• 한국주조공학회지
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• 제41권3호
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• pp.235-240
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• 2021

진공 가스분사법으로 제조된 Fe₇₅B₁₃P₅Nb₂Hf₁C₄ 합금의 응고중 액상의 크기와 이에 따른 냉각속도의 변화가 정출상의 형성에 미치는 영향에 대한 고찰을 하였다. 고온 액상에서 동일한 조건으로 응고된 서로 다른 크기의 액상이 구형의 분말형태로 응고될 때 크기에 따른 임계냉각속도의 차이를 계산하였으며, 액상의 평균 반지름이 3배정도 크기 차이가 날 경우 고상으로 변태할 때 임계냉각속도가 13.5배까지 차이가 나는 것을 알 수 있었다. 이러한 임계냉각 속도의 차이에 따른 정출상의 형성과 정출상의 형태와 크기에 따른 탄화물의 형성 거동을 조사하여 열역학 계산으로 예측된 결과와 비교 분석하였으며, 분말입자의 크기가 20~45 마이크론일 경우 Hf과 Nb이 포함된 MC타입의 탄화물이 초정으로 형성 되는 것을 알 수 있었으며 이때 Hf과 Nb의 비율은 합금의 조성 및 냉각속도에 따라 변화됨을 관찰 할 수 있었다.

• 한국주조공학회지
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• 제38권5호
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• pp.103-110
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• 2018

코발트기 주조용 초내열합금 X45를 이용하여 다양한 형태의 열처리에 따른 미세조직과 기계적 특성의 변화에 대하여 고찰한 결과를 요약하면 다음과 같다. 1) 합금의 응고 시 결정립계와 수지상간 경계를 따라 Cr이 다량 함유된 조대한 $M_{23}C_6$ 탄화물과 W과 Co의 함량이 높은 $M_6C$ 탄화물이 형성되어 있었고, $1274^{\circ}C$에서 용체화 처리하면 대부분의 탄화물이 용해되었다. $1150^{\circ}C$에서의 용체화 처리 동안 일부 결정립계 탄화물이 용해되지만 공정탄화물 근처에서 새로운 탄화물의 석출이 일어났다. $927^{\circ}C$와 $982^{\circ}C$에서 시효처리만 했을 때 용체화 처리 후 시효처리 한 시편 보다 공정 탄화물 근처에서 석출되는 탄화물의 양이 많았고, 크기가 작았다. 2) $1150^{\circ}C$에서 용체화 처리한 후 시효처리 하면 경도의 증가가 뚜렷하지 않으며, $927^{\circ}C$와 $982^{\circ}C$에서 시효처리만 했을 때 다량의 매우 미세한 탄화물의 석출에 의하여 경도의 증가 폭이 더 컸다. 상온 항복강도는 $927^{\circ}C$에서 시효처리 했을 때 가장 컸지만 인장강도와 연신율은 $982^{\circ}C$에서 12시간 시효처리 했을 때 가장 컸다. 고온 크리프 특성은 $982^{\circ}C$에서 12시간 시효처리 했을 때 가장 우수하였다. 3) 장시간 고온 노출 되는 동안 탄화물의 석출과 성장이 일어났고, 8000시간 고온에서 노출시킨 시편에서는 수지상 중심부에도 탄화물이 석출되어 크리프 파단 수명이 증가하였다.

• 한국세라믹학회지
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• 제50권1호
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• pp.37-42
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• 2013

Tristructural-isotropic (TRISO)-coated particles were fabricated by a fluidized-bed chemical vapor deposition (FBCVD) method for use in a very high temperature gas-cooled reactor (VHTR). ZrC as a constituent layer of TRISO coating layers was deposited by a chloride process using $ZrCl_4$ and $CH_4$ source gases in a temperature range of $1400^{\circ}C$ and $1550^{\circ}C$. The change in the microstructure of ZrC depending on the deposition temperature and its effect on the hardness were evaluated. As the deposition temperature increased to $1500^{\circ}C$, the grain size of the ZrC increased and the hardness of the ZrC decreased according to the Hall-Petch relationship. However, at $1550^{\circ}C$, the ZrC layer was highly non-stoichiometric and carbon-rich and did not obey the Hall-Petch relationship in spite of the decrease of the grain size. A considerable amount of pyrolytic carbon at the grain boundaries of the ZrC as well as coarse granular pyrolytic carbon were locally distributed in the ZrC layer deposited at $1550^{\circ}C$. Therefore, the hardness decreased largely due to the formation of a large amount of pyrolytic carbon in the ZrC layer.

• 한국세라믹학회지
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• 제39권10호
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• pp.948-954
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• 2002

차세대 발전 시스템에서 사용되는 고온 가스 필터용 지지층 소재를 제조하기 위하여 용융 Si 침윤 방법으로 기공율이 32∼36%, 주기공 크기가 37∼90 ${\mu}m$ 범위를 갖는 고강도 다공질 반응소결 탄화규소(RBSC)를 개발하였다. 반응소결 탄화규소 다공체의, 최대 파괴강도는 120MPa이었으며, 용융 Si 침윤 방법으로 제조된 반응소결 탄화규소 다공체에서는 SiC 입자 사이에 SiC/Si로 이루어진 기지상이 형성되어 있기 때문에 파괴 강도 및 열충격 특성이 점토 결합 탄화규소 다공체 보다 우수하였다. 반응소결 탄화규소 다공체의 기공율 및 기공 크기는 잔류 Si의 양 및 성형체에 사용한 SiC 입자 크기에 따라 다르게 나타났다.

• 열처리공학회지
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• 제12권1호
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• pp.31-39
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• 1999

In the present study, oxidation behavior of 304 and 316 stainless steels was investigated. After solution treatment, specimens were polished up to $1{\mu}m$ $Al_2O_3$ grade and then subjected to oxidation treatment in dry air. The range of temperature was used for oxidation treatment at $300^{\circ}C{\sim}500^{\circ}C$ and TEM was used for analyzing the components and structure of oxide film. Also, these results were compared with the results of ESCA and TG. According to the results of TEM analysis, it was found that Cr oxide film was formed on top of the surface after room temperature oxidation but amorphous Fe oxide was formed on top of the surface and polycrystalline $(Cr,Fe)_2O_3$ was formed below the amorphous Fe oxide layer after $500^{\circ}C$ oxidation treatment. The oxidized specimens at $500^{\circ}C$ showed that 316 stainless steel resists more strongly to grain and grain boundary oxidation than 304 stainless steel. These results suggested that Mo component resolved in 316 stainless steel matrix suppressed the formation of Cr carbide which may results in local Cr deplete area.

• 한국재료학회지
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• 제10권5호
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• pp.343-349
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• 2000

자전연소합성(SHS)법을 이용하여 탄소섬유와 티타늄, 지르코늄, 니오븀, 규소, 붕소, 중석, 몰리브덴의 분말로부터 여러 가지 섬유상 탄화물의 합성을 시도하였다. 티타늄과 지르코늄은 예열없이, 그 이외의 경우는 전기로 또는 화학로를 사용하여 예열하여 반응을일으킨 결과, TiC, ZrC, NbC, SiC, $B_4$C, WC,$ Mo_2$C 의 순수한 탄화물의 형성되었다. TiC, ZrC, NbC 및 $B_4$C 탄화물의 형상은 속의 빈 섬유상이었고, SiC는 보다 작은 입자와 미세 휘스커로 이루어진 섬유상을 하고 있었고 WC와 $Mo_2$C 는 비섬유상을 하고 있었다. 여러 가지 형상의 원인에 대하여 합리적 설명을 시도하였으며 정성적 메카니즘을 제안하였다.

• 한국재료학회지
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• 제20권4호
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• pp.217-222
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• 2010

Zirconium diboride (ZrB2) and mixed diboride of (Zr0.7Ta0.3)B2 containing 30 vol.% silicon carbide (SiC) composites were prepared by hot-pressing at $1800^{\circ}C$. XRD analysis identified the high crystalline metal diboride-SiC composites at $1800^{\circ}C$. The TaB2 addition to ZrB2-SiC showed a slight peak shift to a higher angle of 2-theta of ZrB2, which confirmed the presence of a homogeneous solid solution. Elastic modulus, hardness and fracture toughness were slightly increased by addition of TaB2. A volatility diagram was calculated to understand the oxidation behavior. Oxidation behavior was investigated at $1500^{\circ}C$ under ambient and low oxygen partial pressure (pO2~10-8 Pa). In an ambient environment, the TaB2 addition to the ZrB2-SiC improved the oxidation resistance over entire range of evaluated temperatures by formation of a less porous oxide layer beneath the surface SiO2. Exposure of metal boride-SiC at low pO2 resulted in active oxidation of SiC due to the high vapor pressure of SiO (g), and, as a result, it produced a porous surface layer. The depth variations of the oxidized layer were measured by SEM. In the ZrB2-SiC composite, the thickness of the reaction layer linearly increased as a function of time and showed active oxidation kinetics. The TaB2 addition to the ZrB2-SiC composite showed improved oxidation resistance with slight deviation from the linearity in depth variation.

• Carbon letters
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• 제12권2호
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• pp.95-101
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• 2011

To investigate new applications for illite as an additive for carbon-based composites, the composites were prepared with and without illite at different heat-treatment temperatures. The effects of the heat-treatment temperature on the chemical structure, microstructure, and thermal oxidation properties of the resulting composites were studied. As the heat-treatment temperature was increased, silicon carbide SiC formation via carbothermal reduction increased until all the added illite was consumed in the case of the samples heat-treated at $2,300^{\circ}C$. This is attributed to the intimate contact between the $SiO_2$ in the illite and the phenol carbon precursor or the carbon fibers of the preform. Among composites prepared at all temperatures, those with illite addition exhibited fewer pores, voids, and interfacial cracks, resulting in larger bulk densities and lower porosities. A delay of oxidation was not observed in the illite-containing composites prepared at $2,300^{\circ}C$, suggesting that the illite itself absorbed energy for exfoliation or other physical changes. Therefore, if the illite-containing C/C composites can reach a density generally comparable to that of other C/C composites, illite may find application as a filler for C/C composites. However, in this study, the illite-containing C/C composites exhibited low density, even when prepared at a high heat-treatment temperature of $2300^{\circ}C$, although the thermal oxidation of the resulting composites was improved.

• 한국분말재료학회지
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• 제23권3호
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• pp.247-253
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• 2016

In this study, solid solution heat treatment of consolidated nickel-based superalloy powders is carried out by hot isotactic pressing. The effects of the cooling rate of salt quenching, and air cooling on the microstructures and the mechanical properties of the specimens are analyzed. The specimen that is air cooled shows the formation of serrated grain boundaries due to their obstruction by the carbide particles. Moreover, the specimen that is salt quenched shows higher strength than the one that is air cooled due to the presence of fine and close-packed tertiary gamma prime phase. The tensile elongation at high temperatures improves due to the presence of grain boundary serrations in the specimen that is air cooled. On the contrary, the specimen that is salt quenched and consists of unserrated grain boundaries shows better creep properties than the air cooled specimen with the serrated grain boundaries, due to the negative creep phenomenon.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 1997년도 춘계학술대회 논문집
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• pp.135-140
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• 1997

The influences of ZrB$_2$ additions to SiC on microstructural, DDM(Electrical Discharge Machining), mechanical and electrical properties were investigated. composites were prepared by adding 15, 30, 45 vol.% ZrB$_2$particles as a second phase to SiC matrix. SiC-ZrB$_2$ composites obtained by hot pressing for high temperature structural application were fully dense with the relative densities over 99%. The fracture toughness of the composites were increased with the ZrB$_2$contents. In case of composite containing 30vol.% ZrB$_2$, the flexural strength and fracture toughness showed 45% and 60% increase, respectively compared to that of monolithic SiC sample. The electrical resistivities of SiC-ZrB$_2$ composites decreased significantly with the ZrB$_2$ contents. The electrical resistivity of SiC-30vol.% ZrB$_2$ composite showed 6.50$\times$10$^{-4}$ $\Omega$.cm. Cutting velocity of EDM of SiC-ZrB$_2$ composites are directly proportional to duty factor of pulse width. Surface roughness, however, are not all proportional to pulse width. Higher-flexural strength composites show a trend toward smaller crater volumes, leaving a smoother surface; the average surface roughness of the SiC-ZrB$_2$ 15 vol.% composite with the flexural strengthe of 375㎫ was 3.2${\mu}{\textrm}{m}$, whereas the SiC-ZrB$_2$ 30.vol% composite of 457㎫ was 1.35${\mu}{\textrm}{m}$. In the SEM micrographs of the fracture surface of SiC-ZrB$_2$ composites, the SiC-ZrB$_2$ two phases are distinct; the white phase is the ZrB$_2$and the gray phase is the SiC matrix. In the SEM micrographs of the EDM surface, however, these phases are no longer distinct because of thicker recast layer of resolidified-melt-formation droplets present. It is shown that SiC-ZrB$_2$ composites are able to be machined without surface cracking.