Design and Fabrication of Heat Storage Thermoelectric Harvesting Devices

被引:77
作者
Kiziroglou, Michail E. [1 ]
Wright, Steven W. [1 ]
Toh, Tzern T. [1 ]
Mitcheson, Paul D. [1 ]
Becker, Th. [2 ]
Yeatman, Eric M. [1 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Elect & Elect Engn, London SW7 2BT, England
[2] EADS Innovat Works, Elect & Syst Integrat, D-81663 Munich, Germany
关键词
Avionics; energy harvesting; heat storage; phase-change material (PCM); thermoelectric; wireless sensor networks;
D O I
10.1109/TIE.2013.2257140
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Thermoelectric energy harvesting requires a substantial temperature difference Delta T to be available within the device structure. This has restricted its use to particular applications such as heat engine structural monitoring, where a hot metal surface is available. An alternative approach is possible in cases where ambient temperature undergoes regular variation. This involves using a heat storage unit, which is filled with a phase-change material (PCM), to create an internal spatial temperature difference from temperature variation in time. In this paper, key design parameters and a characterization methodology for such devices are defined. The maximum electrical energy density expected for a given temperature range is calculated. The fabrication, characterization, and analysis of a heat storage harvesting prototype device are presented for temperature variations of a few tens of degrees around 0 degrees C, corresponding to aircraft flight conditions. Output energy of 105 J into a 10-Omega matched resistive load, from a temperature sweep from +20 degrees C to -21 degrees C, then to +25 degrees C is demonstrated, using 23 g of water as the PCM. The proposed device offers a unique powering solution for wireless sensor applications involving locations with temperature variation, such as structural monitoring in aircraft, industrial, and vehicle facilities.
引用
收藏
页码:302 / 309
页数:8
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