• Title/Summary/Keyword: 탄소 섬유 복합 재료

Search Result 268, Processing Time 0.029 seconds

A Study on the Fracture Behavior of CFRP in Tensile and Fracture Toughness Tests by Acoustic Emission (음향방출법에 의한 탄소 섬유 복합 재료의 인장 및 파괴 인성시험시의 파괴 거동에 관한 연구)

  • Lee, Sang-Guk;Oh, Sae-Kyoo;Nam, Ki-Woo;Kim, Og-Gyun
    • Journal of the Korean Society for Nondestructive Testing
    • /
    • v.15 no.1
    • /
    • pp.277-290
    • /
    • 1995
  • The study was carried out to analyze the fracture behavior and the acoustic emission(AE) characteristics and to find the relationship among tensile strength, fracture toughness and cure pressure in owe process of the carbon fiber reinforced composites of two types, $[0^{\circ}/90^{\circ}]_{2S}$ and $[0^{\circ}\;_2/90^{\circ}\;_2]_S$. AE signals were detected during the curing process, tensile tests and fracture toughness tests by acoustic emission(AE) measurements, respectively. Tensile strengths showed that the less cure pressurizing steps and the side of $[0^{\circ}/90^{\circ}]_{2S}$ specimens had the higher strengths than those of the others. Fracture toughness by the change of test temperature showed nearly same values in the same temperature region, but the higher test temperature had the lower fracture toughness values. In order to examine the relationship between fracture behavior of CFRP in tensile and fracture toughness tests and AE signals, the post processing for AE parameters of AE data and the observations of microscope and SEM have been carried out respectively.

  • PDF

Fracture Behaviour Analysis of the Crack at the Specimen with the Type of Mode I Composed of the Bonded Carbon Fiber Reinforced Plastic (접합된 CFRP로 구성된 Mode I형 시험편 크랙의 파괴 거동 해석)

  • Lee, Jung-Ho;Cho, Jae-Ung;Cheon, Seong-Sik;Kook, Jeong Han
    • Composites Research
    • /
    • v.28 no.6
    • /
    • pp.356-360
    • /
    • 2015
  • In this paper, the carbon fiber reinforced plastic is processed as the double cantilever beam in order to estimate the fracture behavior of composite and is carried out with the static analysis as the mode I. The specimen sizes are 25 mm, 30 mm, 35 mm and 40 mm. And the material property is used with carbon. As the analysis result of mode I, the adhesive part is detached latest by the small force at the specimen thickness of 25 mm. The largest force is happened at the specimen thickness of 40 mm. The defection of the adhesive interface is shown slowest at the displacement of 9.75 mm at the specimen thickness of 25 mm. And the defection is shown quickest at the displacement of 7.82 mm at the specimen thickness of 40 mm. This defection is due to the fracture of specimen. The result of this study on the defection of the adhesive interface and the reaction force due to this defection is thought to be contributed to the safe structural design of the carbon fiber reinforced plastic.

Comparative Analysis of Biomechanical Behaviors on Lumbar with Titanium and Carbon Fiber Reinforced PEEK Connecting Rods for Fusion Surgery (티타늄과 탄소 섬유 강화 PEEK로 구성된 요추 유합술용 연결봉의 의공학적 영향에 대한 비교 분석)

  • Seo, Hye-Sung;Kang, Hae-Seong;Chun, Houng-Jae
    • Composites Research
    • /
    • v.34 no.3
    • /
    • pp.186-191
    • /
    • 2021
  • The lumbar spinal fusion is a treatment performed to restore the stability of the degenerated lumbar. In this study, the intervertebral discs between two or more segments are removed and a bone graft is inserted to harden the segments. The pedicle screw system is inserted to vertebral bodies to fix two or more segments so that they can be firmly fused. In this study, a total of 7 patient-specific lumbar finite element models were created and pedicle screw systems were installed. The connecting rods made of titanium and CFR-PEEK was inserted to the generated models. Finite element analysis was conducted for four representative spine behaviors and statistical analysis was performed to investigate the biomechanical effects by the material properties of connecting rods. The intradiscal pressure of adjacent segments and the range of motion of the joints of each segment were investigated. In the subjects who used CFR-PEEK instead of Ti for connecting rods, the intradiscal pressure of adjacent segments tend to decrease and the range of motion of each segment tend to increase. However, no statistically significant difference in tendency was observed under all loading conditions.

The Study of Simulation Dynamic Behavior of CFRP Structural Members (CFRP 구조 부재의 시뮬레이션 동적 거동에 관한 연구)

  • Kim, Jung-Ho;Bang, Jung-Min;Kim, Ji-Hoon
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.35 no.5
    • /
    • pp.561-565
    • /
    • 2011
  • The structural vehicles are steel members of square or circle tube with definite shape. These members support various components and absorb impact energy to protect passengers during accidentswhen crash happen. Structural members need to be lightweight and stable. In this study, we do an impact simulation of a CFRP square member using finite element analysis program Ls-Dyna in order to predict fracture shape and energy absorb feature of CFRP member. Also, we make square member shape of CFRP and do an impact experiment. We compare the analytical and experimental results and consider the fracture shape and energy features of CFRP members.

Study of Cure Kinetics of Vacuum Bag Only Prepreg Using Differential Scanning Calorimetry (시차주사열량계를 이용한 진공백 성형 프리프레그의 경화 거동 연구)

  • Hyun, Dong Keun;Lee, Byoung Eon;Shin, Do Hoon;Kim, Ji Hoon
    • Composites Research
    • /
    • v.33 no.2
    • /
    • pp.44-49
    • /
    • 2020
  • The cure kinetics of carbon fiber-reinforced prepreg for Vacuum Bag Only(VBO) process was studied by differential scanning calorimetry (DSC). The total heat of reaction (ΔHtotal = 537.1 J/g) was defined by the dynamic scanning test using prepregs and isothermal scanning tests were performed at 130℃~180℃. The test results of isothermal scanning were observed that the heat of reaction was increased as the temperature elevated. The Kratz model was applied to analyze the cure kinetics of resin based on the test results. To verify the simulation model, the degree of cure from panels using different cure cycles were compared with the measurement. The simulation model showed that the error against the experimental value was less than 3.4%.

Low Velocity Impact Property of CF/Epoxy Laminate according to Interleaved Structure of Amorphous Halloysite Nanotubes (비정질 할로이사이트 나노입자의 교차적층 구조에 따른 탄소섬유/에폭시 라미네이트의 저속 충격 특성)

  • Ye-Rim Park;Sanjay Kumar;Yun-Hae Kim
    • Composites Research
    • /
    • v.36 no.4
    • /
    • pp.270-274
    • /
    • 2023
  • The stacking configuration of fiber-reinforced polymer (FRP) composites, achieved via the filament winding process, exhibits distinct variations compared to conventional FRP composite stacking arrangements. Consequently, it becomes challenging to ascertain the influence of mechanical properties based on the typical stacking structures. Thus, it becomes imperative to enhance the mechanical behavior and optimize the interleaved structures to improve overall performance. Therefore, this study aims to investigate the impact of incorporating amorphous halloysite nanotubes (A-HNTs) within different layers of five unique layer arrangements on the low-velocity impact properties of interleaved carbon fiber-reinforced polymer (CFRP) structures. The low-velocity impact characteristics of the laminate were validated using a drop weight impact test, wherein the resulting impact damage modes and extent of damage were compared and evaluated under microscopic analysis. Each interleaved structure laminate according to whether nanoparticles are added was compared at impact energies of 10 J and 15 J. In the case of 10 J, the absorption energy showed a similar tendency in each structure. However, at 15 J, the absorption energy varies from structure to structure. Among them, a structure in which nanoparticles are not added exhibits the highest absorption energy. Additionally, various impact fracture modes were observed in each structure through optical microscopy.

Acoustic Emission Monitoring of Compression-after-Impact Test of Nano-Particles-Coated CFRP Damaged by Simulated Lightning Strikes (나노입자 코팅 CFRP의 모의 낙뢰 충격손상 후 압축시험에서의 음향방출 거동)

  • Shin, Jae-Ha;Kwon, Oh-Yang;Seo, Seong-Wook
    • Journal of the Korean Society for Nondestructive Testing
    • /
    • v.31 no.1
    • /
    • pp.62-67
    • /
    • 2011
  • Nanoparticles-coated and impact-damaged carbon-fiber reinforced plastics(CFRP) laminates were tested under compression-after-impact(CAI) mode and the propagation of damage due to compressive loading has been monitored by acoustic emission(AE). The impact damage was induced not by mechanical loading but by a simulated lightning strike. CFRP laminates were made of carbon prepregs prepared by coating of conductive nano-particles directly on the fibers and the coupons were subjected to simulated lightning strikes with a high voltage/current impulse of 10~40 kA within a few microseconds. The effects of nano-particles coating and the degree of damage induced by the simulated lightning strikes on the AE activities were examined, and the relationship between the compressive residual strength and AE behavior has been evaluated in terms of AE event counts and the onset of AE activity with the compressive loading. The degree of impact damage was also measured in terms of damage area by using ultrasonic C-scan images. From the results assessed during the CAI tests of damaged CFRP showed that AE monitoring appeared to be very useful to differentiate the degree of damage hence the mechanical integrity of composite structures damaged by lightning strikes.

Finite Element Analysis of Instrumented Posterior Lumbar Interbody Fusion Cages for Reducing Stress Shielding Effects: Comparison of the CFRP cage and Titanium cage (요추유합술에서 응력방패 현상 감소를 위한 케이지의 유한요소해석 : CFRP 케이지와 티타늄 케이지 비교 연구)

  • Kang, Kyung-Tak;Chun, Heoung-Jae;Kim, Ho-Joong;Yeom, Jin-S.;Park, Kyoung-Mi;Hwang, In-Han;Lee, Kwang-Ill
    • Composites Research
    • /
    • v.25 no.4
    • /
    • pp.98-104
    • /
    • 2012
  • In recent years, degenerative spinal instability has been effectively treated with a cage. However, little attention is focused on the stiffness of the cage. Recent advances in the medical implant industry have resulted in the use of medical carbon fiber reinforced polymer (CFRP) cages. The biomechanical advantages of using different cage material in terms of stability and stresses in bone graft are not fully understood. A previously validated three-dimensional, nonlinear finite element model of an intact L2-L5 segment was modified to simulate posterior interbody fusion cages made of CFRP and titanium at the L4-L5 disc with pedicle screw, to investigate the effect of cage stiffness on the biomechanics of the fused segment in the lumbar region. From the results, it could be found that the use of a CFRP cage would not only reduce stress shielding, but it might also have led to increased bony fusion.