| Literature DB >> 33266489 |
Saša Zelenika1,2, Zdenek Hadas3, Sebastian Bader4, Thomas Becker5, Petar Gljušćić1,2, Jiri Hlinka3, Ludek Janak3, Ervin Kamenar1,2, Filip Ksica3, Theodora Kyratsi6, Loucas Louca6, Miroslav Mrlik7, Adnan Osmanović8, Vikram Pakrashi9, Ondrej Rubes3, Oldřich Ševeček3, José P B Silva10, Pavel Tofel11, Bojan Trkulja12, Runar Unnthorsson13, Jasmin Velagić8, Željko Vrcan1.
Abstract
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.Entities:
Keywords: airplane; energy harvesting; kinetic; non-destructive evaluation; power management; smart skin; solar; thermoelectric
Year: 2020 PMID: 33266489 PMCID: PMC7700503 DOI: 10.3390/s20226685
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.576