Latest developments in commercial jet engine design
Piotr Ułasiuk
ulasiuk15102@nauka.panschelm.edu.plPaństwowa Akademia Nauk Stosowanych w Chełmie (Poland)
Abstract
The aviation market in Poland, as well as worldwide, is developing dynamically and is attracting the attention of many investors. As never before, major aviation companies are looking in every possible way for ways to reduce the production costs, operation and fuel consumption of their aircraft. Without doubt, the most important component of an aircraft and the one where a number of new technologies and optimisations of individual parts can be introduced is the jet engine. This article describes the latest developments that are being introduced by major aircraft propulsion manufacturers and their impact on improving performance. Selected design solutions and technologies used in the latest designs, such as Rolls Royce ltraFan, General Electric GEnx and Pratt & Whitney's PW 1100G, are presented.
Keywords:
jet engines, optimalisation, aviation market, aviation technologies, fuel savings, aviation engines developmentReferences
Brauhn, R.D. (2015). Aviation Maintenance Technician Certification Series: Gas Turbine Engines. Module 15, Aircraft Technical Book Co.
Google Scholar
Balicki, W., Głowacki, P., Szczeciński, S., & Kozakiewicz, A. (2016). Bilans energetyczny wirników dwuprzepływowych silników odrzutowych. Prace Instytutu Lotnictwa, 3(244), 321–328.
Google Scholar
Hodson, H., & Howell, R. (2005). The role of transition in high-lift low-pressure turbines for aeroengines. Progress in Aerospace Sciences, 41, 419–454.
Google Scholar
Russell, J. (2021, October 27). NASA, US Industry Accelerate Advancement of Small Core Aircraft Engines. Explore. https://www.nasa.gov/aeronautics/nasa-us-industry-accelerate-advancement-of-small-core-aircraft-engines/
Google Scholar
Alves, P., Silvestre, M. & Gamboa, P. (2020). Aircraft Propellers – Is There a Future?. Energies, 13(16). https://doi.org/10.3390/en13164157
Google Scholar
Gas turbine. (2024, September 17). In Wikipedia. https://en.wikipedia.org/wiki/Gas_turbine
Google Scholar
Guynn, M., Berton, J. J., Fisher, K. L., Haller, W. J., Tong, M. & Thurman, D. R. (2013, August 24). Engine Concept Study for an Advanced Single-Aisle Transport. NASA NTRS.
Google Scholar
Rolls Royce. (2024, September 17). The Ultimate TurboFan. https://www.rolls-royce.com/innovation/ultrafan.aspx
Google Scholar
Graham-Rowe, D. (2021, December 13). More Efficient Jet Engine Gets in Gear. MIT Technology Review. https://www.technologyre-view.com/2010/12/13/24891/more-efficient-jet-engine-gets--in-gear/
Google Scholar
Fehrm, B. (2016, March 4). Engine architectures. Leeham News and Analysis. https://leehamnews.com/2016/03/04/bjorns-corner-engine-architectures/
Google Scholar
Epstein, N. (1981). CFM56-3 High By-Pass Technology for Single Aisle Twins. In 1981 AIAA/SAE/ASCE/ATRIF/TRB International Air Transportation Conference, 26–28 May 1981. American Institite of Aeronautics and Astronautics. https://arc.aiaa.org/doi/abs/10.2514/6.1981-808
Google Scholar
Fromm, J. (2016). Composite Fan Blades and Enclosures for Modern Commercial Turbo Fan Engines. ASEN 5063: Gas Turbine Propulsion. https://www.colorado.edu/faculty/kantha/sites/default/files/attached-files/fromm.pdf
Google Scholar
Mecham, M. (2006, 17 April). GEnx Development Emphasizes Composites, Combustor Technology. https://aviationweek.com/genx-development-emphasizes-composites-combustor-technology
Google Scholar
Ranasinghe, K., Guan, K., Gardi, A., & Sabatini R. (2019). Review of Advanced Low-Emission Technologies for Sustainable Aviation. Energy, 188. https://doi.org/10.1016/j.energy.2019.115945
Google Scholar
Miller, S. G., Handschuh, K. M., Sinnott, M. J., Kohlman, L. W., Roberts, G. D., Martin, R. E., Ruggeri, Ch. R. & Pereira, J. M. (2015, February 15). Materials, Manufacturing, and Test Development of a Composite Fan Blade Leading Edge Subcomponent for Improved Impact Resistance. NASA NTRS. https://ntrs.nasa.gov/citations/20150002113
Google Scholar
National Aeronautics and Space Administration. (2006). Damage-Tolerant Fan Casings for Jet Engines. NASA Spinoff. https://spinoff.nasa.gov/Spinoff2006/T_1.html
Google Scholar
Ohnabe, H., Masaki, S., Onozuka, M., Miyahara, K., Sasa, T. (1999). Potential application of ceramic matrix composites to aero-engine components, Composites Part A: Applied Science and Manufacturing, 4(30), 489-496. https://doi.org/10.1016/S1359-835X(98)00139-0
Google Scholar
U.S. Department of Transportation. (2013, June). TAPS II Combustor Final Report Continuous Lower Energy, Emissions and Noise (CLEEN) Program. Federal Aviation Administration. https://www.faa.gov/sites/faa.gov/files/about/office_org/headquarters_offices/apl/TAPS_II_Public_Final_Report.pdf
Google Scholar
Lukas Souza. (2024, October 15). A large jetliner sitting on top of an airport tarmac. [Photograph]. Unsplash. https://unsplash.com/photos/a-large-jetliner-sitting-on-top-of-an-airport-tarmac-M_wNYGi9o3s
Google Scholar
Chandler, Ch. (2014, February 27). Turbine Technology: Innovations in Turbine Engines. Aviation Pros. www.aviationpros.com/article/10617063/turbine-technology-innovations-in-turbine-engines
Google Scholar
Fehrm, B. (2024, April 19). New engine development. Part 4. Propulsive efficiency. Leeham News and Analysis. https://leehamnews.com/2024/04/19/bjorns-corner-new-engine-development-part-4-propulsive-efficiency/
Google Scholar
Authors
Piotr Ułasiukulasiuk15102@nauka.panschelm.edu.pl
Państwowa Akademia Nauk Stosowanych w Chełmie Poland
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