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Open AccessArticle
Analysis of Influencing Factors on the Feasible Operating Range of a Triple-Bypass Adaptive Variable Cycle Engine Compression System
by
Xianjun Yu
Xianjun Yu 1,2
,
Dongbo Hao
Dongbo Hao 1,
Ruoyu Wang
Ruoyu Wang 1,2,*,
Songlin Miao
Songlin Miao 1
and
Baojie Liu
Baojie Liu 1,2
1
Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
2
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Beihang University, Beijing 102206, China
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(9), 775; https://doi.org/10.3390/aerospace12090775 (registering DOI)
Submission received: 16 July 2025
/
Revised: 28 July 2025
/
Accepted: 26 August 2025
/
Published: 28 August 2025
Abstract
The operation range of the adaptive cycle engine (ACE) compression system is constrained by both the compression components and the bypass ducts, resulting in intricate matching mechanisms. Conventional analysis methods struggle to adequately evaluate the feasible operating range or the coupled constraints between components. This study employs an integrated hybrid-dimensional approach, combining zero-dimensional bypass analysis with one-dimensional/quasi-two-dimensional component analysis, to systematically investigate the matching effects of a triple-bypass compression system. The influence of key matching parameters, including the compression component operating points, high-pressure (HP) and low-pressure (LP) shaft speeds, and the core-driven fan stage (CDFS) variable inlet guide vane (VIGV) angles, is investigated. Results indicate that compression component matching primarily influences adjacent downstream bypass ratios, while HP/LP shaft speeds and the CDFS VIGV angle predominantly regulate the first and second bypass ratios. The feasible operating envelope is determined by the superimposed effects of these control parameters. To maximize the total bypass ratio, optimal operation requires increasing the front fan stall margin, elevating LP shaft speed, reducing HP shaft speed, and implementing partial CDFS VIGV closure to enhance pre-swirl. These findings provide critical guidance for control logic refinement and design optimization in advanced variable-cycle compression systems.
Share and Cite
MDPI and ACS Style
Yu, X.; Hao, D.; Wang, R.; Miao, S.; Liu, B.
Analysis of Influencing Factors on the Feasible Operating Range of a Triple-Bypass Adaptive Variable Cycle Engine Compression System. Aerospace 2025, 12, 775.
https://doi.org/10.3390/aerospace12090775
AMA Style
Yu X, Hao D, Wang R, Miao S, Liu B.
Analysis of Influencing Factors on the Feasible Operating Range of a Triple-Bypass Adaptive Variable Cycle Engine Compression System. Aerospace. 2025; 12(9):775.
https://doi.org/10.3390/aerospace12090775
Chicago/Turabian Style
Yu, Xianjun, Dongbo Hao, Ruoyu Wang, Songlin Miao, and Baojie Liu.
2025. "Analysis of Influencing Factors on the Feasible Operating Range of a Triple-Bypass Adaptive Variable Cycle Engine Compression System" Aerospace 12, no. 9: 775.
https://doi.org/10.3390/aerospace12090775
APA Style
Yu, X., Hao, D., Wang, R., Miao, S., & Liu, B.
(2025). Analysis of Influencing Factors on the Feasible Operating Range of a Triple-Bypass Adaptive Variable Cycle Engine Compression System. Aerospace, 12(9), 775.
https://doi.org/10.3390/aerospace12090775
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