Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 14, 30 November 2023


Open Access | Article

Mechanisms and advantages of the variable cycle engine

Yifu Li * 1
1 Beijing No.9 Middle School

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 14, 52-57
Published 30 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 Yifu Li. Mechanisms and advantages of the variable cycle engine. TNS (2023) Vol. 14: 52-57. DOI: 10.54254/2753-8818/14/20240878.

Abstract

Designed for aircrafts to fly mixed missions (i.e., at subsonic, transonic, and supersonic flight speeds) with low levels of fuel consumption, the variable cycle engine is ideal for many high-speed planes. The variable cycle engine has the characteristics of both a high-bypass engine (for subsonic flight speed) and a low-bypass engine (for supersonic flight speed). As modern jet engines develop, they inevitably face a bottleneck. Therefore the VCE is seen by most as the next stage of the engines. More and more companies are beginning to invest in this new technology. This paper is targeted to explore the basic mechanism of various VCEs and to see how this new engine brings people better performance over conventional jets. Through Documental Analysis and case study, this research discovered the variable cycle engine greatly improves efficiency and reduces heat of the exiting exhaust in subsonic flight and generates higher thrust during afterburner.

Keywords

Engin, Variable Cycle Engine, Bypass

References

1. Bei Liu. Overall Performances of Interstage Turbine Mixed Architecture Variable Cycle Engine, Journal of Propulsion Technology, ISSN 1001-4055, CN 11-1813/v,2022:2

2. GE Aerospace XA100 Adaptive Cycle Engine, 2023, https://www.geaerospace.com/ propulsion/military/xa100

3. Pratt and Whitney. Pratt and Whitney Military Engines, 2023, https://www.prattwhitney.com/

4. RunFu Liu. Numerical of mixing characteristic of rear variable area bypass injector with lobed structure. Journal of Aerospace Power, ISSN 1000-8055, CN 11-2297/V , 2022:4

5. Wang Hao. Mode Transition Modeling and Control Law Design Method of Variable Cycle Engine, Journal of Propulsion Technology, 1001-4055(2022) 01-210058-10, 2022:5

Data Availability

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

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License. Authors who publish this series agree to the following terms:

1. Authors retain copyright and grant the series right of first publication with the work simultaneously licensed under a Creative Commons Attribution License that allows others to share the work with an acknowledgment of the work's authorship and initial publication in this series.

2. Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the series's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgment of its initial publication in this series.

3. Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See Open Access Instruction).

Volume Title
Proceedings of the 3rd International Conference on Computing Innovation and Applied Physics
ISBN (Print)
978-1-83558-191-9
ISBN (Online)
978-1-83558-192-6
Published Date
30 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/14/20240878
Copyright
30 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