• 한국해양공학회지
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• 제12권1호
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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.

• 한국해양공학회지
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• 제13권4호통권35호
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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.

• 한국정밀공학회지
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• 제26권7호
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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.

• 한국정밀공학회지
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• 제27권9호
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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.

• 한국정밀공학회지
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• 제28권12호
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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.

• 대한기계학회논문집A
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• 제35권2호
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• pp.157-162
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• 2011

발전설비 및 자동차의 엔진에서 고온과 응력이 발생하므로 안전을 위하여 제품을 생산하기 전에 재료의 수명설계가 필요하다. 본 연구에서는 온도, 응력, 파단 시간으로 이루어진 무기력계수를 이용하여 수명설계를 수식화하였다. 통합수명식을 이용하여 SP-Creep 시험 데이터와 계산된 데이터를 비교하였다. SP-Creep 시험은 X20CrMoV121강의 파단시간을 획득하기 위하여 수행하였고 수명설계식을 통해 하중, 온도, 하중-온도가 작용하는 3가지 경우를 고려하였다. 첫째로, 무기력계수는 SP-Creep 시험에서 획득한 파단응력과 시간에 의해 계산하였다. 두 번째로, 온도 조건을 주어 수명을 예상하였다. 세 번째로, 부재는 피로와 크리프가 동시에 작용할 때 커플링 효과 때문에 더 열악한 상태에 놓이게 된다. 수명은 커플링 효과 때문에 현저하게 감소하는 것으로 나타났다.

• 한국해양공학회지
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• 제12권2호통권28호
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• pp.65-70
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• 1998

In this report, the creep properties and creep life estimation by Larson-Miller Parameter(LMP) Method for 2.25Cr1Mo steel to be used as power plant tubes or other components were presented at the high temperatures of 500, 550, and $600^{\circ}C$. It was confirmed experimentally and quantitatively that a creep life estimation equation at such various high temperatures was well derived by LMP and could be used very effectively within the creep life of 10$^3$ hours, but very unreliable and even dangerous for design in a long term of creep life such as 10$^4$ or $10^5$ hours.

• 대한기계학회논문집A
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• 제37권3호
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• pp.405-412
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• 2013

본 논문은 크리프 파단 수명평가에 주요인자인 정상상태 크리프 응력을 직관 용접부에 대해 정량화한다. 모재와 용접부의 크리프 특성 불균일이 응력에 미치는 영향을 체계적으로 분석하기 위해, 다양한 용접부 불균일에 대해 이차원 유한요소 크리프 탄성해석을 수행하였다. 용접부는 열영향부를 고려하였으며 각각의 재료는 이상화된 탄성-멱 크리프 법칙을 따른다고 가정하였다. 하중에 따른 영향을 보기 위해 내압과 인장하중에 대해 연구를 수행하였다. 용접부 크리프 응력의 정량화를 위해 크리프 불균일 지수를 도입하였으며, 무차원화된 단면평균응력과 선형적인 관계를 확인하였다. 불균일 지수로 정량화한 응력과 Type IV 영역을 모사한 용접부의 유한요소해석 결과 및 영국전력의 R5 문헌값의 비교를 통해 연구결과의 유효성을 검증하였다.

• 한국해양공학회지
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• 제12권2호통권28호
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• pp.71-78
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• 1998

In this report for the assessment of creep properties of high-temperature tube materials in power plants, the long-time($10^4$~105h) creep life prediction by ISM for 2.25Cr1Mo steel was studied. It was clarified experimentally and quantitatively that the newly developed long-time creep life prediction equation was very coincident with the actual experimental data with high confidence, and the model was $t_r=\alpha\varepsilon_0^{\beta}\sigma^{-1}$.

• 동력기계공학회지
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• 제5권2호
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• pp.57-62
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• 2001

Gas turbine performance is highly dependent on the engine performance which is closely related to the engine materials since they are exposed to severe working environments, i.e, high temperature and high stresses. For this reason, advanced materials with improved properties are required for the engine. The purpose of this research is to develop key materials technologies for aircraft industry and to tester domestic production of related parts. In this paper, the real-time prediction of high temperature creep strength and creep life for nickel-based superalloy Udimet 720(high-temperature and high-pressure the gas turbine engine materials) was performed on round-bar type specimens under pure load at the temperatures of 538, 649 and $704^{\circ}C$.