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Review of Regenerative Adsorption Heat Pumps

机译:蓄热式吸附热泵综述

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摘要

NASA is again considering a permanent lunar base as part of its new "Exploration Vision." Because the lunar surface reaches 100℃ near the equator during the lunar day (14.75 Earth days) and -100℃ during the lunar night (also 14.75 Earth days), some type of heat pump is needed to elevate the temperature of absorbed sunlight and interior waste heat in order to reject it to space. An earlier investigation by M. A. Lambert ("Conceptual Design of a Regenerative Adsorption Heat Pump for a Lunar Base," AIAA Paper 99-0465, 1999) identified adsorption (solid-vapor) heat pumps as one of two technologies best suited to this application, the other being a mechanical vapor compression device with a high-efficiency centrifugal compressor. In order to properly preface the creation of a detailed design for an adsorption heat pump, this investigation reviews the state of the art in adsorption heat pumps, specifically the recently developed, much more efficient, regenerative variants. The principal figures of merit are the coefficient of performance for cooling (COP_c) and the specific cooling power. Nonregenerative adsorption heat pumps exhibit a COP_c of only 0.3 to 0.4, whereas regenerative designs have achieved a COP_c of 1.1 with 70 % regeneration of waste heat. Attention has focused on maximizing overall heat transfer coefficient and minimizing nonadsorbent mass of the most critical component, the adsorption bed, while maintaining adequate vapor permeability. This involves establishing a thermal wave temperature gradient traversing the bed, which minimizes the temperature difference for heat transfer and entropy generation. A number of novel designs have resulted. The most studied adsorbents are zeolites (a class of highly nanoscopically porous minerals), activated graphite, and silica gel. The refrigerants receiving the greatest attention are ammonia, methanol, and water.
机译:NASA再次考虑将永久性登月基地作为其新的“探索远景”的一部分。由于在月初(14.75地球日)的月球表面到达赤道附近,在月球晚上(也是14.75地球日)的赤道表面达到-100℃,因此需要某种类型的热泵来提高吸收的阳光和室内温度浪费热量以将其排入太空。 MA Lambert先前进行的一项调查(“月球基地的再生式吸附式热泵的概念设计”,AIAA论文99-0465,1999年)将吸附式(固体蒸汽)热泵确定为最适合此应用的两种技术之一,另一个是带有高效离心压缩机的机械蒸汽压缩装置。为了适当地为吸附式热泵的详细设计的创建做序,本研究回顾了吸附式热泵的最新技术水平,特别是最近开发的效率更高的蓄热式变体。优点的主要指标是冷却的性能系数(COP_c)和比冷却功率。非蓄热式吸附热泵的COP_c只有0.3到0.4,而再生设计的COP_c为1.1,废热的再生率为70%。注意力集中在最大化总传热系数和最小化最关键组分(吸附床)的非吸附剂质量上,同时保持足够的蒸汽渗透性。这涉及建立穿过床层的热波温度梯度,从而使传热和产生熵的温度差最小化。产生了许多新颖的设计。研究最多的吸附剂是沸石(一类高度纳米多孔的矿物),活性石墨和硅胶。最受关注的制冷剂是氨,甲醇和水。

著录项

  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2005年第4期|p.471-485|共15页
  • 作者

    M. A. Lambert; B. J. Jones;

  • 作者单位

    San Diego State University, San Diego, California 92182-1323;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 理论物理学;
  • 关键词

  • 入库时间 2022-08-18 03:01:38

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