• 제목/요약/키워드: Finite Element Impact Analysis

검색결과 787건 처리시간 0.026초

승용차 시트프레임의 강도해석 (The Strength Analysis of Passenger Car Seat Frame)

  • 임종명;장인식
    • 한국자동차공학회논문집
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    • 제11권6호
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    • pp.205-212
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    • 2003
  • This paper may provide a basic design data for the safer car seat mechanism and the quality of the material used by finding out the passenger's dynamic behavior when protected by seat belt during collision. A computer simulation with finite element method is used to accomplish this objective. At first, a detailed geometric model of the seat is constructed using CAD program. The formation of a finite element from a geometric data of the seat is carried out using Hyper-Mesh that is the commercial software for mesh generation and post processing. In addition to seat modeling, the finite element model of seat belt and dummy is formed using the same software. Rear impact analysis is accomplished using Pam-Crash with crash pulse. The part of the recliner and right frame is under big stress in rear crash analysis because the acceleration force is exerted on the back of the seat by dummy. The stress condition of the part of the bracket is checked as well because it is considered as an important variable on the seat design. Front impact model which including dummy and seal belt is analyzed. A Part of anchor buckle of seat frame has high stress distribution because of retraction force due to forward motion of dummy at the moment of collision. On the basis of the analysis result, remodeling and reanalysis works had been repeatedly done until a satisfactory result is obtained.

코트 스포츠화의 착지충격 평가를 위한 유한요소 해석 (Finite Element Analysis for the Landing Impact Evaluation of Court Sport Shoes)

  • 김성호;조진래;류성헌;최주형
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.438-443
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    • 2004
  • Court sport shoes is consisted of several functional parts such as soles, upper and midfoot reinforcements. Currently, intensive research for court sport shoes considering functional parts is in progress world widely, but the shoes design relies only on the view point of kinesilogy and biomechanics until now. Thus, more scientific and reliable evaluation of shoes characteristics is definitely required. In this paper, we evaluate the landing impact of court sport shoes by using finite element method. We construct a shoes-leg coupled FEM model which can simulate effectively impact in running mode. From the numerical analysis results, the designer can establish the advanced design concepts and build up the detailed design standard for the specific court sport shoes under consideration.

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Analysis of the 3-D Stress Wave in a Plate under Impact Load by Finite Element Method

  • Jin, Sung-Hoon;Hwang, Gab-Woon;Cho, Kyu-Zong
    • International Journal of Precision Engineering and Manufacturing
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    • 제2권2호
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    • pp.5-10
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    • 2001
  • This paper attempt to explore the shape of stress wave propagation of 3-dimensional stress field which in made in the process of the time increment. A finite element program about 3-dimensional stress wave propagation is developed for investigating the changing shape of the stress by the impact load. The finite element program, which is the solution for the 3-dimensional stress wave analysis, based on Galerkin and Newmark-${\beta}$ method at time increment step. The tensile stress and compressive stress become larger with the order of the middle , the upper and the opposite layers when the impact load is applied. In a while the shear stress become larger according to the order of the upper, the middle and the opposite layers when impact load applied.

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착지모드에 따른 신발-족 연계모델의 충격특성 유한요소 해석 (Finite Element Analysis of Impact Characteristics of Shoes-Leg Coupled Model to landing Mode)

  • 류성헌;김성호;조진래
    • 대한기계학회논문집A
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    • 제29권9호
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    • pp.1191-1198
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    • 2005
  • This paper is concerned with the numerical investigation of the landing impact characteristics of sport shoes to the landing mode. In most court sport activities, jumping and landing are fundamental motions, and the landing motion is largely composed of forefoot and rearfoot landing modes. Since the landing impact may, but frequently, lead to unexpected injuries of players, the investigation of its characteristics and the sport shoes design for reducing it are of a great importance. To investigate the landing impact characteristics to the landing mode, we construct a shoes-leg coupled model and carry out the numerical simulation by an explicit finite element method.

터보팬 엔진 나셀용 샌드위치 복합재 구조물의 손상 거동 연구 (Study on Impact Damage Behavior of Turbo Fan Engine Nacelle Sandwich Composite Structure)

  • 공창덕;박현범;이승현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.75-78
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    • 2007
  • 본 연구에서는 터보 팬 엔진 나셀 복합재 구조의 충격 손상에 관한 연구를 수행하였다. 연구 결과의 신뢰성 검증을 위해 선행 연구된 결과와 비교 분석하였다. 샌드위치 구조의 형상은 카본/에폭시 면재와 폼 코어로 형성되어있다. 샌드위치 패널의 유한 요소 해석 결과 해석 결과의 타당성을 확인하였다. 초기 손상이 발생하는 속도가 평가되었고 예측된 속도에서 충격 해석이 수행되었다. 충격 해석 결과 예측된 충격 손상에서 손상이 발생하는 것으로 확인되었다.

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유압브레커의 모델링 및 피스톤과 치즐간의 탄성충돌을 고려한 해석 (Modeling and Analysis of a Hydraulic Breaker Considering Elastic Impact between the Piston and the Chisel)

  • 고승환;임종혁
    • 대한기계학회논문집
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    • 제19권2호
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    • pp.338-347
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    • 1995
  • Equations of motion and continuity equations of a hydraulic breaker are derived. Hydraulic pressures are defined with 6 state variables corresponding to 6 control volumes. Impact analysis procedure of the piston and chisel is developed based on the finite element nodal displacement description. Computer simulation is performed with given design parameters and the results are compared with experimental results.

Analysis of impact response and damage in laminated composite cylindrical shells undergoing large deformations

  • Kumar, Surendra
    • Structural Engineering and Mechanics
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    • 제35권3호
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    • pp.349-364
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    • 2010
  • The impact behaviour and the impact-induced damage in laminated composite cylindrical shell subjected to transverse impact by a foreign object are studied using three-dimensional non-linear transient dynamic finite element formulation. A layered version of 20 noded hexahedral element incorporating geometrical non-linearity is developed based on total Langragian approach. Non-linear system of equations resulting from non-linear strain displacement relation and non-linear contact loading are solved using Newton-Raphson incremental-iterative method. Some example problems of graphite/epoxy cylindrical shell panels are considered with variation of impactor and laminate parameters and influence of geometrical non-linear effect on the impact response and the resulting damage is investigated.

후방 충격압출 성형 공정의 FVM과 FEM의 적용성에 관한 연구 (A Study on the comparison of FEM and FEM for Backward Impact Extrusion Process)

  • 정상원;조규종;김성훈
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2003년도 춘계학술대회 논문집
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    • pp.1565-1568
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    • 2003
  • The backward extrusion process is one of the commonly used metal forming processes. In this paper. a battery case which has the rectangular section, is analyzed using a 3D metal forming package(MSC.Superforge). This pacakge uses the finite volume analysis method. It is shown that the MSC.Superforge package using finite volume method provides result very close to those obtained from a finite element analysis package(MSC.Superform). However, the simulation time using the finite volume method was almost 10 % of the simulation time consumed by the other package using finite element method. Moreover, the finite volume method used in MSC.Superforge can eliminate the remeshing problems that make the simulating a metal forming process with severe deformation, such as the extrusion process, so difficult.

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Finite element analysis of RC walls with different geometries under impact loading

  • Husem, Metin;Cosgun, Suleyman I.;Sesli, Hasan
    • Computers and Concrete
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    • 제21권5호
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    • pp.583-592
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    • 2018
  • Today, buildings are exposed to the effects such as explosion and impact loads. Usually, explosion and impact loads that act on the buildings such as nuclear power plants, airports, defense industry and military facilities, can occur occasionally on the normal buildings because of some reasons like drop weight impacts, natural gas system explosions, and terrorist attacks. Therefore, it has become important to examine the behavior of reinforced concrete (RC) structures under impact loading. Development of computational mechanics has facilitated the modeling of such load conditions. In this study, three kinds of RC walls that have different geometric forms (square, ellipse, and circle) and used in guardhouses with same usage area were modeled with Abaqus finite element software. The three configurations were subjected to the same impact energy to determine the geometric form that gives the best behavior under the impact loading. As a result of the analyses, the transverse impact forces and failure modes of RC walls under impact loading were obtained. Circular formed (CF) reinforced concrete wall which has same impact resistance in each direction had more advantages. Nonetheless, in the case of the impact loading occurring in the major axis direction of the ellipse (EF-1), the elliptical formed reinforced concrete wall has higher impact resistance.

후방 충격압출 공정개선을 위한 유한요소 해석기법 연구 (A Study on FE Analysis For Improvement of Backward Impact Extrusion Process)

  • 정상원;정용호;김규하;조규종
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2002년도 추계학술대회 논문집
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    • pp.641-645
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    • 2002
  • In case of aluminum-cased battery, The ratio of height and base of square is generally above the ten times, square-shaped and problem of non-axis symmetry. It is typical model to set up the analysis method of finite element. The reliable analysis of finite element method is suggested, which is used to investigate the possibility that multi-stage deep drawing and ironing used currently is replaced by backward impact extrusion favorable in the respect of cost production and productivity. The influence of parameter was analyzed and compared, which was considered to analyze the process of large deformation plasticity such as extrusion. Die and billet was made as the same shape of finite element model. The results of experiment show good forming without the rupture and wrinkles with the optimum velocity 100mm/sec obtained by analysis.

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