• 제목/요약/키워드: Optimal design weight

검색결과 696건 처리시간 0.024초

Conceptual Design Optimization of Tensairity Girder Using Variable Complexity Modeling Method

  • Yin, Shi;Zhu, Ming;Liang, Haoquan;Zhao, Da
    • International Journal of Aeronautical and Space Sciences
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    • 제17권1호
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    • pp.29-36
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    • 2016
  • Tensairity girder is a light weight inflatable fabric structural concept which can be used in road emergency transportation. It uses low pressure air to stabilize compression elements against buckling. With the purpose of obtaining the comprehensive target of minimum deflection and weight under ultimate load, the cross-section and the inner pressure of tensairity girder was optimized in this paper. The Variable Complexity Modeling (VCM) method was used in this paper combining the Kriging approximate method with the Finite Element Analysis (FEA) method, which was implemented by ABAQUS. In the Kriging method, the sample points of the surrogate model were outlined by Design of Experiment (DOE) technique based on Optimal Latin Hypercube. The optimization framework was constructed in iSIGHT with a global optimization method, Multi-Island Genetic Algorithm (MIGA), followed by a local optimization method, Sequential Quadratic Program (SQP). The result of the optimization gives a prominent conceptual design of the tensairity girder, which approves the solution architecture of VCM is feasible and efficient. Furthermore, a useful trend of sensitivity between optimization variables and responses was performed to guide future design. It was proved that the inner pressure is the key parameter to balance the maximum Von Mises stress and deflection on tensairity girder, and the parameters of cross section impact the mass of tensairity girder obviously.

조합 유전 알고리듬을 이용한 증기 터빈 회전체-베어링 시스템의 최적설계 (Optimal Design for Steam-turbine Rotor-bearing System Using Combined Genetic Algorithm)

  • 김영찬;최성필;양보석
    • 한국소음진동공학회논문집
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    • 제12권5호
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    • pp.380-388
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    • 2002
  • This paper describes the optimum design for low-pressure steam turbine rotor of 1,000 MW nuclear power plant by using a combined genetic algorithm, which uses both a genetic algorithm and a local concentrate search algorithm (e.g. simplex method). This algorithm is not only faster than the standard genetic algorithm but also supplies a more accurate solution. In addition, this algorithm can find the global and local optimum solutions. The objective is to minimize the resonance response (Q factor) and total weight of the shaft, and to separate the critical speeds as far from the operating speed as possible. These factors play very important roles in designing a rotor-bearing system under the dynamic behavior constraint. In the present work, the shaft diameter, the bearing length, and clearance are used as the design variables. The results show that the proposed algorithm can improve the Q factor and reduce the weight of the shaft and the 1st critical speed.

파워스티어링 오일펌프용 풀리의 피로수명을 고려한 형상최적화 (Shape Optimization Considering Fatigue Life of Pulley in Power-Steering Pulley)

  • 심희진;김정규
    • 대한기계학회논문집A
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    • 제30권9호
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    • pp.1041-1048
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    • 2006
  • The pulley is one of core mechanical elements in the power steering system for vehicles. The pulley operates under both the compressive loading and the torque. Therefore, to assure the safety of the power steering system, it is very important to investigate the durability and the optimization of the pulley. In this study, the applied stress distribution of the pulley under high tension and torsion loads was obtained by using finite element analysis. Based on these results the fatigue life of the pulley with the variation of the fatigue strength was evaluated by a durability analysis simulator. The results at 50% and 1% for the failure probability were compared with respect to the fatigue life. In addition to the optimum design for the fatigue life is obtained by the response surface method. The response function utilizes the function of the life and weight factors. Within range for design life condition the minimization of the weight, one of the formulation, is obtained by the optimal design. Moreover the optimum design by considering its durability and validity is verified by the durability test.

3D 공간정보를 활용한 터널 설계 자동화 기술 개발 및 적용 사례 : 남해 서면-여수 신덕 국도 건설공사 BIM기반 설계를 중심으로 (Development and Application of Tunnel Design Automation Technology Using 3D Spatial Information : BIM-Based Design for Namhae Seomyeon - Yeosu Shindeok National Highway Construction)

  • 조은지;김우진;김광염;정재호;방상혁
    • 터널과지하공간
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    • 제33권4호
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    • pp.209-227
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    • 2023
  • 정부는 건설산업의 생산성 혁신을 위해 BIM 기반 스마트 건설기술 활성화방안을 지속적으로 발표하고 있다. 설계단계에서는 BIM 데이터와 다른 첨단기술을 융합하여 설계 자동화와 최적화 수행을 목표로 한다. 국내 해저터널 사업인 남해 서면-여수 신덕 국도 건설공사 기본설계에서는 터널설계 프로세스에 따라 3D 공간정보를 이용한 터널설계 자동화 기술을 개발하여 BIM 기반의 설계를 수행하였다. 터널의 선형설계에 제너레이티브 디자인 기법을 사용하여 만 여건 이상의 케이스를 36시간 내에 도출하고, 설계자가 정의한 목적함수의 정량적 평가를 수행하여 설계자가 요구하는 조건의 최적 선형을 도출했다. AI 기반의 지반분류와 3D Geo Model을 구축하여 최적 선형의 경제성 및 안정성을 평가하였다. AI 기반의 지반분류는 시추 코어 1공당 약 30종의 지반분류를 수행하여 그 정밀도를 향상시켰고, 3D Geo Model의 경우 시공 중 추가되는 지반 데이터를 누적할 수 있다는 점에서 그 활용도를 기대할 수 있다. 3D 발파설계의 경우 Dynamo 상에서 노선상의 모든 보안물건을 검토하여 최적 장약량을 5분 만에 도출하고, 직관적이고 편리한 시공관리를 위해 3D 공간상에 설계 결과를 시각화함으로서 시공 중에 직접 활용할 수 있도록 했다.

고압을 받는 MIL-S-46119 원형 밀폐링의 형상 최적화 (The Shape Optimization of MIL-S-46119 Ring Obturator Under the High Pressure)

  • 채제욱;이영신;박태규
    • 대한기계학회논문집A
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    • 제27권1호
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    • pp.1-7
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    • 2003
  • The optimal design for the shape of MIL-S-46119 ring obturator under the high pressure using parameter stud:』 on the stress analysis considering effects of design variable is presented, and it is compared to experimental results. The trends of parametric study are in good agreement with the experimental results. The more thickness the higher stress. The more taper the higher stress. And maximum stress of circumferential surface is larger than maximum stress of forward surface. The design variable!; are such as thickness, taper, radius of shape of the obturator. In order to optimize the shape of obturation ring, the weight is maximized subject to maximum stress of the obturator within allowable stress. The design constraints are geometric elements of design variables.

Empirical Design of an On and Off Type Solenoid Actuator For Valve Operation

  • Sung, Baek-Ju;Lee, Eun-Woong;Kim, Hyoung-Eui
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • 제4B권2호
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    • pp.39-46
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    • 2004
  • Modern users demand that the on and off type solenoid actuator should be smaller, lighter in weight, lower in consumption power, and higher in response time. The complete design satisfying such requirements can be achieved when electromagnetic theories and empirical knowledge are combined. This paper presents various types of empirical coefficients essentially needed for optimal design of a solenoid actuator. The values of these empirical coefficients are obtained through extensive experiments over a great length of time for various kinds of solenoid actuators. We have developed a design program that is composed by combination of governing equations and empirical coefficients, and have also manufactured a prototype solenoid actuator based on the final results of the design program. The propriety of the design program and empirical coefficients have been proven by experiments.

고압을 받는 금속 밀폐링의 형상 최적화에 관한 연구 (A Study on the Shape Optimization of Metal Ring Obturator under the High Pressure)

  • 이영신;채제욱;박태규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집A
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    • pp.315-320
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    • 2000
  • The optimal design for the shape of metal ring obturator under the high pressure using parameter study on the stress analysis considering effects of design variable is presented and is compared to experimental results. The design variables are such as thickness, taper, radius of shape of the obturation ring. For optimization of the obturation ring, the weight is maximized subject to maximum stress of the obturator within allowable stress. The design constraints are geometric elements of design variables. The trends of parametric study are in good agreement with the experimental results.

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위상최적설계 결과를 이용한 CAD 인터페이스 (CAD Interface using Topology Optimization)

  • 김성훈;민승재;이상헌
    • 한국CDE학회논문집
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    • 제14권4호
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    • pp.281-289
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    • 2009
  • Topology optimization has been widely used for the optimal structure design for weight reduction and high performance. Since the result of three-dimensional topology optimization is represented by the discrete material distribution in finite elements, it is hard to interpret from a design point of view. In this paper, the method for interpreting three-dimensional topology optimization resuIt into a series of cross-sectional curve representation is proposed and interfaced with the existing CAD system for the practical use. The concept of node density and virtual grid is introduced to transform element density values into grid density and material boundaries in each cross section are identified based on the element volume rate to satisfy the amount of material specified in the original design intent. Design exampIes show that three-dimensional topology result can be converted into a form of curve CAD model and the seamless interface with CAD software can be achieved.

관절형 차량의 알루미늄 합금 차체 설계에 관한 연구 (A Study on Design of Aluminium Carbody for Articulated Trailer)

  • 권영규;장동화;이광일;박광복;장대성
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 1998년도 추계학술대회 논문집
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    • pp.568-582
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    • 1998
  • This study was carried about the basic design and FEM analysis of aluminium carbody for articulated trailer of Korean High Speed Train of maximum operating speed of 350㎞/h. The integral design by extra-long extruded sections made possible through the use of aluminium alleys and continuous window shape with skin were adopted in the basic design of aluminium carbody. Articulated structures in each trailer's end were welded laterally on both sides of gangway. FEM analysis showed that the design satisfied the specified load criteria. Futher study should be carried out for optimal design which enables the weight of carbody structure to reduce adequately.

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적층 시퀀스 데이터베이스를 이용한 복합재 날개 구조물의 최적화 설계 (Optimal Design of Thick Composite Wing Structure using Laminate Sequence Database)

  • 장준환;안상호
    • Composites Research
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    • 제30권1호
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    • pp.52-58
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    • 2017
  • 본 논문에서 제시한 복합재 날개 구조물의 최적설계 기법은 파손모드를 통합한 최적화 프레임 웍을 사용하여 복합재 날개 구조물의 안전율을 자동으로 계산한다. 개발된 최적화 프레임 웍은 복합재 구조물의 설계요소에 가장 큰 영향을 주는 파손모드 즉, 최초 파손모드, 좌굴 파손 모드 및 베어링-바이패스 파손을 확인하여 구축된 적층 데이터베이스 안에서 적층수를 찾아낸다. 이는 개발과정에서 수정 및 반복되는 설계 및 해석 시간을 단축시킬 수 있는 효과가 있다. 설계변수는 계단형태로 이루어진 적층 데이터베이스이며 응답은 변형률, 좌굴, 볼트 주변부의 응력장이며 목적함수는 날개구조의 질량이다. 그리고 최적화 프레임 윅을 구동하는 Composite Optimizer의 해석결과를 검증하기 위하여 유한요소모델의 좌굴해석 결과와 비교하여 유효성을 검증하였다.