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Proceedings Paper

Design and material aspects for thermoelectric energy harvesting devices in aircrafts
Author(s): A. Elefsiniotis; N. Kokorakis; Th. Becker; U. Schmid
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Paper Abstract

Greener, more power efficient technologies as well as cost reduction are driving forces in energy efficient systems. Energy autonomous wireless health monitoring systems can potentially reduce aircraft maintenance costs by requiring no conventional power supply or supervision and by providing information of the health of an aircraft without human interaction. Thermoelectric energy harvesting seems the best choice for aircraft related applications, since sufficient energy can be generated to power up a wireless sensor node. The general concept is based on an artificially enhanced temperature difference across a thermoelectric generator (TEG), which is created by attaching one side to the fuselage and the other side to a thermal mass, which, in this case, is a phase change material. In detail, two different geometries and three different container materials are evaluated. As input and output parameters, the temperature profiles as well as the voltage of the TEGs are given. The output power and the total energy are determined by connecting a load resistor in parallel. Furthermore, the power to weight ratio for each combination is provided according to theoretical considerations and experimental tests done in a climate chamber mimicking a real flight profile.

Paper Details

Date Published: 17 May 2013
PDF: 8 pages
Proc. SPIE 8763, Smart Sensors, Actuators, and MEMS VI, 87631N (17 May 2013); doi: 10.1117/12.2017311
Show Author Affiliations
A. Elefsiniotis, EADS IW Deutschland (Germany)
N. Kokorakis, EADS IW Deutschland (Germany)
Th. Becker, EADS IW Deutschland (Germany)
U. Schmid, Vienna Univ. of Technology (Austria)


Published in SPIE Proceedings Vol. 8763:
Smart Sensors, Actuators, and MEMS VI
Ulrich Schmid; José Luis Sánchez de Rojas Aldavero; Monika Leester-Schaedel, Editor(s)

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