• Journal of Advanced Marine Engineering and Technology
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• 제35권8호
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• pp.1048-1054
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• 2011

레이저 표면경화처리는 고밀도 에너지 열원에 의해 레이저 조사부위만 급속 가열한 후 표면의 열이 내부로 전도되어 급속히 자기냉각 됨으로써 표면을 경화시키는 방법이다. 이 표면처리 방법은 열처리에 의한 열변형이 거의 없고, 표면경화처리 이후 다른 공정을 수반하지 않는다. 또한 국부적인 가공이 가능하기 때문에 복잡한 형상을 가지는 금형에는 적합한 표면처리 방법이다. 본 연구에서는 열처리에 적합한 빔 프로파일을 가진 고출력 다이오드 레이저를 이용하여 금형재료용 주철의 표면처리를 실시하였다. 프레스 금형 공정에 따른 금형의 형상이 다르기 때문에 적용부위에 따라 시험편을 평면과 모서리부로 나누어 열처리를 실시하였다. 이때 모서리부의 열처리는 광학헤드를 $10^{\circ}$ 기울인 상태에서 진행하였다. 그 결과, 모서리부의 열처리는 평면부와 비교하여 형상에 따른 열전달 루트가 제한되므로, 입열이 집중되기 쉬워 평면 열처리보다 빠른 이송속도에서 경화가 이루어졌다.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2003년도 추계학술대회논문집
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• pp.229-232
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• 2003

In the roll forming process, a sheet or strip of metal is continuously and progressively formed into a desired cross-sectional profile by feeding it through a series of forming roll. Accordingly, it is important to maintain the material properties of the initial sheet and deform uniformly during the roll forming. The roll forming process was estimated in consideration of some factors such as material properties, strip thickness, roll diameter, roll velocity, and the deformation of the material that influence the forming length. The hydroforming technology has been recognized as a new technique in manufacturing industry, especially in automotive industry. The formed pipe in used in hydroforming process is manufactured by the roll forming. The formability during hydroforming is very sensitive to the state of pipes which are made by roll forming. Particularly the amount of hardening during roll forming affects the formability. Therefore, it is necessary to design the optimum roll flower to reduce the local hardening. In this paper, optimum roll flower which has uniform strain distribution through sheet width was obtained by comparing strain distribution in various roll flower. Finite element analysis(FEA) is performed to estimate the strain distribution related to hardening by roll forming. A numerical analysis is carried out by SHAPE-RF.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.256-261
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• 2000

In this study, we derived work-hardening exponent using continuous indentation test technique. Continuous indentation test technique is a powerful method to evaluate mechanical properties, such as hardness, modulus, ${\sigma}-{\varepsilon}$ curves and etc. It has many merits conventional indentation test has. The relationship between true stress and mean contact pressure and between strain and indentation depth were derived. While the indenter pushes the materials, the region around the indenter is deflected elastically. It is called elastic deflection. And pile-up phenomenon related to plastic deformation around the indenter increased the contact depth, and sink-in phenomenon decreases. So we calibrated contact depth change by considering elastic deflection and pile-up/sink-in. Using calibrated contact depth we redefined the relationship between true stress and mean contact pressure and between strain and contact depth. Through these relationship we could derive work-hardening exponent by analyzing load-depth curves. And it showed good agreement with tensile test results.

• 한국재료학회지
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• 제23권3호
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• pp.199-205
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• 2013

The mechanical properties and microstructures of aluminum-matrix composites fabricated by the dispersion of fine alumina particles less than $20{\mu}m$ in size into 6061 aluminum alloys are investigated in this study. In the as-quenched state, the yield stress of the composite is 40~85 MPa higher than that of the 6061 alloy. This difference is attributed to the high density of dislocations within the matrix introduced due to the difference in the thermal expansion coefficients between the matrix and the reinforcement. The difference in the yield stress between the composite and the 6061 alloy decreases with the aging time and the age-hardening curves of both materials show a similar trend. At room temperature, the strain-hardening rate of the composite is higher than that of the 6061 alloy, most likely because the distribution of reinforcements enhances the dislocation density during deformation. Both the yield stress and the strain-hardening rate of the T6-treated composite decrease as the testing temperature increases, and the rate of decrease is faster in the composite than in the 6061 alloy. Under creep conditions, the stress exponents of the T6-treated composite vary from 8.3 at 473 K to 4.8 at 623 K. These exponents are larger than those of the 6061 matrix alloy.

• Corrosion Science and Technology
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• 제11권4호
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• pp.151-156
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• 2012

The cavity formed by the ultrasonic generation in the fluid with the application of water cavitation peening collides into the metal surface. At this time, the surface modification effect such as the work hardening presents by the compressive residual stress formed due to the localized plastic deformation. In this investigation, the water cavitation peening technology in the distilled water with the lapse of time was applied to 5052-O aluminum alloy for aluminum ship of a high value. So, the optimum water cavitation peening time on the effect for surface hardening and anti-corrosion property was investigated. Consequently, the water cavitatin peening time on excellent hardness and corrosion resistance characteristic presented 3.5 min. and 5.0 min, respectively. The surface hardness in the optimum water cavitation peening time was improved approximately 45% compared to the non-WCPed condition. In addition, corrosion current density was decreased.

• 대한조선학회논문집
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• 제43권2호
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• pp.220-227
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• 2006

In case of welding, the inherent strains are generated, because a structure experiences the plastic yielding. The inherent strain is defined as the irrecoverable strain after removing structural restraints and loading. For the analysis method of welding distortion, equivalent loading method based on inherent strain is in general use due to its efficiency and effectiveness. However, it is generally difficult to know the final strain of the welded structure if additional loadings were applied after welding. for this reason, this study introduced the concept of the hardening and added the hardening term to the equivalent loading method based on inherent strain. Therefore, the purposes of this study are to develop the inherent strain formula considering the hardening effect and to calculate residual Stresses Using Proposed inherent Strain. Also, this Study Verified the availability Of proposed inherent strain method by loading-unloading experiment on welded plate.

• Steel and Composite Structures
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• 제28권1호
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• pp.1-11
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• 2018

In this paper, local ratcheting behavior of 1045 steel plates with circular cutout was investigated. Experimental tests were carried out by a Zwick/Roell HB 100 servo hydraulic machine. In order to measure the local strain at notch root, a data acquisition system with strain gauge was used. Various notch diameters and distances of strain gauges mounted from the notch root were found influential in the magnitude of local ratcheting strain. It was found that the local maximum principal stress plays a crucial role in increasing the local plastic deformation. Numerical simulation was done by ABAQUS software using nonlinear isotropic/kinematic hardening model. Material parameters of hardening model were attained from several stabilized cycles of flat specimens subjected to symmetric strain cycles. The nonlinear kinematic hardening model along with the Neuber's rule was employed to assess local ratcheting at the notch root of steel plates. The results of the numerical simulations agreed closely with those measured values in this study. Both ratcheting progress and mean stress relaxation occurred simultaneously at the notch root.

• 대한기계학회논문집A
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• 제28권4호
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• pp.427-434
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• 2004

Ferritic stainless steel is recently used in high temperature structures because of its good properties of thermal fatigue resistance, corrosion resistance, and low price. Tensile and low-cycle fatigue (LCF) tests on 429EM stainless steel used in exhaust manifold were performed at several temperatures from room temperature to 80$0^{\circ}C$. Elastic Modulus, yield strength, and ultimate tensile strength monotonically decreased when temperature increased. Cyclic hardening occurred considerably during the most part of the fatigue life. Dynamic strain aging was observed in 200~50$0^{\circ}C$, which affects the cyclic hardening behavior. Among the fatigue parameters such as plastic strain amplitude, stress amplitude, and plastic strain energy density (PSED), PSED was a proper fatigue parameter since it maintained at a constant value during LCF deformation even though cyclic hardening occurs considerably. A phenomenological life prediction model using PSED was proposed considering the influence of temperature on fatigue life.

• 한국재료학회지
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• 제23권10호
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• pp.568-573
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• 2013

The deformation properties of a TiC-Mo eutectic composite were investigated in a compression test at temperatures ranging from room temperature to 2053 K and at strain rates ranging from $3.9{\times}10^{-5}s^{-1}$ to $4.9{\times}10^{-3}s^{-1}$. It was found that this material shows excellent high-temperature strength as well as appreciable room-temperature toughness, suggesting that the material is a good candidate for high-temperature application as a structure material. At a low-temperature, high strength is observed. The deformation behavior is different among the three temperature ranges tested here, i.e., low, intermediate and high. At an intermediate temperature, no yield drop occurs, and from the beginning the work hardening level is high. At a high temperature, a yield drop occurs again, after which deformation proceeds with nearly constant stress. The temperature- and yield-stress-dependence of the strain is the strongest in this case among the three temperature ranges. The observed high-temperature deformation behavior suggests that the excellent high-temperature strength is due to the constraining of the deformation in the Mo phase by the thin TiC components, which is considerably stronger than bulk TiC. It is also concluded that the appreciable room-temperature toughness is ascribed to the frequent branching of crack paths as well as to the plastic deformation of the Mo phase.

• 콘크리트학회논문집
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• 제24권2호
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• pp.195-204
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• 2012

신구 콘크리트 접합부에서는 굽힌 후 편 철근을 이용한 이음이 발생한다. 철근의 굽힘과 펴는 과정에는 필연적으로 소성 변형이 발생하며, 이 과정에서 가공 경화, 바우싱거 효과, 시효 경화 현상이 발생된다. 이 연구에서는 강종, 지름, 굽힘 내면 반지름, 굽힌 후 펴기까지의 존치기간을 변수로 굽힌 후 편 철근의 인장에 대한 기계적 성질을 조사하였다. 연구 결과, 굽힌 후 편 철근은 비례한계점이 낮아지는 비선형성이 직선 철근에 비해 일찍 발생되었으며, 항복마루 없이 바로 변형경화가 발생하였다. 이것은 굽힘 가공에서 압축을 받은 부분의 바우싱거 효과에 의해 항복점이 낮아졌고, 굽힘 가공에서 인장을 받은 부분의 가공 경화에 의해 항복마루가 없어졌기 때문이다. 높은 강종일수록 항복강도의 저하가 크게 발생되었으며, SD400 철근의 항복강도는 설계기준강도보다 낮았다. 철근은 표면부의 강도가 내부보다 높기 때문에, 높은 강종일수록 굽힌 후 펴면 바우싱거 효과가 크게 발생된다. 굽힌 후 펴기까지의 존치기간이 길면 시효 경화에 의해 항복강도의 상승과 연성의 저하가 발생되었다. Ramberg-Osgood 모델을 기본 형태로 실험 자료를 회귀분석하여 항복강도와 존치기간을 고려한 굽힌 후 편 철근의 응력-변형률 관계를 구성하였다. 이 모델은 굽힌 후 편 철근이 사용된 접합부의 강성 평가에 활용될 수 있다.