• 제목/요약/키워드: Impact Strength

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Shear and impact strength of waste plastic fibre reinforced concrete

  • Karanth, Savithri S;Ghorpade, Vaishali G;Rao, H Sudarsana
    • Advances in concrete construction
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    • 제5권2호
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    • pp.173-182
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    • 2017
  • This paper is aimed at determining the shear and impact strength of waste plastic fibre reinforced concrete. M30 grade of concrete is prepared with waste plastic door fibres cut into 5 mm width and aspect ratios of 30, 50, 70, 90 and 110. Fibres are used in a volume fraction of 0 to 1.5% with an increment of 0.25%. L shaped specimens are cast for shear strength tests and flat plates of size $250{\times}250{\times}30mm$ are used for impact tests. "Drop ball method" is used for checking the impact strength. Shear strength is checked with L shaped specimens under UTM with a special attachment. It was found that up to 1.25% of waste plastic fibres can be effectively used for better strength of concrete both in shear and impact. Shear and impact strength were found to be increasing up to a volume fraction of fibres of 1.25%.

콘크리트 슬래브 압축강도에 따른 바닥충격진동 및 소음특성 (Floor Impact Sound and Vibration Characteristics Affected by the Compressive Strength of Concrete)

  • 정정호;유승엽;전진용
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 추계학술대회논문집
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    • pp.796-799
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    • 2005
  • In 2005, a regulation on the heavy-weight impact sound was released, which restricted concrete slab thickness of standard floor to 210mm. To reduce heavy-weight impact sound, damping materials and structural reinforcement system have been proposed. In this study, the effect of compressive strength on the heavy-weight impact vibration and sound were investigated. FEM analysis was conducted for the 34PY apartment with different concrete strength (210, 350, 420kg/cm$^2$). In addition, apartment floors with different concrete strength were constructed and the floor impact vibration and sound were measured. Results of FEM analysis and measurement show that the resonance frequency of concrete slab was increased by the increment of concrete strength. However, floor impact sound pressure level did not decrease because the nor impact vibration and sound pressure level in 63Hz band increased.

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CFRP 적층판의 충격손상이 잔류 굽힘 피로강도에 미치는 영향 (Influence of Residual Bending Fatigue Strength on Impact Damage of CFRP Composites)

  • 양용준;양인영
    • 한국안전학회지
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    • 제30권3호
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    • pp.7-12
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    • 2015
  • CFRP composites are used as primary structural members in various industrial fields because their specific strength and specific stiffness are excellent in comparison to conventional metals. Their usage is expanding to high added-value industrial fields because they are more than 50% lighter than metals, and have excellent heat resistance and wear resistance. However, when CFRP composites suffer impact damage, destruction of fiber and interface delamination occur. This causes an unexpected deterioration of strength, and for this reason it is very difficult to ensure the reliability of the excellent mechanical properties. Therefore, for the destruction mechanism in bending with impact damage, this study investigated the reinforcement data regarding various external loads by identifying the consequential strength deterioration. Specimens were damaged by impact with a steel ball propelled by air pressure. Decrease in bending strength caused by the tension and compression of the impact side, and depending on the lamination direction of fiber and interface inside the specimen. From the bending test it was found that the bending strength reduced when the impact energy increased. Especially in the case of compression on the impact side, as tensile stress occurred at the damage starting point, causing rapid failure and a substantially reduced failure strength.

충격시 CFRP 복합재 판의 거동과 충격후 압축강도에 관한 실험적 연구 (Experimental Investigation on the Behaviour of CFRP Laminated Composites under Impact and Compression After Impact (CAI))

  • Lee, J.;Kong, C.;Soutis, C.
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2003년도 춘계학술발표대회 논문집
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    • pp.129-134
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    • 2003
  • The importance of understanding the response of structural composites to impact and CAI cannot be overstated to develop analytical models for impact damage and CAI strength predictions. This paper presents experimental findings observed from quasi-static lateral load tests, low velocity impact tests, CAI strength and open hole compressive strength tests using 3mm thick composite plates ($[45/-45/0/90]_{3s}$ - IM7/8552). The conclusion is drawn that damage areas for both quasi-static lateral load and impact tests are similar and the curves of several drop weight impacts with varying energy levels (between 5.4 J and 18.7 J) fallow the static curve well. In addition, at a given energy the peak force is in good agreement between the static and impact cases. From the CAI strength and open hole compressive strength tests, it is identified that the failure behaviour of the specimens was very similar to that observed in laminated plates with open holes under compression loading. The residual strengths are in good agreement with the measured open hole compressive strengths, considering the impact damage site as an equivalent hole. The experimental findings suggest that simple analytical models for the prediction of impact damage area and CAI strength can be developed on the basis of the failure mechanism observed from the experimental tests.

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충격손상을 받은 항공기용 복합재료의 잔류강도 평가 (Evaluation of Residual Strength in Aircraft Composite Under Impact Damage)

  • 최정훈;강민성;신인환;구재민;석창성
    • 한국정밀공학회지
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    • 제27권2호
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    • pp.94-101
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    • 2010
  • Composite materials have a higher specific strength and modulus than traditional metallic materials. Additionally, these materials offer new design flexibilities, corrosion and wear resistance, low thermal conductivity and increased fatigue life. These, however, are susceptible to impact damage due to their lack of through-thickness reinforcement and it causes large drops in the load-carrying capacity of a structure. Therefore, the impact damage behavior and subsequently load-carrying capacity of impacted composite materials deserve careful investigation. In this study, the residual strength and impact characteristics of plain-woven CFRP composites with impact damage are investigated under axial tensile test. Impact test was performed using drop weight impact tester. And residual strength behavior by impact was evaluated using the caprino model. Also we evaluated behavior of residual strength by change of mass and size of impactor. Examined change of residual strength by impact energy change through this research and consider impactor diameter in caprino model.

도어 임팩트 빔의 3점 굽힘 최대강도와 차량 장착 시 굽힘 좌굴강도와의 관계 (The Relation of Bending Buckling Strength in Vehicle and Three Point Bending Maximum Strength of Door Impact Beam)

  • 강성종;이상민
    • 자동차안전학회지
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    • 제11권1호
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    • pp.40-47
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    • 2019
  • First, three point bending analysis for the inclined press door impact beam was carried out to investigate inclination angle effect on the maximum strength with varying support distance. Next, for the system model with spring elements representing body stiffness at door mounting area, the bending structural behavior of impact beam mounted on vehicle was estimated. The mounting distance and inclination angle were changed and the beam bending buckling strength was presumed at the head displacement below which spring stiffness change has little effect on the load. Finally strength ratio to predict the bending buckling strength of impact beam mounted on vehicle from three point bending maximum strength of fixed support distance was suggested.

항공기 복합재료 적용 시편의 압축 강도 연구 (A Study on Compressive Strength of Aircraft Composite Specimens)

  • 공창덕;박현범;김상훈;이하승
    • 항공우주시스템공학회지
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    • 제3권1호
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    • pp.12-16
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    • 2009
  • The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it was investigated the residual strength of carbon fiber laminate after impact damage by the experimental investigation. The tensile strength test and compressive strength test were used to find the mechanical properties, previously. Impact test was performed using low-velocity drop-weight test equipment. The impact damages were finally assessed by the compressive strength test. The investigation results revealed the residual strength of the damaged specimens due to the impact damage.

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제지 슬러지-폴리프로필렌수지 복합재의 기계적 성질 (Mechanical Properties of Paper Sludge-Polypropylene Composites)

  • 이필우;손정일
    • Journal of the Korean Wood Science and Technology
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    • 제27권3호
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    • pp.51-62
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    • 1999
  • 본 연구는 자원환경적인 측면에서 산업폐기물이자 환경오염원인 제지 슬러지를 이용함에 있어 용융형 목질-플라스틱 복합재의 강화충전제로 적용하여 그 사용가능성을 알아보고 또한 복합재의 물성에 대한 기초적인 자료을 제시하는데 그 목적이 있다. 그 결과 제지 슬러지의 혼합비율이 증가할수록 복합재의 밀도는 증가하였으며 제지 슬러지의 입자 크기와 결합제 종류 및 함량은 복합재의 밀도에 크게 영향을 미치지 않았다. 제지 슐러지의 혼합비율이 증가할수록 복합재의 휨강도적 성질은 향상되었으며, 제지 슐러지의 입자 크기가 작을수룩 복합재의 휨강도는 증가하였으나 휨탄성계수는 증가하였다. 또한 복합재의 휨강도적 성질은 결합제의 종류에 관계없이 그 함량이 증가할수록 향상됨을 알 수 있었으며, 결합제의 분자량이 더 큰 Epolene G-3003의 경우 그 효과가 더 큼을 알 수 있었다. 대체로 제지 슬러지의 혼합비율이 증가할수록 복합재의 충격강도는 다소 감소하는 경향을 볼 수 있지만, 전체적으로 notched impact strength는 크게 감소하지는 않았다. unnotched impact strength의 경우 제지 슬러지의 혼합비율이 증가할수록 그 감소 폭이 컸다. 제지 슬러지의 입자크기가 복합재의 충격강도에 미치는 영향을 보면 notched impact strength의 경우 제지 슬러지의 입자 크기에 따라 충격강도에 미치는 영향은 거의 없었으며, unnotched impact strength의 경우 입자 크기가 가장 작은 100mesh 이하일 때 가장 우수하였고 그 다음으로 20~40mesh, 60~80mesh 순이었다. 복합재의 notched impact strength 는 결합제의 종류와 함량에 따라 미치는 영향은 거의 없음을 알 수 있었으나 unnotched impact strength는 Epolene E-43의 경우 첨가량이 증가할수록 충격강도가 감소하였고, Epolene G-3003의 경우는 첨가량이 증가할수록 충격강도가 감소하다가 다시 증가하는 경향을 보였다.

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Impact damage and residual bending strength of CFRP composite laminates involved difference of fiber stacking orientation and matrics

  • 심재기;양인영;오택열
    • 한국정밀공학회지
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    • 제10권4호
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    • pp.152-162
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    • 1993
  • The purpose of this study is to investigate problems of residual bending strength and the impact damage experimentally when CFRP composite laminates are subjected to Foreign object damage. The specimens composed of four types of CR/EPOXY and a CF/PEEK composite laminates which involved difference of fiber stracking orientation and matrics. The result were summariged as follows : 1) It is found that both orthotropic and guasi-isotropic composite laminates are increasimg lineally between impact energy and damage delamination area. 2) Delamination devel- opment energy(mm$^{2}$J) OF cf/epoxy composite aminates is less than that of CF/PEEK. 3) When impact energy is applied to specimens within 3J, the residual strength of orthotropic is greater than guasi-isotropic composite laminates. On the other hand, it is predicted that residual bending strength of orthotropic composite laminates is less than that of quasi-isotropic when impact energy is more thaen 3J. 4) It is found in CF/PEEK that for the impact side compression, residual of bending strength versus impact energy is almost constant, while in case of impact side tension, residual bending strength is decreased rapidly near 1.2J. of impact energy due to the effect of delamination buckling.

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옆문강도 및 측면충돌 성능을 고려한 알루미늄 도어 임펙트빔 최적화 연구 (Optimization of the Aluminum Door Impact Beam Considering the Side Door Strength and the Side Impact Capability)

  • 양지혁
    • 한국산학기술학회논문지
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    • 제12권5호
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    • pp.2025-2030
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    • 2011
  • 최근에 많은 완성차 업계에서 차량 중량을 줄이기 위해 알루미늄 재질의 도어 임팩트빔을 사용하고 있으나, 이는 옆문강도 및 측면충돌 성능을 저하시킬 수 있다. 따라서 이 논문에서는 옆문강도 법규를 만족시키고 스틸 도어 빔 수준의 측면충돌 성능을 유지할 수 있는 알루미늄 빔의 최적화된 단면 형상과 설계수치를 제시하고자 한다.