Determination of CO2 emissions for selected flight parameters of a business jet aircraft

• Autorzy: Pawlak Małgorzata , Kuźniar Michał

Identyfikatory

DOI

10.2478/kones-2019-0069

• Języki publikacji: EN

Abstrakty

EN

In the last two decades, there has been observed a noticeable increase in the popularity and availability of air transport services, including regional ones. This intensive development of transport is accompanied by an increase in the adverse impact to the environment, increases noise level, and exhausts emissions, despite the modification and modernization of engines. Determining the emission for regional flights takes into account the specificity of the aircrafts design, such as the size of the aircraft and the performance of the engines. In this article, an attempt was made to determine the CO2 emissions of a business jet flying from Gdansk to Rzeszow. The methodology of the research (the method of calculating emissions based on fuel consumption) and the performance characteristics of the aircraft engines have been described. In the first part of the article, the speed-altitude characteristics of the DGEN-380 engine for different cruise parameters were determined using the virtual engine test bench WESTT CS/B. These characteristics have enabled the engine to match the flight characteristics (altitude, speed). For specific flight parameters, the thrust and fuel consumption were determined. On this basis, for the adopted trajectory and flight time of an aircraft equipped with two DGEN-380 engines, total fuel consumption and CO2 emission factors and values in CRUISE phase was determined with regard to the wind speed and direction. The obtained results were illustrated graphically and discussed.

Słowa kluczowe

EN

CO2 emissions; jet engines; business jet aircraft

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2019
• Tom: Vol. 26, No. 3
• Strony: 155--163
• Opis fizyczny: Bibliogr. 30 poz., rys.

Twórcy

autor

Pawlak Małgorzata

• Gdynia Maritime UniversityFaculty of Navigation Department of Ship Operation Jana Pawla II Av. 3, 81-345 Gdynia, Poland tel.: [phone]

autor

Kuźniar Michał

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautics Department of Aircraft and Aircraft Engines Powstańców Warszawy Av. 8, 35-959 Rzeszow, Poland tel.: [phone]

Bibliografia

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Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).