Detail publikace

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

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

Originální název

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

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

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

Autoři

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

Rok RIV

2014

Vydáno

9. 1. 2014

Nakladatel

Springer Berlin Heidelberg

Místo

Berlin

ISSN

0946-7076

Periodikum

Microsystem Technologies

Ročník

20

Číslo

4-5

Stát

Spolková republika Německo

Strany od

841

Strany do

843

Strany počet

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"
}