Mode Ⅲ 형 DCB 알루미늄 폼에 대한 정적 파괴 및 검증
Static Fracture and Verification on DCB aluminum foam of with Type Mode Ⅲ
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초록
As a part of light weight, the adhesive has been applied to joint the mechanical structure. The porous material is used with aluminum foam in case of the structure bonded with only adhesive. In order to confirm the durability, it is necessary to investigate the fracture toughness at the bonded joint. So, the fracture property at joint interface of aluminum foam different from the non-porous material becomes especially important. In this study, the static facture analysis was carried out with DCB specimen bonded with adhesive as the loading type of mode Ⅲ. The thicknesses of specimens are 35, 45 and 55 mm. When the forced displacements 5 mm applied on the specimen proceed at specimen thicknesses of 35, 45 and 55 mm, the maximum stresses is shown to be happened at the range from 3.3 MPa to 3.6 MPa. The maximum equivalent stress happened at the specimen thickness of 35mm becomes highest among four kinds of specimens. The static experiment is carried on in order to verify these analyses representatively. As the experimental data become similar with the simulation data, it is thought that these analysis data can be applied at analyzing them into the adhesive joint of real porous material.
Abstract
As a part of light weight, the adhesive has been applied to joint the mechanical structure. The porous material is used with aluminum foam in case of the structure bonded with only adhesive. In order to confirm the durability, it is necessary to investigate the fracture toughness at the bonded joint. So, the fracture property at joint interface of aluminum foam different from the non-porous material becomes especially important. In this study, the static facture analysis was carried out with DCB specimen bonded with adhesive as the loading type of mode Ⅲ. The thicknesses of specimens are 35, 45 and 55 mm. When the forced displacements 5 mm applied on the specimen proceed at specimen thicknesses of 35, 45 and 55 mm, the maximum stresses is shown to be happened at the range from 3.3 MPa to 3.6 MPa. The maximum equivalent stress happened at the specimen thickness of 35mm becomes highest among four kinds of specimens. The static experiment is carried on in order to verify these analyses representatively. As the experimental data become similar with the simulation data, it is thought that these analysis data can be applied at analyzing them into the adhesive joint of real porous material.
참고문헌 (7)
- 최해규, "알루미늄 폼 복합재료로 된 접합된 DCB 시험편의 구조 해석에 관한 연구", 한국산학기술학회논문지, 13(4), pp.1488~1495 (2012), 한국산학기술학회
- 방혜진, "접착제로 접합된 이중외팔보 알루미늄폼의 파괴 거동에 관한 연구", 대한기계학회논문집 A, 38(5), pp.521~526 (2014), 대한기계학회
- 최해규, "접착제로 접합된 DCB 시험편의 피로 해석에 관한 연구", 한국산학기술학회논문지, 13(7), pp.2865~2871 (2012), 한국산학기술학회[DOI]
- 최해규, "알루미늄 폼으로 된 DCB 모델의 피로해석에 관한 연구", 한국기계기술학회지, 14(6), pp.39~43 (2012), 한국기계기술학회
- 최해규, "알루미늄 폼으로 된 이중외팔보 시험편의 파괴 거동에 관한 실험적 연구", 한국기계기술학회지, 14(5), pp.37~41 (2012), 한국기계기술학회
- 김정석, "정적 및 피로시험에 의한 틸팅열차용 볼스터의 구조강도평가", 대한기계학회논문집 A, 30(2), pp.210~218 (2006), 대한기계학회
- Y. H. Seo, "Desing, Fabrication, Static Test and Uncertainty Analysis of a Resonant Microaccelerometer Using Laterallydriven Electrostatic Microactuator", Journal of the Korean Society of Mechanical Engineers, 25(3), pp.520~528 (2001)
