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곡률 브라켓 구조물의 구조강도 개선효과 검증에 관한 실험적 연구

Study on Verification of Structural Strength Improvement Effect of Curvature Bracket Structure

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키워드

주제분류산업공학

초록

Weapon systems used in the defense field are classified according to each mission/function, from weapons that perform relatively simple functions to system units that are combined with components with core performance. However, even if defects occur during operation in some components due to the characteristics of such a system unit weapon system, there are limitations to structurally confirm the effect of the resulting improvement plan at the system unit. Therefore, a method of confirming the effect of improving the structure by using a limited structural test for the defective part and structural analysis using a FEM is generally used. In fact, during the operation of the rotorcraft, a crack occurred in the bracket-rivet joint inside the exhaust duct, and the structure was improved accordingly. However, the exhaust duct was manufactured in a cylindrical shape and had a curvature, and there were limitations in finding an accurate test method for the curvature bracket structure. In this study, a test was conducted to confirm the structural improvement effect of a bracket structure with curvature by referring to the test method for a commonly used flat metal structure, and by analyzing the test results, the lifespan improvement in the system unit was confirmed.

Abstract

Weapon systems used in the defense field are classified according to each mission/function, from weapons that perform relatively simple functions to system units that are combined with components with core performance. However, even if defects occur during operation in some components due to the characteristics of such a system unit weapon system, there are limitations to structurally confirm the effect of the resulting improvement plan at the system unit. Therefore, a method of confirming the effect of improving the structure by using a limited structural test for the defective part and structural analysis using a FEM is generally used. In fact, during the operation of the rotorcraft, a crack occurred in the bracket-rivet joint inside the exhaust duct, and the structure was improved accordingly. However, the exhaust duct was manufactured in a cylindrical shape and had a curvature, and there were limitations in finding an accurate test method for the curvature bracket structure. In this study, a test was conducted to confirm the structural improvement effect of a bracket structure with curvature by referring to the test method for a commonly used flat metal structure, and by analyzing the test results, the lifespan improvement in the system unit was confirmed.

참고문헌 (7)

  1. "ASTM E8, Standard Test Methods for Tension Testing of Metallic Materials", American Society for Testing Materials, ~ (2001)
  2. "ASTM E9, Standard Test Methods of Compression Testing of Metallic Materials at Room Temperature", American Society for Testing Materials, ~ (2019)
  3. "ASTM D790, Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials", American Society for Testing Materials, ~ (2017)
  4. "ASTM E606, Standard Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing", American Society for Testing Materials, ~ (2019)
  5. 최형준, "항공기 Bulkhead 체결구조의 균열 원인 및 개선에 관한 연구", 한국산학기술학회논문지, 21(6), pp.448~454 (2020), 한국산학기술학회[DOI]
  6. 이윤우, "회전익 항공기 수평 안정판의 설계 개선을 통한 비행 안전성 향상", 한국산학기술학회논문지, 20(6), pp.134~141 (2019), 한국산학기술학회[DOI]
  7. 이명우, "굽힘 하중하의 고장력강 용접 연결부의 피로 평가", 대한기계학회논문집 A, 38(10), pp.1163~1169 (2014), 대한기계학회

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