• 대한기계학회논문집
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• 제18권9호
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• pp.2374-2385
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• 1994

SiCw/Al composite material is especially attractive because of their superior specific strength, specific stiffness, corrosion fatigue resistance, creep resistance, and wear resistance compared with the corresponding wrought Al alloy. In this study, Fatigue crack growth behavior and fatigue crack path morphology(FCPM) of SiC whisker reinforced Al 6061 alloy with 25% SiC volume fraction and Al 6061 allay were performed. Result of the fatigue crack growth test sgiwed that fatigue crack growth rate of SiCw/Al 6061 composite was slower than that of Al 6061 matrix therefore it was confirmed that Sic whisker have a excellent fatigue resistance. And Al 6061 matrix had only FCPM perpendicular to loading direction. On the other hand SiCw/Al 6061 composite had three types in fatigue crack path morphology. First type is that both sides FCPM of artificial notch are perpendicular to loading direction. Second type is that a FCPM in artifical notch has slant angle to loading direction and the other side FCPM is perpendicular to loading direction. Third type is that both sides FCPM of notch have slant angle to loading direction. It was considered that this kinds of phenomena were due to non-uniform distribution of SiC whisker and confirmed by SEM observation for fracture mechanism study.

• 한국재료학회지
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• 제10권12호
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• pp.793-798
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• 2000

석출경화형 6061Al기지합금과 SiC입자크기를 0.7$\mu\textrm{m}$ 및 7.0$\mu\textrm{m}$로 변화시켜 강화한 SiCp/6061Al 합금복합재료의 시효 거동을 경도측정, DSC 시험 및 TEM관찰을 통하여 조사하였다. 17$0^{\circ}C$에서 등온시효시 6061Al기지합금에 비하여 복합화한 0.7$\mu\textrm{m}$SiCp/6061Al합금복합재료 및 7.0$\mu\textrm{m}$SiCP/6061Al합금복합재료에서 최고경도에 도달하는 시간이 짧았으며, 또한 강화재의 크기가 큰 7.0$\mu\textrm{m}$SiCp/6061Al합금복합재료에서 시효촉진이 보다 크게 나타났다. 이것은 복합화 및 SiC입자크기 증가에 따른 전위 밀도 상승에 기인한다. 6061Al기지합금 및 복합재료에서 최고시효처리시의 주강화상은 봉상의 중간상 $\beta$(Mg$_2$Si)이며,$\beta$상 생성의 활성화에너지는 복합화 및 SiG입자크기의 증가에 따라 감소되었다

• 대한기계학회논문집
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• 제19권2호
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• pp.475-485
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• 1995

In this study, statistical analysis of fatigue data which had obtained from respective 24 fatigue crack, was examined for SiC whisker reinforced aluminium 6061 composite alloy (SiC$_{w}$/A16061) and aluminium 6061 alloy. SiC volume fraction in composite alloy is 25%. The analysis results stress intensity factor range and 0.1 mm fatigue crack initiation life for SiC$_{w}$/A16061 composite & A16061 matrix are the log-normal distribution. And regression analysis by linear model, exponential model and multiplicative model were performed to find out the relationship between fatigue crack growth rate(da/dN) and stress intensity for find out the relationship between fatigue crack growth rate(da/dN) and stress intensity factor range(.DELTA.K) in the SiC$_{w}$/A16061 composite and examine the applicability of Paris' equation to SiC$_{w}$A16061 composite. Also computer simulation was performed for fatigue life prediction of SiC$_{w}$/A16061 composite using the statistical results of this study.udy.

• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part2
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• pp.855-856
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• 2006

In the present work, hot workability of particulate-reinforced Al6061-20%SiC composite produced by direct hot extrusion technique was studied. Uniaxial hot compression test at various temperatures and strain rates was used and the workability behavior was evaluated from the flow curves and the attendant microstructures. It was shown that the presence of SiC particles in the soft Al6061 matrix deteriorates the hot workability. Bulging of the specimens and flow lines were observed, which indicate the plastic instability during hot working. Microstructure of the composites after hot deformation was found to be heterogeneous, i.e. the reinforcement clusters were observed at the flow lines. The mechanism of deformation was found to be controlled primarily by dynamic recrystallization.

• 한국분말재료학회지
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• 제9권1호
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• pp.11-18
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• 2002

The 6061 Al alloy based composites reinforced with 10 vol% SiC whiskers were prepared by powder metallurgy with the powders having the different sizes, i.e. < $30{\mu}m$ and > $30{\mu}m$ The composites were subjected to equal channel angular pressing (ECAP) at various conditions and the microstructural changes during ECAP were examined In the composites SiC whiskers were clustered and randomly aligned. The clusters were relatively well distributed in the composite with the smaller initial powder size. After ECAP, the clusters were aligned parallel to flow direction and became smaller. In addition, the shape of clusters was changed from irregular to round. The microstructure of the ECAPed samples were compared with those of the conventionally hot-extruded composites. The uniform microstructure and enhanced microhardness could be obtained by using the powders having the smaller size, decreasing ECAP temperature and repeating ECAP.

• 한국재료학회지
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• 제4권8호
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• pp.945-951
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• 1994

분말야금법으로 제조된 $SiC_{p}$/6061 Al 복합재료의 열간 압출가공에 있어서 압출성에 미치는 빌렛의 특성과 압출조건의 영향에 대하여 조사하였다. 압출가공성의 난이도를 판단 할 수 있는 기준이 되는 최대압출력과 변형저항 값($K_{w}$)은 350ton 압출기를 이용한 압출압력의 측정과 Watanabe등의 경험식에 의해 도출되었다. 6061Al합금기 복합재료 빌렛의 전단변형저항고 압출압력은 강화재($SiC_{p}$)의 부피분율이 증가함에 따라 증가하고 있으나, 증가되는 비율은$SiC_{p}$인 경두가 $SiC_{w},Al_{2}O_{3f}$/보다 작았다. 강화입자 크기가 작을 수록 변형저항 값이 증가하였고 압출성도 양호하였다. 변형저항 값의 증가는 기지금속의 가공경화에 기인하며, 최대압출력을 나타내는 피이크는 강화재의 입자가 미세할 수록, 즉 가공경호가 클 수록 뾰족한 형상을 나타내었다. 압출온도가 증가할 수록 변형저항 값이 낮아져서 작은 압출력으로도 복합재료의 압출이 가능하나, $500^{\circ}C$이상인 경우 압출재 표면에 극심한 tearing현상이 발생하였다.

• 한국세라믹학회지
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• 제34권4호
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• pp.343-350
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• 1997

To fabricate the ceramic/metal(SiC/ Al alloy) composite, SiC preform was prepared by Pressureless Powder Packing Forming Method and 6061 Al alloy was infiltrated into the preform. Uniform compact having an average pore size of 10 ${\mu}{\textrm}{m}$ and narrow pore size distribution was prepared. Phenolic resin solution(40 wt%) was penetrated into the SiC compact, and then the compact was preheated at the temperature of 120$0^{\circ}C$. The pore size distribution and the microstructure of the preform were not changed by preheating. An uniform microstructure without any crack in the preform was obtained in SiC-Al alloy composite. The infiltration of 6061. Al alloy into the preform began at the temperature of 130$0^{\circ}C$ and the amount of infiltration increased in proportion to the infiltration temperature and the soaking time. The increasement rate of the infiltration amount decreased after 3 h. As a result of the infiltration at 140$0^{\circ}C$ for 4 h, Al alloy was well distributed in the interparticle channels and the relative density of the composite was above 98%. The strength and the fracture toughness of the composite were 303 MPa and 21.65 MPam1/2, respectively.

• 한국분말재료학회지
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• 제1권1호
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• pp.42-51
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• 1994

6061Al-SiCP metal matrix composite materials(MMCs) were fabricated by injecting SiCP particles directly into the atomized spray. The main attraction of this technique is the rapid fabrication of semi-finished, composite products in a combined atomization, particulate injection(10 $\mu\textrm{m}$, 40 $\mu\textrm{m}$, SiCP) and deposition operation. Conclusions obtained are as follows; The microstructure of the unreinforced spray formed 6061Al alloy consisted of relatively fine(50 $\mu\textrm{m}$) equiaxed grains. By comparision, the microstructure of the I/M materials was segregated and consisted of relatively coarse(150 $\mu\textrm{m}$) grains. The probability of clustering of SiCP particles in co-sprayed metal matrix composites increased it ceramic particle size(SiCP) was reduced and the volume fraction was held constant. Analysis of overspray powders collected from the spray atomization and deposition experiments indicated that morphology of powders were nearly spherical and degree of powders sphercity was deviated due to composite with SiCp particles. Interfacial bonding between matrix and ceramics was improved by heat treatment and addition of alloying elements(Mg). Maximum hardness values [Hv: 165 kg/mm2 for Al-10 $\mu\textrm{m}$ SiCp Hv--159 kg/mm2 for Al-40 $\mu\textrm{m}$SiCp] were obtained through the solution heat treatment at $530^{\circ}C$ for 2 hrs and aging at $178^{\circ}C$, and there by the resistance were improved.

• 한국주조공학회지
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• 제16권2호
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• pp.132-140
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• 1996

Both cast and extruded composites of SiC whisker reinforced 6061 Al alloy matrix were fabricated by high pressure infiltration of the alloy melt into the SiC preform and subsequent hot extrusion of the composite ingots. The micro structures, age hardening behavior and mechanical properties have been examined on the both cast and extruded composites of SiCw/6061. The cast composites of SiCw/6061 were obtained in which SiC whiskers were randomly oriented. Hot extrusion of these cast composites lead to alignment of the whisker in the direction of extrusion. Strengthening effect of whisker in the extruded composites is lower than that of the cast composites. The cast composites of SiCw/6061 showed higher thensile strength and lower elongation than extruded composites of SiCw/6061 at all testing temperatures. Lower tensile strength and higher elongation of the extruded composites were attributable to fine grain structures in which grain boundary sliding occruued preferentially at elevated temperatures.

• 한국재료학회지
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• 제5권7호
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• pp.765-774
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• 1995

입자강화 알루미늄 복합재료의 고온거동을 조사하기위하여, 온도 623K~823K에서 $10^{-2}$ ~1.0 S$^{-1}$ 변형속도로 열간 압축 가공 시험을 행하여 복합재의 고온유동응력에 미치는 강화입자의 첨가량, 강화입자의 종류 및 크기와 변형속도 및 변형온도 등의 영향을 조사하였다. 강화입자의 체적분율이 증가함에 따라서 고온유동음력은 증가하였으나 항복점에서의 차이가 변형량이 증가되어도 그대로 유지되고 있었다. 변형속도 민감도(m)로 볼때 SiCp첨가된 복합재가 A1$_2$O$_3$p를 첨가한 복합재보다 비교적 균일하게 가공할 수 있음을 알 수 있었으며, 823K에서 최적변형속도는 0.1Sec$^{-1}$ 이었다. 변형에 필요한 활성화 에너지는 A6061기지금속이 290KJmole$^{-1}$, A6061-20vo1% SiCp = 327KJmo1e$^{-1}$, A6061-20vo1% $Al_2$O$_3$= 531KJmole$^{-1}$이었다. 이것은 알루미늄의 자기활성화에너지 138KJmo1e$^{-1}$보다 큰 값으로 A1$_2$O$_3$강화복합재료가 SiCp 강화 복합재료보다 열간가공이 어렵다는 것을 나타내는 것이다.