• Title/Summary/Keyword: 수지최적설계기법

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Study on optimal design of IED aperture according the material using (1+1) Evolution strategy ((1+1) 진화전략 기법을 이용한 IED 함체 재질에 따른 개구면 최적 설계 연구)

  • Ko, Jae-Hyeong;Kim, Koon-Tae;Lee, Je-Kwang;Kim, Hyeong-Seok
    • Proceedings of the KIEE Conference
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    • 2011.07a
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    • pp.1644-1645
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    • 2011
  • 초고주파 영역에서 전자파 영향을 감소시키기 위해 IED의 개구면에 대하여 (1+1) 진화전략 기법을 이용하여 최적 설계 연구를 수행하였다. 함체 재질이 ABS 수지와 steel-stainless의 경우에 대하여 개구면의 최적 설계를 수행하였다. 진화전략 기법을 이용하여 개굼녀의 최적 설계 결과 개구면의 크기가 감소하면서 상단에 위치할 때 고주파에서 PCB에 유기되는 전계가 약 47% 감소하는 것을 확인 할 수 있었다.

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A Study on Numerical Optimization Method for Aerodynamic Design (공력설계를 위한 수치최적설계기법의 연구)

  • Jin, Xue-Song;Choi, Jae-Ho;Kim, Kwang-Yong
    • The KSFM Journal of Fluid Machinery
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    • v.2 no.1 s.2
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    • pp.29-34
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    • 1999
  • To develop the efficient numerical optimization method for the design of an airfoil, an evaluation of various methods coupled with two-dimensional Naviev-Stokes analysis is presented. Simplex method and Hook-Jeeves method we used as direct search methods, and steepest descent method, conjugate gradient method and DFP method are used as indirect search methods and are tested to determine the search direction. To determine the moving distance, the golden section method and cubic interpolation method are tested. The finite volume method is used to discretize two-dimensional Navier-Stokes equations, and SIMPLEC algorithm is used for a velocity-pressure correction method. For the optimal design of two-dimensional airfoil, maximum thickness, maximum ordinate of camber line and chordwise position of maximum ordinate are chosen as design variables, and the ratio of drag coefficient to lift coefficient is selected as an objective function. From the results, it is found that conjugate gradient method and cubic interpolation method are the most efficient for the determination of search direction and the moving distance, respectively.

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증류탑의 제어 시스템 설계

  • 양대륙
    • ICROS
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    • v.2 no.1
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    • pp.93-100
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    • 1996
  • 본 논문에서는 증류탑 제어 구조의 선택과 선택된 조작변수를 이용한 조성제어 전략에 대하여 고찰해 보았다. 제어구조 설계시 증류탑의 양끝에서 물질 수지와 에너지 수지제어를 조합해 주는 두 파라미터에 의해, 예상되어지는 제어구조를 동적 구조 변환 기법을 사용하여 쉽게 분석할 수 있으며, Combined balance 방법으로부터 시작하여, 증류탑에 대한 3가지의 새로운 방법을 소개하였다. 제어구조를 결정하는데 ITAE와 같은 닫힌 루프 성능지표에 기초한 최적 combined balance 구조는 multiloop dual 조성 제어에 대해 다른 구조보다 뛰어난 성능을 보이고 있다. 이 방법은 새로운 증류탑의 제어구조를 설계할 때나, 기존의 증류탑 성능을 향상시키는 데에 사용할 수 있다. 이상과 같이 제어구조가 결정된 후 사용할 수 있는 여러 가지 제어전략을 소개하였다. 제어전략의 선택은 사용자의 목적에 따라 적절한 것을 선택하면 되는데, 대부분의 경우는 적당한 제어구조를 Combined balance 구조로서 결정하게 되면 간단한 형태의 전통적 제어기를 사용해도 무방하며 제어구조의 선택이 선행되지 않으면 MPC와 같은 고급 제어전략을 사용하여 상호작용 등에 의하여 생기는 문제를 해결하는 것이 바람직하다.

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Genetic Algorithms for Optimal Augmentation of Water Distribution Networks (유전자 알고리즘을 이용한 배수관망의 최적 확장 설계)

  • Lee, Seung-Cheol;Lee, Sang-Il
    • Journal of Korea Water Resources Association
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    • v.34 no.5
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    • pp.567-575
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    • 2001
  • A methodology is developed for designing the minimum-cost water distribution network. The method is based on network simulations and an optimization scheme using genetic algorithms. Being a stochastic optimization scheme, genetic algorithms have advantages over the conventional search algorithms in solving network problems known for their nonlinearities and herculean computational costs. While existing methods focus on the design of either entirely new or parallel augmentation of network systems, the proposed method can be applied to problems having both new branches of tree-type and paralle augmentation in loops. The applicability of the method was shown through a case study for Baekryeon water supply system. The optimized design resulted in the maximum 5.37% savings compared to the conventional design without optimization, while meeting the hydraulic constraints.

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Study on design of the composite torque link for a landing gear system of a helicopter (헬리콥터 착륙장치를 위한 복합재 토크링크의 설계에 대한 연구)

  • Kim, Jin-Bong;Um, Moon-Kwang;Lee, Sang-Yong;Kim, Tae-Uk;Shin, Jeong-Woo
    • Composites Research
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    • v.22 no.2
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    • pp.30-36
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    • 2009
  • In this paper, we propose the design method for the composite torque link of a landing gear for a helicopter. The composite torque link has to be light weighted and very stiff to keep the shock absorber in the landing gear of helicopter. The configuration and structural shape has to be designed in consideration of the RTM (Resin Transfer Molding) manufacturing process which is adopted to minimize the manufacturing cost. The mechanical properties are obtained through the coupon tests with the specimens made by the same manufacturing process for the composite structure. The optimal design process was performed through iterative modifications of the models which were verified by stress analysis using FEM. The composite torque link has lug-shaped parts and is very thick, so 3D Layered solid elements of ABAQUS were used to get the stress field including the stress components in thickness direction and non-linear static analysis using contact B.C. of rigid-deform condition was used to get the optimal design.