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Title: Vacuum enclosures for solar thermal panels Part 1: Fabrication and hot-box testing
Authors: Arya, Farid
Moss, Roger
Hyde, Trevor
Shire, Stan
Henshall, Paul
Eames, Philip C.
Keywords: Vacuum enclosure
Vacuum glazing
Solar absorber
Vacuum insulation
Evacuated flat plate solar collector
Ultrasonic soldering
Hot box calorimeter
Issue Date: 2018
Publisher: Elsevier © The Authors
Citation: ARYA, F. ... et al, 2018. Vacuum enclosures for solar thermal panels Part 1: Fabrication and hot-box testing. Solar Energy, 174, pp.1212-1223.
Abstract: Non-concentrating solar thermal collectors are generally available in two forms, flat plate or evacuated tube. Recently a third configuration, the evacuated flat plate, has attracted interest due to enhanced performance and aesthetic characteristics. By isolating a solar absorber in a vacuum space (<1 Pa) heat loss from the absorber can be minimized resulting in improved efficiency. In addition the improved thermal insulation performance of evacuated panels over conventional glazing systems makes them attractive solutions for integration into energy efficient building facades. This two part paper describes the design, construction techniques and thermal performance of two vacuum enclosures, fabricated at Ulster University, as prototype components for evacuated flat solar collectors. The first enclosure consists of two glass panes sealed to an edge spacer and separated by an array of support pillars on a regular square grid to form a narrow evacuated space. The second enclosure incorporates an uncooled copper sheet to represent a solar thermal absorber. The enclosures were tested at three conditions i.e. with an internal pressure of high vacuum (0.0021 Pa), low vacuum (8.4 Pa) and no vacuum (atmospheric pressure). Part 1 of this paper describes the fabrication process for the vacuum enclosures and the measurement of their thermal insulation properties using a hot box calorimeter. The theory of heat transfer through an enclosure with support pillars is discussed; experimental results are compared with mathematical models predictions. A fabrication methodology has been successfully established and a U-value of 1.35 W/m2 K for an enclosure with an internal pressure of 0.0021 Pa has been demonstrated. The experimental results are in good agreement with the predictions. Part 2 of this paper describes solar simulator testing of the enclosure containing a copper plate. The highest stagnation temperature (121.8 °C) was reached under steady-state conditions in the high vacuum test and was in good agreement with predictions. The transient plate and glass surface temperatures were measured and found to be consistent with the predicted curves.
Description: This is an Open Access Article. It is published by Elsevier under the Creative Commons Attribution 4.0 International Licence (CC BY). Full details of this licence are available at: https://creativecommons.org/licenses/by/4.0/
Sponsor: The authors are grateful to the Engineering and Physical Sciences Research Council (EPSRC) for funding this work as part of a collaborative programme between the University of Warwick, Loughborough University and Ulster University, reference EP/K009915/1, EP/K010107/1 and EP/K009230/1.
Version: Published
DOI: 10.1016/j.solener.2018.10.064
URI: https://dspace.lboro.ac.uk/2134/36342
Publisher Link: https://doi.org/10.1016/j.solener.2018.10.064
ISSN: 0038-092X
Appears in Collections:Published Articles (Mechanical, Electrical and Manufacturing Engineering)

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