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Full Length Article | Open Access

Flow control of double bypass variable cycle engine in modal transition

Haoying CHENChangpeng CAIJiayi LUOHaibo ZHANG( )
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

To study the change mechanism and the control of the variable cycle engine in the process of modal transition, a variable cycle engine model based on component level characteristics is established. The two-dimensional CFD technology is used to simulate the influence of mode selection valve rotation on the engine flow field, which improves the accuracy of the model. Furthermore, the constant flow control plan is proposed in the modal transition process to reduce the engine installed drag. The constant flow control plan adopts the augmentation linear quadratic regulator control method. Simulation results indicate that the control method is able to effectively control the bypass ratio and demand flow of the variable cycle engine, and make the engine transform smoothly, which ensures the stable operation of the engine in modal transition and the constant demand flow of the engine.

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Chinese Journal of Aeronautics
Pages 134-147

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Cite this article:
CHEN H, CAI C, LUO J, et al. Flow control of double bypass variable cycle engine in modal transition. Chinese Journal of Aeronautics, 2022, 35(10): 134-147. https://doi.org/10.1016/j.cja.2022.02.001

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Received: 06 May 2021
Revised: 25 May 2021
Accepted: 19 July 2021
Published: 24 February 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).