• Title/Summary/Keyword: 실물충돌시험

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Analysis between Computer Simulation and Real-car Crash Test of Energy Absorption Facilities for Various Road Environments (다양한 환경에 적용 가능한 충격흡수시설의 시뮬레이션 분석 및 실물충돌시험 결과 분석)

  • No, Min Hyung;Park, Jea Hong;Seo, Chang Won;Sung, Jung Gon;Yun, Duk Geun
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.42 no.3
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    • pp.399-407
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    • 2022
  • Energy absorption facilities installed on roads should follow the performance standards of the real-car crash test of 'Installation and Maintenance Guidelines for Roadside Safety Facilities'. However, due to different installation conditions, such as differing structure widths on roads, some energy absorption facilities do not provide adequate performance. In order to apply varied environments on roads, an energy absorption structure was designed in this study with 150 mm height and four layers of W-shape guardrail at 200 mm intervals, and the performance was verified using LS-DYNA computer simulation. Through a real-car crash test, the performance of the facility designed by LS-DYNA was tested and was found to meet the performance of the CC2 category for crash cushions. The conclusion of the comparison demonstrates that the simulation and the real-car crash tests are both significant.

Assessment on the Possibility of Increase of SB5-B Small Car Impact Velocity (SB5-B 소형차 충돌속도의 상향 가능성 평가)

  • Kim, Kee-Dong;Ko, Man-Gi;Joo, Jae-Woong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.6
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    • pp.3013-3022
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    • 2013
  • Satisfying the large car impact condition of the high level SB5-B for "SMART Highway" longitudinal barriers, the possibility of increase of the small car impact velocity from 120km/h to 130km/h was investigated. Through computer simulation using input parameters calibrated to full-scale crash test results, various longitudinal semi-rigid barrier models were improved such that for the small car impact speed of 120km/h the change of longitudinal and transverse velocities of the impact vehicle can satisfy the THIV limit. The barrier model determined through this process satisfied the performance assessment criteria for SB5-B impact conditions. Varying the wing angle of slip block-outs of the passed barrier model, the possibility of increase of the small car impact velocity was investigated by FEA and a full-scale crash test was conducted. It has been shown that the possibility to increase the small car impact speed to 130km/h is high if the test facility condition for 130km/h impact velocity is better equipped.

Study on Analysis of Occupant Safety Index & Behavior Using Full-Scale Crash Test Data of Crash Cushion (충격흡수시설의 실물차량 충돌시험 데이터를 이용한 탑승자 안전도 및 충돌거동 분석에 관한 연구)

  • Joo, Jae Woong;Kum, Ki Jung;Jang, Dae Young;Kim, Bum Jin
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.28 no.2D
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    • pp.163-170
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    • 2008
  • According to the rules, a crash cushion is supposed to set up products that is satisfied with the standard of a performance test after performing the car crash test by road safety facilities and management guide. For development of crash cushion, performance should be estimated through the car crash test eventually. However, there is no reasonable design method which considers passenger's safety and only depend on crash test without an alternative plan. Therefore it incurs a loss materially and takes a lot. Therefore, we are asked to create a systematic design of the crash cushion. This study shows that a scientific basis of applying single degree of freedom when it designs the crash cushion after analyzing vehicle crash test data of crash cushion and also represents design of crash cushion through single degree of freedom response spectrum using calculated by crash test data on crash cushion.

Crashworthiness Evaluation of Bridge Barriers Built with Hot-dip Zinc-aluminium-magnesium Alloy-coated Steel (고내식성 용융합금도금강판 적용 교량난간의 충돌성능 평가)

  • Noh, Myung-Hyun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.3
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    • pp.171-176
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    • 2016
  • This paper proposes road safety facilities applying Hot-dip zinc-aluminum-magnesium alloy-coated steel sheets and coils to reduce the loss of function caused by the corrosion of steel in the service state. Vehicle crash simulations and full-scale crash tests were carried out to provide reliable information on evaluating the crash performance with the products of road safety facilities built with hot-dip zinc-aluminum-magnesium alloy-coated steel. From the results of the simulations and full-scale crash tests, the impact behaviors evaluated by the three-dimensional crash simulations considering the strain-rate dependency in a constitutive model were similar to those obtained from the full-scale crash test results. The full-scale crash test results met the crashworthiness evaluation criteria; hence, the proposed bridge barrier in this paper is ready for field applications.

A Study on the Performance Comparison of S2 type Bridge Rails (S2급 교량용 방호울타리의 성능비교 연구 (F형 콘크리트와 철재 교량용 방호울타리를 중심으로))

  • 정봉조;주재웅;이성관;장명순
    • Journal of Korean Society of Transportation
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    • v.20 no.2
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    • pp.117-124
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    • 2002
  • 새로 개발한 철재 교량용 방호울타리는 기존 시설에 비해 충격흡수기능과 조망권 확보, 융설작업, 유지보수가 용이하도록 설계되었다. 본 연구는 새로 개발한 철재 교량용 방호울타리를 건설교통부의 $\ulcorner$도로안전시설 설치 및 관리지침 - 교량용 방호울타리 편. 1999$\lrcorner$ 의 설계기준에 따라 기존 고속도로에 사용하고 있는 F형 콘크리트 교량용 방호울타리와 성능비교를 통해 평가하고자 하였다. 비교평가는 S2급 교량용 방호울타리의 시험기준으로 실시하였으며 결과는 다음과 같이 나타났다. 첫째, 소형승용차를 대상으로 한 운전자의 안전도 평가에서는 두가지 시설 모두 강도성능, 충돌 후 차량 안전성능 구성 부재 비산 억제 성능 등 세 가지 기준을 만족하였으나, 가속도 기준에 있어서는 철재 교량용 방호울타리는 기준인 20g 이하인 18.2605g로 나타나 안전기준을 만족하였고, F형 콘크리트 교량용 방호울타리는 20.1791g로 나타나 기준을 약간 상회하는 것으로 나타났으나 안전기준의 범위에 있는 것으로 평가하였다. 둘째. 대형차량을 대상으로 한 방호울타리의 구조적 안정성 평가에 있어서는 F형과 철재 교량용 방호울타리 모두 평가기준에 적합한 것으로 나타났다. 새로 개발한 철재 교량용 방호울타리는 국내 최초로 모의충돌시험과 실물차량 충돌시험을 통해 개발하였다는 의의를 가지고 있으며 성능측면에서도 기존의 시설에 비해 충분히 안전하다는 것을 증명하였다. 그러나 측정시설의 미비로 충돌후의 차량의 이탈속도나 이탈각도에 대하여 만족할 만한 수준의 결과를 제시하지는 못하였다.

Numerical Simulation of Full-Scale Crash Impact Test for Fuel Cell of Rotorcraft (회전익항공기 연료셀 충돌충격시험 Full-Scale 수치모사)

  • Kim, Hyun-Gi;Kim, Sung Chan;Kim, Sung Jun;Kim, Soo Yeon
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.26 no.5
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    • pp.343-349
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    • 2013
  • Crashworthy fuel cells have a great influence on improving the survivability of crews. Since 1960's, the US army has developed a detailed military specification, MIL-DTL-27422, defining the performance requirements for rotorcraft fuel cells. In the qualification tests required by MIL-DTL-27422, the crash impact test should be conducted to verify the crashworthiness of fuel cell. Success of the crash impact test means the improvement of survivability of crews by preventing post-crash fire. But, there is a big risk of failure due to huge external load in the crash impact test. Because the crash impact test itself takes a long-term preparation efforts together with costly fuel cell specimens, the failure of crash impact test can result in serious delay of a entire rotorcraft development. Thus, the numerical simulations of the crash impact test has been required at the early design stage to minimize the possibility of trial-and-error with full-scale fuel cells. Present study performs the numerical simulation using SPH(smoothed particle hydro-dynamic) method supported by a crash simulation software, LS-DYNA. Test condition of MIL-DTL-27422 is reflected on analysis and material data is acquired by specimen test of fuel cell material. As a result, the resulting equivalent stresses of fuel cell itself are calculated and vulnerable areas are also evaluated.

Analysis of Crash Load in Crash Impact Test for Fuel Tank of Rotorcraft (항공기용 연료탱크 Phase I 충돌충격시험 충격하중 분석)

  • Kim, Hyun-gi;Kim, Sung Chan
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.16 no.6
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    • pp.3736-3741
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    • 2015
  • Crash impact test is conducted to verify the crashworthiness of fuel tank. Success of the crash impact test means the improvement of survivability of crews by preventing post-crash fire. But, there is a big risk of failure due to huge external load in the crash impact test. The failure of crash impact test can result in serious delay of a entire rotorcraft development because of the design complement and re-production of the test specimens requiring a long-term preparation. Thus, the numerical simulations of the crash impact test has been required at the early design stage to minimize the possibility of trial-and-error in the real test. Present study conducts on the numerical simulation of phase I crash impact test using SPH supported by crash simulation software, LS-DYNA. Test condition of MIL-DTL-27422 is reflected on analysis and material data is acquired by specimen test of fuel cell material. As a result, the crash load on the skin material, overlap area and metal fitting is estimated to confirm the possibility of acquisition of the design load for the determination of the overlap area and adhesive strength.

Verification of the Reliability of the Numerical Analysis for the Crash Impact Test of Rotorcraft Fuel Tank (회전익항공기용 연료탱크 충돌충격시험에 대한 수치해석 신뢰성 검증)

  • Kim, Sungchan;Kim, Hyun-Gi
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.12
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    • pp.918-923
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    • 2018
  • The main function of a fuel tank is to store fuel. On the other hand, the structural soundness of the fuel tank is related directly to the survival of the crew in an emergency situation, such as an aircraft crash, and the relevant performance is demonstrated by a crash impact test. Because crash impact tests have a high risk of failure due to the high impact loads, various efforts have been made to minimize the possibility of trial and error in the actual test at the beginning of the design. Numerical analysis performed before the actual test is a part of such efforts. For the results of numerical analysis to be reflected in the design, however, the reliability of numerical analysis needs to be ensured. In this study, the results of numerical analysis and actual test data were compared to ensure the reliability of numerical analysis for the crash impact test of a rotorcraft fuel tank. For the numerical analysis of a crash impact test, LS-DYNA, crash analysis software, was used and the ALE (arbitrary Lagrangian Eulerian) technique was applied as the analysis method. To obtain actual test data, strain gages were installed on the metal fittings of the fuel tank and linked to the data acquisition equipment. The strain and stress of the fuel tank fitting were calculated by numerical analysis. The reliability of the numerical analysis was enhanced by assessing the error between the strain measurement of the upper fitting obtained from an actual fuel tank and the strain calculated from numerical analysis.

A Study on Dynamic Behavior of Guardrail Associated with Design Variables (설계변수에 의한 가아드레일의 동력학적 거동에 관한 연구)

  • Woo, K. S.;Ko, M. G.;Cho, S. H.;Kim, W.
    • Computational Structural Engineering
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    • v.7 no.2
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    • pp.89-99
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    • 1994
  • The nonlinear dynamic behaviors of guardrail established on the local or high way have been investigated using BARRIER VII program with respect to four design variables such as section type of beams and posts, impact angle, impact velocity and vehicle weight. Computer simulation programs are sophisticated analytical models for analyzing dynamic vehicle/barrier interactions and provide a relatively inexpensive alternative to full scale crash testing. This study has been focused on the structural adequacy, occupant risk, and vehicle trajectory. For this purpose, the maximum defection and impact force have been calculated to design the clear zone and to analyze effect of impact attenuation. Also, the acceleration of vehicle and exit angle after collision have been computed to estimate the occupant risk. From this study, it is suggested that we should strengthen the design criteria of guardrail to prevent from disastrous traffic accidents.

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