This study is investigated by the analyses of modal and harmonic response on BH motor, VI motor and DH motor. The natural frequency of DH motor becomes lower than that of VI motor. As the maximum amplitude of displacement is shown to be 2.06×10-2mm at 1300 Hz in case of BH motor, BH motor can be thought to be the best structure in comparison with VI motor and DH motor. The deformation of 0.34806 mm happens at the critical frequency in case of BH motor. And the maximum deformation happens at the joint connected between screw axis and seat in cases of three kinds of motors. By applying the result of this study to the designs of these kinds of motors, it is thought that the damage of linked parts is prevented. As the durability can be examined and anticipated, this result can be utilized really

In this study, the models before and after improving the support structure of seat motor gear nut are investigated by comparing with vibration analysis. The maximum deformation model 1 becomes higher than model 2. The natural frequency of model 2 becomes higher model 1. The design model to be applied into the safe driving is useful effectively by using the analysis result of the height driving module for automotive power seat.

In this study, carbon fiber reinforced plastic and aluminum foam used in impact absorber are assembled and modelled. These models are investigated by impact simulation and verified by experimental data. Impact energies of 30 J, 60 J and 100 J are applied on these specimens by striker. For example the experiment for impact energy of 30 J is done and verified by referring to analysis result. As the structural safeties of these assembled composite materials can be anticipated through this study result, these simulation analysis results can be applied into real field.

In this study, tapered double cantilever beam bonded with aluminum foam composite is modelled and analyzed by finite element analysis. The bonding strength on Mode II of this structure is evaluated and investigated. In cases of inclined angles of 6°, 8° and 10°, maximum equivalent stresses occur 1.29, 1.59 and 2.6 MPa respectively at the range of forced displacement of 5 to 6 mm. And maximum reaction forces become 186, 208 and 235 N individually at this range of displacement in these cases. By the analysis result on 3 kinds of models, the maximum reaction load increases as angle of inclination of model increases. And the elapsed time to approach the maximum load and the time to disappear away become shorter. This study result can be applied into the real composite structure with aluminum foam in case that the surface bonded with adhesive is inclined. This fracture behavior can also be investigated and the impact property can be examined

In this study, the strength property is investigated through structural and vibration analysis on the lead screw of height drive module for automotive power seat. The positions of applied loads are lowest, middle and highest on the model of lead screw in cases of 1, 2 and 3. Natural frequencies are examined about three kinds of models and critical frequencies are also checked by harmonic responses. Maximum deformations are shown as 0.033mm, 0.026mm and 0.551mm respectively in models of 1, 2 and 3. In case 3 at highest position, this strength becomes weakest by comparing with cases 2 and 3. By use of this analysis result, it is possible to design the model effectively applied at automotive safe driving.

Various motors have been used in many cars to control the height of automotive seats. As the motor is connected with seat, it can be moved as the convenience of passenger and vibration affects passenger when motor is being driven. In this study, three models are designed. The lengths of link parts and screw axes are increased or decreased respectively in the order of models 1, 2 and 3. The case of motor is made of aluminum alloy and the rest is made of structural steel. As model 1 has the maximum amplitude displacement at 1360Hz by the basis of vibration analysis, model 1 has the most durability among three models. This study result can be effectively utilized with the design on height motor by investigating prevention and durability against its damage.

차량, 수송, 조선 등 많은 산업이 발전함에 따라 기계장치를 구성하고 있는 각종 재료의 특성 또한 날로 발전하고 있다. 과거 단순 강만 사용하여 기계를 설계하던 것과 달리 현재는 특수합금강과 복합재료를 사용하여 기계의 성능을 향상시키고 있다. 이처럼 많은 산업 분야에서 재료의 특성을 파악하여 적시 적소에 사용하여 기계를 설계하는 것은 기계설계자들에게 매우 중요한 과제가 되었다. 본 논문에서는 알루미늄 폼 복합재료로 된 TDCB(이중외팔보) 시험편의 파괴 거동을 시뮬레이션 해석과 실험 검증하였다. 실험과 해석에 사용된 모델은 영국 공업규격과 ISO국제규격에 의거한 3D 형태로 하였다. θ=12°일 때의 해석 결과로 한쪽 Beam이 일정한 속도로 이동하면서 접착력에 대한 반력이 발생하는데 Beam이 약 5mm 이동하였을 때 약 270N의 최대 반력이 나타나는 것을 볼 수 있다. 본 연구에서는 실험과 유한요소법을 통한 비교분석으로 물성데이터를 확보하고, 실험결과와 해석결과의 유사성을 검증하여 보다 쉽고 빠른 소재의 특성을 파악하는 방법을 검증해 보았다.

본 논문에서는 탄소 섬유 강화 플라스틱 샌드위치 복합재료의 시뮬레이션 해석을 통해 기계적 충격특 성에 대해 연구를 하였다. 스트라이커에 30 J, 60 J, 100 J의 충격에너지를 부여하여 고정 된 시험편에 충격을 가했다. 시뮬레이션 해석 방법은 ANSYS를 이용하여 실제와 같은 경계조건을 주며 유한요소해 석을 진행하였다. 그 결과는 100J의 충격에 에너지를 가해졌을 때 스트라이커가 시험편을 완전히 관통하는 모습이 보이고 충격에너지 30J과 60J일 때는 스트라이커가 시험편을 관통하지 않았다. 본 연구의 결과로 탄소 섬유 강화 플라스틱과 알루미늄 폼으로 조립한 복합재료의 구조적 안전성을 예측과 구조적 안전성이 높이는 사료가 된다.

본 연구에서는 텅스텐합금강의 상부구조와 폴리에틸렌소재로 구성된 하부구조의 인공관절이 하중을 받았을때의 인공관절의 하중분포와 인공관절의 설치를 위한 지지구멍에 가해지는 응력분포에 대하여 유한요소해석을 통하여 결과값을 도출하였으며, 실물을 이용한 다음 실험을 위한 기초자료를 얻을 수 있었다. 이를 통하여 나온 해석결과의 하중분포는 텅스텐합금의 상부구조가 모서리 끝부분부터 하중이 집중되어 크랙이 발생하며 이는 의학계에 보고된 인공관절파손에 의한 조직괴사사례와 그 거동이 일치 하였다.

Britsh StandardBS 7991)에 명시된 DCB 시험편을 본 연구에 맞게 수정 후 두께 25mm, 35mm, 45mm, 55mm, 그리고 65mm의 DCB시험편을 제작하였다. 이 후 시험편을 Single-lap 방식으로 접착한 후 정적실험에서 도출된 최대 전단력을 각 시험편에 10Hz로 피로하중을 가하였다. 실험 결과값에 대한 수치해석적 검증을 하고자 상용 해석 프로그램인 ANSYS를 통해 실험과 동일한 시험편과 조건 하에 해석을 수행하였다. 접착력 해석을 하기 위해서 Mesh의 절점(node)들의 관계가 매우 중요하기 때문에 접착된 부분의 모든 절점들은 동일 선상에 있게 Mesh를 형성하였다. 실험 결과와 해석 결과를 비교해 본 결과 피로하중이 약 200cycle 반복되었을 때 최대 등가응력이 발생 하였고, 이때 전단방향으로 변위가 약 11mm 진전 된 것을 볼 수 있었다. 이후 4000cycle가량 피로하중이 반복 될 동안 변위는 일정하게 점점 증가한 후 피로하중이 약 4800cycle 반복 되었을 때 실험과 해석 데이터 모두 접착계면에서 완전한 전단 파괴가 일어난 것을 볼 수 있었다. 이때 변위는 약 20mm 진행 되었다. 해석을 통해 실험 데이터를 검증해 본 결과 두 결과 값은 완전 하게 같지는 않지만 유한요소법 해석 결과에 대한 신뢰를 확보 할 수 있었다. 이는 실제 구조물에 실험 없이 간단한 재료 물성치만으로도 해석을 통하여 구조적 안전성을 알아 볼 수 있는 한 방법이 될 수 있을 것이라고 사료된다.

Adhesive joint method has been used instead of welding, reveted joint, bolt and nut in various industry fields recently. Aluminum foam has hole or crack on adhesive interface which is different from common composite material. To investigate shear characteristic of adhesive interface between aluminum foams, double cantilever beams(DCB) with thicknesses of 25mm, 45mm and 65mm bonded with single-lab joints are designed. The relation between nodes at finite element model is important to investigate adhesive strength in this study. All meshes are generated and some nodes are located on adhesive zone along collinear axis. As reaction force obtained by static experiment is applied, fatigue analysis is carried with 10Hz. In advance, adhesive property is obtained by preliminary experiment for applying adhesive strength to input into simulation analysis. With these conditions, the analysis results show that 2.97MPa, 3.10MPa and 4.2MPa of maximum equivalent stresses are shown respectively in case model thicknesses are 25mm, 45mm and 65mm. By use of the simulation result at this study, it is possible to find adhesive behavior of aluminum foam and be applied to real adhesive joint structure without experiment by sparing experimental cost and time

In this study, recliner is modelled and compared with 2 types of models as conventional recliner and round recliner by investigating stress and displacement through strength analysis. The maximum deformation of 0.018mm at round recliner is much smaller than that of 0.18mm at conventional recliner. It can be seen that the round recliner has more safety than conventional recliner. Round recliner model has more durability and safety than conventional model by the result of structural and vibration analysis. The model design of automotive recliner can be designed effectively at applying the safe driving of automobile practically by using the result of this study.

In this study, the property of crack growth in structural steel is investigated according to length and angle of crack at the analysis result of model. Strain energy, deformation and stress obtained by finite element analysis are compared with various configuration of crack. Stress intensity factors as fracture toughness are calculated by the basis of strain energy, deformation and stress. As there are almost no errors by comparing stress intensity factors with those from the standard formula, these calculated factors can be confirmed in order to be applied at real structure. In case cracks or holes at structure are existed, the fatigue damage possibility can be examined by use of this study result.

Tapered double cantilever beam (TDCB) specimens are the most commonly used test configurations to measure the fracture toughness of composites and adhesive joints. The material used in this study is aluminum alloy. For the impact analysis, load and displacement applied from pin onto end block as well as the crack energy release rate are calculated and compared with the finite element analysis results. The energy release rate increases with the velocity increases. As TDCB model with the same condition as experiment is simulated and analyzed, the fracture behavior can be estimated with the analysis result similar to experiment. The simulation results can be agreed with experimental graph and all experimental data at this study can be verified. These experimental results can be applied into real field effectively. It is found that the energy release rates measured from impact tests on the specimens can be predicted by the finite element model suggested in this study.

In this study, simulation analyses on the impact property of aluminum foam are carried and verified by experimental results. When aluminum foams with thicknesses of 25mm and 35mm are applied by impact energy of 14J, impact energy and deformation happened at aluminum foam are investigated by comparing experimental and analysis results. Experimental and analysis results of deformations or absorbed impact energy become similar each other. After verifying these simulation results with experimental results, impact properties of aluminum foams with thicknesses of 45mm and 55mm are also investigated by simulation results. As impact properties of aluminum foam can be studied effectively through only simulation results, it is thought to spare much time and cost by investigating various impact properties of aluminum foams with simulation analysis.

This study aims to evaluate structural safety through FEM on the hollow shaft and the shaft filled with aluminum foam as the impact beam made of high tensile strength steel, Force reactions of impact beams are investigated when the forced displacement of 50mm is applied equally on two beams. When impact velocity of 80km/h is applied onto impact beams equally with the limit velocity of automobile on national road, how much impact energies can be absorbed by beams are also investigated. As study result, impact beams without aluminum foam and with aluminum foam show the maximum reaction forces of 15.53kN and 20.34kN respectively in case of the forced displacement of 50mm. As impact analysis result, impact beams without aluminum foam and with aluminum foam can absorb impact energies of 560J and 820J respectively. As impact beam with aluminum foam has reaction force and impact energy more than 23% and 30% than without aluminum foam, impact beam with aluminum foam has more safety than without aluminum foam.

알루미늄 폼을 볼트나 너트를 이용하여 체결한다면 경량성이 감소되므로 접착제로 접합하는 것이 가 장 효율적이다. 이런 알루미늄 폼 접착 구조물에 대한 충격 피로 특성과 접착 합면에 대한 파괴인성 연 구는 매우 부족하며 또한 중요하다. 이에 따라 본 연구에서는 알루미늄 폼으로 만들어진 DCB모델을 접 착제로 접합한 후 두께를 변수로 하여 25mm 부터 45mm까지 10mm차이를 두어 실험과 컴퓨터 시뮬레 이션을 통하여 수행하였다. 실험은 MTS사의 인장 시험기를 사용하여 강제 변위 100mm를 주어 변위에 따른 전단력을 알아보았고, 실험과 똑같은 조건하에 ANSYS를 이용하여 유한요소해석을 수행하였다. 실험과 유한요소해석 값을 비교하여 접착제로 접합된 알루미늄 폼 구조물의 접착 합면에 대한 파괴인성을 고찰하였다.

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.