• Title/Summary/Keyword: Preliminary Design Procedure

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Efficient Design Procedure of Concrete Dome and Ring Beam in Containment Structures (콘크리트 격납구조물 돔 및 링빔의 효율적인 설계 기법)

  • Jeon, Se-Jin;Kim, Young-Jin
    • Proceedings of the Korea Concrete Institute Conference
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    • 2010.05a
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    • pp.139-140
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    • 2010
  • Combined analysis is required for the concrete dome and ring beam of containment structure due to the interaction in section forces. In this study, an efficient design procedure is proposed that can be used to determine the preliminary sections of the dome and ring beam as well as a proper level of prestress in the ring beam, prior to a detailed design. The procedure applies the membrane theory of the shell of revolution.

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Seismic Design of Building Using LRB(Lead Rubber Bearing) (납 면진받침을 적용한 건축물의 내진 설계)

  • 김두훈
    • Proceedings of the Earthquake Engineering Society of Korea Conference
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    • 1998.10a
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    • pp.258-265
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    • 1998
  • Seismic isolation has developed to the point where it may be considered as a viable design alternate for a wide range of building structures. However, it needs to consider various aspects to adopt a suitable isolation system for buildings practically. This report presents the basis for the preliminary design procedure which has been developed for the seismic isolation system using the lead rubber bearings. The design procedures have been developed to ensure that the bearings will safely support the maximum gravity load throughout the life of the structure while they provide a period shift and hysteretic damping during the design earthquake.

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Structural Sizing for Optionally Piloted PAV Preliminary Design (유무인 겸용 개인항공기(OPPAV) 개념설계를 위한 구조물 사이징)

  • Kim, Sung Joon;Lee, Seung-gyu
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.83-89
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    • 2020
  • Personal air vehicle (PAV) is considered by aviation engineers as a solution to provide fast urban mobility. The purpose of designing a optionally piloted PAV (OPPAV) is to provide an individual air vehicle. The airframe structure is designed with high strength carbon fiber composite to reduce the aircraft weight. This paper presents an overview of sizing process for OPPAV at the conceptual design level. It consists of load analysis, structural sizing and development of efficient design allowable values for composite material. The weight is estimated based on sizing process, including strength and stiffness requirements. The objective of this study is to present a overview of structural sizing procedure and fast tool for preliminary design phases.

Preliminary Design of Fuel System for the Smart UAV (스마트 무인기 연료시스템 설계에 관한 연구)

  • Kang Myoung-Cheol;Lee Chang-Ho;Kong Chang-Duk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.5-8
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    • 2004
  • In this study, the fundamental design procedure for the Smart UAV fuel supply system was set up, and the preliminary design was peformed to meet the vehicle system requirements. The fuel system layout was determined through consideration of vehicle system requirements, and then fuel tank layout, design of components such as booster pump, jet pump, pipe, vent system, weight estimation, etc. were carried out.

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Engineering design procedure for gas turbine combined cycle power plant with post-combustion CO2 capture (CO2 포집을 고려한 가스터빈 복합화력 발전 플랜트의 시스템 대안 평가를 위한 공학 설계)

  • Lee, Soohyeon;Choi, Sangmin
    • 한국연소학회:학술대회논문집
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    • 2014.11a
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    • pp.333-335
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    • 2014
  • As the user demand for power plants becomes various, design objective becomes complicated. To review the system feasibility, system objective and evaluation criteria need to be newly defined. In this study, engineering design procedure of the multi-purpose power plant, such as barge-mounted combined cycle power plant with $CO_2$ capture, was shown as a previous work for the feasibility review of the system alternatives. For the system design, heat and mass balance for each system configuration was firstly performed. Using the thermal analysis results, conceptual design of system alternatives was carried out. And then, preliminary design of the major equipment was done. The engineering calculation results of this study would be used as the evaluation data for system feasibility review.

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A Preliminary Study on the Role of Industrial Design in Attributes of Products (제품속성에 대한 디자인의 역할에 관한 기초적 연구)

  • 이현이;김명석
    • Proceedings of the ESK Conference
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    • 1997.04a
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    • pp.212-226
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    • 1997
  • Industrial design aiming the mutual benefit of both user and manufacturer demands grasping and analyzing the needa and wants of consumer for the establishrment of the optimum plan and production by attribute oriented approach. Inspite of its usefulness, however, it might be impossible to help industrial designers to develop a new product effectively without full understanding of industrial design activity in attributes of products and using the appropriate methodology for grasping the main attributes. This thesis is purposed for developing the guideline of research models of consumer for industrial design by studying characteristics of industrial design activity in attributes of products through bibliography and defining the clear limit of design research focused on consumer selection through comparison with real purchase decision making procedure at every phase. Through the observation and analysis of the real purchase decision making procedure following the proposed guideline, the possibility of difference between the two cases has been shown in both theoretical and practical aspects.

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Computational Grid Generation for Navier-Stokes Design of Axial-Flow Compressors (축류압축기의 Navier-Stokes설계를 위한 계산격자점 생성기법 연구)

  • Chung H. T.
    • 한국전산유체공학회:학술대회논문집
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    • 1997.10a
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    • pp.38-42
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    • 1997
  • A multiblock grid generation has been applied to a Navier-Stokes design procedure of a axial-flow compressors. A multiblock structure simplifies the creation of structured H-grids about complex turbomachinery geometries and facilitate the creation of a grid in the tip flow region. The numerical algorithm adopts the combination of the algebraic and elliptic method to create the internal grids efficiently and quickly. The input module is made of the results of the preliminary design, i.e., flow-path, aerodynamic conditions along the spanwise direction, and the blade profile data. The final grids generated from each module of the system are used as the preprocessor for the performance prediction of the sectional blade, the blade-stacking process and the three-dimensional flow simulation inside the blade passage. Application to the blade design of the LP compressor was demonstrated to be very reliable and practical in support of design activities. This customized system are coupled strongly with the design procedure of the turbomachinery cascades using the Navier-Stokes technique.

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Design and Efficiency Characteristic Test of 340W Home Appliance Synchronous Reluctance Motor (가전용 340W급 동기형 릴럭턴스 전동기 설계 및 효율특성 실험)

  • 이중호
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.52 no.2
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    • pp.39-52
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    • 2003
  • This paper deals with an automatic design procedure for the maximum torque density and power factor in a synchronous reluctance motor (SynRM). The focus of this paper is the design relative to the number of flux barrier and the ratio Kw of flux barrier width to iron sheet width of a SynRM under the mechanical constraint. The Finite Elements Analysis (FEA) has been used to evaluate the maximum torque density and power factor with each rotor shape. The proposed procedure allows to define the rotor geometric dimensions starling from an existing mootor or a preliminary design. The maximum torque density and power factor of a SynRM has been resulted with the rotor design variation. To prove the propriety of the designed SynRM, the Digital Signal Processor (DSP) installed experimental devices are equipped and the efficiency characteristic test is Performed.

Design Solutions to Minimize Iron Gore Loss in Synchronous Reluctance Motors Using Preisach Model & FEM (프라이자흐 모델이 결합된 유한요소 해석을 이용한 동기형 릴럭턴스 전동기의 철손 최소화 회전자 구조 설계)

  • Lee, D.D.;Lee, M.M.;Sim, J.M.;Lee, J.H.
    • Proceedings of the KIEE Conference
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    • 2002.11d
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    • pp.138-140
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    • 2002
  • This paper deals with an automatic design procedure for the minimization of iron core loss in a synchronous reluctance motor (SynRM). The focus of this paper is the design relative to hysteresis loss on the basis of rotor shape of a SynRM in the same torque density. The coupled Finite Elements Analysis (FEA) & Preisach model have been used to evaluate the iron core loss with the rotor shape. The proposed procedure allows to define the rotor geometric dimensions starting from an existing motor or a preliminary design. The iron loss has been reduced with a rotor design variation.

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Molding Design Factors Optimization for Maximizing Shrinkage Uniformity of Injection Molded Part using Design of Experiments (실험계획법을 이용한 사출품의 균일 수축을 위한 성형 설계인자의 최적화)

  • Park, Jong-Cheon;Kim, Kyung-Mo;Yin, Jeong-Je;Lee, Jae-Hoon
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.10 no.6
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    • pp.70-76
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    • 2011
  • This paper presents an optimization procedure for reducing warpage of injection molded part by using a volumetric shrinkage deviation as an objective function. A design of experiments based on orthogonal arrays was used in the optimization procedure, and the entire optimization was performed through a two stage process - a preliminary experimentation and a principal experimentation. Proposed optimization method was applied to the design of a CPU-base part in computer. With the moderate number of experiments, an optimal molding condition for uniform distribution of volumetric shrinkage was obtained, as a result, the warpage of the molded part was significantly reduced.