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A case study of a methodological approach to the verification of UAV propeller performance
ID
Vorotović, Goran
(
Avtor
),
ID
Burazer, Jela
(
Avtor
),
ID
Bengin, Aleksandar
(
Avtor
),
ID
Mitrović, Časlav
(
Avtor
),
ID
Januzović, Miloš
(
Avtor
),
ID
Petrović, Nebojša
(
Avtor
),
ID
Novković, Đorđe
(
Avtor
)
PDF - Predstavitvena datoteka,
prenos
(2,92 MB)
MD5: 8A349FF0121F2ADF52E9D31DF7D52BDB
URL - Izvorni URL, za dostop obiščite
https://www.sv-jme.eu/sl/article/case-study-of-a-methodological-approach-to-the-verification-of-uav-propeller-performances/
Galerija slik
Izvleček
Understanding the behaviour of propeller-driven aircraft has been the primary goal of aviation since the brothers Orville and Wilbur Wright. Traction characteristics, which have over time become dominant in the field of aviation in addition to thrust, both examined and analysed, nevertheless represent a sort of oxymoron in modern aviation. In this sense, the authors of the paper present the possibilities of static performance characteristics and vibrations of aircraft propellers through the analysis of low-powered aircraft. The use of low-powered aircraft as “expendable” material is the reality we live in, but ensuring the safety of their use is the primary goal of the researchers who deal with this issue. Accordingly, the authors of this paper present indications of the methodology of testing the blades of low-power aircraft in the atmosphere with an observation that the same indications can be used with aircraft of higher power, as well as with the aircraft on celestial bodies that have not been tested or available. A test bench for the quantification of thrust, torque, and vibration of small unmanned aerial vehicles’ (UAV) vehicle propellers is presented. The obtained results realistically describe the complex behaviour of propellers in operation.
Jezik:
Angleški jezik
Ključne besede:
propeller
,
traction-dynamic characteristics
,
oscillations
,
acquisition
,
dynamics
Vrsta gradiva:
Članek v reviji
Tipologija:
1.01 - Izvirni znanstveni članek
Organizacija:
FS - Fakulteta za strojništvo
Status publikacije:
Objavljeno
Različica publikacije:
Objavljena publikacija
Leto izida:
2023
Št. strani:
Str. 199-207
Številčenje:
Vol. 69, no. 5/6
PID:
20.500.12556/RUL-146673
UDK:
629.7
ISSN pri članku:
0039-2480
DOI:
10.5545/sv-jme.2022.432
COBISS.SI-ID:
154369795
Datum objave v RUL:
06.06.2023
Število ogledov:
550
Število prenosov:
75
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Objavi na:
Gradivo je del revije
Naslov:
Strojniški vestnik
Skrajšan naslov:
Stroj. vestn.
Založnik:
Zveza strojnih inženirjev in tehnikov Slovenije [etc.], = Association of Mechanical Engineers and Technicians of Slovenia [etc.
ISSN:
0039-2480
COBISS.SI-ID:
762116
Licence
Licenca:
CC BY 4.0, Creative Commons Priznanje avtorstva 4.0 Mednarodna
Povezava:
http://creativecommons.org/licenses/by/4.0/deed.sl
Opis:
To je standardna licenca Creative Commons, ki daje uporabnikom največ možnosti za nadaljnjo uporabo dela, pri čemer morajo navesti avtorja.
Sekundarni jezik
Jezik:
Slovenski jezik
Naslov:
Študija primera metodološkega pristopa k verifikaciji zmogljivosti propelerjev brezpilotnih letalnikov
Ključne besede:
propeler
,
dinamične lastnosti vleka
,
oscilacije
,
zajem podatkov
,
dinamika
Projekti
Financer:
MESTD - Ministry of Education, Science and Technological Development of Republic of Serbia
Program financ.:
TR35046
Številka projekta:
2022451-03-68/2022-14/200105
Financer:
MESTD - Ministry of Education, Science and Technological Development of Republic of Serbia
Program financ.:
TR35045
Številka projekta:
2022451-03-68/2022-14/200105
Financer:
MESTD - Ministry of Education, Science and Technological Development of Republic of Serbia
Program financ.:
TR35040
Številka projekta:
2022451-03-68/2022-14/200105
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