• 자동차안전학회지
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• 제9권3호
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• pp.13-18
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• 2017

Since 2015, Euro-NCAP and C-NCAP have enhanced regulation on submarine of rear female passenger. This submarine regulation is a big obstacle to achieve the highest level crash performance. So the objective of this study is to develop new technical way to protect rear female passenger against submarine. In this study, we figured out how design factors of seatbelt affect submarine of rear female passenger by sled test. And we verified that rear passenger submarine can be improved by increasing intersection angle of seatbelt anchor and rotation amount of seatbelt buckle. Based on these results, this paper proposes a new invention of seatbelt buckle and anchor that can improve rear passenger submarine. One is seatbelt buckle that can be detached from stopper to prevent rotation and the other is seatbelt anchor that can be changed the structure so as to incline forward during crash. Finally we proved that submarine of rear female passenger can be improved by the effectiveness of new inventions.

• Nuclear Engineering and Technology
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• 제53권9호
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• pp.3085-3099
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• 2021

Investigations of large commercial aircraft impact effect on nuclear power plant (NPP) buildings have been drawing extensive attentions, particularly after the 9/11 event, and this paper aims to numerically assess the damage and vibrations of NPP buildings subjected to aircrafts crash. In Part I of present paper, two shots of reduce-scaled model test of aircraft impact on NPP were conducted based on the large rocket sled loading test platform. In the present part, the numerical simulations of both scaled and prototype aircraft impact on NPP buildings are further performed by adopting the commercial program LS-DYNA. Firstly, the refined finite element (FE) models of both scaled aircraft and NPP models in Part I are established, and the model impact test is numerically simulated. The validities of the adopted numerical algorithm, constitutive model and the corresponding parameters are verified based on the experimental NPP model damages and accelerations. Then, the refined simulations of prototype A380 aircraft impact on a hypothetical NPP building are further carried out. It indicates that the NPP building can totally withstand the impact of A380 at a velocity of 150 m/s, while the accompanied intensive vibrations may still lead to different levels of damage on the nuclear related equipment. Referring to the guideline NEI07-13, a maximum acceleration contour is plotted and the shock damage propagation distances under aircraft impact are assessed, which indicates that the nuclear equipment located within 11.5 m from the impact point may endure malfunction. Finally, by respectively considering the rigid and deformable impacts mainly induced by aircraft engine and fuselage, an improved Riera function is proposed to predict the impact force of aircraft A380.

• 대한의용생체공학회:의공학회지
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• 제24권1호
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• pp.15-21
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• 2003

본 연구에서는 경량휠체어 탑승자의 차량 전방충돌시 안전성 평가를 위하여 동적 슬래드 충격실험을 하였다. 실험은 총 6회 시행하였으며 충격속도는 20g/48 $\pm$2km/h 였고, Hybrid III 50%ile 성인남자 인체모형을 사용하여 두부손상기준(Head Injury Criteria), 목의 굴전모멘트, 축 인장력, 전단력, 흉부 가속도. 두부, 휠체어, 무릎의 전방 쏠림량을 측정하였으며 미국자동차학회 규격인 SAE J2249에서 제안한 동작기준 (Motion Criteria)과 미국 제너럴모터스사의 자체기준(GM-IARV)인 복합상해기준(Combined Injury Criteria)을 이용하여 안전성평가를 하였다. 실험결과는 경량 휠체어 탑승자의 전방 충돌 시 최대 상해치를 100%로 봤을 때 휠체어와 탑승자 거동의 위험도지수 MC는 52%, 탑승자의 상체 위험도지수 CIC는 60.1% 였다.

• 대한기계학회논문집A
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• 제35권10호
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• pp.1187-1191
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• 2011

이 응용논문에는 적응형 로드리미터에 대해 기술되어 있다. 적응형 로드리미터는 안전벨트의 구성품 중 하나이며, 이는 승객의 다양한 체중과 키에 따라 하중량을 고하중과 저하중으로 변환시킬 수 있는 장치이다. 최근, FMVSS 208규정은 다양한 더미크기에 대해 엄격한 안전기준을 요구하고 있다. 이에 따라 우리는 고하중 조건과 저하중 조건 시 각각 더미에 흉부 상해정도를 알아보았고, 실험을 통해서 벤치마킹모델의 하중조건을 확인하였다. 이를 토대로 적응형 듀얼레벨 로드리미터를 개발하여 성능 실험을 실시하였고, 유한요소해석을 통해 설계 개선점을 확인하였다.

• Composites Research
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• 제32권4호
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• pp.171-176
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• 2019

본 연구는 복합재를 사용한 휠체어 고정구의 구조 강도 특성에 대하여 평가하였다. 이를 위해 특별교통수단 내 휠체어 고정구의 시험 기준 ISO 10542에 의거하여 전방 충돌 슬레드 유한요소해석을 진행하였고, 이를 통해 얻은 고정구에 작용하는 하중데이터를 휠체어 고정구 유한요소해석의 초기 조건으로 사용하였다. 고정구는 블록, 가이드, 레일로 구성되어 있으며, 이 중에서 레일의 중량 비율이 가장 높기 때문에 탄소섬유 에폭시 복합재를 레일에 적용하는 것이 적합한 것으로 나타났다. 또한 기존의 레일에서 하단 부분을 복합재로 적용한 하이브리드 레일은 기존 SAPH 440으로 제작된 레일의 구조강도와 비슷하게 설계할 경우, 약 27% 정도 경량화를 달성할 수 있는 것으로 나타났다.

• Nuclear Engineering and Technology
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• 제53권9호
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• pp.3068-3084
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• 2021

Investigations of large commercial aircraft impact effect on nuclear power plant (NPP) buildings have been drawing extensive attentions, particularly after the 9/11 event, and this paper aims to experimentally assess the damage and vibrations of NPP buildings subjected to aircraft crash. In present Part I, two shots of reduce-scaled model test of aircraft impacting on NPP building were carried out. Firstly, the 1:15 aircraft model (weighs 135 kg) and RC NPP model (weighs about 70 t) are designed and prepared. Then, based on the large rocket sled loading test platform, the aircraft models were accelerated to impact perpendicularly on the two sides of NPP model, i.e., containment and auxiliary buildings, with a velocity of about 170 m/s. The strain-time histories of rebars within the impact area and acceleration-time histories of each floor of NPP model are derived from the pre-arranged twenty-one strain gauges and twenty tri-axial accelerometers, and the whole impact processes were recorded by three high-speed cameras. The local penetration and perforation failure modes occurred respectively in the collision scenarios of containment and auxiliary buildings, and some suggestions for the NPP design are given. The maximum acceleration in the 1:15 scaled tests is 1785.73 g, and thus the corresponding maximum resultant acceleration in a prototype impact might be about 119 g, which poses a potential threat to the nuclear equipment. Furthermore, it was found that the nonlinear decrease of vibrations along the height was well reflected by the variations of both the maximum resultant vibrations and Cumulative Absolute Velocity (CAV). The present experimental work on the damage and dynamic responses of NPP structure under aircraft impact is firstly presented, which could provide a benchmark basis for further safety assessments of prototype NPP structure as well as inner systems and components against aircraft crash.