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undergraduate thesis
Avionski motor GEnX
2024. urn:nbn:hr:190:986763
Licul, Philippe
University of Rijeka
Faculty of Engineering
Department of Thermodynamics and Energy Engineering

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Licul, P. (2024). Avionski motor GEnX (Undergraduate thesis). Rijeka: University of Rijeka, Faculty of Engineering. Retrieved from https://urn.nsk.hr/urn:nbn:hr:190:986763

Licul, Philippe. "Avionski motor GEnX." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2024. https://urn.nsk.hr/urn:nbn:hr:190:986763

Licul, Philippe. "Avionski motor GEnX." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2024. https://urn.nsk.hr/urn:nbn:hr:190:986763

Licul, P. (2024). 'Avionski motor GEnX', Undergraduate thesis, University of Rijeka, Faculty of Engineering, accessed 09 January 2025, https://urn.nsk.hr/urn:nbn:hr:190:986763

Licul P. Avionski motor GEnX [Undergraduate thesis]. Rijeka: University of Rijeka, Faculty of Engineering; 2024 [cited 2025 January 09] Available at: https://urn.nsk.hr/urn:nbn:hr:190:986763

P. Licul, "Avionski motor GEnX", Undergraduate thesis, University of Rijeka, Faculty of Engineering, Rijeka, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:190:986763

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Metadata
TitleAvionski motor GEnX
Title (english)Aircraft Engine GEnX
AuthorPhilippe Licul
MentorTomislav Senčić (mentor)
Committee memberSamir Žic (predsjednik povjerenstva)
Committee memberTomislav Senčić (član povjerenstva)
GranterUniversity of Rijeka
Faculty of Engineering
(Department of Thermodynamics and Energy Engineering)
Rijeka
Defense date and country2024-09-12, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Process Energy Engineering
Abstract
Na početku rada opisana su otkrića i inovacije u povijesnom razvoju plinskih turbina koje su prethodile razvitku današnjih modernih zrakoplovnih motora. Opisan je značaj turbo-ventilatorskih motora za razvoj zračnog putničkog prijevoza te njihova unaprijeđenja i poteškoće pri razvoju. Napravljen je tehnički opis GEnX motora pri čemu je objašnjen njegov princip rada. Opisani su glavni dijelovi motora i njihova mnogobrojna unaprijeđenja i prednosti. Proveden je termodinamički proračun u kojemu je opisan Braytonov kružni proces GEnX motora. Dobivene su karakteristične točke procesa i specifični radovi ventilatora te niskotlačnih i visokotlačnih kompresora i turbina. Temeljem dobivenih podataka izračunati su pretičak zraka, specifična potrošnja goriva te iskoristivost procesa. Napravljen je sklopni crtež GEnX-1B-70 motora s glavnim dijelovima i shema pomoćnih sustava.
Abstract (english)
At the beginning of this work, the discoveries and innovations in the historical development of gas turbines that preceded the development of today’s modern aircraft engines are described. The importance of turbo-fan engines for the development of air passenger transport and their improvements and difficulties during development is stated. A technical description of the GEnX engine is made, explaining its working principles. The main parts of the engine and their many improvements and advantages are described. A thermodynamic analysis of the engine is carried out in which the Brayton cycle is described, the characteristic points of the process are calculated and specific works of the fan, low- and high-pressure compressors and turbines are obtained. Based on the obtained data, excess air, specific fuel consumption and the efficiency of the process are calculated. An assembly drawing of the GEnX-1B-70 engine with its main parts and an auxiliary systems schematics was made.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:190:986763
Study programmeTitle: Mechanical Engineering
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence Attribution 4.0 International (CC BY 4.0) icon
Created on2024-09-11 11:06:21