Vibration Power Generator for Aeronautics Applications
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F08%3APU74391" target="_blank" >RIV/00216305:26210/08:PU74391 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Vibration Power Generator for Aeronautics Applications
Original language description
This paper deals with an alternative for supplying wireless sensors with energy in aeronautic applications. It shows that ambient energy can be a suitable source for the electrical energy of several wireless sensors with an expected power consumption ofseveral mW. Mechanical vibrations of a helicopter are used as a source for an energy harvesting devices, where electrical power is generated by use of a vibration power generator. The generator feeds embedded wireless sensor without or as a supplement tothe use of primary battery in some aeronautics applications. The generator is a maintenance-free device and it extends the lifetime of the wireless sensor in case that the generator and the wireless sensor are placed in an environment which is excited by sufficient vibration during the flight operation of the helicopter.
Czech name
Vibration Power Generator for Aeronautics Applications
Czech description
This paper deals with an alternative for supplying wireless sensors with energy in aeronautic applications. It shows that ambient energy can be a suitable source for the electrical energy of several wireless sensors with an expected power consumption ofseveral mW. Mechanical vibrations of a helicopter are used as a source for an energy harvesting devices, where electrical power is generated by use of a vibration power generator. The generator feeds embedded wireless sensor without or as a supplement tothe use of primary battery in some aeronautics applications. The generator is a maintenance-free device and it extends the lifetime of the wireless sensor in case that the generator and the wireless sensor are placed in an environment which is excited by sufficient vibration during the flight operation of the helicopter.
Classification
Type
D - Article in proceedings
CEP classification
JA - Electronics and optoelectronics
OECD FORD branch
—
Result continuities
Project
—
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2008
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of the EUSPEN 10th anniversary international conference Volume I - Volume II
ISBN
978-0-9553082-5-3
ISSN
—
e-ISSN
—
Number of pages
5
Pages from-to
—
Publisher name
Copy & Druck Wein
Place of publication
Zurich
Event location
Zurich
Event date
May 18, 2008
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
—