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Seong Lee 6 Articles
Research Trend of Mo based Superalloys
Jong Min Byun, Seok Hyun Hwang, Seong Lee, Young Do Kim
J Powder Mater. 2013;20(6):487-493.
DOI: https://doi.org/10.4150/KPMI.2013.20.6.487
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  • Preparation of Spherical Mo5Si3 Powder by Inductively Coupled Thermal Plasma Treatment
    Jang-Won Kang, Jong Park, Byung Choe, Seong Lee, Jung Park, Ki Park, Hyo Kim, Tae-Wook Na, Bosung Seo, Hyung-Ki Park
    Metals.2018; 8(8): 604.     CrossRef
Characterization of Hot Isostatically Pressed Ni-Based Superalloy IN 713C
Youngmoo Kim, Eun-Pyo Kim, Seong-Taek Chunga, Seong Lee, Joon-Woong Noh, Sung Ho Lee, Young-Sam Kwon
J Powder Mater. 2013;20(4):264-268.
DOI: https://doi.org/10.4150/KPMI.2013.20.4.264
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Nickel-based superalloy IN 713C powders have been consolidated by hot isostatic pressing (HIPing). The microstructure and mechanical properties of the superalloys were investigated at the HIPing temperature ranging from 1030°C to 1230°C. When the IN 713C powder was heated above gammaprime solvus temperature (about 1180°C), the microstructure was composed of the austenitic FCC matrix phase gamma plus a variety of secondary phases, such as gammaprime precipitates in gamma matrix and MC carbides at grain boundaries. The yield and tensile strengths of HIPed specimens at room temperature were decreased while the elongation and reduction of area were increased as the processing temperature increased. At 700°C, the strength was similar regardless of HIPing temperature; however, the ductility was drastically increased with increasing the temperature. It is considered that these properties compared to those of cast products are originated from the homogeneity of microstructure obtained from a PM process.

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  • Sintering and Microstructures of SUS 316L Powder Produced by 3D Printing Process
    W.J. Kim, H.-H. Nguyen, H.Y. Kim, M.-T. Nguyen, H.S. Park, J.-C. Kim
    Archives of Metallurgy and Materials.2017; 62(2): 1215.     CrossRef
Microstructural Evolution during Hot Deformation of Molybdenum using Processing Map Approach
Young-Moo Kim, Sung-Ho Lee, Seong Lee, Joon-Woong Noh
J Korean Powder Metall Inst. 2008;15(6):458-465.
DOI: https://doi.org/10.4150/KPMI.2008.15.6.458
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The hot deformation characteristics of pure molybdenum was investigated in the temperature range of 600sim1200°C and strain rate range of 0.01sim10.0/s using a Gleeble test machine. The power dissipation map for hot working was developed on the basis of the Dynamic Materials Model. According to the map, dynamic recrystallization (DRX) occurs in the temperature range of 1000sim1100°C and the strain rate range of 0.01sim10.0/s, which are the optimum conditions for hot working of this material. The average grain size after DRX is 5µm. The material undergoes flow instabilities at temperatures of 900sim1200°C and the strain rates of 0.01sim10.0/s, as calculated by the continuum instability criterion.
Application of Refractory Metal Powders to Military Material Fields
Young-Moo Kim, Eun-Pyo Kim, Seong Lee, Joon-Woong Noh
J Korean Powder Metall Inst. 2007;14(4):221-229.
DOI: https://doi.org/10.4150/KPMI.2007.14.4.221
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  • Synthesis and Nucleation Behavior of MoO3 Nano Particles with Concentration of Precursors
    Seyoung Lee, Namhun Kwon, Jaeseok Roh, Kun-Jae Lee
    Journal of Korean Powder Metallurgy Institute.2020; 27(5): 394.     CrossRef
  • Fabrication of Ultra Fine Grained Molybdenum and Mechanical Properties
    Se-Hoon Kim, Young-Ik Seo, Dae-Gun Kim, Myung-Jin Suk, Young-Do Kim
    Journal of Korean Powder Metallurgy Institute.2010; 17(3): 235.     CrossRef
A Study on the Reduction Mechanism of Tungsten and Copper Oxide Composite Powders
Seong Lee, Moon-Hee Hong, Eun-Pyo Kim, Sung-Ho Lee, Joon-Woong Noh
J Korean Powder Metall Inst. 2003;10(6):422-429.
DOI: https://doi.org/10.4150/KPMI.2003.10.6.422
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The reduction mechanism of the composite powders mixed with WO_3 and CuO has been studied by using thermogravimetry (TG), X-ray diffraction, and microstructure analyses. The composite powders were made by simple Turbula mixing, spray drying, and ball-milling in a stainless steel jar with the ball to powder ratio of 32 to 1 at 80 rpm for 1 h without process controlling agents. It is observed that all the oxide composite powders are converted to W-coated Cu composite powder after reducing treatment under hydrogen atmosphere. For the formation mechanism of W-coated Cu composite powder, the sequential reduction steps are proposed as follows: CuO contained in the ball-milled composite powder is initially reduced to Cu at the temperature range from 200°C to 300°C. Then, WO_3 powder is reduced to W O_2 via W O_2.9 and W O_2.72 at higher temperature region. Finally, the gaseous phase of WO_3(OH)_2 formed by reaction of WO_2 with water vapour migrates to previously reduced Cu and deposits on it as W reduced by hydrogen. The proposed mechanism has been proved through the model experiment which was performed by using Cu plate and WO_3 powder.
A Study on the Microstryctural Evoulution of the Reagion Aheas of Craters Created by Copper and W-Cu Shaped Charge Jets
Seong Lee, Moon-Hee Hong, Woon-Hyung Baek
J Korean Powder Metall Inst. 1999;6(1):69-74.
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The microstructure of the reagion of carters, created by Cu and W-Cu shaped charge jets, in a 1020 mild steel target has been intestiaged. The region ahead of the crater created by the Cu shaped charge jet, reveals dramatic grain refinement implying the occurrence of a dynamic recrystallization, while that of W-Cu one dose a martensitic transformation indicative of heating up to an austenitic region followed by rapid cooling.The impacting pressure calculated when the W-Cu shaped charge jet encounters the target is higher than that of the Cu one. The micro-hardness of the region ahead of the crater created by the W-Cu shaped charge jet is also higher than that of the Cu one. The microstructure of W-Cu slug remained in the inside of the craters depicts the occurrence of the remarkable elongation of W particles during the liner collaphse. From these results, the microstructural variation of the region ahead of the crater with Cu and W-Cu shaped charge jets is discussed in trems of the pressure dependency of the transformation region of ferrite and austenite phases.

Journal of Powder Materials : Journal of Powder Materials