Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora

undergraduate thesis

• Title (english): Performance Calculations of Airbus A320 Aircraft with One Engine Inoperative
• Author: Danijel Šimon
• Mentor: Davor Franjković (mentor)
• Committee member: Anita Domitrović (predsjednik povjerenstva)
• Committee member: Tomislav Radišić (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: 2018-03-06, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

Ovaj rad bavi se problematikom određivanja performansi zrakoplova Airbus A320 u slučaju otkaza jednog od dvaju njegovih motora. Objašnjena je važnost određivanja performansi nekog zrakoplova u takvom slučaju, zakonski zahtjevi performansi s jednim neispravnim motorom, oblici i uzroci otkaza mlaznih motora te općenite karakteristike Airbusa A320. Prikazan je i objašnjen izračun performansi navedenog zrakoplova s jednim neispravnim motorom u fazama polijetanja, penjanja, krstarenja te spuštanja, uz konkretne primjere izračunavanja parametara kao npr. maksimalne dopuštene mase tijekom polijetanja, potrebne vrijednosti potiska motora, potrebne duljine zaleta u polijetanju, vremena penjanja i spuštanja, potrošnje goriva, brzine leta, optimalne i maksimalne visine leta te specifičnog doleta. Performanse u letu s jednim neispravnim motorom uspoređene su s performansama u letu s oba motora ispravna. Opisane su potrebne procedure i postupci posade zrakoplova u slučaju otkaza motora u različitim fazama leta.

Abstract (english)

This paper describes the determination of the performance of the Airbus A320 aircraft in case of failure of one of its two engines. The importance of determination of performance in such cases is described, along with the legal performance requirements, modes and causes of jet engine failures and general characteristics of the Airbus A320 aircraft. The calculation of performance of the mentioned aircraft with one engine inoperative is explained for the take-off, climb, cruise and descent phases of flight, with examples of the calculation of parameters such as maximum take-off mass, required engine thrust, take-off distance required, time for climb and descent, fuel flow, airspeed, optimum and maximum altitude, and specific range. The performance with one engine inoperative is compared with the performance with all engines operative. The required procedures and acts of the crew after engine failure are described for different phases of flight.

• Keywords: Airbus A320; performanse; otkaz motora; višemotorni zrakoplov
• Keywords (english): Airbus A320; performance; engine failure; multi-engine aeroplane
• Language: croatian
• URN:NBN: urn:nbn:hr:119:898043
• 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
• Created on: 2018-03-26 13:55:06