• 대한기계학회논문집
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• 제19권9호
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• pp.2122-2132
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• 1995

There are some cases which require to grasp the abrasion resistance property in the fields of the high-technology to be required the high specific strength and modulus. In this study, wear test with the various test temperature and velocity were performed in the SiCw/A16061 composite and A16061 matrix using the wear test machine of the ring-on-disc type. As the results, the friction and wear properties by various test temperature and velocity were examined. The worn surface has observed by scanning electron microscope in order to examine the wear mechanism.

• 대한기계학회논문집
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• 제19권1호
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• pp.122-131
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• 1995

The research trends for metal matrix composites have been on basic mechanical properties, fatigue behavior after aging and fractographic observations. In this study, the fatigue crack initiation as well as the fatigue crack growth behavior and the fracture mechanism were investigated through observations of the fracture surface on silicon carbide particles reinforced aluminum metal matrix composites(SiCp/Al). Based on the fractographic study done by scanning electron microscope and replica, crack growth path model and fracture mechanism are presented. The mechanical properties, such as the tensile strength, yield strength and elongation of SiCp/Al composites are improved in a longitudinal direction, however, the fatigue life is shorter than the basic Al6061 alloys. From fractographic observations, it is found that the failure mode is ductile in basic Ai6061 alloys. And because some SiC particles were pulled out from the matrix and a few SiC particles could be seen on the fracture surface of SiCp/Al, crack growth paths are believed to follow the interface of the matrix and its particles.

• Composites Research
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• 제16권1호
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• pp.1-12
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• 2003

본 연구는 보강재의 부피분율이 49%, 56%, 63%첨가된 패키징용 SiC/Al복합재료를 가압주조법을 통해 개발하였다. SiC/Al복합재료는 0.8%의 무기성형제와 $Al_2$O$_3$섬유가 SiC입자에 비해 부피비 1:10의 비율로 첨가되었으며 새로이 고안된 몰드에서 제조되었다. 제조된 SiC/Al복합재료에 대해 30-300 구간에서 열팽창 계수를 측정하고, FEM수치해석과 비교하여 온도에 따른 특성을 분석하였다. 실험결과 SiC/Al복한재료의 열팽창계수는 혼합법칙, Turner모델의 중간값을 가졌으며 상온에서는 Turner모델에 가깝다가 온도가 높아질수록 혼합법칙에 가까와졌다. 이러한 특성은 모재의 소성변형 및 잔류응력에 의한 것으로 본 연구에서 제안한 모재와 보강재 사이에 작용하는 평균응력 차이로부터 분석이 된다. 해석결파 모재의 소성변형이 시작되는 온도에서 SiC/Al복합재료의 열팽창계수가 급격히 증가하였으며, 가공 잔류응력은 이러한 소성변형의 시작온도를 고온으로 이동시킴으로써 열팽창계수에 영향을 끼침을 밝혔다. 이러한 일련의 연구를 통해 온도에 따른 열팽창 특성은 복수입자모델에 의한 2차인 해석을 통해 성공적으로 분석됨을 보였다.

• 한국분말재료학회지
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• 제7권1호
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• pp.35-41
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• 2000

Al2O3$.$SiC particle was prepared was prepared by the self-propagting high temperature sYthesis(SHS) process from a mixture of SiO2, Al and C powders, The fabricated Al2O3$.$SiC particle was applied to 2024Al/(Al2O3$.$SiC)pcomposite as a reinforcement. Aluminum matix composites were fabricares by the powder extrusion method using the synthesized Al2O3$.$SiC particle and commercial 2024Al powder. Theoptimum preparation conditions for Al2O3$.$SiC partticle by SHS process were described. The influence of the Al2O3$.$SiC voiume fraction on the mechanical was composite was also discussed. Despite adiabatic temperature was about 2367K, SHs reaction was completed not by itself, but by using pre-heating. Mean particle size of final particle synthesized was 0.73 ${\mu}$m and most of the particle was smaller than 2${\mu}$m. Elastic modulus and tensile strength of the composite increased with increase the volume fraction of reinforcement but, tensile strength depreciated at 30 vol% of reinforcement.

• 한국정밀공학회지
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• 제11권2호
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• pp.95-103
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• 1994

The purpose of this paper is to provide the experimenters who use the oblique incidence ultrasonic method for anisotropic elastic constants measurement eith some useful relations. In particular, the equivalence of the times of flight by the energy ad phase velocities, which is key to the oblique incidence method, is proved explicitly. This equivalence greatly simplifies the analysis of immersion measurement results. In oredr to correctly measure the transit time of an immersed sample using the oblique incidence, the receiving transducer should be shifted laterally, and an expression in given for this shift. A method for determining all nine elastic constants of an orthotropic material is briefly described and the measurement results are listed for SiC particulate reinforced A1 matrix composites.