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열-구조 연성해석을 통한 i-SMR CRDM 하우징의 임계 두께에 관한 수치적 연구 KCI 등재

A Numerical Study on the Critical Thickness of i- SMR CRDM Housing through Thermal-Structural Coupled Analysis

곽효서
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한국기계항공기술학회지(구 한국기계기술학회지) (Journal of the Korean Society of Mechanical and Aviation Technology)
한국기계항공기술학회(구 한국기계기술학회) (Korean Society of Mechanical Technology)
초록

This study evaluates the structural integrity and design optimization of the i-SMR CRDM housing under operating conditions (15.5 MPa, 325°C). Using a thermal-structural coupled FE analysis, a parametric study was conducted by varying the housing thickness from 10 mm to 3 mm. Results showed that while radial deformation remained stable (~0.33 mm) due to thermal expansion, axial displacement increased by 17.1% as thickness decreased. Stress linearization, based on ASME Section III NB-3200, identified 4 mm as the critical minimum thickness, yielding a combined stress ( ) of 275.24 MPa, which satisfies the shakedown limit () of 282 MPa. In contrast, the 3 mm model exceeded the limit at 357.62 MPa. The baseline 10 mm design exhibited a high safety factor of 3.21, confirming its conservative reliability. These findings provide a quantitative basis for the lightweight design of SMR pressure boundaries while ensuring strict nuclear safety standards.

키워드
혁신형 소형 모듈형 원자로CRDM 제어봉 하우징열-구조 연성해석응력 선형화 i-SMRCRDM HousingThermal-structural coupled analysisStress linearization
목차
Abstract
1. 서 론
2. 이론적 배경 및 평가 기준
    2.1 Stress Classification and Linearization
    2.2 Design Limits
    2.3 ASME 규격에 따른 두께 계산
3. Parametric study
    3.1 Mesh
    3.2 Analysis Setting
    3.3 Result of Thermal-Structural CoupledAnalysis
4. Conclusions
References
저자
  • 곽효서(Assistant professor, Mechanical Engineering Major) | Hyo-seo Kwak Corresponding author