• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 춘계학술발표대회 논문집
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• pp.159-162
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• 2000

Interfacial and microfailure properties of carbon fiber/epoxy matrix composites were evaluated using both tensile fragmentation and compressive Broutman tests with acoustic emission (AE). Amino-silane and maleic anhydride polymeric coupling agents were used via the dipping and electrodeposition (ED), respectively. Both coupling agents exhibited higher improvements in interfacial shear strength (IFSS) under tensile tests than compressive cases. However, ED treatment showed higher IFSS improvement than dipping case under both tensile and compressive test. The typical microfailure modes including fiber break, matrix cracking, and interlayer failure were observed during tensile test, whereas the diagonal slippage in fiber ends was observed during compressive test. For both the untreated and treated cases AE distributions were separated well under tensile testing. On the other hand, AE distributions were rather closer under compressive tests because of the difference in failure energies between tensile and compressive loading. Under both loading conditions, fiber breaks occurred around just before and after yielding point. Maximum AE voltage fur the waveform of carbon or basalt fiber breakage under tensile tests exhibited much larger than those under compressive tests.

• Macromolecular Research
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• 제10권1호
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• pp.24-33
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• 2002

Interfacial and microfailure properties of carbon fiber/epoxy composites were evaluated using both tensile fragmentation and compressive Broutman tests. A monomeric and two polymeric coupling agents were applied via the electrodeposition (ED) and the dipping applications. A monomeric and a polymeric coupling agent showed significant and comparable improvements in interfacial shear strength (IFSS) compared to the untreated case under both tensile and compressive tests. Typical microfailure modes including cone-shaped fiber break, matrix cracking, and partial interlayer failure were observed under tension, whereas the diagonal slipped failure at both ends of the fractured fiber appeared under compression. Adsorption and shear displacement mechanisms at the interface were described in terms of electrical attraction and primary and secondary bonding forces.

• Composites Research
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• 제13권4호
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• pp.54-66
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• 2000

탄소섬유/에폭시 복합재료의 계면 및 미세파괴 물성을 인장 fragmentation과 압축 Broutman 두 시험법과 음향방출 시험을 이용하여 평가하였다. Maleic anhydride polymeric coupling agent와 amino-silane를 각각 전기증착법 및 dipping을 통하여 섬유표면에 적용하였다. 두 coupling agents를 사용한 섬유와 기지간의 계면전단강도는 인장 및 압축 두 시험에서 모두 미처리와 비교하여 큰 증가를 나타내었다. 인장시험 동안에, 원추모양의 섬유파단과 기지의 cracking 그리고 부분적인 interlayer failure로 이루어진 전형적인 미세파괴 형태가 발생하였다. 이에 비하여, 압축시험에서는 부러진 섬유의 끝에서 대각선 방향이 슬립거동이 관찰되었다. 주어진 두 힘의 하중상태에서 섬유의 파단은 항복점 전후 부근에서 일어났다. 음향방출분포는 인장에서 섬유표면 처리와 미처리의 두 조건에서 미세파괴 신호가 잘 분리되었으며, 한편, 압축에서는 signal이 다소 중복되어 나타났다. 이는 탄소섬유의 인장력/압축력 간의 파괴에너지 차이에 기인한다고 고려된다. 탄소와 basalt 섬유복합재료의 섬유파단 waveform의 최대 voltage는 압축보다 인장시험에서 상당히 크게 나타났으며, 이들은 음향방출시험으로 파괴에너지 차이를 명확히 비교 및 확인할 수 있었다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.79-83
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• 2000

Interfacial and microfailure properties of carbon liber/bismaleimide (BMI) composites were evaluated using both tensile fragmentation and compressive Broutman tests with acoustic emission (AE). Since BMI is rather difficult matrix to apply for the conventional fragmentation test because of its too low elongation and too brittle and high modulus properties, dual matrix composite system was applied. After carbon fiber/BMI composite was prepared for rod shape by controlling differing curing stage, composites rod was embedded in toughened epoxy as outer matrix. The typical microfailure modes including fiber break, matrix cracking, and interlayer failure were observed during tensile testing, whereas the diagonal slippage in fiber ends was observed during compressive test. On the other hand, AE amplitudes of BMI matrix fracture were higher than carbon fiber tincture under tensile test because BMI matrix has very brittle and high modulus. The waveform of signals coming from BMI matrix fractures was consistent with AE amplitude result under tensile tests.

• 접착 및 계면
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• 제2권1호
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• pp.9-17
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• 2001

전기저항 측정법과 인장 및 압축 시험을 이용하여, 탄소섬유/에폭시 복합재료의 정화특성과 계면물성을 평가하였다. 계면이 존재하지 않는 탄소섬유 자체만을 사용했을 경우에는 경화 초기와 최종단계의 저항차이는 없었으며, 계면이 존재하는 탄소섬유/에폭시 시편의 경우에는 매트릭스 경화 수축에 의해 저항차가 크게 나타났다. 인장 하충하의 저항 변화 측정에서, 전기증작된 시편은 섬유의 첫 파단에 의해 저항이 무한대로 도달하는 시간이 미처리에 비해 다소 지연되는 현상을 보였다. 인장 및 압축 시험에서 표면처리된 시연은 미처리섬유에 비해 계면전단 강도가 현저히 크게 증가하였다. 인장의 경우, 미처리 섬유에서는 debonding 형태, 그리고 표면처리된 섬유에서는 cone 형태의 판단이 관찰되었다. 압축에서는 부러진 섬유 끝에서 대각선으로 미끄러지는 파단 현상이 두 경우 모두에서 나타났는데, 미처리섬유는 창 끝과 같은 예리한 파단이 일어나며, 전기증착된 섬유는 다소 둔한 판단이 나타났다. 이를 통해 전기증착에 의한 표면처리가 계면접착력과 미세파괴구조에 인장 및 압축하에서 각각 다른 영향을 주는 것을 확인하였다.

• Advanced Composite Materials
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• 제17권1호
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• pp.75-87
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• 2008

Aerospace structural applications, along with high performance marine and automotive applications, require high-strength efficiency, which can be achieved using metal matrix composites (MMCs). Rotating components, such as jet-engine blades and gas turbine parts, require materials that maximize strength efficiency and metallurgical stability at elevated temperatures. Titanium matrix composites (TMCs) are well suited in such applications, since they offer an enhanced resistance to temperature effects as well as corrosion resistance, in addition to optimum strength efficiency. The overall behavior of the composite system largly depends on the properties of the interface between fiber and matrix. Characterization of the fiber.matrix interface at operating temperatures is therefore essential for the developemt of these materials. The fiber fragmentation test shows good reproducibility of results in determining interface properties. This paper deals with the evaluation of fiber fragmentation characteristics in TMCs at elevated temperature and the results are compared with tests at ambient temperature. It was observed that tensile testing at $650^{\circ}C$ of single-fiber TMCs led to limited fiber fragmentation behavior. This indicates that the load transfer from the matrix to the fiber occurs due to interfacial friction, arising predominantly from mechanical clamping of the fiber by radial compressive residual and Poisson stresses. The present work also demonstrates that composite processing conditions can significantly affect the nature of the fiber.matrix interface and the resulting fragmentation of the fiber.

• Geomechanics and Engineering
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• 제30권5호
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• pp.401-411
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• 2022

To obtain the dynamic mechanical properties, fracture modes, energy and brittleness characteristics of Furong Baijiao coal rock, the dynamic impact compression tests under 0, 4, 8 and 12 MPa confining pressure were carried out using the split Hopkinson pressure bar. The results show that failure mode of coal rock in uniaxial state is axial splitting failure, while it is mainly compression-shear failure with tensile failure in triaxial state. With strain rate and confining pressure increasing, compressive strength and peak strain increase, average fragmentation increases and fractal dimension decreases. Based on energy dissipation theory, the dissipated energy density of coal rock increases gradually with growing confining pressure, but it has little correlation with strain rate. Considering progressive destruction process of coal rock, damage variable was defined as the ratio of dissipated energy density to total absorbed energy density. The maximum damage rate was obtained by deriving damage variable to reflect its maximum failure severity, then a brittleness index BD was established based on the maximum damage rate. BD value declined gradually as confining pressure and strain rate increase, indicating the decrease of brittleness and destruction degree. When confining pressure rises to 12 MPa, brittleness index and average fragmentation gradually stabilize, which shows confining pressure growing cannot cause continuous damage. Finally, integrating dynamic deformation and destruction process of coal rock and according to its final failure characteristics under different confining pressures, BD value is used to classify the brittleness into four grades.