• Title/Summary/Keyword: carbide precipitation

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Effect of Alloying Elements and Heat Treatment Temperatures on the Retained Austenite of Austempered Ductile iron (오스템퍼드구상흑연주철(球牀黑鉛鑄鐵)의 잔류(殘留)오스테나이트 조직(組織)에 미치는 합금원소(合金元素) 및 열처리온도(熱處理溫度)의 영향(影響)에 관한 연구(硏究))

  • Kim, Deog-Ryul;Cheon, Byung-Wook;Kim, Chang- Gue;Choi, Chang-Ock
    • Journal of Korea Foundry Society
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    • v.13 no.1
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    • pp.50-61
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    • 1993
  • Retained austenite in matrix of austempered ductile iron has been well-known as a parameter in controlling mechanical properties, but investigation to obtain quantitative relationship with mechanical properties lack. Therefore, this study executed austempering treatment at various temperatures on ductile iron alloyed with Mo, Ni, Cu. In consequence, microstructure of retained austenite transformed coarse, and quantity increased according as austempering temperature increased. After heat-treatment, microstructure of specimen alloyed with Ni was fine, and toughness improved. At austempering temperature up to $400^{\circ}C$, carbide precipitation started in retained austenite. In consequence, afforded cause of hardness increase, a lot of increase did not arise for coarse structure.

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Long-Term Aging Diagnosis of Rotor Steel Using Acoustic Nonlinearity

  • Kim, Chung-Seok;Park, Ik-Keun;Jhang, Kyung-Young;Hyun, Chang-Yong
    • Journal of the Korean Society for Nondestructive Testing
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    • v.31 no.6
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    • pp.642-649
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    • 2011
  • The long-term aging of ferritic 2.25CrMo steel was characterized using the acoustic nonlinear effect in order to apply to diagnose the degradation behavior of structural materials. We measured the acoustic nonlinearity parameter for each thermally aged specimen by the higher harmonic-generation technique. The acoustic nonlinearity parameter increased with aging time due to equilibrium M6C carbide precipitation, and has a favorable linear relation with Rockwell hardness. This study suggests that acoustic nonlinearity testing may be applicable to diagnostics on strength degradation in rotor steels.

The Effect of Microstructures on Yield Strength and Impact Properties of a Microalloyed Steel (미세합금강의 조직이 항복강도와 충격치에 미치는 영향)

  • Jo, Jong-Chun;Werner Osterler
    • 한국기계연구소 소보
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    • s.16
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    • pp.29-39
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    • 1986
  • Several heat treatment were applied to on HSLA steel of type StE47 (German standard) to produce five ferrite microstructures of different strength and at least two different grain sizes respectively. Whereas the ferrite microstructure had a strong influence on yield strength the effect of grain size was negligible. The different strength levels could be explained by regarding the arrangement of dislocations and vanadium carbide particles, and their mutual interaction. Specimens tranformed at $600^{\circ}C$ showed the highest strength levels. In this case precipitation has occured after the $\gamma$- $\alpha$ transformation. Very small VC particles are arranged mostly along dislocation lines. Increasing both, grain size and pearlite volume fraction leads to a remarkable shift of transition temperature which was further enhanced by increasing ferrite strength.

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Contribution of the Interface Energies to the Growth Process of Cemented Carbides WC-Co

  • Lay, Sabine;Missiaen, Jean-Michel;Allibert, Colette H
    • Proceedings of the Korean Powder Metallurgy Institute Conference
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    • 2006.09a
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    • pp.332-333
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    • 2006
  • The driving forces and the probable processes of WC-Co grain growth are reanalysed from recent data of interface energy and microstructure. Grain growth is driven by the disappearing of the high energy WC/WC and WC/Co interfaces with habit planes different from {0001}, ${10\bar{1}0}$ and ${11\bar{2}0}$ facets and by the area decrease of the WC/WC and WC/Co interfaces with {0001} and ${10\bar{1}0}$ habit planes. Grain growth mainly results of dissolution-precipitation. Abnormal grains are likely formed by defects assisted nucleation.

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Study on Softening Characteristics of 9Cr-1Mo Steel Weldments for High Temperature and Pressure Vessels Application (고온고압장치 적용을 위한 9Cr-1Mo강 용접부의 연화특성에 관한 연구)

  • 이영호;이규천;윤의박;김기철
    • Journal of Welding and Joining
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    • v.10 no.3
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    • pp.40-53
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    • 1992
  • 고온고압장치(High Temperature and Pressure Vessels)의 적용을 위한 기초연구로서 9Cr-1Mo강 용접부의 연화특성에 대하여 검토하였다. 9Cr-1Mo 강재에 Bead-on-Plate용접을 실시한 후, 용접부의 기계적 성질과 그 현미경조직관찰 및 미세경도를 측정한 결과, As-Welded 및 용접 후열처리(PWHT)등의 조건에 관계없이 용접열향부의 변태역과 템퍼링역의 경계에서 모재의 경 도보다 낮은 경도값(연화역)을 나타내었으며 이러한 원인은 결정립계(Grain boundary)에 석출 되는 탄화물의 형성에 의한 뜨임 현상임이 판명되었다.

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Investigation of Changes in Structural Characteristics and Chemical Composition after Heat Treatment Process of JIS-SUJ2 Bearing Steel (JIS-SUJ2 베어링강의 열처리 이후 표면 및 심부에서 나타나는 구조적, 화학적 물성 변화)

  • Donghee Lee;Kyun Taek Cho;Hyeonmin Yim;Seung-Hwan Oh;Tae Bum Kim;Woo-Byoung Kim
    • Korean Journal of Materials Research
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    • v.33 no.12
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    • pp.558-564
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    • 2023
  • In this study, we designed and manufactured a large angular contact ball bearing (LACBB) with low deformation using JIS-SUJ2 steel and analyzed changes in its structural characteristics and chemical composition upon heat treatment. The bearing was produced by hot forging and heat treatment including a quenching and tempering (Q/T) process, and its properties were analyzed using 4 mm thick specimens. A difference in the size distribution of the carbide in the outer and inner parts of the bearing was observed and it was confirmed that large and non-uniform carbide was distributed in the inner part of the bearing. After heat treatment, the hardness value of the outer part increased from 13.4 HRC to 61 HRC and the inner part increased from 8.0 HRC to 59.7 HRC. As a result of X-ray diffraction (XRD) measurements, the volume fraction of the retained austenite contained in the outer part was calculated to be 3.5~4.8 % and the inner part was calculated to be 3.6~5.0 %. The surface chemical composition and the content of chemical bonds were quantified through X-ray photoelectron spectroscopy (XPS), and a decrease in C=C bonds and an increase in Fe-C bonds were confirmed.

Microstructure and Morphology of Carbide Precipitates in $Ni_3Al$ and TiAl ($Ni_3Al$과 TiAl 중에 석출한 탄화물의 미세구조와 형태)

  • Han, Chang-Suk;Koo, Kyung-Wan;Kim, Jang-Woo
    • Journal of the Korean Society for Heat Treatment
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    • v.19 no.1
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    • pp.10-19
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    • 2006
  • Microstructure and morphology of precipitates in $Ni_3Al$- and TiAl-based intermetallics containing carbon have been investigated in terms of transmission electron microscopy(TEM). In an $L1_2$-ordered $Ni_3Al$ alloy with 4 mol.% of chromium and 0.2~3.0 mol.% of carbon, fine octahedral precipitates of $M_{23}C_6$ type carbide were formed in the matrix by aging at temperatures around 973 K after solution annealing at 1423 K. TEM examination revealed that the $M_{23}C_6$ phase and the matrix lattices have a cube-cube orientation relationship and keep partial atomic matching at the {111} interface. After prolonged aging or by aging at higher temperatures, the $M_{23}C_6$ precipitates then adopt a rod-like morphology elongated parallel to the <100> directions. In the $L1_0$-ordered TiAl containing 0.1~2.0 mol.% carbon, TEM observations revealed that needle-like precipitates, which lie only in one direction parallel to the [001] axis of the $L1_0$ matrix, appear in the matrix and preferentially at dislocations. Selected area electron diffraction(SAED) patterns analyses have shown that the needle-shaped precipitate is $Ti_3AlC$ of perovskite type. The orientation relationship between the $Ti_3AlC$ and the $L1_0$ matrix is found to be $(001)_{Ti3AlC}//(001)_{L10\;matrix}$ and $[010]_{Ti3AlC}//[010]_{L10\;matrix}$. By aging at higher temperatures or for longer period at 1073 K, plate-like precipitates of $Ti_2AlC$ with a hexagonal structure are formed on the {111} planes of the $L1_0$ matrix. The orientation relationship between the $Ti_2AlC$ and the $L1_0$ matrix is $(0001)_{Ti2AlC}//(111)_{L10\;matrix}$ and $_{Ti2AlC}//_{L10\;matrix}$.

The Effects of the Structural Changes and Mechanical Properties of the Austenitized and Tempered Martensitic STS 410 Stainless Steel on Its Temper Embrittlement (STS 410 마르텐사이트계 Stainless 강의 템퍼취성과 조직 및 기계적 성질에 관한 연구)

  • S.H., Lee;T.H., Go;W.S., Lee;S.D., Kim
    • Journal of the Korean Society for Heat Treatment
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    • v.35 no.6
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    • pp.303-313
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    • 2022
  • The purpose of this study was to test and analyze the effects of the mechanical properties and structural changes of the austenitized and tempered martensite STS 410 stainless steel containing 11.5~13%Cr and 0.10%C on its temper embrittlement. The STS 410 stainless steel test pieces for each 3 hours at 960℃, 1000℃ and then, tempered them for 2 hours at 300℃, 350℃, 400℃, 450℃, 500℃, 550℃, 600℃, 650℃ and 700℃ known as the intervals vulnerable to temper embrittlement to observe the changes of their structures and mechanical properties. In case autenitizing was insufficient due to lower temperature of thermal treatment for solution, unsolved carbides and ferrites remained in the structure after quenching, which meant that the parts could wear out and corrode to embrittle at the room temperature. Elongation and impact energy changes with Tempering conditions showed minimum results in range of 400~500℃. The decrease in elongation and impact energy at 400~500℃ was the hardening effect of the subgrain due to the precipitation of many M3C or M7C3, M23C6. And STS 410 stainless steel corrosion tested in 10% NaCl solution at 30℃ after tempering treatment. The degree of corrosion sensitization showed increasing tendency with increase of tempering temperature and Cr carbide precipitation were observed in grain boundary.

Effect of Cr/Ti/Al Elements on High Temperature Oxidation Behavior of a Ni-Based Superalloy with Thermal Exposure (고온 노출 니켈기 초내열합금 터빈 블레이드의 Cr/Ti/Al 성분이 고온 산화에 미치는 영향)

  • Byung Hak Choe;Sung Hee Han;Dae Hyun Kim;Jong Kee Ahn;Jae Hyun Lee;Kwang Soo Choi
    • Korean Journal of Materials Research
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    • v.33 no.2
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    • pp.77-86
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    • 2023
  • High-temperature oxidation of a Ni-based superalloy was analyzed with samples taken from gas turbine blades, where the samples were heat-treated and thermally exposed. The effect of Cr/Ti/Al elements in the alloy on high temperature oxidation was investigated using an optical microscope, SEM/EDS, and TEM. A high-Cr/high-Ti oxide layer was formed on the blade surface under the heat-treated state considered to be the initial stage of high-temperature oxidation. In addition, a PFZ (γ' precipitate free zone) accompanied by Cr carbide of Cr23C6 and high Cr-Co phase as a kind of TCP precipitation was formed under the surface layer. Pits of several ㎛ depth containing high-Al content oxide was observed at the boundary between the oxide layer and PFZ. However, high temperature oxidation formed on the thermally exposed blade surface consisted of the following steps: ① Ti-oxide formation in the center of the oxide layer, ② Cr-oxide formation surrounding the inner oxide layer, and ③ Al-oxide formation in the pits directly under the Cr oxide layer. It is estimated that the Cr content of Ni-based superalloys improves the oxidation resistance of the alloy by forming dense oxide layer, but produced the σ or µ phase of TCP precipitation with the high-Cr component resulting in material brittleness.

High Temperature Deformation Behavior of a NIMONIC 80A Ni-based Superalloy (Ni계 초내열합금 NIMONIC 80A의 고온변형거동)

  • Ha, M.C.;Hwang, S.W.;Kim, C.S.;Kim, C.Y.;Park, K.T.
    • Transactions of Materials Processing
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    • v.22 no.5
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    • pp.258-263
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    • 2013
  • The deformation behavior of NIMONIC 80A was studied in the high temperature range of $900{\sim}1200^{\circ}C$ and for strain rates varying between 0.02 and $20s^{-1}$ via the hot compression test. Processing maps for hot working were constructed on the basis of the power dissipation efficiency using a dynamic material model. The results showed that the strength during hot compression increased with increasing strain rate and decreasing temperature. At low strains, the processing map of NIMONIC 80A did not reveal any instability domain regardless of the strain rate and temperature. However, at high strains, the processing map exhibited an instability domain at a low strain rate of $0.2s^{-1}$ and within a temperature range of $900{\sim}960^{\circ}C$. In the instability domain, the deformed microstructure exhibited shear bands and carbide precipitation while, in the safe domain, full recrystallization occurred.