• Title/Summary/Keyword: configuration design

Search Result 3,128, Processing Time 0.025 seconds

A New LMR SG with a Double Tube Bundle Free from SWR

  • Sim Yoon-Sub;Kim Seong-O;Kim Eui Kwang;Hahn Do Hee
    • Nuclear Engineering and Technology
    • /
    • v.35 no.6
    • /
    • pp.566-580
    • /
    • 2003
  • To resolve the concern of the SWR possibility in LMR and improve the economic feature of LMR, relative performance of various SG designs using a double tube bundle configuration is evaluated and a new SG design concept is proposed. The new steam generator design houses two tube bundles that are functionally different and its tube bundle region is radially divided into two. It prevents the occurrence of sodium water reaction while sodium is still used as the coolant for the primary heat transport system. The feasibility of the SG with a double tube bundle for actual use in an LMR plant is evaluated by setting up the skeleton of the NSSS for various possible configurations of the SG tube bundles. The evaluation revealed the relative advantages and disadvantages of the configurations and the new SG design concept performs good and can be actually used in an LMR plant.

Analysis of large deformation and fatigue life of fabric braided composite hose subjected to cyclic loading

  • Cho, J.R.;Kim, Y.H.
    • Steel and Composite Structures
    • /
    • v.21 no.4
    • /
    • pp.949-962
    • /
    • 2016
  • The braking hose in the automotive hydraulic braking system exhibits the complicated anisotropic large deformation while its movable end is moving along the cyclic path according to the steering and bump/rebound motions of vehicle. The complicated large deformation may cause not only the interference with other adjacent automotive parts but also the durability problem resulting in the fatal microcraking. In this regard, the design of high-durable braking hose with the interference-free layout becomes a hot issue in the automotive industry. However, since it has been traditionally relied on the cost-/time-consuming trial and error experiments, the cost- and time-effective optimum design method that can replace the experiment is highly desirable. Meanwhile, the hose deformed configuration and fatigue life are different for different hose cyclic paths, so that their characteristic investigation becomes an important preliminary research subject. As a preliminary step for developing the optimum design methodology, we in this study investigate the hose deformed configuration and the fatigue life for four representative hose cyclic paths.

Configuration of Network Based GNSS Correction System for Land Transportation Navigation (육상교통 항법을 위한 네트워크기반 위성항법보정 시스템의 구성)

  • Son, Minhyuk;Son, Eunseong;Lee, Eunsung;Heo, Moon-Beom;Nam, Gi-Wook
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.21 no.4
    • /
    • pp.17-26
    • /
    • 2013
  • In this paper, a configuration procedure of a transportation infrastructure system for GNSS based very precise real-time positioning is proposed. This infrastructure system consists of several receiving station, a central station, and communication sub-systems. The required performance, design, implementation and verification of each sub-system are explained respectively. The required performance can be broken down into accuracy, integrity, stability, processing time. The design of the each sub-system is performed in accordance with the required performance and each sub-system is built with regard to the design. Lastly the implemented system is verified in comparison with the required performance.

틸트로터 설계특성 및 주요 사이징 변수에 대한 요구

  • Ahn, Oh-Sung;Kim, Jai-Moo
    • Aerospace Engineering and Technology
    • /
    • v.3 no.1
    • /
    • pp.277-286
    • /
    • 2004
  • In this study, summary of past tilt-rotor concept development presented, and based on that, major pros and cons of tilt-rotor technology compared to other air-vehicle concept was presented. Also presented were major design features, considerations and sizing constraints of tilt-rotor configuration implemented to the development of Smart UAV. It is hoped that this paper be served to understand the tilt-rotor air-vehicle design and development.

  • PDF

Extraction of Design Parameters for Planar Coupled Lines (유한 요소 해석에 의한 평면형 결합 선로의 설계 파라미터 추출)

  • Lee, Pil-Yong;Park, Jun-Seok;Ahn, Dal;Kim, Hysons-Seok
    • Proceedings of the KIEE Conference
    • /
    • 2000.07c
    • /
    • pp.2213-2215
    • /
    • 2000
  • In this paper we implemented a novel re-entrant mode microstrip directional coupler for realizing the high directivity characteristic using finite element (FE) analysis. In microstrip configuration, the high directivity can be reached by matching the even- and odd-mode effective phase velocities. Through the values of capacitance obtained from 2-dimensional finite element(FE) analysis, the phase velocities for each mode and the design parameter were extracted for the proposed coupled-line configuration. Based on the extracted design parameter with phase matching condition we designed and fabricated 30dB directional coupler at 850MHz. Experimental results show good performance with excellent isolation.

  • PDF

Design Space Exploration of Many-Core Architecture for Sound Synthesis of Guitar on Portable Device (휴대 장치용 기타 음 합성을 위한 매니코어 아키텍처의 디자인 공간 탐색)

  • Kang, Myeongsu;Kim, Jong-Myon
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2014.01a
    • /
    • pp.1-4
    • /
    • 2014
  • Although physical modeling synthesis is becoming more and more efficient in rich and natural high-quality sound synthesis, its high computational complexity limits its use in portable devices. This constraint motivated research of single-instruction multiple-data many-core architectures that support the tremendous amount of computations by exploiting massive parallelism inherent in physical modeling synthesis. Since no general consensus has been reached which grain sizes of many-core processors and memories provide the most efficient operation for sound synthesis, design space exploration is conducted for seven processing element (PE) configurations. To find an optimal PE configuration, each PE configuration is evaluated in terms of execution time, area and energy efficiencies. Experimental results show that all PE configurations are satisfied with the system requirements to be implemented in portable devices.

  • PDF

A Study on the Spatial Configuration of A Small Art Museum through the Analysis of Visual Perception in Spatial Layouts (공간의 시지각적 분석에 의한 소규모 미술관의 공간구성에 관한 연구)

  • 김재욱;김용승
    • Korean Institute of Interior Design Journal
    • /
    • no.29
    • /
    • pp.120-127
    • /
    • 2001
  • The study aims at finding out the spatial configuration of a small art museums through the analysis of visual Perception in spatial layouts. In so doing to analyze the characteristics of spatial perception in visual layouts and identity of space to evaluate the spatial construction with relation to the role of small art museums. Purpose of this study is to offer basic data to contribute effectiveness of the architectural planning of a small art museums by understanding of visual element of design and ultimately to make efficient use of space.

  • PDF

Lifter Design for Enhanced Heat Transfer in Rotating Counter-Current Flow Reactor and Application to One Dimensional Heat Balance Model (회전식 대향류 반응기 내 열전달 증진을 위한 리프터 설계와 1차원 열평형 모델로의 적용)

  • Lee, Hookyung;Choi, Sangmin
    • 한국연소학회:학술대회논문집
    • /
    • 2013.06a
    • /
    • pp.51-54
    • /
    • 2013
  • Rotary kiln reactors are frequently equipped with an axial burner with which solid burden material is directly heated. Lifters are commonly used along the length of the system to lift particulate solids and increase the heat transfer between the solid bed and the combustion gas. The material cascading from the lifters undergoes drying and reacting through direct contact with the gas stream. In this study, volume distribution of materials held within lifters was modeled according to the different lifter configuration and appropriate configuration was used for the design purpose. This was applied to the one-dimensional heat balance model of a counter-current flow reactor, which contributes to the increase of the effective contact surface, and thereby enhances the heat transfer.

  • PDF

Design of Bio-Information Process based on Digital Composite Sensing (디지털 복합센싱 생체정보 프로세스 설계)

  • Lee, Tae-Gyu;Shin, Seong-Yoon;Lee, Hyun-Chang
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2014.05a
    • /
    • pp.507-510
    • /
    • 2014
  • The initial process configuration of biometric information system is performed by the same sequences statically and consistently without changing after the system is running. However, this static process configuration appears an inefficient performance to the applications of the mobile biometric information system in the mobile computing environment. This work proposes the dynamic process design and execution method as a way to overcome these inefficient processes.

  • PDF

Flap Design Optimization for KLA-100 Aircraft in compliance with Airworthiness Certification (인증규정을 고려한 KLA-100항공기 고양력장치 최적화 설계)

  • Park, Jinhwan;Tyan, Maxim;Nguyen, Nhu Van;Kim, Sangho;Lee, Jae-Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.41 no.8
    • /
    • pp.649-656
    • /
    • 2013
  • High-lift devices have a major influence on takeoff, landing and stall performance of an aircraft. Therefore, a slotted flap design optimization process is proposed in this paper to obtain the most effective flap configuration from supported 2D flap configuration. Flap deflection, Gap and Overlap are considered as main contributors to flap lift increment. ANSYS Fluent 13.0.0$^{(R)}$ is used as aerodynamic analysis software that provides accurate solution at given flight conditions. Optimum configuration is obtained by Sequential Quadratic Programing (SQP) algorithm. Performance of the aircraft with optimized flap is estimated using Aircraft Design Synthesis Program (ADSP), the in-house performance analysis code. Obtained parameters such as takeoff, landing distance and stall speed met KAS-VLA airworthiness requirements.