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Turbofan Engines Efficiency, Historical Trends, and Future Prediction: A Review

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Technological development in the aviation business is usually dictated by diverse safety, economic, environmental, and social goals set by governments, regulatory agencies, and the market. Recently, a rapidly increasing interest in making air transportation climate neutral has been observed. The objective of this study is to analyze the historical trends of aircraft engine fuel efficiency, identify parameters affecting engine efficiency and initiate a discussion about future technology development needed to meet the expectations. The commercial turbofan engines test data comparison is provided in this study, followed by a theoretical assessment. The presented test data trends show a clear correlation between specific fuel consumption decrease and engine parameters like bypass ratio and overall pressure ratio increase, which is confirmed by theoretical assessment. Based on performed analysis results, a bypass ratio increase was indicated as the one potential path to reduce aircraft engine fuel consumption. Bypass ratio improvement could be achieved by fan diameter increase and rotation speed reduction in the case of turbofan engine architecture. A larger fan rotor requires a high torque drive and significantly increases engine weight which could be compensated by the lightweight design of the engine components, e.g., by applying composite materials.
Czasopismo
Rocznik
Tom
2
Strony
82--90
Opis fizyczny
Bibliogr. 18 poz., rys., tab.
Twórcy
Bibliografia
  • 1. CFM international. (2016, March, 11th). Type-certificate data sheet, LEAP-1A & LEAP-1C series engines. European Aviation Safety Agency.https://www.easa.europa.eu/sites/default/files/dfu/EASA%20E%20110%20TCDS%20Issue%202%20LEAP-1A_1C_20161103_1.0.pdf
  • 2. CFM International. (2017). LEAP Brochure. CFM International. https://www.cfmaeroengines.com/wp-content/uploads/2017/09/Brochure_LEAPfiches_2017.pdf
  • 3. CFM International. The LEAP engine. CFM International. https://www.cfmaeroengines.com/engines/leap/
  • 4. COP26 (2021, November, 10th). International Aviation Climate Ambition Coalition, COP26 Declaration. 2021 United Nations Climate Change Conference. https://ukcop26.org/cop-26-declaration-international-aviation-climate-ambition-coalition/
  • 5. Corning, J. (2021, July, 2nd). FAA Aerospace, Forecast, Fiscal Years 2021-2041. Federal Aviation Administration. https://www.faa.gov/data_research/aviation
  • 6. El-Sayed, A. F. (2017). Aircraft Propulsion and Gas Turbine Engines, Second Edition. Taylor & Francis. https://doi.org/10.1201/9781315156743
  • 7. Epstein, A. Technology and Environment department, Pratt & Whitney (2015, September). The Pratt & Whitney PurePower ® Geared Turbofan ™ Engine. Air and Space Academy. https://academieairespace.com/en/documents-et-medias/the-pratt-whitney-purepower-geared-turbofan-engine/
  • 8. Farokhi, S. (2014). Aircraft Propulsion, Second Edition. John Wiley & Sons, Ltd.
  • 9. General Electric US. (2021, June, 14th). GE Aviation and Safran Launch Advanced Technology Demonstration Program for Sustainable Engines; Extend CFM Partnership to 2050. GE Aviation webpage. https://www.geaviation.com/press-release/other-news-information/ge-aviation-and-safran-launch-advanced-technology
  • 10. Hager, R. D., & Vrabel, D. (1988). Unducted Fan (UDF) Concept. In R. D. Hager, and D. Vrabel, Advanced Turboprop Project (pp. 84-100). National Aeronautics and Space Administration. https://ntrs.nasa.gov/api/citations/19890003194/downloads/19890003194.pdf
  • 11. International Civil Aviation Organization based on Aviation Benefits Report. (last updated: 2022, March, 8th). Economic Impacts of COVID-19 on Civil Aviation. International Civil Aviation Organization. https://www.icao.int/sustainability/Pages/Economic-Impacts-of-COVID-19.aspx
  • 12. International Civil Aviation Organization. (2021, July). ICAO Aircraft Engine Emissions Databank. European Aviation Safety Agency. https://www.easa.europa.eu/domains/environment/icao-aircraft-engine-emissions-databank
  • 13. Kjelgaard, Ch. (2021, November, 10th). Commercial-Engine OEMs Detail Emissions Work. Aviation International News. https://www.ainonline.com/aviation-news/air-transport/2021-11-10/commercial-engine-oems-detail-emissions-work
  • 14. Mattingly, J. D. (2006). Elements of Propulsion: Gas Turbines and Rockets, Second Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.103711
  • 15. Pratt & Whitney US. (2018, July). PW1100G-JM. Pratt & Whitney webpage. https://prattwhitney.com/-/media/project/pw/pw-internet/pwu/pwu/products/commercial/pw1100gjm.pdf?rev=635c7adfad9e43d686692f2e68c16cdd
  • 16. Raytheon Technologies Corporation – Pratt & Whitney Division. (2019, December, 9th). Type-certificate data sheet, PW1100G-JM Series Engines. European Aviation Safety Agency. https://www.easa.europa.eu/sites/default/files/dfu/TCDS%20EASA.IM_.E.093%20Issue%2007.pdf
  • 17. Sforza P. (2012). Theory of Aerospace Propulsion. Elsevier Inc. DOI: 10.1016/B978-1-85617-912-6.10001-5
  • 18. Taylor, J. W. R. (1970). Jane’s All The World’s Aircraft 1969-70. The Aeronautical Journal, Volume 74 (710), pp. 166.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-92c81387-51d4-40b7-98b5-35970c43c09d
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