diplomsko delo Visokošolskega strokovnega študijskega programa I. stopnje Strojništvo - Projektno aplikativni program
Jure Carlevaris (Author), Igor Petrović (Mentor)

Abstract

Vzlet in nadaljni odlet letala predstavlja ključen dogodek v procesu leta letala. Zaradi bližine terena, visoke hitrosti letala in zmanjšane zmogljivosti vzpenjanja, so lahko posledice, ki sledijo odpovedi motorja ob vzletu katastrofalne in lahko rezultirajo v velikem številu izgubljenih življenj. Iz tega razloga se le ta smatra kot ena izmed najnevarnejših faz leta. Ker svet letalstva konstantno stremi k izboljšanju varnosti v industriji so za take primere definirani posebni odletni postopki v primeru odpovedi motorja imenovani EOSID. V zaključni nalogi je preučeno ozadje snovanja EOSID procedur, vključno s temeljno teorijo potrebno za razumevanje EOSID procedur. Z upoštevanjem regulatorskih predpisov ter ustaljenih praks je izdelana EOSID procedura za letališče Cerklje ob Krki. V nalogi so analizirani teren in ovire v okolici letališča, podani izračuni konstrukcije EOSID-a ter predstavljen končni izgled EOSID procedure za obravnavano letališče. Dodatno so analizirane metode za ročni izračun parametrov vzleta in podana je implementacija izdelane EOSID procedure za letalo Let L-410 Turbolet.

Keywords

diplomske naloge;postopki v sili;odpoved motorja;načrtovanje procedur;oddaljenost od ovir;zmogljivosti pri vzletu;

Data

Language: Slovenian
Year of publishing:
Typology: 2.11 - Undergraduate Thesis
Organization: UL FS - Faculty of Mechanical Engineering
Publisher: [J. Carlevaris]
UDC: 614.8:656.082:629.7.077(043.2)
COBISS: 171627523 Link will open in a new window
Views: 33
Downloads: 8
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Other data

Secondary language: English
Secondary title: Planning and analysis of departure procedures in the event of engine failure at Cerklje ob Krki airport for the Let L-410 Turbolet aircraft
Secondary abstract: The takeoff and subsequent departure of an aeroplane presents a crucial moment in the flight process. Due to the proximity of the terrain, the high speed of the aircraft and the reduced climb capablity, the consequences following an engine failure on takeoff can be catastrophic and may result in a large number of loss of life. For this reason, this alone is considered one of the most dangerous phases of the flight. As the world of aviation constantly strives to improve safety in the industry, special emergency departure procedures called EOSID have been defined for such cases. In this paper, the background of the design of EOSID procedures is examined, including the basic theory necessary for understanding contingency departure procedures. The EOSID procedure for the Cerklje ob Krki airport has been developed in accordance with regulatory regulations and established practices. In the paper, the terrain and obstacles in the vicinity of the airport are analyzed, the calculations of the construction of the contingency procedure are given and the final appearance of the EOSID procedure for the airport in question is presented. In addition, the methods for manual calculation of takeoff parameters are analyzed and the implementation of the developed emergency procedure for the Let L-410 Turbolet aircraft is given.
Secondary keywords: contingency procedures;engine failure;procedures design;obstacle clearance;takeoff performance;
Type (COBISS): Bachelor thesis/paper
Study programme: 0
Embargo end date (OpenAIRE): 1970-01-01
Thesis comment: Univ. v Ljubljani, Fak. za strojništvo
Pages: XXII, 66 str.
ID: 20488388
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