• 열처리공학회지
• /
• 제9권1호
• /
• pp.69-77
• /
• 1996

The fatigue crack initiation behavior of plasma ion nitrided SACM645 steel was investigated through the rotary bending fatigue test and residual stress measurement by XRD. It was shown by XRD and EPMA that the plasma ion nitrided surface was composed of ${\gamma}^{\prime}(Fe_4N)$phase and ${\varepsilon}(Fe_{2-3}N)$phase, and that the nitrogen atoms existed in Fe matrix in diffusion layer. The OM, SEM and Auger spectroscopy showed that the depth of compound layer, mixed compound and diffusion layer, and diffusion layer was $8{\mu}m$, $30{\mu}m$ and $300{\mu}m$, respectively. However, the microhardness test showed that the depth of hardened layer was $500{\mu}m$. The tensile strength of the ion nitrided SACM645 was lower than that of the unnitrided SACM645, and the ion nitrided specimen was fractured without plastic deformation. The nitrided SACM645 showed much poorer low cycle fatigue properties than the unnitrided one. In rotary bending fatigue, the fatigue strength of the ion nitrided SACM645 was higher than that of the unnitrided specimen, and the fatigue crack initiation sites changed by applied fatigue stress levels. The XRD result showed that the ion nitrided SACM645 has the compressive residual stress from surface to $600{\mu}m$ deep and the tensile residual stress from $600{\mu}m$ to deeper site. It is thought that crack initiation takes place at the point where the total stress of residual stress and applied stress is maximum.

• 비파괴검사학회지
• /
• 제28권4호
• /
• pp.323-330
• /
• 2008

소구경 배관 소켓 용접부의 고주기 피로특성윽 평가하고 피로 균열의 발생을 음향방출법을 이용하여 실시간 모니터링 하였다. 스테인리스 316L강 시험편은 가스텅스텐아크용접 공정으로 루트부에 결함이 없는 시험편과 용입불량 결함이 있는 시험편으로 준비하였다. 피로파단은 고응력 일때는 토우부, 상대적으로 저응력일 때는 루트부에서 일어났다. 피로시험동안 음향방출 카운트가 급격히 증가하는 시점을 균열의 발생 싸이클 ($N_i$)로 정의하였고 방사선투과법과 전자현미경을 이용하여 피로균열 생성 싸이클 전과 후에서 균열을 확인하였다. 소켓용접배관의 굽힘피로 손상 진단 및 감시를 위해 균열의 존재와 파괴모드 그리고 균열의 발생 싸이클에 관한 연구를 수행하였다.

• 대한기계학회논문집
• /
• 제8권4호
• /
• pp.305-312
• /
• 1984

본 연구에서는 STS 316강의 고온 저사이클 피로강도와 파괴거동을 고찰하고자 고온 대기중에서 변형율 제어에 의한 인장.압축 저사이클 피로시험을 실시하였다. 전 변형율축, 탄성 변형율축 및 소성 변형율축과 피로수명과의 관계를 일정 변형율 속 도하에서 응력축, 온도 및 주파수의 영향과 파괴거동을 고찰하였다.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2004년도 춘계학술대회 논문요약집
• /
• pp.72-72
• /
• 2004

대부분의 금속 재료는 제조 공정 중에 인장, 압축, 압연, 압출, 인발 등 소성 변형을 수반하는 가공의 단계를 거치게 된다. 가공 단계에서 가해준 변형률 및 이에 따라 형성된 전위구조 등은 생산재의 기계적 성질에 많은 영향을 미친다. 그리고 소성 변형이 수반되는 또 하나의 과정은 피로, 크리프 손상 등의 소성 변형을 수반하게 되는 기계적 손상이다 이러한 기계적 손상에 의해서도 전위가 도입되며, 전위의 집적부위에서 균열이 생성되기도 한다. 따라서 기계적 손상을 비파괴적으로 평가하는데 있어서도 소성 변형의 영향을 파악하는 것이 하나의 중요한 문제가 된다.(중략)

• Journal of Mechanical Science and Technology
• /
• 제16권7호
• /
• pp.919-926
• /
• 2002

In this study, the numerical prediction of the thermal fatigue lie? of a $\mu$BGA (Micro Ball Grid Array) solder joint was focused. Numerical method was performed using the three-dimensional finite element analysis for various solder alloys such as Sn-37%Pb, Sn-3.5%Ag, Sn-3.5%Ag-0.7%Cu and Sn-3.5%Ag-3%In-0.5%Bi during a given thermal cycling. Strain values obtained by the result of mechanical fatigue tests for solder alloys, were used to predict the solder joint fatigue life using the Coffin-Manson equation. The numerical results showed that Sn-3.5%Ag with the 50-degree ball shape geometry had the longest thermal fatigue life in low cycle fatigue. A practical correlation for the prediction of the thermal fatigue life was also suggested by using the dimensionless variable γ. Additionally Sn-3.5Ag-0.75Cu and Sn-2.0Ag-0.5Cu-2.0Bi were applied to 6$\times$8$\mu$BGA obtained from the 63Sn-37Pb Solder. This 6$\times$8$\mu$BGA were tested at different aging conditions at 130$\^{C}$, 150$\^{C}$, 170$\^{C}$ for 300, 600 and 900 hours. Thickness of the intermetallic compound layer was measured thor each condition and the activation energy thor their growth was computed. The fracture surfaces were analyzed using SEM (Scanning Electron Microscope) with EDS ( Energy Dispersive Spectroscopy).

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2009년도 제33회 추계학술대회논문집
• /
• pp.382-386
• /
• 2009

극심한 작동환경에 노출되는 부품은 일반적으로 수명이 줄어들게 된다. 액체로켓의 터보펌프는 높은 회전속도로 인한 높은 원심력과 높은 온도와 같은 환경에서 작동한다. 이와 같은 환경에서 작동하는 터보펌프는 극심한 피로와 크리프의 영향으로 재료의 내구성이 떨어지게 된다. 75톤급 터보펌프 터빈의 내구성을 확보하기 위하여 피로와 크리프의 영향을 고려한 손상률을 계산하였다. 터보펌프 피로해석에는 ABAQUS/CAE와 MSC.Fatigue를 사용하여 해석을 수행하였으며, 크리프 해석을 수행하기 위해서 Larson-Miller parameter 곡선과 로빈슨 법칙을 사용하였다. 본 연구에서는 터보펌프의 터빈에 대한 내구성을 확보하기 위하여 피로의 영향과 크리프의 영향을 비교, 분석하였다.

• Structural Engineering and Mechanics
• /
• 제30권6호
• /
• pp.665-678
• /
• 2008

The beams components subjected to the loading such as axial, bending and cyclic thermal loads were studied in this research. The used constitutive equations are those of elasto-plasticity coupled to ductile and/or creep damage. The nonlinear kinematic hardening behavior was considered in elastoplasticity modeling. The unified damage law proposed for ductile failure and fatigue by the author of Sermage et al. (2000) and Kachanov's creep damage model applied to cyclic creep and low cycle fatigue of beams. Based on the results of the analysis, the shakedown limit loads were determined through the calculation of the residual strains developed in the beam analysis. The iterative technique determines the shakedown limit load in an iterative manner by performing a series of full coupled elastic-plastic and continuum damage cyclic loading modeling. The maximum load carrying capacity of the beam can withstand, were determined and imposed on the Bree's interaction diagram. Comparison between the shakedown diagrams generated by or without creep and/or ductile damage for the loading patterns was presented.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2004년도 추계학술대회
• /
• pp.148-153
• /
• 2004

This paper represents that parts of a large generator operating in 1000 MW are affected by centrifugal forces due to high-speed rotation in 3600 rpm and 3D FEM Analyses are required to obtained the structural reliability of the generator. From these results, one would know the weakest locations and the stress distributions. The fatigue life is calculated in order to grasp the remaining life of generator. 2D and 3D analyses are performed to calculate stresses of the generator rotor and the retaining ring. From 2D results, we find the SCF at the slot and sub-slot of the rotor. 3D analysis is applied at the end part of generator rotor, which represents complex geometry, and rotor and retaining ring shrink thermally. With these results, designers of rotor and retaining ring can compare with the results of design code and verify the stress distributions of generator rotor and retaining ring, and then calculate the remaining life from the low-cycle fatigue data.

• 수산해양기술연구
• /
• 제26권4호
• /
• pp.380-386
• /
• 1990

The high stress, low cycle fatigue test were carried out on HT80 plates with artificial part-through notch. The LBB conditions by the net section stress approach was examined in detail. Finite element methods for the state of deformation were also applied and the results were compared with the results from experiments. From the test results, it was noted that the LBB condition in fatigue test was dependent upon the maximun load change before and after the crack penetration. The LBB criterion By the net section stress approach were slightly dependent on initial crack size. It was shown that the state of deformation can be used to predict whether the component is likely to show LBB condition or they will be broken rapidly.

• 한국정밀공학회지
• /
• 제25권7호
• /
• pp.131-138
• /
• 2008

The microstructural effects on the ultrasonic nonlinearity were investigated in isothermally degraded ferritic 2.25Cr-1Mo steel and low cycle fatigued copper. The variation in ultrasonic nonlinearity (${\beta}/{\beta}_0$) was interpreted as resulting from microstructural changes supported by the electron microscopy and X-ray diffraction, in addition to the mechanical test (Victor's hardness and ductile-brittle transition temperature). The ultrasonic nonlinearity of 2.25Cr-1Mo steel increased abruptly in the initial 1,000 h of degradation, and then changed little due to the coarsening of carbide and precipitation of stable $M_6C$ carbide during isothermal degradation. The ultrasonic nonlinearity of copper increased with the fatigue cycles due to the evolution of dislocation cell substructure.