손상변수기반 점진적 파손이론을 이용한 복합재 이중 겹침 볼트 체결부의 강도 해석
Strength Analysis of Composite Double-lap Bolted Joints by Progressive Failure Theory Based on Damage Variables
2
조회
0
다운로드
4
인용
0
참고문헌
키워드
초록
복합재 이중-겹침 볼트 체결부의 파손을 예측하기 위해 손상계수를 고려한 강성저하 방법과 Hashin의 3차원 파손판정식에 근거한 3차원 유한요소해석 방법을 제안하였다. 기지 혹은 면내(In-plane) 전단 손상을 고려하기 위해 손상변수를 이용하는 Ladeveze 이론을 섬유방향 강성저하와 연계하여 사용하였고, 수지 압축/전단, 수지 인장/전단, 섬유 압축, 섬유 인장 등 4가지 파손모드를 고려하였다. 상업용 유한요소 프로그램인 ABAQUS를 이용하여 마찰력과 볼트 체결력을 고려하였고, 강성저하모델 처리를 위해 ABAQUS의 사용자 정의 부프로그램을 이용하였다. 제안된 유한요소해석 방법을 검증하기 위해 복합재 이중겹침 볼트 체결부 시험 결과와 파손강도를 비교한 결과 7~16% 오차를 보임을 확인하였다.
Abstract
A three-dimensional finite analysis method was proposed to predict the failure of composite double-lap bolted joints, which is based on the stiffness degradation method using damage variables and Hashin's threedimensional failure criteria. Ladeveze's theory using damage variables to consider the matrix/shear damage was combined with stiffness degradation in fiber direction. Four different failure modes were considered including matrix compression/shear, matrix tension/shear, fiber compression, and tension failures. The friction between bolt and composite and the clamping force were considered using a commercial finite element software ABAQUS. The damage model was incorporated using the user-defined subroutine of the software. The predicted result was verified with the existing test result for bearing tension double shear and showed the deviation ranging 7~16% from test results.
참고문헌 (20)
- IBOLT: A Composite Bolted Joint Static Strength Prediction Tool, Joining and Repair of Composite Structures, "Eisenmann, J. R.", ASTM International, ~, pp.ASTM STP 1455
- 안현수, "복합재 체결부의 파손해석을 위한 새로운 특성길이 결정 방법", Composites Research, 16(4), pp.10~21 (2003), 한국복합재료학회
- Chang, F. K., "Strength of Mechanically Fastened Composite Joints", Journal of Composite Materials, 16, pp.470~494 (1982)
- Manalo, A., "Behavior of Fiber-reinforced Composite Beams with Mechanical Joints", Journal of Composite Materials, 46, pp.483~496 (2011)
- Wang, H. S., "Bearing Failure of Bolted Composite Joints. Part I : Experimental Characterization", Journal of Composite Materials, 30(12), pp.1284~1313 (1996)
- Hung, C. L., "Bearing Failure of Bolted Composite Joints. Part II : Model and Verification", Journal of Composite Materials, 30(12), pp.1359~1400 (1996)
- Hung, C. L., "Strength Envelope of Bolted Composite Joints under Bypass Loads", Journal of Composite Materials, 30(13), pp.1402~1435 (1996)
- Hashin, Z., "Failure Criteria for Uni-directional Fiber Composites", Journal of Applied Mechanics, 47, pp.329~334 (1980)
- Kweon, J. H., "A Two-dimensional Progressive Failure Analysis of Pinned Joints in Uni-directional- Fabric Laminated Composites", Journal of Composite Materials, 41, pp.2083~2104 (2007)
- McCarthy, C. T., "Progressive Damage Analysis of Multi-Bolt Composite Joints with Variable Bolt-Hole Clearance", Composites Part B : Engineering, 36, pp.290~305 (2005)
- McCarthy, M. A., "Finite Element Analysis of the Effects of Clearance on Single-shear, Composite Bolted Joints", Plast, Rubber Compos, 32(2), pp.65~70 (2002)
- Tserpes, K. I., "Strength Prediction of Bolted Joints in Graphite", Epoxy Composite Laminates, 2002, pp.33, 521~529
- Camanho, P. P., "A Progressive Damage Model for Mechanically Fastened Joints in Composite Laminates", Journal of Composite Materials, 33(24), pp.2248~2280 (1999)
- Sun, H. T., "The Response of Composite Joints with Bolt-clamping Loads, Part I : Model Development", Journal of Composite Materials, 36(1), pp.47~67 (2002)
- Sun, H. T., "The Response of Composite Joints with Bolt-clamping Loads, Part II : Model Verfication", Journal of Composite Materials, 36(1), pp.69~91 (2002)
- Ladeveze, P., "Damage Modelling of the Elemmentary Ply for Laminated Composites", Composites Science and Technology, 43, pp.257~267 (1992)
- "ABAQUS 6.7 User's Manual" (2007), Simulia, Inc.
- Hearakovich, C. T., "Mechanics of Fibrous Composites" (1998), John Wiley & Sons, Inc.
- Laminate Statistical Allowable Generation for Fiber-reinforced Composite Materials: Lamina Variability Method, "Tomblin, J", ~, pp.DOT (2009), FAA[DOI]
- "ASTM D3518, Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45o Laminate", ~
