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Title:ELEKTRIČNI VLAČILEC ZA ŠPORTNA LETALA
Authors:ID Dolinar, Andrej (Author)
ID Belšak, Aleš (Mentor) More about this mentor... New window
ID Ulbin, Miran (Comentor)
Files:.pdf UNI_Dolinar_Andrej_2012.pdf (4,33 MB)
MD5: DBFE509C73A76AA7A04FFA0A23AD0305
PID: 20.500.12556/dkum/44b76f49-e0ec-4a36-af62-75d70835fbf6
 
Language:Slovenian
Work type:Undergraduate thesis
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Abstract:V diplomski nalogi je predstavljeno dimenzioniranje električnega vlačilca za lahka športna letala. Vlačilec je namenjen za obratovanje v okviru vnaprej predpisanih tehničnih omejitev, vezanih na velikost in maso letal. V prvem delu diplomske naloge so predstavljeni ti okvirji, predvidene obremenitve, pogoji uporabe in zahteve za dimenzioniranje. Temu sledi dimenzioniranje pogonskega sklopa naprave. Za tem je na vrsti konstruiranje same naprave na podlagi teh zahtev s pomočjo CAD programske opreme. Poseben poudarek pri konstruiranju je bil dan na izbiro samih elementov, saj je vlačilec je v veliki meri sestavljen iz standardnih in lahko dobavljivih komponent, kar ima seveda velik vpliv na ceno in hitrost izdelave same naprave. Rezultat diplomskega dela je podrobno izdelan načrt za izdelavo učinkovitega električnega vlačilca, primernega tudi za delovanje v zaprtih prostorih.
Keywords:Električni, vlačilec, letala, konstruiranje, verižni
Place of publishing:Maribor
Publisher:[A. Dolinar]
Year of publishing:2012
PID:20.500.12556/DKUM-23586-e0faef41-3d69-e2b2-e1f6-8694870daebf New window
UDC:621.867.1-045.43(043.2)
COBISS.SI-ID:16933654 New window
NUK URN:URN:SI:UM:DK:IUDA394F
Publication date in DKUM:29.06.2012
Views:2274
Downloads:384
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FS
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Secondary language

Language:English
Title:ELECTRIC AIRCRAFT TUG FOR LIGHT SPORT AIRCRAFT
Abstract:The thesis is about the design and construction of electric aircraft tug for light general aviation aircraft. The tug is meant to be operated within some constraints concerning the size and weight of aircraft towed. In the first part of this work, there are some basics about existing aircraft tugs, the physics of airplane towing, expected working conditions, expected performance etc. Next part is designing of the drive train. Following that, the virtual model of the tug is created with the help of CAD software. One of the main goals of the construction was the use of standard and easily available parts, resulting in lower price and faster fabrication of the device. The end result of this thesis is a detailed plan for construction of efficient electric aircraft tug, suited for indoor and outdoor use.
Keywords:Electric, tug, aircraft, airplane, design


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