Analiza operativnih ograničenja za avion u klasi performansi A

undergraduate thesis

• Title (english): Analysis of Operating Limitations for a Performance Class A Airplane
• Author: Mila Ivanković
• Mentor: Davor Franjković (mentor)
• Committee member: Karolina Krajček Nikolić (predsjednik povjerenstva)
• Committee member: Petar Andraši (član povjerenstva)
• Committee member: Anita Domitrović (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2024-07-02, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

U zrakoplovstvu je naglasak na sigurnosti, te se zbog brojnih avionskih nesreća pokazalo potrebitim propisati i definirati operativna ograničenja. Operativna ograničenja su limiti definirani od strane proizvođača zrakoplova koji će osigurati sigurne letačke operacije zrakoplovom. Ona su propisana od strane proizvođača i nadležnih vlasti, te je nužno pridržavati ih se tijekom svih režima leta. Pri proizvodnji zrakoplova testiranjem čvrstoće njegove konstrukcije i performansi u letu prikupljaju se operativna ograničenja koja je nužno ispisati u pilotske priručnike. Europska agencija za sigurnost zračnog prometa (EASA, European Aviation Safety Agency) određuje regulativu koja propisuje operativna ograničenja. Nadležne zrakoplovne vlasti pojedine države dužne su pratiti primjenu regulative. Na performanse zrakoplova, pa tako i operativna ograničenja, utječu vanjski čimbenici poput različitih atmosferskih stanja i dostupnih duljina uzletno-sletnih staza pri zaletu, polijetanju i slijetanju zrakoplova. Ovaj rad analizira operativna ograničenja masa i brzina.

Abstract (english)

In aviation, the emphasis is on safety, and due to numerous aircraft accidents, it has become necessary to determine and define operational limitations. Operational limitations are limits defined by aircraft manufactures that will ensure safe flight operations. They are prescribed by manufacturer and competent authorities, and it is necessary to adhere to them during all flight regimes. During the production of an aircraft, by testing the strength of its construction and performance in flight, operational limitations are collected, which must be printed in the pilot’s manuals. European Aviation Safety Agency (EASA) determines the regulation that prescribes operational requirements. The competent aviation authorities of individual countries are obliged to monitor the application of the regulation. Aircraft performance, including operational limitations, are affected by external factors such as different atmospheric conditions and available distances of runway during take-off run, take-off and landing. In this thesis an analysis of operational limitations for mass and velocity was made.

• Keywords: operativna ograničenja; masa zrakoplova; brzina zrakoplova; CS-25; Airbus A320; Boeing B777
• Keywords (english): operational limitations; mass of an aircraft; velocity of an aircraft; CS-25; Airbus A320; Boeing B777
• Language: croatian
• URN:NBN: urn:nbn:hr:119:607882
• Study programme: Title: Aeronautics; specializations in: Pilot, Air Traffic Management; Course: Pilot; 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: 2024-07-12 09:34:53