Publication detail

Model-based design and test of vibration energy harvester for aircraft application

HADAŠ, Z. VETIŠKA, V. HUZLÍK, R. SINGULE, V.

Original Title

Model-based design and test of vibration energy harvester for aircraft application

Type

journal article in Web of Science

Language

English

Original Abstract

This paper deals with a development process of a vibration energy harvesting device in aircraft applications. The vibration energy harvester uses ambient energy of mechanical vibration and it provides an autonomous source of energy for wireless sensors or autonomous applications. This application presents a complex engineering problem and the vibration energy harvester consists of precise mechanical part, electro-mechanical converter, electronics and a powered application. It can be perceive as a mechatronic system and a mechatronic approach was used for development of our vibration energy harvester. An essential step of development process is simulation modeling which is based on mechatronic approach. Presented model-based design of vibration energy harvester is very useful during development process and the whole development process of the autonomous energy source is presented in this paper. The main aim of the paper is an introduction of our development methodology and our approach is presented on a sample of the vibration energy harvester for aircraft applications under project ESPOSA.

Keywords

Energy Harvesting, Model-based design, vibration energy harvester, simulation modeling

Authors

HADAŠ, Z.; VETIŠKA, V.; HUZLÍK, R.; SINGULE, V.

RIV year

2014

Released

9. 1. 2014

Publisher

Springer Berlin Heidelberg

Location

Berlin

ISBN

0946-7076

Periodical

Microsystem Technologies

Year of study

20

Number

4-5

State

Federal Republic of Germany

Pages from

841

Pages to

843

Pages count

13

BibTex

@article{BUT105771,
  author="Zdeněk {Hadaš} and Vojtěch {Vetiška} and Rostislav {Huzlík} and Vladislav {Singule}",
  title="Model-based design and test of vibration energy harvester for aircraft application",
  journal="Microsystem Technologies",
  year="2014",
  volume="20",
  number="4-5",
  pages="841--843",
  doi="10.1007/s00542-013-2062-y",
  issn="0946-7076"
}