prikaz prve stranice dokumenta Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu
  Download
PDF 2.22 MB
undergraduate thesis
Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. urn:nbn:hr:119:388433
Martinović, Ivan
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

Martinović, I. (2021). Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:388433

Martinović, Ivan. "Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:388433

Martinović, Ivan. "Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:388433

Martinović, I. (2021). 'Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 15 January 2025, https://urn.nsk.hr/urn:nbn:hr:119:388433

Martinović I. Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2021 [cited 2025 January 15] Available at: https://urn.nsk.hr/urn:nbn:hr:119:388433

I. Martinović, "Tehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:119:388433

Metadata
TitleTehnologija primjene vodika kao pogonskog goriva u zrakoplovstvu
Title (english)Technology of application of hydrogen as a power propellant in aviation
AuthorIvan Martinović
MentorAnita Domitrović (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberTino Bucak (član povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2021-09-14, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Zrakoplovstvo se suočava s izazovom značajnog reduciranja emisija stakleničkih plinova. Promjene će biti radikalne s obzirom da je nužno uvesti nova održiva pogonska goriva. Vodik, zbog svojih izvanrednih svojstava, a i činjenice da može biti proizveden bez stakleničkih emisija, smatra se da može biti rješenje za dekarbonizaciju u smislu potpunog eliminiranja ugljikovih oksida iz zrakoplovne industrije. Izazov održive proizvodnje zelenog vodika treba savladati u nadolazećim godinama. Također, vodik zahtijeva posebnu aerodromsku i transportnu infrastrukturu. Pogonski sustavi na vodik značajno su tiši od postojećih današnjih i emitiraju manje ostalih popratnih plinova. Postoje dva tipa pogonskih sustava na vodik, motori s unutarnjim izgaranjem i PEM gorivi članci. U radu su detaljnije opisana oba ova tipa pogonskih sustava te su navedeni segmenti zrakoplova u kojima bi ih bilo optimalno ugraditi s obzirom na njihove karakteristike.
Abstract (english)
Aviation is facing the challenge of significantly reducing greenhouse gas emissions. The changes will be radical as it is necessary to introduce new sustainable fuels. Hydrogen, due to its outstanding properties, and the fact that it can be produced without greenhouse gas emissions, is considered to be a solution for decarbonization in terms of the complete elimination of carbon oxides from the aviation industry. The challenge of sustainable green hydrogen production needs to be overcome in the coming years. Also, hydrogen requires special airport and transport infrastructure. Hydrogen power systems are significantly quieter than today's ones and emit less other associated gases. There are two types of hydrogen propulsion systems, internal combustion engines and PEM fuel cells. This thesis describes in more detail both of these types of propulsion systems and lists the segments of aircraft in which it would be optimal to install them due to their characteristics.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:388433
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 on2021-10-11 12:06:49