from NIST REFPROP software. With the results from the numerical model, the design of the Re-Entrant fuel-channel was optimized to improve its efficiency.;The Re-Entrant fuel-channel consists of three tubes, the inner tube (flow tube), pressure tube and an outer tube. The fuel bundles are placed in the inner tube. An annulus is formed between the flow and pressure tubes, through which the primary coolant flows. A ceramic insulator is placed between the pressure tube and the outer tube. The coolant flows through the annulus receiving heat from the inner tube from one end of the channel to another. At the far end, the flow will reverse direction and enter the inner tube, and hence the fuel-string. At the inlet, the temperature is 350°C for a high-pressure coolant (pressure of 25 MPa), which is just below the pseudocritical point. At the outlet, the temperature is about 625ºC at the same pressure (the pressure drop is small and can be neglected). The objective of this work was to design the Re-Entrant channel and to estimate the heat loss to the moderator for the proposed new fuel-channel design.
机译:当前的CANDU型核反应堆使用直流燃料通道,其环形气体将其与慢化剂隔离。 CANDU型超临界水冷堆(SCWR)的当前参考设计是消除环隙,并使用陶瓷插件将冷却剂与慢化剂隔离。尽管这种设计可行,但替代燃料通道设计概念正在开发中,以探索短波堆的最佳效率。一种这样的替代方法称为Re-Entrant燃料通道。;建立了一个数值模型,并使用MATLAB来计算绝缘的Re-Entrant燃料通道的热量损失以及温度分布和传热系数。给定一组流量,压力,温度和功率边界条件。热物理性质是从NIST REFPROP软件获得的。根据数值模型的结果,优化了Re-Entrant燃料通道的设计以提高其效率。; Re-Entrant燃料通道由三个管组成:内管(流量管),压力管和一根外管。燃料束放置在内胎中。在流量管和压力管之间形成环形空间,主冷却剂流过该环形空间。在压力管和外管之间放置了一个陶瓷绝缘子。冷却剂流过环形空间,从通道的一端到另一端从内管接收热量。在远端,流体将反向流动并进入内管,从而进入燃料管。在入口处,高压冷却剂(压力为25 MPa)的温度为350°C,该温度刚好低于伪临界点。在出口处,在相同压力下温度约为625ºC(压降很小,可以忽略不计)。这项工作的目的是设计折返通道,并为拟议的新燃料通道设计估算减速器的热量损失。

著录项

  • 作者

    Samuel, Jeffrey.;

  • 作者单位

    University of Ontario Institute of Technology (Canada).;

  • 授予单位 University of Ontario Institute of Technology (Canada).;
  • 学科 Alternative Energy.;Engineering Nuclear.
  • 学位 M.A.Sc.
  • 年度 2011
  • 页码 160 p.
  • 总页数 160
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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