undergraduate thesis
Practical Design of Small Aircraft Pitot-static System

Denis Likić (2016)
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics
Metadata
TitleKonstrukcija pitot-statičkog sustava malog zrakoplova
AuthorDenis Likić
Mentor(s)Jurica Ivošević (thesis advisor)
Abstract
Svaki pilot zrakoplova neovisno o tome upravlja li velikim ili malim zrakoplovom, mora u kokpitu imati instrumente koji će mu osigurati ispravno prikazivanje parametara kao što su brzina leta, visina leta i vertikalna brzina penjanja odnosno spuštanja, kako bi pilot mogao sigurno upravljati letom. Važana veličina koja omogućava prikazivanje traženih parametara na instrumentima za upravljanje letom, i prema kojemu su ti instrumenti u konačnici i konstruirani je tlak zraka. Tlak zraka ima promjenjiva svojstva koja ovise o atmosferi, odnosno o njenome stanju. U ovom radu obrađeni su i analizirani instrumenti za upravljanje letom, te je uz pomoć praktične izvedbe prikazan odnos tlaka zraka i vrijednosti koju instrument prikazuje. Raščlanjene su sve sastavnice mjernog lanca, i detaljno analizirane kako bi se mogao donijeti zaključak kako cijeli sustav u stvarnosti funkcionira.
Keywordsflying instruments flight manouvering air pressure meassure chain
Parallel title (English)Practical Design of Small Aircraft Pitot-static System
Committee MembersJurica Ivošević (committee chairperson)
Tino Bucak (committee member)
Doris Novak (committee member)
Željko Marušić (committee member)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
Lower level organizational unitsDivision of Aeronautics
Department of Aeronautics
PlaceZagreb
StateCroatia
Scientific field, discipline, subdisciplineTECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Study programme typeuniversity
Study levelundergraduate
Study programmeAeronautics
Academic title abbreviationuniv. bacc. ing. aeronaut.
Genreundergraduate thesis
Language Croatian
Defense date2016-09-13
Parallel abstract (English)
Every pilot of an aircraft no matter if he is flying a large or a small aircraft, must have in his cockpit flying instruments that will provide correct indications of parameters like airspeed, altitude and vertical climbing or descending speed which will help the pilot with safe manouvering. An important unit that provides the requested parameters on the instruments and for which the instruments are ultimately made is air pressure. Air pressure has changing properties which depend on the state of atmosphere. In this paper, analysis and elaborations have been made of instruments for safe manouvering, and with a working model a demonstration has been made showing the differences between air pressure and the value that is shown on the instrument. A detailed description of every part of the meassure chain has been made so that a conclusion can be made about how the whole system functions in reality.
Parallel keywords (Croatian)zrakoplovni instrumenti upravljanje letom tlak zraka mjerni lanac
Resource typetext
Access conditionOpen access
Terms of usehttp://rightsstatements.org/vocab/InC/1.0/
URN:NBNhttps://urn.nsk.hr/urn:nbn:hr:119:318796
CommitterMojca Brenko-Puzak