Araştırma Makalesi

General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)

Cilt: 2 Sayı: 2 30 Ağustos 2020
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General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)

Öz

The general aviation, energetic and exergetic performance analyses of a micro turbojet engine (MTJE) used on drones and UAVs and its major subcomponents are made for different operation modes (Mode-1,-2,-3,-4) in detail. Used performance metrics in this study help to measure the system performance level and to develop the system and its subsystems. The results indicate that the MTJE has the best performance values at the maximum operation modes (Mode-4) because the military engines, especially turbojet engine, are designed to be the most efficient in the maximum operation/take-off modes. The MTJE has the maximum energy efficiency via 19.190% at Mode-4 when it has the maximum exergy efficiency by 18.079% at Mode- 4, respectively. Between the components, the combustion chamber has the lowest exergy efficiency values, the lowest sustainable efficiency factors, the highest exergy destruction rates, the highest exergetic improvement potential rates, the highest fuel exergy waste ratios and the highest productivity lack ratios for all operation modes. When the exergetic performance parameters are taken into consideration, the bad factor for the system is the combustion chamber by far. Therefore, all exergetic performance indicators show that the system owners and researchers focus on the components of the compressor and combustion chamber to improve the exergetic efficiency values of these components.

Anahtar Kelimeler

Kaynakça

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  3. Baharozu E., Soykan G., Ozerdem M.B. (2017). Future aircraft concept in terms of energy efficiency and environmental factors. Energy, 140, 1368-1377.
  4. Balli O. (2017a). Advanced exergy analysis of a turbofan engine (TFE): Splitting exergy destruction into unavoidable/avoidable and endogenous/exogenous. International Journal of Turbo&Jet Engines. ISSN (Online) 2191-0332. ISSN (Print) 0334-0082. DOI:https://doi.org/10.1515/tjj-2016-0074
  5. Balli O. (2017b). Advanced exergy analyses of an aircraft turboprop engine (TPE). Energy, 124, 599-612.
  6. Balli O. (2017c). Advanced exergy analyses to evaluate the performance of a military aircraft turbojet engine (TJE) with afterburner: Splitting exergy destruction into unavoidable/avoidable and endogenous/exogenous. Applied Thermal Engineering, 111, 152-169.
  7. Balli O. (2017d).Exergy modeling for evaluating sustainability level of a high by-pass turbofan engine used on commercial aircrafts. Applied Thermal Engineering, 123,138-155.
  8. Balli O. (2019). A Parametric Study of Hydrogen Fuel Effects on Exergetic, Exergoeconomic and Exergoenvironmental Cost Performances of an Aircraft Turbojet Engine. International Journal of Turbo and Jet Engines, https://doi.org/10.1515/tjj-2019-0043

Ayrıntılar

Birincil Dil

İngilizce

Konular

Uzay Mühendisliği

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

30 Ağustos 2020

Gönderilme Tarihi

25 Nisan 2020

Kabul Tarihi

17 Mayıs 2020

Yayımlandığı Sayı

Yıl 2020 Cilt: 2 Sayı: 2

Kaynak Göster

APA
Balli, Ö. (2020). General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV). Journal of Aviation Research, 2(2), 115-141. https://izlik.org/JA54ZW63XM
AMA
1.Balli Ö. General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV). JAR. 2020;2(2):115-141. https://izlik.org/JA54ZW63XM
Chicago
Balli, Özgür. 2020. “General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)”. Journal of Aviation Research 2 (2): 115-41. https://izlik.org/JA54ZW63XM.
EndNote
Balli Ö (01 Ağustos 2020) General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV). Journal of Aviation Research 2 2 115–141.
IEEE
[1]Ö. Balli, “General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)”, JAR, c. 2, sy 2, ss. 115–141, Ağu. 2020, [çevrimiçi]. Erişim adresi: https://izlik.org/JA54ZW63XM
ISNAD
Balli, Özgür. “General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)”. Journal of Aviation Research 2/2 (01 Ağustos 2020): 115-141. https://izlik.org/JA54ZW63XM.
JAMA
1.Balli Ö. General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV). JAR. 2020;2:115–141.
MLA
Balli, Özgür. “General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV)”. Journal of Aviation Research, c. 2, sy 2, Ağustos 2020, ss. 115-41, https://izlik.org/JA54ZW63XM.
Vancouver
1.Özgür Balli. General Aviation and Thermodynamic Performance Analyses of a Micro Turbojet Engine Used on Drones and Unmanned Aerial Vehicles (UAV). JAR [Internet]. 01 Ağustos 2020;2(2):115-41. Erişim adresi: https://izlik.org/JA54ZW63XM

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