Simulation of a thermoelectric power generation system with multiple heat storage for lunar habitat

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
Seheon Kim , Hansol Lim , Beom-Jun Kim , Taeyeon Kim , Sang-Hwan Park , Jae-Weon Jeong
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Abstract

The global demand for space research has surged, driven by advancements in technology and the pursuit of extraterrestrial resource utilization. As the development of lunar resources and infrastructure necessitates a sustained human presence, establishing a lunar habitat is imperative for the long-term advancement of space exploration. To ensure continuous power supply to such a habitat, thermoelectric generators (TEGs), which directly transform heat flux into electrical energy, can be utilized, leveraging the extreme temperature gradient on the lunar surface, which ranges from 90 to 390 K. However, although some studies suggest that the transient-state operation may enhance the TEG efficiency, its feasibility under lunar conditions remains unexplored. Therefore, as switching heat storage (HS) induces the transient state by altering the temperature of the working fluid and HS is generally necessary due to the Moon's prolonged nights, this study aims to assess the suitability of a multiple-HS system to generate a thermally transient state in the TEG through HS switching. The results showed that the multiple-HS structure increased power generation by approximately 48.9 % under the lunar environment, pointing temperature altering can enhance the power generation of the TEG-based system on the moon. Additionally, the effects of switching timing of multiple-HS and size of HS were assessed, but its impact is relatively low, +0.3 % for switching timing and −0.5 % for size. The findings should contribute to lunar research, providing insights for the transient characteristics of TEGs.
月球栖息地多蓄热热电发电系统仿真
在技术进步和对地外资源利用的追求的推动下,全球对空间研究的需求激增。由于月球资源和基础设施的开发需要人类持续存在,因此建立月球栖息地对于太空探索的长期推进至关重要。为了确保这样一个栖息地的持续供电,可以利用热电发电机(teg),将热流直接转化为电能,利用月球表面90至390 K的极端温度梯度。然而,尽管一些研究表明瞬态操作可能会提高TEG效率,但其在月球条件下的可行性仍有待探索。因此,由于切换储热(HS)通过改变工作流体的温度来诱导瞬态,并且由于月球的夜晚较长,通常需要HS,因此本研究旨在评估多HS系统通过HS切换在TEG中产生热瞬态的适用性。结果表明,多hs结构在月球环境下的发电能力提高了约48.9%,定向温度改变可以提高基于teg的系统在月球上的发电能力。此外,我们还评估了多重HS的切换时机和HS尺寸的影响,但其影响相对较低,切换时机的影响为+ 0.3%,尺寸的影响为- 0.5%。这些发现将有助于月球研究,为teg的瞬态特征提供见解。
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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