Konstrukcija pitot-statičkog sustava malog zrakoplova

undergraduate thesis

• Title (english): Practical Design of Small Aircraft Pitot-static System
• Author: Denis Likić
• Mentor: Jurica Ivošević (mentor)
• Committee member: Tino Bucak (predsjednik povjerenstva)
• Committee member: Doris Novak (član povjerenstva)
• Committee member: Željko Marušić (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2016-09-13, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Aviation, Rocket and Space Technology; Aircraft Construction and Design

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.

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.

• Keywords: zrakoplovni instrumenti; upravljanje letom; tlak zraka; mjerni lanac
• Keywords (english): flying instruments; flight manouvering; air pressure; meassure chain
• Language: croatian
• URN:NBN: urn:nbn:hr:119:318796
• Study programme: Title: 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 resource: Text
• File origin: Born digital
• Access conditions: Open access
• Repository: Faculty of Transport and Traffic Sciences
• Created on: 2016-09-20 13:48:31