Temat: flight level - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Unmanned Vehicles and Safety in the Context of EU and Slovak Legislation
Autorzy:: Mamojková, Mária
Powiązania:: https://bibliotekanauki.pl/articles/1807997.pdf
Data publikacji:: 2020-03-17
Wydawca:: Wyższa Szkoła Bezpieczeństwa Publicznego i Indywidualnego Apeiron w Krakowie
Tematy:: unmanned vehicle
drone
civil aviation
EASA
maximum cleared flight level
VLOS
UAV
UAS
Opis:: The study which follows on findings from the scientific-research task named “Analysis of the use of unmanned airborne vehicles in selected Police Force services” conducted by the Academy of the Police Force in Bratislava in cooperation with the Police Force Headquarters focuses on theoretical and application contexts of selected issues in regulation of unmanned vehicles within EU. The author closely examines the newly adopted drone legislation which affects the Slovak regulation. The author points out to EU regulation, drawing attention to her own findings determined by her own scientific and pedagogical activities, and presents her explanation of elements which may be considered the core elements of unmanned vehicles legislation.
Źródło:: Security Dimensions; 2019, 31(31); 74-88
2353-7000
Pojawia się w:: Security Dimensions
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Results of using sustainable aviation fuel in transport aircraft on different flight levels and their influence on carbon-dioxide Co2 emissions
Autorzy:: Lazic, Dragan
Grujic, Vladimir
Cvetkovic, Dragan
Powiązania:: https://bibliotekanauki.pl/articles/27311348.pdf
Data publikacji:: 2023
Wydawca:: Politechnika Śląska. Wydawnictwo Politechniki Śląskiej
Tematy:: sustainable aviation fuel
flight level
carbon dioxide
turboprop aircraft
zrównoważone paliwo lotnicze
wysokość lotu
dwutlenek węgla
samolot turbośmigłowy
Opis:: During the recent 40 years, the quantity of energy sources globally has been reduced, and the consequence of this situation that the oil in the world becomes more expensive. Many manufacturers have been forced to initiate the development of completely new concepts of developing commercial aircraft which would be more rational regarding fuel consumption by completely retaining the best quality of passenger services. A continuous uptrend of the propellant cost globally since 1990s has forced not only smaller companies but also the most powerful enterprises in aviation industry, such as the “General Electric”, to return to the research and development programs of Turbo Prop engines. In the case of the aircraft DHC Dash 8 Q 400, the engineering preparation of the flight for calculating the changes of travel propellant while the switch of the flight altitude was being done. By analyzing nine various levels of flight, the conclusion has been indisputably reached that regardless of the vast altitudes of a flight and the horizontal distance covered during climb and descent, the fuel consumption is significantly lower than while flying at much lower altitudes with much lower horizontal distance in climb and descent. All the indicators that have been reached undeniably confirm the fact that a flight at great altitudes enables lower consumption of fuel and less necessary time of the flights. By such analysis and setting sustainable aircraft fuels into equations, numerous improvements in the world of aviation, which directly influence the quality of life on the global level, are achieved. Likewise, it will indicate the possibility of substitution of classical hydrocarbon (fossil) fuels with biofuels which, while burning, release much lower emission of exhaust gases.
Źródło:: Zeszyty Naukowe. Transport / Politechnika Śląska; 2023, 119; 105--123
0209-3324
2450-1549
Pojawia się w:: Zeszyty Naukowe. Transport / Politechnika Śląska
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Funkcje rekonfiguracji lotu - próba poprawy bezpieczeństwa lotu w przypadku działań o charakterze terrorystycznym
Flight reconfiguration function - tending to A/C safety level augmentation in case of onboard hostile action
Autorzy:: Krawczyk, M.
Rogalski, T.
Powiązania:: https://bibliotekanauki.pl/articles/213363.pdf
Data publikacji:: 2010
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: rekonfiguracja lotu
bezpieczeństwo lotu
projekt SOFIA
flight reconfiguration function
safety level augmentation
SOFIA project
Opis:: W pracy zaprezentowano główne założenia projektu europejskiego SOFIA, podejmującego próbę zbudowania systemu umożliwiającego automatyczne sprowadzenie samolotu na ziemię w przypadku wystąpienia na jego pokładzie działań o charakterze terrorystycznym. Podana została ogólna struktura systemu oraz omówiono przyjęte sposoby jego implementacji na czterech platformach badawczych: trzech symulatorach oraz dwóch samolotach: I23 Manager oraz D42 Diamond. Kolejno przedstawiono ogólne założenia planu badań oraz zaprezentowano i omówiono wybrane wyniki prób w locie.
In the article main assumptions of the SOFIA VI FP are presented. The SOFIA project is a response to the challenge of development concepts and techniques enabling the aircraft to return automatically and safely to the airport in case of hostile actions on board. The main structure of Flight Reconfiguration Function module was presented as well as some problems, which appeared during the implementation on four experimental platforms, are discussed. Such platforms are: two research simulators and two aircraft. As a conclusion, the test trials program and some remarks about test flights results are provided.
Źródło:: Prace Instytutu Lotnictwa; 2010, 4 (206); 84-92
0509-6669
2300-5408
Pojawia się w:: Prace Instytutu Lotnictwa
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Multiplication of Air Accidents Frequency and Hazard Desirability Coefficients for ICAO Safety Risk Tolerability Matrix Solution
Autorzy:: Borsuk, Sergey Pavlovich
Reva, Oleksiy
Kharchenko, Volodymyr
Powiązania:: https://bibliotekanauki.pl/articles/504648.pdf
Data publikacji:: 2015
Wydawca:: Międzynarodowa Wyższa Szkoła Logistyki i Transportu
Tematy:: flight safety
tolerability matrix
frequency and hazard event desirability coefficients
Harrington function
risk level determination criteria
Opis:: Using mathematical method of priorities arrangement, also known as problem “about leader”, air accidents frequency and hazard desirability coefficients were found. Those coefficients are proposed by ICAO for safety risk tolerability matrix solution. Integral index of mentioned parameters combinations hazard is found with help of Harrington desirability function. Risk levels determination index is introduced for researched matrix.
Źródło:: Logistics and Transport; 2015, 25, 1; 63-70
1734-2015
Pojawia się w:: Logistics and Transport
Dostawca treści:: Biblioteka Nauki

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