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undergraduate thesis
Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. urn:nbn:hr:119:728041
Horvat, Danijel
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Horvat, D. (2016). Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:728041

Horvat, Danijel. "Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:728041

Horvat, Danijel. "Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:728041

Horvat, D. (2016). 'Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 24 July 2024, https://urn.nsk.hr/urn:nbn:hr:119:728041

Horvat D. Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2016 [cited 2024 July 24] Available at: https://urn.nsk.hr/urn:nbn:hr:119:728041

D. Horvat, "Analiza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:119:728041

Metadata
TitleAnaliza perfomansi koncepcije mlaznih motora visokog stupnja optočnosti
Title (english)Performance Analysis of the Turbofan Engine with High By-Pass Ratio
AuthorDanijel Horvat
MentorAnita Domitrović (mentor)
Committee memberŽeljko Marušić (predsjednik povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
Committee memberTino Bucak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2016-09-13, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Uvođenjem reduktora u konstrukciju mlaznih motora s visokim stupnjem optočnosti koji se nalazi između ventilatora i niskotlačnog kompresora omogućuje da se svaki modul (ventilator, niskotlačni kompresor i niskotlačna turbina koja ga pogoni) vrte svojom optimalnom brzinom vrtnje. Za veću efikasnost propulzije ventilator ima manju brzinu vrtnje dok se niskotlačni kompresor i turbina vrte većim brzinama od konvencionalnih mlaznih motora sa visokim stupnjem optočnosti čime se povečava učinkovitost motora. Smanjenjem brzine vrtnje ventilatora smanjuje se buka motora, korištenjem napredne tehnologije u izradi i dizajnu komore izgaranja treće generacije TALON X, te naprednim dizajnom lopatica turbine koje učinkovitije pretvaraju energiju ispušnih plinova u mehanički rad smanjena je potrošnja goriva i emisije ispušnih plinova. Većom brzinom vrtnje jezgre motora (kompresora i turbine) povećana je njihova učinkovitost koja dozvoljava manji broj stupnjeva kompresora i turbine ćime se smanjuju troškovi održavanja i masa motora. U ovom radu analiziraju se performanse i tehničke specifičnosti nove generacije motora sa vrlo visokim stupnjem optočnosti PW1100G-JM i uspoređuju se sa konvencionalnim motorom visokog stupnja optočnosti CFM56-5A1.
Abstract (english)
Introducing reduction gear in the design of high bypass turbofan jet engine which is placed between fan and low pressure compresor, enables for each module (fan, low pressure compresor and low pressure turbine which drives it) to rotare at optimum speed. For achieving higher propulsive efficiency, rotation speed of fan is reduced and rotation speed of low pressure compresor and it's turbine is increased compared to conventional high bypass turbofan engine enabling higher engine efficiency. Engine noise is reduced by reducing rotational speed of fan, introducing new technology in manufacturing and design of third generation combustor TALON X and advanced design of turbine blades which are more efficient in converting gas energy in mechanical work, engine consumption and exhaust gas emissions are reduced. Engine core efficiency (compressor and turbine) is increased by increasing it's speed of rotation, therefore required stages in compresor and turbine are reduced which reduces maintenance cost's and mass. In this paper there are comparison of the performance and technical specification between new generation of the ultra high bypass ratio turbofan engine PW1100G-JM and conventional high bypass turbofan engine CFM56-5A1.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:728041
Study programmeTitle: Aeronautics
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2016-09-19 13:24:18