Energy harvesting technologies for structural health monitoring of airplane components - a review

With the aim of increasing the efficiency of maintenance and fuel usage in airplanes, structural health monitoring (SHM) of critical composite structures is increasingly expected and required. The optimized usage of this concept is subject of intensive work in the framework of the EU COST Action CA1...

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Bibliographic Details
Main Author: Zelenika, Saša (author)
Other Authors: Hadas, Zdenek (author), Bader, Sebastian (author), Becker, Thomas (author), Gljušćić, Petar (author), Hlinka, Jiri (author), Janak, Ludek (author), Kamenar, Ervin (author), Ksica, Filip (author), Kyratsi, Theodora (author), Louca, Loucas (author), Mrlik, Miroslav (author), Osmanovic, Adnan (author), Pakrashi, Vikram (author), Rubes, Ondrej (author), Ševecek, Oldrich (author), Silva, José Pedro Basto (author), Tofel, Pavel (author), Trkulja, Bojan (author), Unnthorsson, Runar (author), Velagíc, Jasmin (author), Vrcan, Željko (author)
Format: article
Language:eng
Published: 2020
Subjects:
Energy harvesting
Airplane
Non-destructive evaluation
Kinetic
Thermoelectric
Solar
Smart skin
Power management
Science & Technology
Online Access:http://hdl.handle.net/1822/68601
Country:Portugal
Oai:oai:repositorium.sdum.uminho.pt:1822/68601
Description
Summary:With the aim of increasing the efficiency of maintenance and fuel usage in airplanes, structural health monitoring (SHM) of critical composite structures is increasingly expected and required. The optimized usage of this concept is subject of intensive work in the framework of the EU COST Action CA18203 "Optimising Design for Inspection" (ODIN). In this context, a thorough review of a broad range of energy harvesting (EH) technologies to be potentially used as power sources for the acoustic emission and guided wave propagation sensors of the considered SHM systems, as well as for the respective data elaboration and wireless communication modules, is provided in this work. EH devices based on the usage of kinetic energy, thermal gradients, solar radiation, airflow, and other viable energy sources, proposed so far in the literature, are thus described with a critical review of the respective specific power levels, of their potential placement on airplanes, as well as the consequently necessary power management architectures. The guidelines provided for the selection of the most appropriate EH and power management technologies create the preconditions to develop a new class of autonomous sensor nodes for the in-process, non-destructive SHM of airplane components.

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