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"Jaehun Choi"

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A Study on Numerical Thermal Design Techniques for High-power Propulsion Motors
Jaehun Choi, Chiwon Park, Heesung Park
J. Korean Soc. Precis. Eng. 2025;42(11):893-900.
Published online November 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.036

Propulsion motors are vital components in marine propulsion systems and industrial machinery, where high torque and operational reliability are paramount. During operation, high-power propulsion motors generate considerable heat, which can adversely affect efficiency, durability, and stability. Therefore, an effective thermal management system is necessary to maintain optimal performance and ensure long-term reliability. Cooling technologies, such as water jackets, are commonly employed to regulate temperature distribution, prevent localized overheating, and preserve insulation integrity under high-power conditions. This paper examines the cooling performance of water jackets for high-power propulsion motors through numerical analysis. We evaluated the effects of three different cooling pipe locations and varying coolant flow rates on thermal balance and cooling efficiency. Additionally, we analyzed temperature variations in the windings and key heat-generating components to determine if a specific cooling flow rate and pipe configuration can effectively keep the winding insulation (Class H) within its 180oC limit. The findings of this study highlight the significance of optimized cooling system design and contribute to the development of efficient thermal management technologies, ultimately enhancing motor reliability, operational stability, and energy efficiency.

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A Study on Numerical Analysis for Determination of Glass Molding Process Conditions for Glass Lenses
Jaehun Choi, Sajan Tamang, Heesung Park
J. Korean Soc. Precis. Eng. 2024;41(3):207-214.
Published online March 1, 2024
DOI: https://doi.org/10.7736/JKSPE.023.136
The Glass Molding Process (GMP) produces large quantities of glass optical parts and provides the advantages of high molding accuracy, short production cycle, low cost, and little pollution. Developments in different sectors, such as cameras and telescopes, are prompting studies on the design of aspherical optical components. Modeling heat transfer and deformation at high temperatures are crucial aspects of studying glass because its properties are significantly influenced by temperature-induced phase changes. In this study, temperature changes and geometric deviations of lenses were studied with respect to heating, pressing, and cooling times and the heat capacity of the heater used. A 3D model was designed for the heating, pressing, and cooling steps, and heat transfer was subjected to numerical analysis considering the specific heat of glass and the temperature dependence of thermal conductivity. Lens molding temperature conditions were then analyzed with the heat capacity of the lens molding heating system. Lens molding conditions were derived by analyzing lens temperatures with respect to heating and cooling capacities at each process step.

Citations

Citations to this article as recorded by  Crossref logo
  • Precision glass aspherical lens manufacturing by compression molding: a review
    Xiaohua Liu, Jian Zhou, Bo Tao, Yang Shu, Zexin Feng, Shih-Chi Chen, Yingying Zhang, Allen Y. Yi
    Light: Advanced Manufacturing.2026; 7: 1.     CrossRef
  • A Study on Temperature and Stress Distribution in a Lens under Multi-Stage Cooling Conditions in Progressive Glass Molding Processes
    Ji Hyun Hong, Jeong Taek Hong, Dong Yean Jung, Young Bok Kim, Keun Park, Chang Yong Park
    Journal of the Korean Society for Precision Engineering.2025; 42(2): 157.     CrossRef
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A Numerical Study on the Cooling Efficiency of the Gas Turbine Vane with the Film Cooling Hole Shape
Jaehun Choi, Hwabhin Kwon, Heesung Park
J. Korean Soc. Precis. Eng. 2020;37(2):107-113.
Published online February 1, 2020
DOI: https://doi.org/10.7736/JKSPE.019.094
Research on advanced cooling system design is significant in achieving a high turbine inlet temperature in the gas turbine industry. The higher turbine inlet temperature of the gas turbine increases thermal efficiency. However, it also aggravates the gas turbine deterioration, lifespan, and efficiency. In this study, a numerical model is developed for simulating the cooling performance of the gas turbine vane with the turbine inlet temperature of 1528 K. The impact of the coolant air flow rate and hole-shape were investigated. The expanded hole shape had better cooling performance than the general cylindrical shape, and showed higher cooling efficiency. We suggest that there is a relationship between the shape of the film cooling holes and the cooling air flow rate that achieves the desired cooling effectiveness.
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