• Title/Summary/Keyword: 크리프 파단 특성

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Microstructural Evolution and Magnetic Property of Creep-Fatigued Ferritic 9Cr Heat-Resisting Steel (크리프-피로 손상된 페라이트기 9Cr 내열강의 미세조직 발달과 자기적 특성)

  • Kim, Chung-Seok;Kwun, S.I.;Park, Ik-Keun
    • Journal of the Korean Society for Nondestructive Testing
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    • v.27 no.5
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    • pp.417-425
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    • 2007
  • The ferritic 9Cr-1Mo-V-Nb heat-resisting steel was experimentally studied in order to characterize its microstructural evolution during creep-fatigue by coercivity measurement. The creep-fatigue test was conducted at $550\;^{\circ}C$ with the tensile holding time of 60s and 600s, respectively. The coercivity decreased until the failure and the hardness monotonously decreased for the whole fatigue life. As the life fraction of creep-fatigue increased, the $M_{23}C_6$ carbide coarsened following the Ostwald ripening mechanism. However, the MX carbonitrides did not grow during creep-fatigue due to so stable at $550\;^{\circ}C$. The width of martensite lath increased because of the dislocation recovery at the lath boundaries. The magnetic coercivity has an influence on the microstructural properties such as dislocation, precipitates and martensite lath boundaries, which interpreted in relation to microstructural changes. Consequently, this study proposes a magnetic coercivity to quantify the level of damage and microstructural change during the creep-fatigue of ferritic 9Cr-1Mo-V-Nb steel.

Relationship between Creep Characteristic Values and Rupture time in STS304 Stainless Steels (스테인리스강의 크리프 특성치와 파단시간과의 관계)

  • KONG YU-SIK;KIM SEON-JIN;LEE BAE-SUB
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2004.11a
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    • pp.228-233
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    • 2004
  • The characteristics of the probability distribution for mechanical properties, e.g. tensile strength, reduction of area ana elongation, for STS304 stainless steel in elevated temperature were investigated from tensile test performed by constant cross head speea controls with 1mm/min, Recently, in order to clarify the strengthening mechanisms at high temperature, a new scheme to improve high temperature mechanical properties is desired. Therefore, the test ,technique development of high temperature creep behaviors for this material is very important. In this paper, the creep praperties and creep life prediction by Larson-Miller parameter method for STS304 stainless steel to be used for other high temperature components were presented at the elevated temperatures of 600, 650 and $700^{\circ}C$.

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Tensile Properties and Creep Rupture Characteristics of Cu-1Cr-0.5Zr/STS316L Friction Welded Joints at Elevated Temperature (Cu-1Cr-0.5Zr 합금과 STS316L강의 마찰용접재의 고온 인장 성질과 크리프 파단 특성)

  • Yoo, I.J.;Kong, Y.S.;Kim, S.J.
    • Journal of Power System Engineering
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    • v.6 no.4
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    • pp.49-55
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    • 2002
  • In this paper, the elevated temperature tensile properties and short-time creep rupture characteristics were investigated for the friction welded joints of dissimilar materials, Cu-1%Cr-0.5%Zr and STS316L. The joining tests on Cu-1%Cr-0.5%Zr/STS316L by friction welding were performed, and optimum joining conditions of the friction welded joints were determined. The characteristics of the elevated temperature tensile strength, hardness, fractographs were examined, and the creep rupture characteristics for the optimum welded joints were investigated under uniaxal static load at 300, 400 and $500^{\circ}C$.

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High Temperature Creep Rupture Characteristics of Ni-Based Alloy718 (니켈기 초내열합금 Alloy718의 고온 크리프 파단 특성)

  • Kwon, Sang-Woo;Kong, Yu-Sik;Kim, Seon-Jin
    • Journal of Ocean Engineering and Technology
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    • v.22 no.6
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    • pp.52-57
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    • 2008
  • The short-term high temperature creep rupture behavior of Ni-based Alloy718 steel was investigated at the elevated temperatures range of 550 to $700^{\circ}C$ under constant stress conditions. The creep rupture characteristics such as creep stress, rupture time, steady state creep rate, and initial strain were evaluated. Creep stress has a quantitative correlation between creep rupture tim and steady state creep rate. The stress exponents (n, m) of the experimental data at 550, 600, 650 and $700^{\circ}C$ were derived as 33.5, -24.9, 26.1, -21.2, 16.8, -12.8 and 10, -8.2, respectively. The stress exponent decreased with increasing creep temperature. The creep lift prediction was derived by the Larson-Miller parameter (LMP) method and the resultant equation was obtained as follows: T($logt_r$+20)=-0.00252 ${\sigma}^2$-1.377${\sigma}$+-22718.

Creep Properties of Aircraft Gas Turbine Materials in relation to Heat Treatment (항공기용 가스터빈 재료의 열처리에 따른 크리프 특성)

  • Kong, Yu-Sik;Oh, Sae-Kyoo;Park, No-Kwang
    • Journal of Ocean Engineering and Technology
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    • v.13 no.4 s.35
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    • pp.112-117
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    • 1999
  • In this paper, the creep properties and creep life prediction by Larson-Miller Parameter method for Udimet 720 to be used for aircraft gas turbine engines or other high temperature components were presented at the elevated temperatures of 538, 649 and $704^{\circ}C$. It was confirmed experimentally and quantitatively that a creep life predictive equation at such various high temperatures was well derived by LMP.

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Thermal Aging and Creep Rupture Behavior of STS 316 (STS 316의 시효 열화 처리와 크리프 거동 특성)

  • 임병수
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.8 no.4
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    • pp.123-129
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    • 1999
  • Although type 316 stainless steel is widely used such as in reactors of petrochemical plants and pipes of steam power plants and s attracting attention as potential basic material for the fast breeder reactor structure alloys in nuclear power plants and is attracting attention as potential basic material for the fast breeder reactor structure alloys in nuclear power plants the effect of precipitates which form during the long term exposure at service temperature on creep properties is not known sufficiently. In this study to investigate the creep properties and the influence of prior aging on the microstructure to form precipitates specimens were first solutionized at 113$0^{\circ}C$ for 20 minutes and then aged for different times of 0 hr, 100 hrs, 1000 hrs and 2200 hrs at 75$0^{\circ}C$ After heat treatments tensile tests both at room temperature and $650^{\circ}C$ and constant load creep ruptuere tests were carried out.

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Life Prediction and AE Evaluation of Pure or Cyclic Creep for Power Plant Materials ; Pure Creep and AE Evaluation (전력용 강재의 정적.동적 크리프의 상관성과 예측 및 AE평가(1); 정적 크리프와 AE평가)

  • 오세규;장홍근;송정근
    • Journal of Ocean Engineering and Technology
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    • v.12 no.1
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    • pp.76-84
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    • 1998
  • In this 1st report, the relationship between pure creep properties and initial strain was studied and also its acoustic emission test was performed during creep test at 500, 600 and $700^{\circ}C$. And the applicability of the acoustic emission technique was investigated to analyze the quantitive relationship between all the pure properties (creep strength, creep repture time or creep life, steady state creep rate, total creep rate, creep strain, total creep strain, etc.) and the initial strains as well as to analyze AE properties during the pure creep loading condition.

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Creep Characteristic of the Polyethylene(PE) at Various Stresses and Temperatures (온도와 응력에 따른 폴레에틸렌(PE)의 크리프특성)

  • Kang, Suk-Choon;Lee, Young-Won
    • Journal of the Korean Society for Precision Engineering
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    • v.26 no.7
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    • pp.99-104
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    • 2009
  • Creep characteristic is an important failure mechanism when evaluating engineering materials that are soft as polymers or used as mechanical elements at high temperatures. One of the popular thermo-elastic plastics, Polyethylene(PE) which is used broadly for engineering purposes, as it has good properties and merits compared to other plastics, was studied for creep characteristic at various level of stresses and temperatures. From the experimental results, the creep limit of PE at room temperature is 75% of tensile strength. Also the creep limits decreased exponentially as the temperatures increased, up to 50% of the melting point. Also the secondary stage among the three creep stages was nonexistent nor was there any rupture failure which occurred for many metals.

Creep Characteristic of the Polycarbonate(PC) at Various Stresses and Temperatures (응력과 온도에 따른 폴리카보네이트(PC)의 크리프특성)

  • Kang, Suk-Choon;Lee, Young-Won
    • Journal of the Korean Society for Precision Engineering
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    • v.27 no.9
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    • pp.78-85
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    • 2010
  • Creep characteristic is an important failure mechanism when evaluating engineering materials that are soft material as polymers or used as mechanical elements at high temperatures. One of the popular thermo-elastic polymers, Polycarbonate(PC) which is used broadly for engineering polymer, as it has excellent mechanical and thermal properties compared to other polymers, was studied for creep characteristic at various level of stresses and temperatures. From the experimental results, the creep limit of PC at room temperature is 85 % of tensile strength. which is higher than PE (75%)at room temperature. Also the creep limits decreased exponentially as the temperatures increased, up to 50 % of the melting point($267^{\circ}C$). Also the first and third stage among the three creep stages was non-existent nor was there any rupture failure which occurred for many metals.

Creep Characteristic of the Polymethyl Methacrylate(PMMA) at Stresses and Temperatures (응력과 온도에 따른 아크릴(PMMA)의 크리프특성)

  • Kang, Suk-Choon
    • Journal of the Korean Society for Precision Engineering
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    • v.28 no.12
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    • pp.1403-1410
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    • 2011
  • Creep characteristic is an important failure mechanism when evaluating engineering materials that are soft material as polymers or used as mechanical elements at high temperatures. One of the popular thermo-elastic polymers, Polymethyl methacrylate(PMMA) which is used broadly for engineering polymer, as it has excellent mechanical and thermal properties compared to other polymers, was studied for creep characteristic at various level of stresses and temperatures. From the experimental results, the creep limit of PMMA at room temperature is 85 % of tensile strength. which is higher than that of PE (75%)at room temperature. Also the creep limits decreased to nil linearly as the temperatures increased, up to $120^{\circ}C$ of the melting point($267^{\circ}C$). Also the first and third stage among the three creep stages were non-existent nor were there any rupture failure which occurred for many metals at high temperatures.