空间核电源热管式辐射散热器热分析与参数优化

Xiu Zhang; Hao Chun Zhang; Xiu Ting Liu; De Zhuang Yin

doi:10.3873/j.issn.1000-1328.2019.04.010

空间核电源热管式辐射散热器热分析与参数优化

Translated title of the contribution: Thermal Analysis and Parameter Optimization of a Heat-Pipe Radiator for Space Nuclear Power

Xiu Zhang
, Hao Chun Zhang
, Xiu Ting Liu
, De Zhuang Yin

School of Energy Science and Engineering, Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

6 Scopus citations

Abstract

In this paper, based on the special conditions of a space radiator, the heat transfer model is established. It is proved that the model and the calculation method are feasible by comparing with the actual designing process. With the fin length and fin thickness and other parameters selected as the variables, the heat dissipation of the fin in the heat pipe radiator and the quality characteristics of the system are analyzed and optimized, and finally the optimal design is found which has potentials in thermal design and analysis.

Translated title of the contribution	Thermal Analysis and Parameter Optimization of a Heat-Pipe Radiator for Space Nuclear Power
Original language	Chinese (Traditional)
Pages (from-to)	452-458
Number of pages	7
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	40
Issue number	4
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2019.04.010
State	Published - 1 Apr 2019
Externally published	Yes

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title = "空间核电源热管式辐射散热器热分析与参数优化",

abstract = "In this paper, based on the special conditions of a space radiator, the heat transfer model is established. It is proved that the model and the calculation method are feasible by comparing with the actual designing process. With the fin length and fin thickness and other parameters selected as the variables, the heat dissipation of the fin in the heat pipe radiator and the quality characteristics of the system are analyzed and optimized, and finally the optimal design is found which has potentials in thermal design and analysis.",

keywords = "Heat-pipe radiator, Optimal design, Space nuclear power radiator, Thermal analysis",

author = "Xiu Zhang and Zhang, \{Hao Chun\} and Liu, \{Xiu Ting\} and Yin, \{De Zhuang\}",

year = "2019",

month = apr,

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doi = "10.3873/j.issn.1000-1328.2019.04.010",

language = "繁体中文",

volume = "40",

pages = "452--458",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

number = "4",

}

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T1 - 空间核电源热管式辐射散热器热分析与参数优化

AU - Zhang, Xiu

AU - Zhang, Hao Chun

AU - Liu, Xiu Ting

AU - Yin, De Zhuang

PY - 2019/4/1

Y1 - 2019/4/1

N2 - In this paper, based on the special conditions of a space radiator, the heat transfer model is established. It is proved that the model and the calculation method are feasible by comparing with the actual designing process. With the fin length and fin thickness and other parameters selected as the variables, the heat dissipation of the fin in the heat pipe radiator and the quality characteristics of the system are analyzed and optimized, and finally the optimal design is found which has potentials in thermal design and analysis.

AB - In this paper, based on the special conditions of a space radiator, the heat transfer model is established. It is proved that the model and the calculation method are feasible by comparing with the actual designing process. With the fin length and fin thickness and other parameters selected as the variables, the heat dissipation of the fin in the heat pipe radiator and the quality characteristics of the system are analyzed and optimized, and finally the optimal design is found which has potentials in thermal design and analysis.

KW - Heat-pipe radiator

KW - Optimal design

KW - Space nuclear power radiator

KW - Thermal analysis

UR - https://www.scopus.com/pages/publications/85069232252

U2 - 10.3873/j.issn.1000-1328.2019.04.010

DO - 10.3873/j.issn.1000-1328.2019.04.010

M3 - 文章

AN - SCOPUS:85069232252

SN - 1000-1328

VL - 40

SP - 452

EP - 458

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 4

ER -

空间核电源热管式辐射散热器热分析与参数优化

Abstract

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