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Title:Integracija turbopropelerskega motorja v zrakoplov Gogetair ONE : magistrsko delo
Authors:ID Slapnik, Jaka (Author)
ID Kramberger, Janez (Mentor) More about this mentor... New window
ID Vrečko, Igor (Mentor) More about this mentor... New window
Files:.pdf MAG_Slapnik_Jaka_2026.pdf (6,28 MB)
MD5: 2992F16973980ECE37D554E0027B53B4
 
Language:Slovenian
Work type:Master's thesis/paper
Typology:2.09 - Master's Thesis
Organization:FS - Faculty of Mechanical Engineering
Abstract:V magistrskem delu je predstavljena tehnična in ekonomska validacija integracije turbopropelerskega motorja Turbotech TP-R90 v zrakoplov Gogetair ONE. Za zagotavljanje strukturne celovitosti so bili razviti in statično testirani novi nosilci motorja ter dodatne opreme v skladu s predpisi CS-23 in CS-VLA 561. Izvedena je bila tudi primerjalna analiza skupnih stroškov lastništva (TCO). Dokazano je bilo, da je nova izvedba G750TP v analiziranem 10-letnem modelu dolgoročno stroškovno učinkovitejša od obstoječega modela z batnim motorjem, kar potrjuje tehnično izvedljivost in ekonomsko upravičenost projekta
Keywords:Gogetair G750TP, Turbotech TP-R90, integracija motorja, statično testiranje, CS-23, analiza stroškov (TCO)
Place of publishing:Maribor
Place of performance:Maribor
Publisher:[J. Slapnik]
Year of publishing:2026
Number of pages:1 spletni vir (1 datoteka PDF (XIV, 82 f.))
PID:20.500.12556/DKUM-97520 New window
UDC:629.7.035.35+657.478.8(043.2)
COBISS.SI-ID:275566339 New window
Publication date in DKUM:10.04.2026
Views:233
Downloads:28
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FS
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Licences

License:CC BY-NC-ND 4.0, Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International
Link:http://creativecommons.org/licenses/by-nc-nd/4.0/
Description:The most restrictive Creative Commons license. This only allows people to download and share the work for no commercial gain and for no other purposes.
Licensing start date:15.03.2026

Secondary language

Language:English
Title:Integration of a turboprop engine into the Gogetair ONE aircraft
Abstract:In this master's thesis, the technical and economic validation of the integration of a Turbotech TP-R90 turboprop engine into the Gogetair ONE aircraft is presented. To ensure structural integrity, new engine and auxiliary equipment mounts were developed and statically tested in accordance with CS-23 and CS-VLA 561 regulations. A comparative Total Cost of Ownership (TCO) analysis was also performed. The new G750TP version was proven to be more cost-effective in the long term in the analyzed 10-year model than the existing piston-engine model, confirming the project's technical feasibility and economic viability.
Keywords:Gogetair G750TP, Turbotech TP-R90, engine integration, static load testing, CS-23, Total Cost of Ownership (TCO)


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