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General Information
Editor-in-chief
Prof. Adrian Olaru
University Politehnica of Bucharest, Romania
I'm happy to take on the position of editor in chief of IJMO. It's a journal that shows promise of becoming a recognized journal in the area of modelling and optimization. I'll work together with the editors to help it progress.
IJMO 2024 Vol.14(3): 104-111
DOI: 10.7763/IJMO.2024.V14.857

Thermal Modeling Analysis and Validation of Drilling Manufacturing Process for Aero-Engine Turbine Blades

Chau-Chung Song1,*, Jian-Hong He2, and Cheng-Hua Wu2
1Aeronautical Engineering and Smart Machine and Intelligent Manufacturing Research Center, National Formosa University, Taiwan
2Aeronautical Engineering, College of Engineering, National Formosa University, Taiwan
Email: ccsong@nfu.edu.tw (C.-C.S.); 10978110@gm.nfu.edu.tw (J.-H.H.); 10978112@gm.nfu.edu.tw (C.-H.W.)
*Corresponding author

Manuscript received October 16, 2023; revised May 25, 2024; accepted July 12, 2024; published August 15, 2024

Abstract—Currently, there is a scarcity of research on film-cooling of engine turbine blades, primarily due to the difficulty in accessing technical materials and the high complexity associated with designing curved surfaces. This study employs the heat flow analysis software Simcenter STAR-CCM+ to strategically plan and design the position, angle, and arrangement of heat dissipation holes for the thermal model of engine turbine blade. Subsequently, a simulation analysis is conducted to validate its heat dissipation efficiency. Additionally, experimental verification of the drilling manufacturing process is performed on aero-engine turbine blades. Based on the heat flow simulation results, a drilling model of engine turbine blade is designed for further thermal analysis of cooling efficiency. The drilling position of the workpiece is then transformed and compiled into an electric discharge machining file using the drilling process editing system integrated with the production line. Finally, an automatic production line for the drilling process is constructed to validate the performance and feasibility of the proposed thermal model for aero-engine turbine blades.

Keywords—engine turbine blades, film cooling, thermal model, heat dissipation simulation analysis, drilling process

[PDF]

Cite: Chau-Chung Song, Jian-Hong He, and Cheng-Hua Wu, "Thermal Modeling Analysis and Validation of Drilling Manufacturing Process for Aero-Engine Turbine Blades," International Journal of Modeling and Optimization, vol. 14, no. 3, pp. 104-111, 2024.


Copyright © 2024 by the authors. This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited (CC BY 4.0).

 

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