Pregled bibliografske jedinice broj: 1125531
Small Piston Engine Aircraft Vibration Measurement and Analysis
Small Piston Engine Aircraft Vibration Measurement and Analysis // 2020 43rd International Convention on Information, Communication and Electronic Technology (MIPRO) - Proceedings / Skala, Karolj (ur.).
Opatija, Hrvatska: Institute of Electrical and Electronics Engineers (IEEE), 2020. str. 2029-2034 doi:10.23919/MIPRO48935.2020.9245202 (pozvano predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
CROSBI ID: 1125531 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Small Piston Engine Aircraft Vibration
Measurement and Analysis
Autori
Juretić, Fabijan ; Gerhardinger, David ; Domitrović, Anita ; Ivošević, Jurica
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
2020 43rd International Convention on Information, Communication and Electronic Technology (MIPRO) - Proceedings
/ Skala, Karolj - : Institute of Electrical and Electronics Engineers (IEEE), 2020, 2029-2034
ISBN
978-953-233-099-1
Skup
43rd International Convention on Information and Communication Technology, Electronics and Microelectronics (MIPRO 2020)
Mjesto i datum
Opatija, Hrvatska, 28.09.2020. - 02.10.2020
Vrsta sudjelovanja
Pozvano predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
piston engine aircraft ; vibration ; Arduino ; operation ; instrument ; accelerometer ; sensors
Sažetak
This paper is focused on vibrations of a small aircraft with piston engine in operation. The aircraft Cessna 172R is chosen for measurement and analysis of vibration. The paper describes sources of vibration, such as landing gear vibrations, powerplant and propeller vibration, which make a significant contribution to vibration of the whole system, aerodynamic vibration etc. Considering importance of vibration on an aircraft in operation, equipment for measuring vibration is assembled. Equipment, e.g., the measuring set consists of one Arduino UNO board, a tilt sensor SW-420 and a ADXL345 accelerometer. The measuring set is mounted on the aircraft, and data is collected during flight. The collected data is analyzed and shown in charts.
Izvorni jezik
Engleski
Znanstvena područja
Tehnologija prometa i transport, Zrakoplovstvo, raketna i svemirska tehnika
POVEZANOST RADA
Ustanove:
Fakultet prometnih znanosti, Zagreb
Citiraj ovu publikaciju:
Časopis indeksira:
- Web of Science Core Collection (WoSCC)
- Conference Proceedings Citation Index - Science (CPCI-S)
- Scopus