• Title/Summary/Keyword: epoxy composites

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Experimental bond behavior of hybrid rods for concrete reinforcement

  • Nanni, Antonio;Nenninger, Jeremy S.;Ash, Kenneth D.;Liu, Judy
    • Structural Engineering and Mechanics
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    • v.5 no.4
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    • pp.339-353
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    • 1997
  • Fiber reinforced plastic (FRP) rods provide certain benefits over steel as concrete reinforcement, such as corrosion resistance, magnetic and electrical insulation, light weight, and high strength. FRP composites can be combined with a steel core to form hybrid reinforcing rods that take advantage of properties of both materials. The objective of this study was to characterize the bond behavior of hybrid FRP rods made with braided epoxy-impregnated aramid or poly-vinyl alcohol FRP skins. Eleven rod types were tested using two concrete strengths. Specific topics examined were bond strength, slip, and type of failure in concentric pull-out tests from concrete cubes. From analysis of identical pull-out tests on both hybrid and steel rods, information on relative bond strength and behavior were obtained. It is concluded that strength is similar but slip in hybrid rods is much higher. Hybrid rods failed either by pull-out or splitting the concrete block (with or without yielding of the steel core). Experimental data showed consistency with similar test results presented in the literature.

Crippling Analysis of Z-Section Composite Stringers (Z-단면 복합재 스트링거의 크리플링 해석)

  • 권진회
    • Composites Research
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    • v.12 no.6
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    • pp.65-73
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    • 1999
  • Crippling stress and failure behavior of Z-section graphite/epoxy composite laminated stringers are investigated by the nonlinear finite element method. Stringers are idealized using 9-node laminated shell element. The complete unloading model is introduced into the finite element method for the progressive failure analysis. A modified Riks method is used to trace the post-failure equilibrium path after local buckling. Finite element results are validated with previous experimental results. The results show that the most important parameter affecting the crippling stress of Z-section stringers is the flange width. In terms of stacking sequence. the highest cripping stress is found at the stringer with $[{\pm}45/0/90]s$ lamination.

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A Study on the Damage Estimation of Uni-directionally Oriented Carbon Fiber Reinforced Plastics using Acoustic Emission (음향방출을 이용한 일방향 탄소섬유강화 플라스틱의 손상평가에 관한 연구)

  • Rhee Zhang-Kyu;Park Sung-Oan;Kim Bong-Gag;Woo Chang-Ki
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.14 no.1
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    • pp.30-36
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    • 2005
  • This study is to investigate a damage estimation of single edge notched tensile specimens as a function of acoustic emission(AE) according to the uni-directionally oriented carbon fiber/epoxy composites, CFRP In fiber reinforced composite materials, AE signals due to several types of failure mechanisms are typically observed. These are due to fiber breakage, fiber pull-out matrix cracking, delamination, and splitting or fiber bundle breaking. And these are usually discriminated on the basis of amplitude distribution, event counts, and energy related parameters. In this case, AE signals were analyzed and classified 3 regions by AE event counts, energy and amplitude for corresponding applied load. Bath-tub curve shows 3 distinct periods during the lifetime of a single-edge-notch(SEN) specimen. The characterization of AE generated from CFRP during SEN tensile test is becoming an useful tool f3r the prediction of damage failure or/and failure mode analysis.

A Study on Analysis of Mode I interlaminar Fracture Toughness of Foam Core Sandwich Structures (FOAM CORE SANDWICH 구조재의 Mode I 층간분리 파괴인성의 해석에 관한 연구)

  • Son, Se-Won;Gwon, Dong-An;Hong, Seong-Hui
    • Journal of the Korean Society for Precision Engineering
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    • v.17 no.9
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    • pp.81-86
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    • 2000
  • This paper was carried out to investigate the characteristics of interlaminar fracture toughness of foam core sandwich structures under opening loading mode by using the double cantilever beam (DCB) specimens in Carbon/Epoxy and foam core composites. instead of using symmetric geometry of DCB specimen non-symmetric DCB specimen was used to calculate the interlaminar fracture toughness. Three approaches for calculating the energy release rate({{{{ {G }_{IC } }}}}) were compared. Fracture toughness of foam core sandwich structures by autoclave vacuum bagging and hotpress were compared and analyzed. Experiment nonlinear beam bending FEM method were performed. Suggested bonding surface compensation and equivalent area inertia moment was used to calculate the energy release rate in nonlinear analytical results. The conclusions among experimental nonlinear analytical and FEM results was observed. The vacuum bagging method was shown to be able to substitute method in stead of autoclave without serious loss of Mode I energy release rate({{{{ {G }_{IC }}}}}) to be able to substitute method in stead of autoclave without serious loss of Mode I energy release rate({{{{ {G }_{IC }}}}}).

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Composite material optimization for heavy duty chassis by finite element analysis

  • Ufuk, Recep;Ereke, Murat
    • Advances in Automotive Engineering
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    • v.1 no.1
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    • pp.41-59
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    • 2018
  • In the study, investigation of fiber- reinforced composite materials that can be an alternative to conventional steel was performed by finite element analysis with the help of software. Steel and composite materials have been studied on a four axle truck chassis model. Three-dimensional finite element model was created with software, and then analyzes were performed. The analyses were performed for static and dynamic/fatigue cases. Fatigue cases are formed with the help of design spectra model and fatigue analyses were performed as static analyses with this design spectra. First, analyses were performed for steel and after that optimization analyses were made for the AS4-PEEK carbon fiber composite and Eglass-Epoxy fiber composite materials. Optimization of composite material analyzes include determining the total laminate thickness, thickness of each ply, orientation of each ply and ply stacking sequence. Analyzes were made according to macro mechanical properties of composite, micromechanics case has not been considered. Improvements in weight reduction up to %50 provided at the end of the composite optimization analyzes with satisfying stiffness performance of chassis. Fatigue strength of the composite structure depends on various factors such as, fiber orientation, ply thickness, ply stack sequence, fiber ductility, ductility of the matrix, loading angle. Therefore, the accuracy of theoretical calculations and analyzes should be correlated by testing.

Evaluation of Mechanical Property Variation of Epoxy Based Compliant Polymer Concretes Exposed to UV Light (에폭시 기반 연성 폴리머 콘크리트의 자외선 노출에 의한 기계적 물성평가)

  • Roh, In-Taek;Jung, Kyung-Chae;Chang, Seung-Hwan
    • Composites Research
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    • v.27 no.6
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    • pp.236-241
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    • 2014
  • This paper aims to evaluate material property variation of polymer concretes under ultra-violet exposure condition. The components and mixing ratio of the polymer composite specimens were determined by the previous research results. The equivalent UV exposure time was calculated with the consideration of the power of metal halide lamp and maximum 3 years were selected for the experiments. From the tests, it was found that the generated heat during UV exposure affected much the material properties of polymer concrete by means of post cure. As a result, the compressive strength increased and ductility factor decreased.

Improved Electrical Conductivity of CFRP by Conductive Nano-Particles Coating for lightning Strike Protection (낙뢰손상방지를 위한 전도성 나노입자 코팅에 의한 탄소섬유 복합재료의 전기전도도 향상 연구)

  • Ha, Min-Seok;Kwon, Oh-Yang;Choi, Heung-Soap
    • Composites Research
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    • v.23 no.1
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    • pp.31-36
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    • 2010
  • The improvement of electrical conductivity of carbon-fiber reinforced plastics (CFRP) has been investigated by silver nano-particles coating for the purpose of lightning strike protection. Silver nano-particles in colloid were sprayed on the surface of carbon fibers, which were then impregnated by epoxy resin to form a CFRP specimen. Electrical resistance was measured by contact resistance meter which utilize the principles of the AC 4-terminal method. Electrical resistance value was then converted to electrical conductivity. The coated silver nano-particles on the carbon fibers were verified by SEM and EDS. The electrical conductivity was increased by three times of the ordinary CFRP.

Thermal Stress-induced Edge Failure of Thin Composite Laminates (열응력에 의한 얇은 복합적층판의 자유경계단 부위 파손)

  • 이성혁;최낙삼
    • Composites Research
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    • v.12 no.1
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    • pp.28-36
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    • 1999
  • Thermal stress-induced failure in the free edge region of various thin carbon/epoxy composite laminates(1mm thick) has been investigated using the three-dimensional finite-element stress analysis, ultrasonic C-scan and microscopic observations. High thermal in-plane and interlaminar stresses were predicted in the interior layer near the free edge boundaries of the laminates. In the interior lamina, not in the skin lamina, of the thin laminates with lay-up of $[0_2/90_2]_s,\;[45_2/-45_0]_s,\;[0_2/60_2]_s$ treated by liquid $N_2$ immersion, many transverse matrix cracks took place due to thermal stress concentration, which agreed qualitatively with the above predictions.

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Blade Development and Test of WinDS$3000^{TM}$ System (WinDS$3000^{TM}$ 시스템의 블레이드 개발 및 시험)

  • Lee, Sang-Il;Lee, Kyeong-Woo;Joo, Wan-Don;Lee, Ki-Hak;Park, Jong-Po
    • 한국신재생에너지학회:학술대회논문집
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    • 2009.11a
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    • pp.448-448
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    • 2009
  • A new blade has been developed to apply to Doosan 3MW offshore wind turbine named as WinDS3000TM. The 3MW blade has been designed by the concept of slim external shape and optimized structure. High-performance glass fiber reinforced epoxy composites were used as the main material of the blade. The blade was manufactured using vacuum infusion process in order to increase the fiber volume fraction and to reduce micro-porosities. The blade has successfully passed the full-scale blade static test for certification. During the test, micro-failure signal and strain change of the blade were measured using acoustic emission sensors and strain gages. The blade has robust structure and weighs lighter compared to conventional blade since the new blade was designed by optimization process. The 3MW blade will be commercially applied to WinDS$3000^{TM}$ in 2010.

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Thermally-Expandable Molding Process for Thermoset Composite Materials (열팽창 치공구를 이용한 열경화성 복합재료의 성형연구)

  • 이준호;금성우;장원영;남재도
    • Polymer(Korea)
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    • v.24 no.5
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    • pp.690-700
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    • 2000
  • In this study, an elastomer-assistered compression molding process was investigated by experiments as well as modeling for the long-fiber reinforced thermoset composites. The consolidation pressure generated by fixed-volume and variable-volume conditions was thermodynamically derived for both elastomer and curing prepregs, and was compared with the pressure measured during curing of epoxy matrix. Exhibiting non-linear viscoelastic characteristics in the compressive stress-strain tests, the measured stress was well compared with a modifed KWW (Kohlrausch-Williame-Watts) equation, which is based on the Maxwell viscoelastic model. Using the developed model equations, the consolidation pressure generated by the elastomer was successfully predicted for the compression molding process of thermoset composite materials in tile closed mold system.

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