• 제목/요약/키워드: optimized

검색결과 12,773건 처리시간 0.044초

A Study on the Optimized Copper Electrochemical Plating in Dual Damascene Process

  • Yoo, Hae-Young;Chang, Eui-Goo;Kim, Nam-Hoon
    • Transactions on Electrical and Electronic Materials
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    • 제6권5호
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    • pp.225-228
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    • 2005
  • In this work, we studied the optimized copper thickness in Cu ECP (Electrochemical Plating). In order to select an optimized Cu ECP thickness, we examined Cu ECP bulge (bump, hump or over-plating amount), Cu CMP dishing and electrical properties of via hole and line trench over dual damascene patterned wafers split into different ECP Cu thickness. In the aspect of bump and dishing, the bulge increased according as target plating thickness decreased. Dishing of edge was larger than center of wafer. Also in case of electrical property, metal line resistance distribution became broad gradually according as Cu ECP thickness decreased. In conclusion, at least $20\%$ reduced Cu ECP thickness from current baseline; $0.8\;{\mu}m$ and $1.0\;{\mu}m$ are suitable to be adopted as newly optimized Cu ECP thickness for local and intermediate layer.

최적화 기법을 이용한 고양력 플랩 설계 (DESIGN OF HIGH LIFT FLAP WITH OPTIMIZATION TECHNIQUE)

  • 김철완;이융교
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.227-228
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    • 2008
  • In the present paper, fowler flap was optimized to maximize the lift with response surface method. Leading edge shape and the gap between main airfoil and flap, were optimized and the aerodynamic characteristics was improved considerably. The optimized flap has more rounded leading edge and bigger gap. Before angle of attack, $10^{\circ}$, lift and drag are improved and the optimized flap shows similar aerodynamic characteristics to the original flap. The flow condition for optimization was angle of attack, $10^{\circ}$, Mach number, 0.2, flap deflection, $40^{\circ}$.

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멀티레벨 인버터의 Optimized Sine-Wave Modulation (Optimized Sine-Wave Modulation of Multi-Level inverters for Electric Propulsion System)

  • 진선호;조관준;곽준호;오진석
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2005년도 후기학술대회논문집
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    • pp.200-201
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    • 2005
  • This paper is analyzed a new modulation method of OSW(Optimized Sine-Wave) modulation strategy for cascaded H-bridge multi-level inverter. The inverter structure was modified with the maximum output voltage level, and the switching angle was calculated easily to adjust the requested Vrms of the output. The suggested modulation method could make output waveform very close to the ideal sine wave, and the THD value was improved also remarkably.

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정면밀링커터의 최적설계에 대한 연구 (2) -공구수명 및 표면조도 중심으로- (A Study on Optimal Design of Face Milling Cutter Geometry(II) -With Respect to Toll Life and Surface Roughness-)

  • 김정현;김희술
    • 대한기계학회논문집
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    • 제18권9호
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    • pp.2225-2233
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    • 1994
  • In order to improve the cutting ability of face mill, a model for optimal cutter shape was developed to minimize resultant cutting force by combing cutting force model and optimal technique. Wear test and surface roughness test for optimized and conventional cutter were performed. The new optimized cutter shows longer tool life of 2.29 times than conventional cutter in light cutting condition and 2.52 times in heavy cutting condition. The surface roughness of workpiece by optimized cutter is improved in heavy cutting condition, but deteriorated in light cutting condition in comparison with conventional cutter. The surface profiles of workpiece were analyzed by Fourier transformation. The distribution of cut lay left on workpiece by optimized cutter is more regular than that by the conventional cutter.

최적화 기법을 이용한 고양력 플랩 설계 (DESIGN OF HIGH LIFT FLAP WITH OPTIMIZATION TECHNIQUE)

  • 김철완;이융교
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.227-228
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    • 2008
  • In the present paper, fowler flap was optimized to maximize the lift with response surface method. Leading edge shape and the gap between main airfoil and flap, were optimized and the aerodynamic characteristics was improved considerably. The optimized flap has more rounded leading edge and bigger gap. Before angle of attack, $10^{\circ}$, lift and drag are improved and the optimized flap shows similar aerodynamic characteristics to the original flap. The flow condition for optimization was angle of attack, $10^{\circ}$, Mach number, 0.2, flap deflection, $40^{\circ}$.

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비파괴 검사용 초음파 탐촉자에서의 정합층 최적 설계법 (Design Method for the Optimized Acoustic Matching Layers of UT Probes)

  • 박치승;김선진
    • 한국재료학회지
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    • 제13권10호
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    • pp.658-662
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    • 2003
  • In this study, we have tried to find the optimized design variables of the matching layer which is important part of thickness mode ultrasonic transducer and finally reach the conclusion that the electrical property of piezo-element must be under consideration when the optimized acoustic impedance is estimated. Proper expression of the effective impedance of front load at free resonant frequency(: $Z_{f}$ $^{(0)}$ /) has been induced by introducing the principle of binomial multilayer transformer and gradient based numerical method is utilized to find the most acceptable value of $Z_{ f}$/$^{(0)}$ . Optimized point of acoustic impedance can be calculated directly from $Z_{f}$ $^{(0)}$ using some simple formula which we propose. We also verify our result by both numerical and experimental method and get a good enhancement especially it concern to the bandwidth of ultrasonic transducer.

센서 네트워크 상에서의 HUMMINGBIRD2 암호화 속도 최적화 구현기법 (A Speed Optimized Implementation Technique of HUMMINGBIRD2 Encryption over Sensor Network)

  • 서화정;김호원
    • 한국통신학회논문지
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    • 제37권6B호
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    • pp.414-422
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    • 2012
  • 본 논문에서는 초경량 대칭키 암호화 기법인 HUMMINGBIRD2 알고리즘을 센서 모트상에서의 최적화 구현기법을 제시한다. 효율적인 구현을 위해 센서보드상에 제공되는 레지스터의 활용을 극대화하며 최적화된 주소접근 기법을 적용하여 암복호화에 소요되는 시간을 최소화하였다. 해당 대칭키 암호화 구현기법을 통해 자원 한정적인 센서 상에서의 안전하고 효율적인 보안 통신이 가능하도록 한다.

선미 스케그 주위의 유동 분석에 의한 선미 형상 설계 (The Stern Hull Form Design using the Flow Analysis around Stern Skeg)

  • 박동우
    • 대한조선학회논문집
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    • 제45권4호
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    • pp.361-369
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    • 2008
  • The optimized distance between skegs and angle of the skeg for a standard twin-skeg type LNG carrier were presented using the CFD and model tests. The evaluation method of self-propulsion performance was derived based on the results of CFD and confirmed the validity through model tests. The analyses to assess self-propulsion performance using CFD were shown by flow line patterns on the skeg surface, nominal wake distribution in the propeller plane and the evaluation for flow balance around stern skegs. The optimized ship that was applied to the optimized two design parameters in stern skeg arrangement for target ship was derived in this work. Finally speed performance of mother ship which is existing ship and optimized ship were compared through CFD and model tests. And the usefulness about the evaluation method of self-propulsion performance was reconfirmed.

인공신경망을 이용한 연약지반 침하량 산정 (Soft Ground Settlement Estimation Using Neural Network)

  • 노재호;원효재;오두환;황선근
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2006년도 추계학술대회 논문집
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    • pp.1405-1410
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    • 2006
  • Purpose of this research is that offers basic data for optimized design using neural network method to calculate consolidation settlement in study area. In this research, preformed the neural network method that analyzed the settlement characteristics of soft ground nearby study area. Thus, data base established on ground properties and consolidation settlement of neighboring area. In addition, designed the optimum neural network model for prediction of settlement through network learning and consolidation settlement prediction using consolidation settlement DB and ground properties DB. Optimized neural network model decided by repeated learning for various case of hidden layers. In this study, proposed that the optimized consolidation settlement calculation method using neural network and verified which is the optimized consolidation settlement calculation method using neural network.

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A Shape Optimization of Universal Motor using FEM and Evolution Strategy

  • Shin, Pan-Seok
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • 제2B권4호
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    • pp.156-161
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    • 2002
  • This paper proposes an optimized universal motor for improving its performance using the finite element method (FEM) with the (1+1) Evolution Strategy (ES) algorithm. To do this, various design parameters are modified, such as air gap length, shape of motor slot, pole shoe, pole width, and rotor shaft diameter. Two parameters (arc length of stator pole and thickness of pole shoe) are chosen and optimized using the program, and the optimized model is built and tested with a performance measuring system. The measured values of the model are compared with those of the initial and the optimized model to prove the algorithm. As a result, the final model improves its performance compared with those of the initial model.