• 제목/요약/키워드: shock absorption performance

검색결과 37건 처리시간 0.024초

여성 노인을 위한 낙상충격 보호팬츠 개발 및 평가 (Development and Evaluation of Fall Impact Protective Clothing for the Elderly Women)

  • 박정현;이진숙;이정란
    • 한국의류산업학회지
    • /
    • 제20권5호
    • /
    • pp.569-582
    • /
    • 2018
  • The purpose of this study is to verify the impact protection performance and to evaluate the activity, design, fit, and pad characteristics of the fall impact protection clothing for elderly women. The protective clothing was designed as pants type and underwear type, and an impact protection pad in the form of a tightly connected regular hexagon piece was inserted in the hip and hip joints. The pad was made of two kinds of foam single pad and foam and gel combination pad so that they could be inserted into pants type and underwear type, respectively. The results of the shock absorption performance of the fall impact protective clothing showed that when the impact force of 4601N was applied to the pants type protective clothing, the impact force was reduced by 29% in the foam pad type and 26% in the gel and foam pad type. When the force of 5113N was applied to the underwear type, it decreased by 40% in the foam pad type and by 34% in the gel and foam pad type. As a result of wearing evaluation of subject group, it was found that fit and activity of underwear type was better than that of pants type. Foam pad type was evaluated to be lighter than gel and foam pad type in both the subject and the expert group and the gel and foam pad was evaluated to be more flexible in the expert group.

Experimental study on Chinese ancient timber-frame building by shaking table test

  • Zhang, Xi-Cheng;Xue, Jian-Yang;Zhao, Hong-Tie;Sui, Yan
    • Structural Engineering and Mechanics
    • /
    • 제40권4호
    • /
    • pp.453-469
    • /
    • 2011
  • A one-story, wooden-frame, intermediate-bay model with Dou-Gon designed according to the Building Standards of the Song Dynasty (A.D.960-1279), was tested on a unidirectional shaking table. The main objectives of this experimental study were to investigate the seismic performance of Chinese historic wooden structure under various base input intensities. El Centro wave (N-S), Taft wave and Lanzhou wave were selected as input excitations. 27 seismic geophones were instrumented to measure the real-time displacement, velocity and acceleration respectively. Dynamic characteristics, failure mode and hysteretic energy dissipation performance of the model are analyzed. Test results indicate that the nature period and damping ratio of the model increase with the increasing magnitude of earthquake excitation. The nature period of the model is within 0.5~0.6 s, the damping ratio is 3~4%. The maximum acceleration dynamic magnification factor is less than 1 and decreases as the input seismic power increases. The frictional slippage of Dou-Gon layers (corbel brackets) between beams and plates dissipates a certain amount of seismic energy, and so does the slippage between posts and plinths. The mortise-tenon joint of the timber frame dissipates most of the seismic energy. Therefore, it plays a significant part in shock absorption and isolation.

불완전 발달 유체 유동을 고려한 MR댐퍼 착륙장치 모델링 (Modeling of MR Damper Landing Gear Considering Incompletely Developed Fluid Flow)

  • 이효상;장대성;황재혁
    • 항공우주시스템공학회지
    • /
    • 제15권1호
    • /
    • pp.7-18
    • /
    • 2021
  • 반능동형 MR댐퍼 착륙장치는 MR유체가 환형 유로를 지날 때 유체감쇠력 및 자장 제어 감쇠력을 발생시키는 댐퍼이다. 환형 유로를 지나는 MR 유체의 경우 필연적으로 불완전 발달 유동이 발생하게 되어, 이는 유체 감쇠력을 포함하는 댐퍼 내력 계산에 오차를 발생시키는 원인이 된다. 이로 인해 댐퍼 구조적 파라미터 설계 및 제어 이득 선정이 부정확해지며, 착륙장치의 동특성 및 충격흡수성능 저하를 초래하게 된다. 본 논문에서는 MR댐퍼 환형 유로의 입구영역에서 발생하는 추가적인 감쇠력을 고려한 MR댐퍼 착륙장치의 수학적 모델을 유도하였다. 본 논문에서 유도한 수학적 모델링을 MR댐퍼 착륙장치의 설계 및 최적화 과정에 적용한다면 좀 더 정확한 내력 예측으로 우수한 성능의 MR댐퍼 착륙장치를 설계할 수 있을 것으로 판단된다.

Polybenzimidazole (PBI) Coated CFRP Composite as a Front Bumper Shield for Hypervelocity Impact Resistance in Low Earth Orbit (LEO) Environment

  • Kumar, Sarath Kumar Sathish;Ankem, Venkat Akhil;Kim, YunHo;Choi, Chunghyeon;Kim, Chun-Gon
    • Composites Research
    • /
    • 제31권3호
    • /
    • pp.83-87
    • /
    • 2018
  • An object in the Low Earth Orbit (LEO) is affected by many environmental conditions unlike earth's surface such as, Atomic oxygen (AO), Ultraviolet Radiation (UV), thermal cycling, High Vacuum and Micrometeoroids and Orbital Debris (MMOD) impacts. The effect of all these parameters have to be carefully considered when designing a space structure, as it could be very critical for a space mission. Polybenzimidazole (PBI) is a high performance thermoplastic polymer that could be a suitable material for space missions because of its excellent resistance to these environmental factors. A thin coating of PBI polymer on the carbon epoxy composite laminate (referred as CFRP) was found to improve the energy absorption capability of the laminate in event of a hypervelocity impact. However, the overall efficiency of the shield also depends on other factors like placement and orientation of the laminates, standoff distances and the number of shielding layers. This paper studies the effectiveness of using a PBI coating on the front bumper in a multi-shock shield design for enhanced hypervelocity impact resistance. A thin PBI coating of 43 micron was observed to improve the shielding efficiency of the CFRP laminate by 22.06% when exposed to LEO environment conditions in a simulation chamber. To study the effectiveness of PBI coating in a hypervelocity impact situation, experiments were conducted on the CFRP and the PBI coated CFRP laminates with projectile velocities between 2.2 to 3.2 km/s. It was observed that the mass loss of the CFRP laminates decreased 7% when coated by a thin layer of PBI. However, the study of mass loss and damage area on a witness plate showed CFRP case to have better shielding efficiency than PBI coated CFRP laminate case. Therefore, it is recommended that PBI coating on the front bumper is not so effective in improving the overall hypervelocity impact resistance of the space structure.

드롭랜딩 시 심박수 증가에 따른 하지의 생체역학적 차이 분석 (Analysis on Biomechanical Differences in Lower Limbs Caused by Increasing Heart Rates During Drop-landing)

  • 홍완기;김도은
    • 한국운동역학회지
    • /
    • 제25권2호
    • /
    • pp.141-147
    • /
    • 2015
  • Objective : This study aimed to understand how increased heart rates at the time of drop landing during a step test would affect biomechanical variables of the lower extremity limbs. Background : Ballet performers do more than 200 landings in a daily training. This training raises the heart rate and the fatigability of the lower extremity limbs. Ballet performance high heart rate can trigger lower extremity limb injury. Method : We instructed eight female ballet dancers with no instability in their ankle joints(mean ${\pm}$ SD: age, $20.7{\pm}0.7yr$; body mass index, $19.5{\pm}1.2kg/m^2$, career duration, $8.7{\pm}2.0yr$) to perform the drop landing under the following conditions: rest, 60% heart rate reserve (HRR) and 80% HRR. Results : First, the study confirmed that the increased heart rates of the female ballet dancers did not affect the working ranges of the knee joints during drop landing but only increased angular speeds, which was considered a negative shock-absorption strategy. Second, 80% HRR, which was increased through the step tests, led to severe fatigue among the female ballet dancers, which made them unable to perform a lower extremity limb-neutral position. Hence, their drop landing was unstable, with increased introversion and extroversion moments. Third, we observed that the increasing 80% HRR failed to help the dancers effectively control ground reaction forces but improved the muscular activities of the rectus femoris and vastus medialis oblique muscles. Fourth, the increasing heart rates were positively related to the muscular activities of the vastus medialis oblique and rectus femoris muscles, and the extroversion and introversion moments. Conclusion/Application : Our results prove that increased HRR during a step test negatively affects the biomechanical variables of the lower extremity limbs at the time of drop landing.

MR댐퍼를 적용한 항공기 착륙장치의 하이브리드 제어기법 연구 (Hybrid Control of Aircraft Landing Gear using Magnetorheological Damper)

  • 탁준모;루엥 비엣;황재혁
    • 항공우주시스템공학회지
    • /
    • 제12권1호
    • /
    • pp.1-9
    • /
    • 2018
  • 본 연구에서는 기존의 하중제어기법을 보완한 하이브리드 제어기법을 제안하였다. 제안된 하이브리드 제어기법은 기존 하중제어기법에서 발생하는 채터링 현상을 제거하고, 높은 충격흡수효율을 얻을 수 있는 제어기법이다. 제어기 설계를 위해 MR댐퍼가 적용된 착륙장치를 구성하고, 착륙장치의 운동방정식을 유도하였다. 다물체 동역학 해석 소프트웨어인 RecurDyn을 이용하여 시뮬레이션 모델을 구성한 후 하이브리드 제어기를 설계하였다. 본 연구의 하이브리드 제어기는 스카이 훅 제어기를 기반으로 최대 스트럿 하중과 변위를 줄일 수 있으며, 부가되는 하중제어 기법을 통해 고효율의 제어기법을 구현할 수 있다. 채터링 방지를 위해 효율적인 제어기법 스위칭과 입력설계(Input Shaping) 기법을 적용하여 낙하 시뮬레이션을 수행하였고, 각각의 결과를 비교하여 착륙 특성에 대해 성능평가를 수행하였다.

방사형 회전이 추가된 임팩트 크러셔를 이용한 콘크리트용 순환굵은골재 품질향상 및 검증 연구 (A Study on Quality Improvement and Verification of Recycled Coarse Aggregate for Concrete Using an Impact Crusher with Radial Rotation)

  • 전덕우;김용성;전찬수;최원영;조원익
    • 한국건설순환자원학회논문집
    • /
    • 제10권2호
    • /
    • pp.133-142
    • /
    • 2022
  • 본 연구는 고품질의 콘크리트용 순환골재를 생산할 수 있는 타격 완충 장치인 방사형 회전판을 하단에 설치한 임팩트 크러셔를 개발하고 이를 이용하여 생산한 순환굵은골재의 품질성능 향상 효과 및 콘크리트 실험을 통해 적용 가능 여부를 검증하는 것을 목적으로 한다. 그 결과, 절대건조밀도, 흡수율, 마모감량, 입자모양판정실적률, 0.08 mm 체 통과량 시험에서 손실된 양, 알칼리골재반응, 점토덩어리량, 안정성, 이물질함유량 등 모든 항목에서 개선된 품질을 나타내었고 순환골재 품질기준에서 규정하는 기준에 부합하는 것으로 나타났다. 또한, 순환굵은골재를 적용한 콘크리트의 공기량 및 슬럼프는 국내 기준에 모두 부합하며 순환굵은골재의 혼입률에 따른 콘크리트의 재령별 압축강도 특성 실험 결과에 따라 순환굵은골재의 혼입률 60% 까지는 적용이 가능할 것으로 확인되었다.