In order to investigate the optimum condition of the autofrettage process for the diesel engine fuel injection pipe, different values of autofrettage pressure, pressure rising time, pressure holding time, and repetition of autofrettage process were applied. Autofrettage was performed by applying the hydrostatic internal pressures of 604MPa, 535MPa, 500MPa on the fuel injection pipe, corresponding to theoretical 50%, 30%, and 20% overstrain levels, respectively. The autofrettage residual stresses in the injection pipe were experimentally determined by using X-ray diffractometer. As the overstrain level increased, the magnitude of compressive residual stress at the bore increased. It was found that the rising time to reach the autofrettage pressure, holding time at the autofrettage pressure, and repeated application of the autofrettage pressure on the pipe had no significant influence on the residual stress distributions.

This paper reports the results of an experimental examination using X-rays to test annealing materials for lapped bearing steel (STB2), to confirm the validity of the weighted averaging analysis method. The distribution behavior for the sin diagram and the presence or absence of differences in the peak method, half-value breadth method, and centroid method were investigated. When lapping the annealed bearing steel (STB2) material, a residual stress state with a non-directional steep gradient appeared in the surface layer, and it was found that the weighted averaging analysis method was effective. If there is a steep stress gradient, the sin diagram is curved and the diffraction intensity distribution curve becomes asymmetric, resulting in a difference between the peak method, half-value breadth method, and centroid method. This phenomenon was evident when the stress gradient was more than 2~3 kg/mm2/μm. In this case, if the position of the diffraction line is determined using the centroid method and the weighted averaging analysis method is applied, the stress value on the surface and the stress gradient under the surface can be obtained more accurately. When the stress gradient becomes a problem, since the curvature of the sin diagram appears clearly in the region of sin > 0.5, it is necessary to increase the inclination angle  as much as possible. In the case of a lapping layer, a more accurate value can be obtained by considering  in the weighted averaging analysis method. In an isotropic biaxial residual stress state, the presence or absence of  can be determined as the presence or absence of strain for sin≈0.4.

Aluminum nitride having a dense hexagonal structure is used as a high-temperature material because of its excellent heat resistance and high mechanical strength; its excellent piezoelectric properties are also attracting attention. The structure and residual stress of AlN thin films formed on glass substrate using TFT sputtering system are examined by XRD. The deposition conditions are nitrogen gas pressures of 1 × 102, 6 × 103, and 3 × 103, substrate temperature of 523 K, and sputtering time of 120 min. The structure of the AlN thin film is columnar, having a c-axis, i.e., a <00·1> orientation, which is the normal direction of the glass substrate. An X-ray stress measurement method for crystalline thin films with orientation properties such as columnar structure is proposed and applied to the residual stress measurement of AlN thin films with orientation <00·1>. Strength of diffraction lines other than 00·2 diffraction is very weak. As a result of stress measurement using AlN powder sample as a comparative standard sample, tensile residual stress is obtained when the nitrogen gas pressure is low, but the gas pressure increases as the residual stress is shifts toward compression. At low gas pressure, the unit cell expands due to the incorporation of excess nitrogen atoms.

Application of a very high internal pressure on the thick-walled pressure vessel induces beneficial compressive tangential residual stresses near the bore of the pressure vessel after unloading the internal pressure. However, a reverse yielding due to the Bauschinger effect during the unloading process causes the reduction of the compressive residual stress near the bore. In order to evaluate the autofrettage residual stress distributions of the thick-walled pressure vessel, the Bauschinger effects were considered. Magnitudes of the compressive residual stresses at the bore determined by considering the Bauschinger effects decreased by about 25 percent, compared to the case of linear elastic unloading, i.e., without Bauschinger effects. Measured residual stress distributions agreed fairly well with the calculated distributions considering the Bauschinger effects.

To improve life time of machine components, higher alloy grade materials are used by adding more metal alloy components and content. Also production processes are further complicated and subdivided such as the forging, preliminary heat treatment, quality heat treatment, rough machining and finished machining process. Those reasons become major cause of large stress in the materials, and the residual stress generated during the manufacturing process causes fatal defects, such as crack, surface tear, warping and deformation of the products. It is necessary to evaluate the residual stress on the entire processes, from forging process to final finished machining process. Also in order to avoid those problems caused by residual stresses, it is necessary to know in advance what process is important to be controlled and what parameters affect residual stress. By the hole drilling method, residual stress was measured in each manufacturing process step. In this study, the hardness of the surface, the cutting force test and the metal analysis were performed to clarify the influence of manufacturing process parameters.

The residual stress analysis and fatigue test of a steel plate with a hole were performed in order to investigate the effects of the cold expansion on the fatigue life of the plate. The cold expansion method is a metal forming process by expanding a hole in order to induce compressive tangential residual stresses near the hole. In this research, a S45C steel plate of 3.2 mm thickness with a hole of 4.318 mm diameter was cold expanded by using a mandrel, resulting in a degree of expansion 1.47%. A significant amount of compressive tangential residual stress of 502 MPa at the hole surface was calculated using the finite element analysis and the compressive residual stress was more widely spreaded in the entry and exit planes than the mid plane in the plate thickness. The compressive tangential residual stresses showed a very beneficial influence on the fatigue life of the plate by increasing 1.2 to 2 times longer lives compared to the plate without cold expansion, depending on the applied load levels. Fatigue crack initiated and propagated at the hole surface of the mandrel entrance region, where relatively lower magnitude of compressive residual stress was found than the other region.

복합재료 사이에 주파수 선택적 투과막(Frequency Selective Surface)을 삽입하여 동시경화 공정을 이용하여 주파수 선택적 투과 기능을 가지는 하이브리드 복합재료를 성형하면 재료들 간의 열팽창 계수와 강성의 차이로 인해 구조 내에 잔류 열응력이 발생하게 되고, 이로 인하여 스프링 백 현상이 발생한다. 따라서 복합재의 적층에 따른 영향을 알아보기 위해 복합재료의 적층각을 선택적 투과막(Frequency Selective Surface)을 중심으로 대칭과 비대칭 적층으로 적용하여 하이브리드 구조의 잔류 열응력을 예측하고, 이에 대한 스프링 백에 대해서 연구하였다.

본 논문에서는 주파수 선택적 투과막(FSS)이 결합된 복합재료 구조에서 구성 재료 간의 열팽창계수 차이로 잔류응력이 발생하므로 이로 인한 층간분리나 FSS의 손상 등 구조적인 파손 가능성과 잔류응력으로 인하여 변형된 FSS가 전파투과특성에 미치는 영향에 대하여 연구하였다. FSS는 단위요소의 종류, 설계변수, 배열에 따라 전파특성이 다르게 나타나므로, PSO 알고리즘을 이용하여 다이폴이 목표주파수에서 투과특성을 갖도록 설계하고 그 설계치수를 다른 N-pole 종류 단위요소(Tripole, Cross dipole, Jerusalem cross)에 적용하여, 복합재료 구조에 발생하는 잔류응력과 그로인한 구조적 손상과 전파특성을 영향성을 관찰하고 FSS패턴과 복합재료의 적층 변화에 따라 비교하였다.

In this study, the effects of cryogenic treatment cycles on the residual stress and mechanical properties of 7075 aluminum alloy (Al7075) samples, in the form of a tube-shaped product with a diameter of 500 nm, were investigated. Samples were first subjected to solution treatment at 470˚C, followed by cryogenic treatment and aging treatment. The residual stress and mechanical properties of the samples were systematically characterized. Residual stress was measured with a cutting method using strain gauges attached on the surface of the samples; in addition, tensile strength and Vickers hardness tests were performed. The detailed microstructure of the samples was investigated by transmission electron microscopy. Results showed that samples with 85 % relief in residual stress and 8% increase in tensile strength were achieved after undergoing three cycles of cryogenic treatments; this is in contrast to the samples processed by conventional solution treatment and natural aging (T4). The major reasons for the smaller residual stress and relatively high tensile strength for the samples fabricated by cryogenic treatment are the formation of very small-sized precipitates and the relaxation of residual stress during the low temperature process in uphill quenching. In addition, samples subjected to three cycles of cryogenic treatment demonstrated much lower residual stress than, and similar tensile strength compared to, those samples subjected to one cycle of cryogenic treatment or artificial aging treatment.

Gas welding is a very important and useful technology in the fabrication of railroad cars and commercial vehicle structures. However, since the fatigue strength of gas-welded joints is considerably lower than that of the parent material due to stress concentration at the weld, the fatigue-strength assessment of gas-welded joints is very important for the reliability and durability of railroad cars and the establishment of a criterion for long-life fatigue design. In this paper, in order to save time and cost for the fatigue design, an accelerated life-prediction method that is based on the theory of statistical reliability was investigated. Its usefulness was verified by comparing the (Δσa)R-Nf relationship that was obtained from actual fatigue test results with the (Δσa)R-(Nf)ALP relationship that was derived from accelerated life testing. And the reliability of the predicted life was evaluated. The reliability of the accelerated life-prediction on the base of actual test data was analyzed to be (81～86)% of the actual test life of the fillet-type gas welded joint.

Crack-free joining of Si3N4 and Al2O3 using 15 layers has been achieved by a unique approach introducing Sialon polytypoids as a functionally graded materials (FGMs) bonding layer. In the past, hot press sintering of multilayered FGMs with 20 layers of thickness 500μm each has been fabricated successfully. In this study, the number of layers for FGM was reduced to 15 layers from 20 layers for optimization. For fabrication, model was hot pressed at 38 MPa while heating up to 1700˚, and it was cooled at 2˚/min to minimize residual stress during sintering. Initially, FGM with 15 layers had cracks near 90 wt.% 12H / 10 wt.% Al2O3 and 90 wt.% 12H/10 wt.% Si3N4 layers. To solve this problem, FEM (finite element method) program based on the maximum tensile stress theory was applied to design optimized FGM layers of crack free joint. The sample is 3-dimensional cylindrical shape where this has been transformed to 2-dimensional axisymmetric mode. Based on the simulation, crack-free FGM sample was obtained by designing axial, hoop and radial stresses less than tensile strength values across all the layers of FGM. Therefore, we were able to predict and prevent the damage by calculating its thermal stress using its elastic modulus and coefficient of thermal expansion. Such analyses are especially useful for FGM samples where the residual stresses are very difficult to measure experimentally.

경사기능 재료는 위치에 따른 특성 변화를 갖고 있어 변화하는 주변 환경에서 사용되는 재료의 응용성을 높일 수 있는 장점이 있다. 적합한 경사기능 재료의 제조를 위해서는 탄성률, 강도, 인성 등의 위치에 따른 변화를 예측하는 것이 필요하다. 그러나 재료 내에서의 탄성률 변화 등으로 인해 경사기능 재료에서 인성을 정량적으로 표현하는데는 어려움이 있으므로 이를 정량적으로 측정하고, R-curve를 결정하는 것은 재료의 응용성에 중요한 인자가 된다. 본 연구에

Plastic deformation was observed by TEM around the intragranular SiC particles in the matrix for nanocomposite system. The dislocations are generated at selected planes and there is a tendency for the dislocations to form a subgrain boundary structure with low-angel grain boundaries and networks. In this study, dislocation generated in the matrix during cooling down from sintering temperatures by the highly localized thermal stresses within and/or around SiC particles caused from the thermal expansion mismatch between matrix and SiC particle was observed. In monolithic and microcomposite system. These phenomena is closely related to the plastic relaxation of the elastic stress and strain energy associated with both thermal misfitting inclusions and creep behaviors. The plastic relaxation behavior was explained by combination of yield stress and internal stress.

최근에 상용차용 디젤 엔진의 성능 향상을 목적으로 엔진 설계가 급격히 변화되면서 캠 팔로우어(cam follower)와 캠(cam) 사이에 작용하는 접동면 하중의 증가로 접동면에서의 마모가 중요한 문제가 되고 있다. 본 연구에서는 기존의 주절체 및 소결합금 캠 팔로우어에 비해 내마모성이 우수한 세라믹 캠 팔로우어를 개발하였다. 잔류 응력을 완화시켜주는 중간층을 사용하지 않고 질화규소(Si3N4) 팁과 중탄소강을 활성납재를 사용하여 직접 접합후 냉각시키는 과정에서 두 모재의 열팽창계수차에 의한 크라우닝(crowning, R) 이 형성되도록 하였다. 접합에 사용한 중탄소강은 열팽창시 이력(hysteresis) 거동을 나타내었으며, Ac1 변태점인 723˚C 이하에서 접합할 경우 원하는 크라우닝이 형성되었다. 접합온도가 723˚C 이상이 되면 크라우닝 (R) 값이 온도에 따라 지수함수적으로 증가하였으며 이는 중탄소강의 상변태에 의한 열팽창.수축의 이력 특성으로 설명되어질 수 있었다. 규격에 맞는 크라우닝이 형성되는 최적 접합 온도는 700~720˚C의 범위였다. 질화규소와 중탄소강의 직접 접합방법으로 접합과 동시에 크라우닝을 형성시키고 제어함으로써 난가공재인 세라믹을 곡면 가공하지 않고도 적당한 곡률을 갖는 저가의 세라믹 캠 팔로우어를 제조할 수 있었다.

최 등1)은 total lagrangian formulation에 근거한 증분 평형방정식을 적용하고, 강도행렬 산정시 회전각의 2차항을 포함시켜 기하학적 비선형 해석시 해의 수렴성을 향상시켰다. 또한 등매개 쉘 유한요소의 단점인 전단구속 현상과 제로 에너지 모드가 발생하는 문제를 극복하기 위하여 가정 변형률장을 적용하여 보강된 판 및 쉘 구조의 비선형 해석법을 개발하였다. 본 연구에서는 잔류응력을 고려한 쉘구조의 극한강도 해석을 수행하기 위하여, 대변형거동과 함께 소성붕괴거동을 추적할 수 있는 알고리즘을 제시한다. 잔류응력을 고려한 증분평형방정식에 return mapping algorithm을 이용한 탄소성 해석법을 결합시켜서 보강된 판 및 쉘구조의 극한거동을 파악한다. 수치해석 예제를 통하여 본 연구에서 제시된 유한요소 및 비선형 해석 알고리즘에 대한 효율성 및 적용성을 확인하였다.

이 논문에서는, 반도체 칩과 리드프레임을 결합하는 과정에서 점탄성 접착제층에 발생하는 잔류응력 문제를 다루고 있다. 접착제층은 열유동단순거동을 한다고 가정하였다. 접착제층에서의 응력들은 경계요소법을 사용하여 조사하였다. 매우 큰 응력 구배가 계면 모서리에서 발생하는데, 그러한 응력들은 국부 항복을 일으키거나, 칩과 리드프레임의 박리를 야기시킬 수 있음을 보여주고 있다.

활성금속브레이징법으로 계면접합된 AlN/Cu 접합체의 잔류응력 완화에 미치는 Mo 중간재의 영향을 조사하였다. 유한요소법에 의한 응력 해석과 접합체 강도 측정, 파단면의 관찰을 행하였으며, 이들 결과를 비교, 분석하였다. 응력 해석 결과로부터, Mo 중간재를 사용할 경우 최대 잔류 주응력이 형성되는 위치가 AlN/삽입금속 계면으로부터 삽임금속/Mo 계면을 통하여 Mo 내부로 이동됨을 확인하였다.접합체의 자유표면에 형성되는 인장성분의 응력집중 위치는 Mo 중간재 두께가 증가됨에 따라 Cu/Mo 계면과 Mo/AlN 계면의 두 곳으로 분리되었으며, AlN측 잔류응력의 크기는 크게 감소하였다. 중간재를 사용하지 않은 경우 최대 접합강도가 52 MPa로 낮은 강도를 보였으나, 두께 400μm 이상의 Mo 중간재를 사용한 접합체의 경우, 200 MPa 이상, 최대 275 MPa의 접합강도를 얻을 수 있었다.