Numerical investigation on startup characteristics of high temperature heat pipe for nuclear reactor

•A numerical code is carried out based on the three-stage model of frozen startup of the heat pipe.•The heat transfer performance of a NaK heat pipe is simulated during startup from the frozen state.•Sensitivity analysis and heat transfer limitations of the NaK heat pipe are carried out. Heat pipe c...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Nuclear engineering and design 2021-07, Vol.378, p.111180, Article 111180
Hauptverfasser: Zhang, Zeqin, Chai, Xiaoming, Wang, Chenglong, Sun, Hao, Zhang, Dalin, Tian, Wenxi, Qiu, Suizheng, Su, G.H
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:•A numerical code is carried out based on the three-stage model of frozen startup of the heat pipe.•The heat transfer performance of a NaK heat pipe is simulated during startup from the frozen state.•Sensitivity analysis and heat transfer limitations of the NaK heat pipe are carried out. Heat pipe cooled reactor (HPR) has a good adaptability to portable power system, which is popular in recent years. Due to the particularity of alkali-metal working fluid, the deep understanding of startup characteristics of high temperature heat pipe from frozen state is essential for the development of HPRs. In this paper, a three-stage frozen startup model is developed to describe the thermal behavior of heat pipe during the startup process, and the continuum flow in the vapor space is modeled as a one-dimensional compressible flow. A numerical code is carried out, in which the governing equations are discretized by Finite Element Method (FEM), and then the code is used to simulate the startup performance of a NaK heat pipe in HPRs. Numerical results indicate that the heat pipe startup behavior can be well described by the three-stage model. The NaK heat pipe is successfully started with a final consistency temperature of 834 K, although the entire second stage is restricted by the sonic limitation. The startup lasts 1550 s in total, and enters the second and third stage at 230 s and 650 s, respectively. After 1500 s, the maximum Mach number of vapor flow is lower than 0.1, which verifies the rationality of the one-dimensional compressible flow model of vapor. This work could provide a reference for the design and application of HPRs.
ISSN:0029-5493
1872-759X
DOI:10.1016/j.nucengdes.2021.111180