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Planning the flight trajectory of a passenger aircraft with regards to the aspect of pollutants emission

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EN
One of the ways to reduce the adverse impact of aircraft on the environment is through the determination of the trajectory of the flight on a given route that leads to reducing fuel consumption and, consequently, emission of pollutants in jet engines exhausts. Planning a flight in terms of minimizing emissions or fuel consumption is a complex task and difficult to implement due to the conditions in which the aircraft travels, but it is possible though. It is necessary to take into account the limitations resulting from the organization of the airspace and the rules therein, as well as the current weather conditions. The weather is one of the main factors determining the amount of fuel consumed, the time and cost of a particular flight on a given route. In addition to the main parameters, such as pressure and air density, it is extremely important to determine the air temperature, as well as the wind speed and direction. The temperature affects the speed of sound, based on which it is possible to determine the Mach number for a plane flying with a given true air speed (TAS). The speed and direction of wind, on the other hand, affect the speed of the aircraft relative to the ground (velocity over ground, VOG), and thus the duration of its flight. The article describes how the developed model of emission of pollutants in the exhausts of jet bypass engines can be useful for determining the trajectory of an aircraft in its cruise phase due to the criterion of pollutants emissions minimization. An exemplary analysis was carried out for selected aircraft moving along the route adopted for the research. The analysis covered various cruising altitudes and various meteorological conditions (wind speed and direction). The obtained results are illustrated graphically and discussed.
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Twórcy
  • Gdynia Maritime University, Faculty of Navigation Department of Ship Operation Jana Pawla II Av. 3, 81-345 Gdynia, Poland tel.: +48 58 5586182
Bibliografia
  • [1] Cichosz, E., Kordziński, W., Łyżwiński, M., Szczeciński, S., Charakterystyka i zastosowanie napędów – napędy lotnicze, Wydawnictwa Komunikacji i Łączności, Warszawa 1980.
  • [2] Flightradar24.com.
  • [3] Jackson, P., Jane’s All the World’s Aircraft, 2013–2014, Development & Production, FRAeS, Publ. Jane’s Information Group, London, UK 2014.
  • [4] Pawlak, M., Kuźniar, M., Analysis of the Wind Dependent Duration of the Cruise Phase on Jet Engine Exhaust Emissions, Journal of KONES Powertrain and Transport, Vol. 25, No. 3, pp. 371-376, Warsaw 2018.
  • [5] Pawlak, M., Majka, A., Kuźniar, M., Pawluczy, J., Analysis of Wind Impact on Emission of Selected Exhaust Compounds in Jet Engines of a Business Jet Aircraft in Cruise Phase, Combustion Engines, Vol. 173, No. 2, pp. 55-60, 2018.
  • [6] Pawlak, M., Metoda modelowania emisji szkodliwych i toksycznych składników spalin turbinowych silników odrzutowych samolotów pasażerskich w warunkach przelotowych, Wyd. Uniwersytetu Morskiego w Gdyni, Gdynia 2019.
  • [7] Schaefer, M., Bartosch, S., Overview on Fuel Flow Correlation Methods for the Calculation of NOx, CO and HC Emissions and Their Implementation into Aircraft Performance Software, Interner Bericht, Deutsches Zentrum für Luft- und Raumfahrt (DLR), Institut für Antriebstechnik, Köln, Germany 2013.
  • [8] Wilson, D. G., Korakianitis, T., The Design of High-Efficiency Turbomachinery and Gas Turbines, The MIT Press, 2nd ed., Cambridge, MA, USA 2014.
  • [9] Windy.com.
Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-4d8bcdde-19dd-4b3d-8660-c5002677cdb1
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