Paper
28 July 2023 Model-based aero engine high-pressure turbine active gap control strategy simulation and analysis
Changkun Xin, Yunfeng She, Fang Wei, Xu Pan
Author Affiliations +
Proceedings Volume 12756, 3rd International Conference on Applied Mathematics, Modelling, and Intelligent Computing (CAMMIC 2023); 127561N (2023) https://doi.org/10.1117/12.2685898
Event: 2023 3rd International Conference on Applied Mathematics, Modelling and Intelligent Computing (CAMMIC 2023), 2023, Tangshan, China
Abstract
This paper mainly focus on the research of the active tip clearance control scheme for a high pressure turbine on aircraft engine. A brief interpretation of this model is illustrated. Then a rum-time based engine control model (including steady and transient control) is added to the high pressure turbine model, the high pressure tip clearance can be simulated upon the rebuilt model. The High pressure turbine tip clearance control method is realized by bleeding the cool air from the fan to the case shroud, the objective of this paper is to derive the reasonable control plan for the Active tip clearance.
© (2023) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Changkun Xin, Yunfeng She, Fang Wei, and Xu Pan "Model-based aero engine high-pressure turbine active gap control strategy simulation and analysis", Proc. SPIE 12756, 3rd International Conference on Applied Mathematics, Modelling, and Intelligent Computing (CAMMIC 2023), 127561N (28 July 2023); https://doi.org/10.1117/12.2685898
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KEYWORDS
Turbines

Control systems

Thermal deformation

Design and modelling

Computer simulations

Control systems design

Temperature metrology

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