• Title/Summary/Keyword: 탄소섬유 강화 복합재료

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Drilling Characteristic of CFRP Composites depend on the number of stacking and drill diameter (CFRP복합재료의 적층수와 드릴직경에 따른 가공 특성)

  • 정성택;박종남;조규재
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2003.04a
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    • pp.190-195
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    • 2003
  • CFRP composite has a lot of merits such as mechanical characteristic, light weight, and thermal resistance. For these merits CFRP is applied to so many industrial area. In this paper, the relationship between the stack thickness and drill diameter is examined from the drilling experiment, which is the drilling of 16, 32, 48 plies specimen with the $\phi$8, $\phi$10, $\phi$12mm cemented carbide drill. The results are analyzed with consideration of cutting force, stack thickness and drill diameter.

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AE Signals Characteristics from Fracture by Type of CFRP Stacking Structure (CFRP 적층 형태에 따른 파괴시 음향방출 신호특성)

  • 남기우;문창권
    • Journal of Ocean Engineering and Technology
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    • v.16 no.2
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    • pp.67-71
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    • 2002
  • Damage process of CFRP laminates was characterized by Acoustic Emission (AE). The main objective of this study is to determine if the sources of AE in CERP laminates could be identified from the characteristics of the waveform signals recorded during monotonic tensile test. The time history and power spectrum of each individual wave signal recorded during test were examined and classified according to their special characteristics. The wave from and frequency of AE signal from a specimens is an aid to the determination of the extent of the different fracture mechanism such as matrix crack, debonding, fiber pull-out and fiber fracture as load is increased. Four distinct types of signals were observed regardless of specimen condition. The result showed that the AE method could be effectively used for analysis of fracture mechanism in CFRP laminates.

Evaluation of Fiber Arrangement Condition of CF/PP Composites Using Electrical Resistance Measurement and Wettability (전기저항 평가법 및 접촉각을 이용한 CF/PP 복합재료 사출성형품 섬유 배열성 평가)

  • Kwon, Dong-Jun;Shin, Pyeong-Su;Kim, Jong-Hyun;Park, Joung-Man
    • Journal of Adhesion and Interface
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    • v.17 no.1
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    • pp.15-20
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    • 2016
  • Fiber arrangement was important for fiber reinforced thermoplastic composites using injection fabrication. In this work, fiber arrangement in CF/PP was investigated to use electrical resistance (ER) method during injection times. There were 3 types of injection products of CF/PP with different ER change ratio by fiber arrangement. High ER change ratio case of injection CF/PP products had better increased tensile strength. This reason was due to the fiber arrangement of CF/PP by injection. Fractured surface and contact angle of CF/PP products were used to evaluate for injection product quality. Uniform fiber arrangement of CF/PP by injection type exhibited the uniform heat condition of melted CF/PP. Steady thermal transfer effect occurred from melted CF/PP to steel injection mold. Steady thermal transfer effect of CF/PP was transmitted to high ER change ratio of mold. Ultimately, good condition CF/PP product by injection molding method could be predicted by using ER method.

A Study of Bearing Strength on Composite Pinned-Joint at Low Temperature (저온환경에서 복합재료 핀 연결부의 Bearing 강도에 관한 연구)

  • Her, N.I.;Lee, S.Y.;Kim, J.H.;Lee, Y.S.;Sa, J.W.;Cho, S.;Im, K.H.;Oh, Y.K.;Choi, C.H.;Do, C.J.;Kwon, M.;Lee, G.S.
    • Proceedings of the KSME Conference
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    • 2001.06a
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    • pp.413-418
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    • 2001
  • Fundamental failure mode in a laminated composite pinned-joint is proposed to assess damage resulting from stress concentration in the plate. The joint area is a region with stress concentrations thus a complicated stress state exists. The modeling of damage in a laminated composite pinned-joint presents many difficulties because of the complexity of the failure process. In order to model progressive from initial to final, finite element methods are used rather than closed form stress analyses. Failure analysis must be a logical combination of suitable failure criteria and appropriate material properties degradation rules. In this study, the material properties which were obtained in previous study, the preparing process of the bearing strength test for a pinned joint CFRP composite plate subjected to in-plane loading at low temperature, and the FEM result of progressive damage model using ANSYS program are summarized to assess the structural safety of CFRP plate used in the magnetic supporting post of KSTAR(Korea Superconducting Tokamak Advanced Research).

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Fracture Behavior of CFRP by Time-Frequency Analysis Method (시간-주파수 해석법에 의한 CFRP의 파괴 거동)

  • Nam, Ki-Woo;Ahn, Seok-Hwan;Lee, Sang-Kee;Kim, Hyun-Soo;Moon, Chang-Kwon
    • Journal of the Korean Society for Nondestructive Testing
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    • v.21 no.1
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    • pp.39-45
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    • 2001
  • Fourier transform has been one of the most common tools to study the frequency characteristics of signals. With the Fourier transform alone, however, it is difficult to tell whether signal's frequency contents evolve in time or not. Except for a few special cases, the frequency contents of most signals encountered in the real world change with time. Time-frequency analysis methods are developed recently to overcome the drawbacks of Fourier transform, which can represent the information of signals in time and frequency at the same time. In this study, damage process of a cross-ply carbon fiber reinforced plastic (CFRP) under monotonic tensile loading was characterized by acoustic emission. Different kinds of CFRP specimens were used to determine the characteristics of AE signals. Time-frequency analysis methods were employed for the analysis of fracture mechanisms in CFRP such as mix cracking, debonding, fiber fracture and delamination.

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Effect of Mechanical and Toughening Characteristics of Epoxy/Carbon Fiber Composite by Polyamide 6 Particles, CTBN Addition Technology (Polyamide 6 입자 및 CTBN 첨가 기술에 따른 에폭시/탄소섬유 복합재의 강인화 효과 및 기계적 특성)

  • Sung-Youl Bae;Kyo-Moon Lee;Sanjay Kumar;Ji-Hun Seok;Jae-Wan Choi;Woo-Hyuk Son;Yun-Hae Kim
    • Composites Research
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    • v.36 no.5
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    • pp.355-360
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    • 2023
  • Epoxy-based carbon fibers reinforced plastic (CFRP) exhibit limitations in their suitability for industrial applications due to high brittleness characteristics. To address this challenge, extensive investigations are underway to enhance their toughness properties. This research focuses on evaluating the toughening mechanisms achieved by Polyamide 6 particles(p-PA6) and Carboxyl-Terminated Butadiene-Acrylonitrile (CTBN) elastomer, with a specific emphasis on utilizing minimal additive quantities. The study explores the impact of varying concentrations of p-PA6 and CTBN additives, namely 0.5, 1, 2.5, and 5 phr, through comprehensive Mode I fracture toughness and tensile strength analyses. The inclusion of p-PA6 demonstrated improvements in toughness when introduced at a relatively low content of 1phr. This improvement manifested as a sustained fracture behavior, contributing to enhanced toughness, while simultaneously maintaining the material's tensile strength. Furthermore, the investigation revealed that the incorporation of p-PA6 affected in particle aggregation, thus influencing the overall toughening mechanism. Incorporation of CTBN, an elastomeric modifier, exhibited a pronounced increase in fracture toughness at higher concentrations of 2.5 phr and beyond. However, this increase in toughness was accompanied by a reduction in tensile strength, resulting in fracture behavior similar to conventional CFRP exhibiting brittleness. The synergy between pPA6, CTBN and CFRP appeared to marginally enhance tensile strength under specific content conditions. As a result of this study, optimized conditions for the application of the p-PA6, CTBN toughening technology have been identified and established.

Test Evaluation of a Linerless Composite Propellant Tank Using the Composite Collapsible Mandrel (복합재 분리형 맨드릴을 이용한 라이너 없는 복합재 추진제 탱크에 대한 시험 평가)

  • Seung Yun Rhee;Kwangsoo Kim;Young-Ha Yoon;Moo-Keun Yi;Hee Chul Kim
    • Composites Research
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    • v.36 no.2
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    • pp.132-139
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    • 2023
  • A linerless composite propellant tank was designed and manufactured by using the carbon fiber-reinforced composite materials which have superior strength-to-weight ratio in order to reduce weight of the tank. In this research, we designed a sub-scale composite propellant tank with a diameter of 800 mm to withstand an MEOP of 1.7 MPa. We manufactured the boss of the tank by using the same composite materials to reduce the thermal expansion difference between the boss and the secondary-bonded composite layers of the barrel in the cryogenic environment. We used the collapsible mandrel to manufacture the tank without any liner. The mandrel was made from epoxy-based composite tooling prepregs to reduce weight of the mandrel. We manufactured the test tanks by laying up the carbon fiber fabric prepregs manually on the mandrel and then applying the autoclave cure process. We performed a proof test, a helium tightness test, a repeated pressurization test, and a burst test in room temperature. The test results demonstrate that the proposed design and manufacture process satisfies all strength requirements as well as an anti-leakage requirement.

Comparison of Optimum Drilling Conditions of Aircraft CFRP Composites using CVD Diamond and PCD Drills (CVD 다이아몬드 및 PCD이 드릴을 이용한 항공용 CFRP 복합재료의 홀 가공성 비교)

  • Kwon, Dong-Jun;Wang, Zuo-Jia;Gu, Ga-Young;Park, Joung-Man
    • Composites Research
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    • v.24 no.4
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    • pp.23-28
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    • 2011
  • Recently CFRP laminate joints process by bolts and nets are developed rapidly in aircraft industries. However, there are serious drawback during jointing process. Many hole processes are needed for the manufacturing and structural applications using composite materials. Generally, very durable polycrystalline crystalline diamond (PCD) drill has been used for the CFRP hole process. However, due to the expensive price and slow process speed, chemical vapor deposition (CVD) diamond drill has been used increasingly which are relatively-low durability but easily-adjustable process speed via drill shape change and price is much lower. In this study, the comparison of hole process between PCD and CVD diamond coated drills was done. First of all, CFRP hole processbility was evaluated using the equations of hole processing conditions (feed amount per blade, feed speed). The comparison on thermal damage occurring from the CFRP specimen was also studied during drilling process. Empirical equation was made from the temperature photo profile being taken during hole process by infrared thermal camera. In addition, hole processability was compared by checking hole inside condition upon chip exhausting state for two drills. Generally, although the PCD can exhibit better hole processability, hole processing speed of CVD diamond drill exhibited faster than PCD case.

Electromagnetic Interference shielding effectiveness of carbon black / Glass fiber woven roving and Carbon fiber unidirectional fabric reinforced composite (카본블랙/섬유강화 복합재료의 전자파 차폐효과)

  • Kim J.S.;Han G.Y.;Ahn D.G.;Lee S.H.;Kim M.S.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.06a
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    • pp.1322-1325
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    • 2005
  • The main objectives of this research work are to develop conductive glass fiber woven roving and carbon fiber unidirectional fabric composite materials and to determine their electromagnetic shielding effectiveness(EMSE). Epoxy is the matrix phase and glass, carbon fiber are the reinforcement phase of the composite material. Carbon black are incorporated as conductive fillers to provide the electromagnetic shielding properties of the composite material. The amount of carbon black in the composite material is varied by changing the carbon black composition, woven roving and unidirectional (fabric) structure. The EMSE of various fabric composites is measured in the frequency range from 300MHz to 800MHz. The variations of EMSE of woven roving and unidirectional composites with fabric structure, metal powder composite are described. Suitability of conductive fabric composites for electromagnetic shielding applications is also discussed.

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Mechanical Behavior of Indentation Stress in Carbon Fiber Reinforced Silicon Carbide Composites with Different Densities (서로 다른 밀도를 갖는 탄소섬유강화 탄화규소 복합재료의 압흔응력에 의한 기계적 거동)

  • Lee, Kee-Sung;Kim, Il-Kyum;Kim, Tae-Woo;Kim, Se-Young;Han, In-Sub;Woo, Sang-Kuk
    • Journal of the Korean Ceramic Society
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    • v.48 no.4
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    • pp.288-292
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    • 2011
  • In this study, we investigated the mechanical behavior of carbon fiber reinforced silicon carbide composites by indentation stress. Relatively porous and dense fiber reinforced ceramic composites were fabricated by liquid silicon infiltration (LSI) process. Densification of fiber composite was controlled by hardening temperature of preform and consecutive LSI process. Load-displacement curves were obtained during indentation of WC sphere on the carbon fiber reinforced silicon carbide composites. The indentation damages at various loads were observed, and the elastic modulus were predicted from unloading curve of load-displacement curve.