Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 12, 17 November 2023


Open Access | Article

Turbofan and turbojet engines: Working process and future development

Kaixiang Wei * 1
1 Virginia Polytechnic Institute and State University

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 12, 114-119
Published 17 November 2023. © 2023 The Author(s). Published by EWA Publishing
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Citation Kaixiang Wei. Turbofan and turbojet engines: Working process and future development. TNS (2023) Vol. 12: 114-119. DOI: 10.54254/2753-8818/12/20230447.

Abstract

This article is based on the fundamental thermodynamics theory to analyze the difference between the turbojet and turbofan engines. The result of this article is that the turbofan engine is suitable for commercial use since it consumes less fuel and has a higher bypass ratio than the turbojet engine. But low bypass ratio engines can serve the military since they have a smaller volume and higher speed, suitable for air combat. The turbojet engine can travel at a supersonic speed since it has extremely high jet flow from the nozzle and much higher fuel consumption, so it is for military use. This article also analyses two cases: i) How the number of fan blades and outlet guide vans affects the noise of the engine produced. ii) When airplanes fly through volcanic ash, how does the ash damage the airplane and the engine? The engineer found that 55 outlet guide vans are better than 37. To prevent airplanes from flying through volcanic ash, satellite weather photos start to show the volcanic ash area.

Keywords

turbofan engine, turbojet engine, bypass ratio, sustainability

References

1. Dr. Robert J. Shaw. How does a jet engine work? May 13, 2021. Retrieved on Jul 9, 2023. Retrieved from: https://www.grc.nasa.gov/www/k-12/UEET/StudentSite/engines.html#

2. ICAO. The World of Air Transport in 2021. 2021. Retrieved on Jul 9, 2023. Retrieved from: https://www.icao.int/sustainability/WorldofAirTransport/Pages/the-world-of-air-transport-in-2021.aspx

3. Liu D and Chen G 2003 Aeroengine: The heart of the aircraft. Aviation Industry Press. pp 59-104

4. Moran M and Shapiro H Fundamentals of engineering thermodynamics McGraw-Hill Book Co p 142

5. Ma M, Jin J and Ji H 2008 Aero engine afterburner technology and novel structure scheme Gas Turbine Test and Research 4 55

6. Nancy H Afterburning Turbojet. May 13, 2021. Retrieved on Jul 9, 2023. Retrieved from: https://www.grc.nasa.gov/www/k-12/airplane/Animation/turbtyp/etar.html

7. Chen J 2018 Overview of the working principle and application of turbofan engines Times Motor 5 115

8. Li D and Yang X 2013 Low Noise design of a large bypass ratio turbofan engine Proceedings of the 3rd Shanghai - Xi 'an Acoustical Society Conference 32 157-158

9. Nancy Hall. Turbofan engine. May 13, 2021. Retrieved on Jul 9, 2023. Retrieved from:https://www.grc.nasa.gov/www/k-12/airplane/aturbf.html#:~:text=Because%20the%20fuel%20flow%20rate,turbofan%20is%20very%20fuel%20efficient

10. Glenn D 2006 Noise Reduction Technologies for Turbofan Engines p 5

11. Code 7700. Feb 22, 2018. Retrieved on Jul 9, 2023. Retrieved from: https://code7700.com/case_study_british_airways_9.htm#section1

Data Availability

The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.

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Volume Title
Proceedings of the 2023 International Conference on Mathematical Physics and Computational Simulation
ISBN (Print)
978-1-83558-135-3
ISBN (Online)
978-1-83558-136-0
Published Date
17 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/12/20230447
Copyright
17 November 2023
Open Access
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited

Copyright © 2023 EWA Publishing. Unless Otherwise Stated