In this study, the fracture property of the bonded structure with aluminum foam is analyzed by using the closed aluminium foam for impact absorber. DCB and TDCB specimens manufactured with the single lap joint method of mode 3 are designed by varying the thickness. The static analysis through ANSYS finite element program is carried out on the specimen model due to each thickness. Also, the static experiment is performed in order to verify the analysis result. This study aims at comparing the shear strengths of the bonded structures of DCB and TDCB made with aluminum foam and investigating the mechanical properties.

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 tapered double cantilever beams(TDCB) with the type of mode Ⅲ are manufactured with aluminum foam. The fracture toughness at the joint of the structure bonded with only a adhesive can be obtained. The static analyses are carried out and verified the results by the experiment. As the results of static analyses, the reaction forces ranged from 0.30 to 0.41 kN at all specimens are shown when the forced displacements are proceeded as much as 7 to 9 mm. As the results of analyses and experiments are compared with each other, there is a little bit of difference between these results. Through the result of this study, the mechanical properties at TDCB specimens with the type of mode Ⅲ can be understood.

The simulation analysis about the mechanical behavior by thickness on the compression procedure of the bonded aluminum foam is carried out in this paper. The maximum equivalent stress is increased very rapidly at three models. This stress approaches the yielding point when the compressive displacement is proceeded as much as 6mm. After yielding point, this stress approaches the maximum point. A value of this stress is about 1.0MPa. The reaction force approaches the maximum point when the compressive displacement is proceeded as much as 6mm. These reaction forces are shown to be 3000N, 5000N, 7100N respectively at the specimen thicknesses of 15, 25 and 25 mm. The maximum deformation energy is abruptly increased from the displacement of 6 mm and the compressive energy in case of the specimen thickness of 15 mm is shown to highest among three specimens when the displacement is proceeded as much as 13 mm. The experiment with the case of specimen thickness of 25mm is carried out in order to verify these analysis results. The mechanical properties of the bonded structures composed of aluminum foams can be thought to be analyzed effectively.

Because aluminum foam is porous material, the frature property is different from that of non-porous material. This aluminum foam can be used with the joint bonded with adhesive in order to utilize the light weight to the maximum. So, the study of fracture property on bonded surface can be important. In this study, the analyses on the specimens with two kinds of configuration as DCB(Double Cantilever Beams) and TDCB(Tapered Double Cantilever Beams) aluminum foams of mode Ⅲ type bonded with adhesive are carried out and compared with each other. And the fracture properties the adhesive surfaces of the structure with bonded aluminum foams are studied as the static experiments on these verifications are done. DCB and TDCB specimens used in this study have the variable of thickness(t) as 35mm, 45mm and 55mm. As the result of this study, the range of reaction forces are 0.3 to 0.8 kN and 0.5 to 1.2 kN at DCB and TDCB specimens respectively. The results of the static experiments can also be confirmed with these similar results. These study results can be obtained by only a simulation without the special experimental procedures. The mechanical properties of the bonded structures composed of DCB and TDCB aluminum foams with mode Ⅲ type can be thought to be analyzed effectively.

Nowadays, the study of CFRP reinforced with carbon fiber is focused on improving the the mechanical property. The study on the fracture data of CFRP are not properly made out than that of the general mechanical joint. In this study, the fracture property of mode 1 at the same condition of tensile experiment is investigated by applying the layer angle to laminated CFRP with the thickness of 15 mm. When the reaction forces until dropping out the bonded surface are compared with the cases of the layer angles of 0°, 45° and 60°, the reaction force is shown to be most and the elapsed time until dropping out the bonded surface is longest at that of 45°. The deformation energy is also shown to have the highest value by dropping out the adhesive interface. As the basis of the analysis result of this study, the most safety with fracture resistance is shown in the case of 45°. the bonded structure applying the appropriate layer angle is thought to have the structural safety.

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.

As the property of the aluminum foam with porosity, the effect of impact is distributed through the distortion of each lattice like honeycomb at impact. So, this porous aluminum foam is widely used at the crash box or the impact absorber guard rail to prevent the damage. In addition, there is a property of low weight by the chemical bonding using the adhesive. As this study investigates the distortion property of the aluminum foam bonded with adhesive, the fracture property and the stress distribution of the bonded interface are examined. The specimen thicknesses are 25, 35, 45, 55 and 65 mm. And the torsional moments corresponding to 100, 200 and 300 J are applied at one side of bonded aluminum foam. The mechanical behaviors at the bonded interface and the fixed part are also investigated. It can be seen that the minimum specimen thickness must become 55 mm and over in order to maintain the bonding force due to the applied impact energy. The analysis result of this study at the bonded interface effected on impact can be effectively applied into the safe design of the structure with the bonded aluminum foam.

An aluminum foam is the super light metal which can be adjusted with the adhesive by using the joint method. In this study, the tapered double cantilever beams(TDCB) with the type of mode Ⅲ are manufactured with aluminum foam. The fracture toughness at the joint of the structure bonded with only a adhesive can be obtained. The static analyses are carried out and verified the results by the experiment. As the results of static analyses, the reaction forces ranged from 0.30 to 0.41 kN at all specimens are shown when the forced displacements are proceeded as much as 8 to 9 mm. The tapered double cantilever specimen for mode Ⅲ with the thickness of 55 mm is carried out by the static experiment representatively to verify the analysis results. As the results of analyses and experiments are compared with each other, there is a little bit of difference between these results. So, the simulation results of this study can be thought to be confirmed. It is thought that even the only analysis data omitting the extra experimental procedure can be verified in order to use the data practically. Through the result of this study, the mechanical properties at TDCB specimens with the type of mode Ⅲ can be understood.

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.

This study investigates the property of crack growth at the specimen of structural steel. The behaviour of fracture mechanics on the specimens with only a center crack and with holes existed symmetrically near a center crack is studied. The tensile load is applied on the specimens with these conditions. Stress intensity factors are obtained by the basis of these experimental values and these values are verified with the structural analysis of finite element method. As the length of center crack becomes larger in case of the specimen with holes existed symmetrically near a center crack, the values of deformation energy and stress become larger. On the contrary, the values of deformation energy and stress become smaller as the length of center crack becomes larger in case of the specimen with only a center crack. By examining the stress intensity factor in this study, this value becomes rather smaller although the length of center crack becomes larger. There is the position where crack is likely to happen or weak part at the mechanical structure or the machine. As the holes are punctured and arranged adequately near this crack or weak part by using the result of this study, the fracture due to it can be prevented.

본 연구에서는 무릎 굽힘각도와 완충재사이의 상관관계를 통해 올바른 걸음걸이의 중요성과 완충재의 마모에 관해 해석하였다. 완충재에 가해지는 등가응력의 분포형상을 볼 때, 그 마모의 정도를 유추할 수 있어 이를 통하여 인공관절 상, 하부 파트의 설계와 인공관절 착용자의 바른 자세를 유도할 근거를 제시할 수 있다. 본 연구를 통하여 얻어진 무릎관절의 역학적 메커니즘과 인공관절을 삽입했을 때 나타나는 메커니즘에 대한 구조 해석 결과를 적용하여 무릎관절에 가해지는 피해량에 대하여 해석할 수 있다. 또한 실제 시험을 위해 예비된 시뮬레이션 해석 결과로서 실제의 생체실험에 대한 기초연구 자료로 제공될 수 있으며 그 실험과의 비교 분석 자료로도 사용할 수 있을 것으로 사료된다.

본 연구에서는 구조용강 시험편 내의 크랙의 성장특성을 주제로 하여 중앙크랙만이 존재하는 시험편과 중앙 크랙의 주변에 대칭으로 구멍들이 존재하는 시험편에 대한 파괴역학적 거동을 규명하고자 하였다. 구조용강으로 만들어진 시험편 내에 두 가지의 조건들을 적용하여 인장실험을 수행하였으며, 이를 통하여 시험편의 응력, Strain energy와 변형량에 대하여 해석하였다. 그리고 이러한 실험값들을 바탕으로 하여 응력확대계수를 구하였으며, 구해진 실험값들의 검증을 위하여 ANSYS 유한요소 해석 프로그램을 사용하여 시뮬레이션 해석을 수행하였다.

본 연구에서는 구조용강 내 크랙의 성장특성을 크랙의 길이와 각도에 따라 규명하였다. 구조용강으로 만들어진 시편 내의 크랙에 위에 언급한 두 가지의 조건들을 적용하여 실험을 수행하였으며, 이를 통해 Strain energy와 변형량에 대해 알 수 있었다. 그리고 이들 Strain energy와 변형량을 바탕으로 응력확 대계수를 구하였으며, 구해진 실험값들의 검증을 위하여 유한요소 해석 프로그램을 사용하여 시뮬레이션 해석을 수행하였다.

본 연구는 전문가집단을 대상으로 식품안전사고 발생 시 ‘보도용어’와 ‘대응용어’에 대한 인식도 차이를 알아보고 용어선택에 따른 피해정도를 개선하기 위한 기초자료를 제공하고자 실시하였다. 식품기업체 식품안전관리책임자 28인과 식품전문기자 17인 총 45인을 대상으로 인식도 조사 및 개선방안에 대해 설문조사하여 통계분석 하였다. 그 결과, 식품안전사건 발생 시 미디어의 영향이 크다는 질문에 기자 70.6%, 기업체 92.9%가 ‘매우 그렇다’의 응답률을 보였다. 미디어의 자극적인 용어사용이 기업피해의 원인이라는 인식에는 기업체의 83%가 ‘매우 그렇다’, 기자의 70.6%가 ‘그렇다’로 답해 양측 모두 자극적 용어사용으로 인한 기업피해를 인식하고 있었다. 미디어의 ‘보도 용어’와 정부, 학계 등의 ‘대응용어’가 소비자의 인식과 사건의 파급에 차이를 주는지를 묻는 질문에 기업체의 92.9% 와 기자의 35.3%가 ‘매우 그렇다’로 답해 두 집단 모두 용어의 차이가 소비자의 인식뿐 아니라 파급을 확대시킨다는데 공통적인 의견을 보였으나 기업이 훨씬 심각하게 느끼고 있었다. ‘보도용어’의 통일 및 사용제한에 대해 기 업체는 전반적으로 긍정적인 입장이고 기자는 긍정과 부정으로 답변이 나뉘어 개인차가 컸다. 식품안전사건 발생 시 소비자와 기업체의 피해를 줄이기 위해 기업과 기자, 전문가간 사용하는 용어의 일치 및 차이를 좁힐 수 있는 방안 마련이 필요하다고 사료된다.