• 대한기계학회논문집A
• /
• 제37권11호
• /
• pp.1339-1347
• /
• 2013

기존 단축 크리프시험에서는 천이 크리프의 영향을 무시하고 정상상태 크리프만을 고려하기 때문에 실제 크리프 특성을 나타내지 못한다. 이에 본 연구에서는 천이크리프를 고려한 압입 크리프 물성평가법을 제시한다. 다양한 재료에 대해 구형압입시험 전산모사를 이용해 크리프 물성변화에 따른 거동을 살펴보고, 크리프 특성을 무차원 변수들의 회귀식으로 표현한다. 이를 토대로 천이크리프를 고려한 압입 크리프 물성평가 프로그램을 생성했다. 제시한 물성평가 프로그램을 통해 압입 하중-변위 곡선으로부터 크리프지수, 계수값들을 각각 1.1%, 2.3% 오차범위에서 예측할 수 있다.

• 한국항공우주학회지
• /
• 제30권8호
• /
• pp.103-111
• /
• 2002

열하중과 원심력을 고려한 발전용 터빈 블레이드의 정상 상태 크리프 해석을 수행하였다. 3차원 터빈 블레이드 유한 요소 모델에 대하여 크리프 변형률과 응력을 계산하고 수치적 방법에 의해 크리프 수명을 예측하였다. 약 200시간 정도의 크리프 해석 결과 GTD111 터빈 블레이드는 아직 파손 응력에 도달하지 않았으며, 크리프 응력은 시간이 경과함에 따라 점차 이완되고 있다. 터빈 블레이드의 최대 크리프 변형률은 익형의 압력면 끝단에서 발생하며 수치적 방법에 의해 약 50,000 시간 이후에 파손 변형률에 도달할 것이다. 따라서 현재 터빈의 기동 중 블레이드는 크리프에 의한 손상을 입지 않는다.

• 한국금형공학회:학술대회논문집
• /
• 한국금형공학회 2008년도 하계 학술대회
• /
• pp.39-44
• /
• 2008

Magnesium alloys have given high attention to the industry of light-weigh as automobile and electronics with aluminium, titanium and composite alloys due to their high strength, low specific density and good damping characteristics. But the magnesium contained structures under high temperature have the problems related to creep deformation and rupture life, which is a reason of developing the new material against creep deformation to use them safely. The purpose of this study is to predict the creep deformation mechanism and rupture time of AZ31 magnesium alloy. For this, creep tests of AZ31 magnesium alloy were done under constant creep load and temperature with the equipment including automatic temperature controller with acquisition computer. The apparent activation energy Qc and the applied stress exponent n, rupture life have been determined during creep of AZ31 Mg alloy over the temperature range of $150^{\circ}C$ to $300^{\circ}C$. In order to investigate the creep behavior. Constant load creep tests were carried out in the equipment including automatic temperature controller, whose data are sent to computer. At around the temperature of $150^{\circ}C{\sim}300^{\circ}C$ the creep behavior obeyed a simple power-law relating steady state creep rate to applied stress and the activation energy for the creep deformation was nearly equal and a little low, respectively, to that of the self diffusion of Mg alloy.

• 대한용접접합학회:학술대회논문집
• /
• 대한용접접합학회 2006년 추계학술발표대회 개요집
• /
• pp.184-186
• /
• 2006

Sn-3Ag-0.5Cu is one of candidate as an alternative approach to conventional lead-tin solder. In order to evaluate that creep characteristic of QFP, we used Sn-3Ag-0.5Cu where the operating temperature is $100^{\circ}C$. The specimens were loaded to failure at average pull strength in the range of 20% to 25%, X-ray machine is used to eliminate effect of void. In this paper, relation of time-displacement and steady state creep rate was studied, and used to analyze the experimental result.

• 열처리공학회지
• /
• 제18권3호
• /
• pp.183-189
• /
• 2005

The effects of duplex-treatment of plasma carburization and CrN coating onto Ti-6Al-4V alloy on its creep properties were investigated by means of a constant stress creep tester. Applying duplex-treatment, specimens having an inner carburized layer of about $150{\mu}m$ in depth and outer CrN layer of about $7.5{\mu}m$ in thickness were prepared. The hardness of duplex-treatment surface was about 1,960 VHN. It also appeared that the duplex-treatment improved the roughness of the surface significantly; $Ra=0.045{\mu}m$ for treated alloy while $Ra=0.321{\mu}m$ for untreated alloy. The steady-state creep behaviors were investigated in a temperature range of $510{\sim}550^{\circ}C$ ($0.42{\sim}0.44T_m$) under an applied stress range of 200~275 MPa. The stress exponent, n, was derived assuming the power law creep behavior. The surface treatment showed a decrease in a value from 9.32 (untreated) to 8.79 (treated). Also the activation energy obtained from an Arrhenius plot increased from 238 to 257 kJ/mol.

• 열처리공학회지
• /
• 제10권3호
• /
• pp.198-208
• /
• 1997

The-steady-state creep mechanism and behavior of Zircaloy-4 used as cladding materials in PWR have been investigated in air environment over the temp, ranges from 600 to $645^{\circ}C$ and stress ranges from 4 to $7kg/mm^2$. The stress exponents for the creep deformation of this alloy, n were decreased 4.81, 4.71, 4.64, and 4.56 at 600, 615, 630 and $645^{\circ}C$, respectively; the stress exponents decreased with increasing the temperature and got closer to about 5. The apparent activation energies, Q, were 62.1, 60.0, 57.9 and 55.4 kcal/mole at stresses of 4, 5, 6, $7kg/mm^2$, respectively; the activation energies decreased with increasing the stress and were close to those of volume self diffusion of Zr in Zr-Sn-Fe-Cr system. In results, it can be considered that the creep deformation for Zircaloy-4 was controlled by the dislocation climb over the ranges of this experimental conditions. Larson-Miller parameter, P, for the crept specimens was obtained as P=(T+460)(logt,+23). The failure plane observed by SEM slightly showed up intergranular fracture at this experiment ranges. However, it was essentially dominated by the dimple phenomenon, which was a characteristics of the transgranular fracture.

• 대한기계학회논문집A
• /
• 제36권1호
• /
• pp.81-90
• /
• 2012

재료시험기법 중 하나인 압입시험은 크리프 특성 분석에 이용될 수 있다. 그러나 많은 기존 연구들이 정상상태의 크리프 특성만을 이용하고 있기 때문에, 단축시험과 압입시험 사이에는 상당한 차이가 발생한다. 따라서 정확한 크리프 평가를 위해서는 천이 크리프 특성을 고려하여야 한다. 본 연구에서는 Ogbonna 등(14)의 구형 압입자를 이용한 천이 크리프 해석을 확장, 자기 유사성을 갖는 원뿔형 압입자에 적용했다. 천이 크리프 특성을 유한요소해석을 통해 분석하여 정리하였으며, 구형 및 원뿔형 압입시험의 천이 특성을 비교했다. 또한 재료의 탄성변형률, 압입자 형상, 압입접촉면적, 대표 변형률 등 기존 평가법들에서 정량적으로 잘 고려되지 못하고 있는 부분들을 살펴보고 그 해결방안을 제시했다.

• 동력기계공학회지
• /
• 제9권4호
• /
• pp.96-101
• /
• 2005

Magnesium alloys have been widely used for many structural components of automobiles and aircraft because of high specific strength and good cast ability in spite of hexagonal closed-packed crystal structure of pure magnesium. In this study, uniaxial tension tests at high temperature and creep tests are done in order to investigate the characteristics of high temperature and mechanisms for creep deformation of AZ31 Mg alloy. Yield stress and ultimate tensile stress decreased with increasing temperature, but elongation increased from results of uniaxial tension test at high temperature. The apparent activation energy Qc, the applied stress exponent n and rupture life have been determined during creep of AZ31 Mg alloy over the temperature range of 473K to 573K and stress range of 23.42 MPa to 93.59 MPa, respectively, in order to investigate the creep behavior. Constant load creep tests were carried out in the equipment including automatic temperature controller, whose data are sent to computer. At around the temperature of $473K{\sim}493K$ and under the stress level of $62.43{\sim}93.59%MPa$, and again at around the temperature of $553K{\sim}573K$ and under the stress level of $23.42{\sim}39.00MPa$, the creep behavior obeyed a simple power-law relating steady state creep rate to applied stress and the activation energy for the creep deformation was nearly equal, respectively, and a little low to that of the self diffusion of Mg alloy including aluminum. Also rupture surfaces at high temperature have had bigger dimples than those at lower temperature by SEM.

• 한국재료학회지
• /
• 제18권6호
• /
• pp.326-333
• /
• 2008

Since the 1990s, the second generation of Zirconium alloys containing main alloy compositions of Nb, Sn and Fe have been used as a replacement of Zircaloy-4 (Zr-Sn-Fe-Cr), a first-generation Zirconium alloy, to meet severe and rigorous reactor operating conditions characterized by high-burn-up, high-power and high-pH operations. In this study, the mechanical properties and creep behaviors of Zr-Sn-Fe-Cr and Zr-Nb-Sn-Fe alloys were investigated in a temperature range of $450{\sim}500^{\circ}C$ and in a stress range of $80{\sim}150\;MPa$. The mechanical testing results indicate that the yield and tensile strengths of the Zr-Nb-Sn-Fe alloy are slightly higher compared to those of Zr-Sn-Fe-Cr. This can be explained by the second phase strengthening of the $\beta$-Nb precipitates. The creep test results indicate that the stress exponent for the steady-state creep rate decreases with the increase in the applied stress. However, the stress exponent of the Zr-Sn-Fe-Cr alloy is lower than that of the Zr-Nb-Sn-Fe alloy in a relatively high stress range, whereas the creep activation energy of the former is slightly higher than that of the latter. This can be explained by the dynamic deformation aging effect caused by the interaction of dislocations with Sn substitutional atoms. A higher Sn content leads to a lower stress exponent value and higher creep activation energy.

• 소성∙가공
• /
• 제17권5호
• /
• pp.364-372
• /
• 2008

In this study, the circumferential creep behaviors ofpilgered advanced Zirconium alloy tubes such as Zr-Nb-O and Zr-Nb-Sn-Fe were investigated in the temperature range of $400\sim500^{\circ}C$ and in the stress range of 80$\sim$150MPa. The test results indicate that the stress exponent for the steady-state creep rate of the Zr-Nb-Sn-Fe alloy decreases with the increase of stress(from 6$\sim$7 to 4), while that of the Zr-Nb-O alloy is nearly independent of stress(5$\sim$6). The activation energy of creep deformation is found to be nearly the same as the activation energy for Zr self diffusion. This indicates that the creep deformation may be controlled by dislocation climb mechanism in Zr-Nb-O. On the other hand, the transition of stress exponent(from 6-7 to 4) in Zr-Nb Sn-Fe strongly suggests the transition of the rate controlling mechanism at high stresses. The lower stress exponent at high stresses in Zr-Nb-Sn-Fe can be explained by the dynamic deformation aging effect caused by interaction of dislocations with Sn substitutional atoms.