• 소성∙가공
• /
• 제16권3호
• /
• pp.172-177
• /
• 2007

The process design for large-scale ring rolling of Ti-6Al-4V alloy was performed by calculation method, processing map approach and FEM simulation. The ring rolling design includes geometry design and optimization of process variables. The calculation method was used to make geometry design such as initial billet and blank sizes, and final rolled ring shape. A commercial FEM code, SHAPE-RR was used to simulate the effect of process variables in ring rolling on the distribution of the internal state variables such as strain, strain rate and temperature. In order to predict the forming defects during ring rolling and the formation of over-heating above $\beta$-transus temperature due to deformation heating, the process-map approach based on Ziegler's instability criterion was used with FEM simulation. Finally, an optimum process design to obtain sound Ti-6Al-4V rings without forming defects was suggested through combined approach of Ziegler's instability map and FEM simulation results.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
• /
• pp.572-577
• /
• 2004

This paper presents numerical study on the performance improvement of the sirocco fan in a range hood. The performance of sirocco fan means a higher flowrate, a higher static pressure and a lower required motor power in a fixed geometry constraint. Various impeller geometric parameters, such as blade profile, blade diameter, blade thickness profile and blade exit angle, were investigated by numerically and the results were compared with each other to know the effects on the performance. In this approach, the volute geometry were fixed with the original shape. The numerical results show that the blade profile with airfoil shape and small exit blade thickness increases the performance. The blade exit angle shows optimum angle within a varied range. The efficiency of the optimized exit angle was about $10\%$ higher than the base blade exit angle and the static pressure was about $28\%$ higher at the flow coefficient 0.22.

• 전자공학회논문지A
• /
• 제32A권2호
• /
• pp.57-65
• /
• 1995

The effects of device geometry and layout on high speed performance such as current gain outoff frequency(f$_{T}$) and maximum oscillation frequency(f$_{max}$) are of very improtant for the scaling-down of geterojunction bipolar transistors(HBT$_{s}$). In this paper AlGaAs/GaAs HBTs are fabricated by MBE epitaxial growth and conventional mesa process, and the experimental data of emitter-base geometru dependency of HBT performance are presented in order to provide the quantitative information for optimum device structure design. It is shown that f$_{T}$ and f$_{max}$ are inversely proportional to the emiter stripe width, while the low emitter perimeter/area ratio is better to f$_{T}$ and worse ot f$_{max}$. It is also demonstrated the f$_{T}$ and f$_{max}$ are highly improved by the emitter-base spacing reduction resulting in less parsitic effects. As the result f$_{T}$ of 42GHz and f$_{max}$ of 23GHz are obtained for fabricated HBT with emitter area of 3${\times}20^{\mu}m^{2}$ and E-B spacing of 0.2$\mu$m.m.m.

• Nuclear Engineering and Technology
• /
• 제53권10호
• /
• pp.3438-3448
• /
• 2021

Dynamic seals are one of the critical components of Absorber Rod Drive Mechanism of Fast Breeder Reactors, requiring separate experimental development. Their significance can't be overemphasized considering that the availability and re-usability of Control Rod Drive Mechanisms of Fast Breeder Test Reactor is governed by the failure rate of dynamic seals (bellows). For prototype and subsequent Fast Breeder Reactors in India, choice of the dynamic seal is changed to an in-house designed & developed labyrinth type V-ring seal. The present work is related to the numerical investigations carried out to gain insights into the sealing mechanism and the thermal behaviour of these seals. The results indicate that the seal geometry is very important for obtaining optimum performance. By changing the geometry of the present seal, performance enhancement by more than 50% in important indices is obtained. Further, the results point out that caution shall be exercised when the seal material & its operating temperature are changed. Also, the numerical model developed in this study will be useful for developing more robust dynamic seals in future.

• 한국지반공학회논문집
• /
• 제25권12호
• /
• pp.131-142
• /
• 2009

보강토 옹벽은 콘트리트 옹벽에 비해 시공성, 경제성, 미관 등이 뛰어나 대체공법으로 각광받고 있으며, 많은 장점들로 인해 일반 옹벽의 대체공법으로서 그 적용성을 인정받고 있다. 최근에 들어서는 도로 및 철도 분야에서 보강토옹벽 구조물이 좌우에 양립하는 형태, 즉 back-to-back(BTB) 형식의 보강토 옹벽이 도로 및 철도 노반을 지지하는 용도로 많이 적용되고 있으나 그에 대한 연구가 충분하지 않은 실정이다. 본 논문에서는 도로분야에 적용되는 BTB 옹벽의 거동 메카니즘 고찰을 위해 유한요소해석을 통하여 다양한 기하조건 및 보강재 길이로 보강된 BTB옹벽의 거동특성을 분석하고 그 결과를 토대로 폭에 따른 거동 메카니즘과 보강재 길이변화를 통해 옹벽 폭에 대한 최적보강재 길이를 검토하였다.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2005년도 춘계학술대회 논문집
• /
• pp.1845-1848
• /
• 2005

The automatic $CO_2$ welding is a manufacturing process to produce high quality joints for metal and it could provide a capability of full automation to enhance productivity. Despite the widespread use in the various manufacturing industries, the full automation of the robotic $CO_2$ welding has not yet been achieved partly because the mathematical model for the process parameters of a given welding task is not fully understood and quantified. Several mathematical models to control welding quality, productivity, microstructure and weld properties in arc welding processes have been studied. However, it is not an easy task to apply them to the various practical situations because the relationship between the process parameters and the bead geometry is non-linear and also they are usually dependent on the specific experimental results. Practically, it is difficult, but important to know how to establish a mathematical model that can predict the result of the actual welding process and how to select the optimum welding condition under a certain constraint. In this research, an attempt has been made to develop an intelligent algorithm to predict the weld geometry (top-bead width, top-bead height, back-bead width and back-bead height) as a function of key process parameters in the robotic $CO_2$welding. A sensitivity analysis has been conducted and compared the relative impact of three process parameters on bead geometry in order to verify the measurement errors on the values of the uncertainty in estimated parameters.

• 한국광학회지
• /
• 제3권4호
• /
• pp.227-233
• /
• 1992

분할디스크형 글라스레이저 증폭기를 개발하기 위하여 이를 해석 설계할 수 있는 시뮬레이션 코드를 작성했다. 레이저매질에서의 열부하를 감소시키고, 플래시램프의 방사스펙트럼과 레이저글라스의 흡수 스펙트럼 간의 결합효율을 높이기 위해서는 전류밀도를 2000-4000A/$\textrm{cm}^{2}$로 유지하여 단파장에서의 방사에너지를 줄여야 한다. 디스크 증폭기에서 같은 부피를 갖는 매질을 3등분하여 냉각표면적을 3배로 늘렸을 때 온도상승치는 30% 정도로 떨어졌다. 단면펌핑 분할 디스크형 증폭기의 설계에서는 각 글라스 간의 $Nd^{3+}$ 도핑율에 차등을 주어야 하고 플래시램프 앞에 있는 매질의 흡수계수 $\alpha$ 와 두께 d의 곱인 $\alpha$d가 0.26 전후가 적절하다는 것을 알았다.

• 한국의학물리학회지:의학물리
• /
• 제15권2호
• /
• pp.84-93
• /
• 2004

정위적 방사선수술(stereotactic radiosurgery, SRS)은 정위적 기구를 이용해 환자를 고정시킨 후 한번에 고선량의 방사선을 병변에 조사하는 방사선 치료법이다. 일반적인 방사선 치료와 달리 단 한번의 조사로 고선량의 방사선이 환자에게 주어지므로 정확한 수술계획의 수립이 필요하다. 현재, 수술계획은 사람이 직접 시행착오를 거듭하며 수립되고 있다. 이로 인해 계획의 재연성과 신뢰성에 문제가 재기되고 있으며, 이를 해결하고자 컴퓨터를 활용한 수술계획 최적화 방법들이 제안되어 왔다. 그러나 기존의 방법들은 최종적인 수출계획을 얻을 때까지 많은 시간이 필요하고 사용되는 수학적 알고리듬의 한계로 국소적 최적해를 최종해로 산출해 낼 위험성을 가지고 있다. 이를 해결하기 위해 이상표적모델을 활용한 정위적 방사선수술계획 최적화 방법을 연구하였다. 병소의 다양한 모양을 근사시킬 이상표적모델을 구형과 원통형, 원뿔형, 타원체의 4종류 가정하였다. 회전중심점(isocenter)을 여러 개 사용하여 이상표적모델을 50％ 등선량 내에 포함시키고, 이 조건을 만족하는 경우의 회전중심점의 위치, 콜리메이터 크기를 데이터베이스화 하였다. 병소가 주어질 경우 기하학적 비교를 통해 병소의 모양을 가장 잘 나타낼 수 있는 이상표적모델, 또는 이상표적모델의 조합을 결정한 후 병소를 근사화하는 과정을 개발하였다. 이후 각 이상표적모델에 대해 데이터베이스에 구축되어 있는 최적변수들을 찾아 회전중심점을 배치시키고 실제 병소에 맞게 최종적인 수정을 통해 최적화 과정을 마치도록 하였다. 이 과정을 가상 표적에 대해 수행한 결과 뛰어난 결과를 보이진 않았으나 회전중심점에 대한 간단한 변화만으로 만족할 만한 결과를 나타내었다. 이는 직접적인 수술에 사용될 수는 없을지라도 수술계획을 함에 있어 최적화 과정의 시작점(Starting Point)으로 받아들이기에 만족할 만한 결과이다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회B
• /
• pp.3080-3085
• /
• 2007

Shape optimization of the 3-dimensional WIG airfoil with 3.0-aspect ratio has been performed by using the multi-objective genetic algorithm. The WIG ship effectively floating above the surface by the ram effect and the virtual additional aspect ratio by a ground is one of next-generation and cost-effective transportations. Unlike the airplane flying out of the ground effect, a WIG ship has possibility to capsize because of unsatisfying the static stability. The WIG ship should satisfy aerodynamic properties as well as a static stability. They tend to strong contradict and it is difficult to satisfy aerodynamic properties and static stability simultaneously. It is inevitable that lift force has to scarify to obtain a static stability. Multi-objective optimization technique that the individual objectives are considered separately instead of weighting can overcome the conflict. Due to handling individual objectives, the optimum cannot be unique but a set of nondominated potential solutions: pareto optimum. There are three objectives; lift coefficient, lift-to-drag ratio and static stability. After a few evolutions, the non-dominated pareto individuals can be obtained. Pareto sets are all the set of possible and excellent solution across the design space. At any selections of the pareto set, these are no better solutions in all design space

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회B
• /
• pp.3050-3055
• /
• 2007

A wind turbine is one of the most popular energy conversion systems to generate electricity from the natural renewable energy source and an axial-flow type wind turbine is the most popular system for the electricity generation in the wind farm nowadays. In this study, a cross-flow type turbine has been studied for the application of wind turbine for electricity generation. The target capacity of electric power generation of the model wind turbine developing on the project is 12 volts, 130A/H (about 1.56kW). The important design parameters of the model turbine impeller are the inlet and exit angle of the turbine blade, number of blade, hub/tip ratio and the exit flow angle of the casing. In this study, the radial equilibrium theorem was used to decide the inlet and exit angle of the impller blade and CFD technique was used to have the performance analysis of the designed model power turbine to find out the optimum geometry of the CPT impeller and casing. The designed CPT with 24 impeller blades at ${\alpha}=82^{\circ}$, ${\beta}=40^{\circ}$ of turbine blade angle was estimated to generate 284.6 N.m of indicated torque and 2.14kW of indicated power.