• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2004년도 춘계 학술발표회 제16권1호
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• pp.416-419
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• 2004

The kinetic energy during ship collision with bridge piers is released as the permanent deformations of structure and friction between the impact surfaces. So the ship collision energy is estimated from the equations of motions for ship-pier collisions which include the influence of the surrounding water, different impact angles and impact locations. The normal impact energy and tangent impact energy at a collision location and angle can be transformed into the normal impact force and friction force acting on the structure. Also the kinetic energy after collisions is calculated from the linear and angular impulse of ship collisions. The collision energy absorption system such as the protective structures for bridges is designed by evaluating the damage portions of ship and structure during the ship-structure collisions varying from the soft impact to hard impact and then the estimation of it will be suited for the design of protective measures.

• Journal of Mechanical Science and Technology
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• 제17권12호
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• pp.1894-1903
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• 2003

It is necessary to have a dummy that describes the anthropometry of a victim with accuracy. This study presents three scaled side impact dummies constructed for the use of MADYMO. They represent five, fifty and ninety-five percentile Korean males ranged from the age of 25 through 39. Thirty-five anthropometric data were used to scale input files required for MADYSCALE. Geometries, inertia, joints and other parameters for dummies were scaled based on the configurations of EuroSID-1. This study proposes the lateral impact response requirements for head, thorax and pelvis of Korean side impact dummies. A lateral drop impact test was conducted for the head at the height of 200 mm. Lateral pendulum impact tests were also carried out for thorax and pelvis at three specific impact velocities. All these test results were obtained from simulation based on MADYMO. All the procedures of the three tests followed the requirement of ISO/TR 9790.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.7-12
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• 2008

A hot stamping technology of vehicle door impact beam made of thin sheet steel has been developed, with the aim of ensuring occupant safety in a side collision. This technology has been implemented to increase the strength of vehicle body parts and to reduce not only the weight of door impact beam but also the number of work processes. Mechanical tests were performed to obtain material properties of hot-stamped specimen and those were used as input data in stamping and structural simulation for optimal design of door impact beam. Strength of hot-stamped door impact beam increased to the value 102% higher than that of conventional pipe-shaped door impact beam and structural simulation showed that hot-stamped door impact beam achieved 28% weight reduction.

• 한국정밀공학회지
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• 제29권6호
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• pp.654-663
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• 2012

Damage induced by low velocity impact loading in aircraft composite is the form of failure which is frequently occurred in aircraft. As the consequences of impact loading in composite laminates, matrix cracking, delamination and eventually fiber breakage for higher impact energies can be occurred. Even when no visible impact damage is observed, damage can exist inside of composite laminates and carrying load of the composite laminates is considerably reduced. The objective of this study is to evaluate and predict residual strength behavior of composite laminates by impact loading and for this, tensile test after impact was carried out on composite laminates made of woven CFRP.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1995년도 추계학술대회 논문집
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• pp.664-667
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• 1995

The purpose of this paper is to consider the disk failure phenomenon based on the second kind Fredholm integral equation and numerical inversion of Laplace transform when the head hit disk asperities at HDI under antiplane impact loading. The model for analysis is a two layeered half-space with a circumferential surface edge crack. The optimum design parameters to reduce the disk failure due to impact are presented

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2003년도 추계학술발표대회 논문집
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• pp.137-140
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• 2003

Impact of Automotive GMT(Glassfiber reinforced Mat Thermoplastic) Bumper for '5Mhp Barrier Test'was simulated using ls-dyna. The FE model consists of foam which is energy absorber, bumper beam and stay etc. Bumper intrusion and deflection was compared with the experimental results. Effects of uncertainty of material property and deviation of impact velocity were considered and results were compared with those of base design. Effects of number of integration points through th thickness was also investigated.

• 디지털융복합연구
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• 제15권7호
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• pp.223-229
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• 2017

유럽, 미국을 비롯한 일본 등 선진 업계에서는 오랜 기간의 시험을 거쳐 충격계수의 시험결과를 보유하고 있으며, 장비를 설계할 때 이를 적용하여 구조물의 안정성을 확보하고 있다. 그러나 국내 산업체의 실정으로는 실제 구조물이 받는 여러 가지 동적인 외력에 의한 영향을 시험을 통해 충격계수를 확보하기에는 많은 비용과 시간이 소요되기 때문에 선진업체에서 제공하는 충격계수를 활용하여 장비를 설계하고 있다. 본 논문에서는 유한요소해석 프로그램인 NX/NASTRAN을 이용하여 반도체 검사 장비인 PCB Handler의 정하중해석과 충격하중에 대한 과도응답 해석을 진행하고, 변위 결과를 비교하는 방법으로 충격계수를 산출하였다. 충격계수 산출 방법은 일본 구조 구격에서 사용하고 있는 방법을 적용하였으며, PCB Handler가 검사를 위해 급출발 또는 급정지 시 충격계수는 1.27로 산출되었다. 해석으로 얻어낸 충격계수는 향후 장비의 구조개선과 기존장비를 기반으로 제품 개발 시 사용할 수 있어 업계에 도움이 될 것으로 판단된다.

• 한국산학기술학회논문지
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• 제12권6호
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• pp.2463-2469
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• 2011

이동전화기의 낙하 충격 시 디스플레이 모듈의 파손은 이동전화기의 재료, 강성 및 형상에 의하여 많은 영향을 받는다. 이동전화기 개발의 초기 단계에서는, 디스플레이 모듈의 내구성을 판단하기 위하여 모듈을 지그에 장착하여 낙하시험을 수행한다. 본 연구에서는 OLED 모듈의 충격 시험을 수행하기 위한 지그를 개발하였다. 지그의 재료, 두께 및 리브의 개수와 방향 등을 설계변수로 고려하여 실제 이동전화기가 낙하할 때 OLED 모듈이 받는 충격 응력과 가장 유사한 응력이 발생하도록 지그를 개발하였다. ABAQUS/Explicit를 사용한 1.5m 높이 충격 해석에서, 개발된 지그에 장착된 OLED 모듈의 유리에서 발생하는 최대주응력은 이동전화기에 장착된 동일 모듈의 유리에서 발생하는 최대주응력과 유사함을 확인할 수 있었다.

• International Journal of Automotive Technology
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• 제6권6호
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• pp.643-655
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• 2005

The frontal crash optimization of S-shaped closed-hat section member using the homogenization method, design of experiment (DOE) and response surface method (RSM) was studied. The optimization to effectively absorb more crash energy was studied to introduce the reinforcement design. The main focus of design was to decide the optimum size and thickness of reinforcement. In this study, the location of reinforcement was decided by homogenization method. Also, the effective size and thickness of reinforcements was studied by design of experiments and response surface method. The effects of various impact velocity for reinforcement design were researched. The high impact velocity reinforcement design showed to absorb the more crash energy than low velocities design. The effect of size and thickness of reinforcement was studied and the sensitivity of size and thickness was different according to base thickness of model. The optimum size and thickness of the reinforcement has shown a direct proportion to the thickness of base model. Also, the thicker the base model was, the effect of optimization using reinforcement was the bigger. The trend curve for effective size and thickness of reinforcement using response surface method was obtained. The predicted size and thickness of reinforcement by RSM were compared with results of DOE. The results of a specific dynamic mean crushing loads for the predicted design by RSM were shown the small difference with the predicted results by RSM and DOE. These trend curves can be used as a basic guideline to find the optimum reinforcement design for S-shaped member.

• 한국철도학회:학술대회논문집
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• 한국철도학회 1998년도 창립기념 춘계학술대회 논문집
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• pp.377-384
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• 1998

The crushable front part of the conventional TGV is composed of 3 energy absorption zones; retractable coupler, protective headstock and honeycomb structure. This frontal part must absorb about 80% of the energy that should be done in a cra shworthy design. The conventional TGV can absorb 2MJ impact energy by the frontal end, but 5MJ is the design target for energy absorption in the next generation TGV. To accomplish this design goal, a new concept of design is necessary for energy absorbing components. In this paper, the design concept of the tube expansion energy absorber will be proposed and analyzed. The crash analysis of the energy absorber are performed by comparing the value of the theoretical equation wi th the simulation calculated from the commercial nonlinear FE-Code ‘PAM-CRASH’ S/W.