prikaz prve stranice dokumenta Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora
Embargo period 2026-09-26
undergraduate thesis
Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. urn:nbn:hr:235:320592
Novosel, Marko
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

Cite this document

Novosel, M. (2024). Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:320592

Novosel, Marko. "Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:320592

Novosel, Marko. "Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:320592

Novosel, M. (2024). 'Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 16 January 2025, https://urn.nsk.hr/urn:nbn:hr:235:320592

Novosel M. Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2024 [cited 2025 January 16] Available at: https://urn.nsk.hr/urn:nbn:hr:235:320592

M. Novosel, "Metoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:235:320592

Metadata
TitleMetoda za polijetanje zrakoplova sa smanjenom snagom mlaznog motora
Title (english)Aeroplane take-off method with reduced jet engine power
AuthorMarko Novosel
MentorTessa Uroić (mentor)
Committee memberMilan Vrdoljak (predsjednik povjerenstva)
Committee memberDario Zlatar (član povjerenstva)
Committee memberDarko Ivančević (član povjerenstva)
Committee memberRudolf Tomić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2024-09-26, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Control
Abstract
Avioni koji se koriste prvobitno u civilne svrhe u velikom značaju ovise o načinu i kvaliteti, kako planskog tako i linijskog održavanja. Cilj ovog rada je usporediti metodu polijetanja sa štednim potiskom s utjecajem nekolicine polijetanja s maksimalnim mogućnostima mlaznog motora. Analiziraju se podaci realnih ciklusa aktivne aviokompanije u usporedbi s teorijskim saznanjima. U tim podacima analizira se teorijska sila potiska i sila potiska koja je dobivena metodom polijetanja s štednim potiskom. Utjecaj glavnog parametra za praćenje ekonomski isplativog održavanja će pokazati koliko je efektivno stanje mlaznog motora poboljšano u periodu kada se koristi štedna metoda. U zadnjim dijelovima rada, analizirane su prednosti, nedostatci i ekonomska isplativost takvog načina operiranja avionom.
Abstract (english)
Aircraft originally used for civil purposes largely depend on the method and quality of both scheduled and routine maintenance. The aim of this paper is to compare the method of fuel-efficient thrust takeoff with the impact of multiple takeoffs using the jet engine's maximum capabilities. Data from real cycles of an active airline are analyzed and compared with theoretical knowledge. In these data, the theoretical thrust force is analyzed alongside the thrust force obtained using the fuel-efficient thrust takeoff method. The impact of the main parameter for monitoring cost-effective maintenance will demonstrate how much the engine's performance improves during the period when the fuel-saving method is applied. In the final sections of the paper, the advantages, disadvantages, and economic feasibility of this aircraft operating method are analyzed.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:320592
Study programmeTitle: Aerospace Engineering
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva i svemirske tehnike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva i svemirske tehnike)
Type of resourceText
File originBorn digital
Access conditionsEmbargoed access
Embargo expiration date: 2026-09-26
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Created on2024-09-28 15:15:36