• Title/Summary/Keyword: Turbo Process

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Development of Expert System for Tool Selection on Turning Operation (선삭공정에 있어서 공구선택용 전문가 시스템의 개발)

  • Paik, In-Hwan;Kwon, Hyeog-Jun
    • Journal of the Korean Society for Precision Engineering
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    • v.9 no.3
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    • pp.53-60
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    • 1992
  • This paper deals with developing an Expert system for tool selection using knowledge base system approach, and its application. For the sake of building of knowledge base, the information from process through sensor, tool handbook and interview with expert are referrenced and managed. The system developed shows good application flexibility in providing the actual cutting process with the selection of tool(insert, holder) and cutting conditions(feed, speed, rake type, and so on), is found as a useful system for real-time machining process. The Expert system for tool selection is written in TURBO PROLOG ver. 2.0 for inference engine capability, and can be run in interactive mode for user friendliness. In order to apply the system developed in actual cutting process, more parameters should be considered and scrutinized, and the system should be further extended in modular basis.

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Improved Drying Process for Electrodes in Production of Lithium-Ion Batteries for Electric Vehicles (전기자동차용 리튬이온 전지의 제조공정을 위해 개선된 극판 건조 기술)

  • Jang, Chan-Hee;Lee, Jae-Chon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.6
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    • pp.37-45
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    • 2018
  • An electric vehicle is an environmentally friendly vehicle because there is no exhaust gas, unlike gasoline automobiles. On the other hand, because the electric vehicle is driven by electric power charged in batteries, the distance to go through a single charge depends on the energy density of the batteries. Therefore, a lithium-ion battery with a high energy density is a good candidate for batteries in electric vehicles. Because the electrode is an essential component that governs the efficiency of a lithium-ion battery, the electrode manufacturing process plays a vital role in the entire production process of lithium-ion batteries. In particular, the drying process during the electrode manufacturing process is a critical process that has a significant influence on the performance. This paper proposes an innovative process for improving the efficiency and productivity of the drying process in electrode manufacturing and describe the equipment design method and development results. In particular, the design procedure and development method for enhancing the electrode adhesion power, atmospheric pressure superheated steam drying technology, and drying furnace slimming technologies are presented. As a result, high-speed drying technology was developed for battery electrodes through the world's first turbo dryer technology for mass production using open/integrated atmospheric pressure superheated steam. Compared to the conventional drying process, the drying furnace improved the productivity (Dry Lead Time $0.7min{\rightarrow}0.5min$).

CAD와 CAPP의 통합화를 위한 형상특징의 자동인식

  • 오수철;조규갑
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1991.04a
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    • pp.309-315
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    • 1991
  • This paper presents a method for automatic part feature recognition from the database of AutoCAD system for automatic process planning input. The parts considered in this study are primastic parts composed of faces perpendicular to the X, Y, Z axes and the types of features considered are through steps, blind steps, through slots, blind slots, and pockets. Features are recognized by using the concept of convex points and concave points. The software program is coded by using Turbo Pascal on the IBM PC/AT.

Development of System Analysis Program of Liquid Rocket Engine II (액체로켓엔진 시스템 통합 해석 프로그램 개발 2)

  • Lee, Sangbok;Son, Min;Seo, Jongcheol;Lim, Taekyu;Roh, Tae-Seong;Koo, Jaye;Kim, Kuisoon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.1
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    • pp.16-25
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    • 2014
  • The system analysis and design program of the liquid rocket engine has been developed for preliminary conceptual design process. The program consists of modular programs analyzing the main thruster, the gas-generator, turbo-pumps, the turbine, pipes, valves and so on. Each module has been developed in order to estimate performance, weight, and shape parameters of the components. The results of them have been verified with experimental data or other programs.

Performance Analysis of a 50㎾ Turbo-Generator Gas Turbine Engine with a Recuperator (리큐퍼레이터를 고려한 50KW급 터보제너레이터 가스터빈 엔진의 성능해석)

  • 김수용;수다레프
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.2
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    • pp.48-55
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    • 1999
  • Performance analysis of a 50KW turbo-generator gas turbine engine with a recuperator was studied. Recuperated cycle has been employed to meet maximum fuel economy and ultra low emissions especially for military and vehicular engines. From thermodynamic stand point, it is known that recuperative cycle can contribute most to enhance thermal cycle efficiency for the Pressure ratios under 10 and of comparatively low turbine inlet temperature. Efficiency of a simple cycle with a recuperator increases relatively about 30% than without one at effectiveness of 0.5. Pressure losses in the heat exchanger less than 5.2% is considered in the design process. A tubular type heat exchanger is selected for this particular engine because it can provide simple construction as well as structural sturdiness and excellent leak tightness.

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An Operation and Safety Assessment Study of Roundabout Types (회전교차로 형태별 운영 및 안전성 평가에 관한 연구)

  • Jang, Ki-Hun;Lee, Sang Soo
    • International Journal of Highway Engineering
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    • v.17 no.5
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    • pp.105-113
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    • 2015
  • PURPOSES: The aim of this study is to analyze and compare the operational effectiveness and safety of three different types of roundabout found in the literatures using a VISSIM and SSAM program. METHODS : The three types roundabout tested are the 2-lane roundabout (2R), the Turbo roundabout (TR), and the Flower roundabout (FR). For each scenario, three roundabout types and traffic conditions such as traffic volume and movement ratio were applied to VISSIM in order to compute the average delays. In addition the total conflict was calculated through SSAM by using trajectory data from VISSIM. RESULTS: From the analysis results, the average delay in TR and FR type was higher than the 2R. Regardless of the roundabout types, the average delay was reduced as the right-turn vehicles increased. The total conflict in TR was fewer than 2R for all traffic conditions. CONCLUSIONS : The results of this study can be used in the planning and design process of roundabout deployment. The data also provides some numerical justifications in transition from at-grade intersection to roundabout.

Performance analysis of Downlink Multi-user MIMO based on TM9 in Rel.10 (Rel.10 의 TM9 기반 다운링크 Multi-user MIMO 성능분석)

  • Song, Hua Yue;Choi, Seung Won
    • Journal of Korea Society of Digital Industry and Information Management
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    • v.10 no.1
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    • pp.47-53
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    • 2014
  • LTE-Advanced is the evolved version of LTE which is currently in progress at the 3GPP. At present, as the number of smart phone users is rapidly increasing, the demand for ever more capacity is driven largely by video usage and high quality data communication and so on, this let more researchers study about LTE-A all over the world. LTE-A aims to achieve improved service and communication quality over 3G system at the aspect of throughput, peak data rate, latency, and spectral efficiency. Among various features in LTE-A, the multi-user MIMO(MU-MIMO), in which the base station transmits several streams to multiple receivers, has expected to give better quality for system. In this paper, we investigate performances of various types of downlink receivers with fixed number of antennas. we first review the development process from LTE to LTE-A. Second we introduce TM9 which is adopted in Rel.10 for MU-MIMO system, including the MU-MIMO system model and the explanation on the algorithm used in system. We also have brief introduction about sub-blocking in turbo decoding, finally we compare the performance between the uncoded case and coded case which is using turbo encoding.

Real operation of 2 kW class reverse-Brayton refrigeration system with using scroll compressor package

  • Kim, Hyobong;Yeom, Hankil;Choo, Sangyoon;Kim, Jongwoo;Park, Jiho;In, Sehwan;Hong, Yong-Ju;Park, Seong-Je;Ko, Junseok
    • Progress in Superconductivity and Cryogenics
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    • v.22 no.4
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    • pp.40-44
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    • 2020
  • This paper describes the real operation of 2 kW class reverse-Brayton refrigeration system with neon as a working fluid. The refrigeration cycle is designed with operating pressure of 0.5 and 1.0 MPa at low and high pressure side, respectively. Compressor package consists of several helium scroll compressors witch are originally used for driving GM cryocooler. Three segments of plate heat exchanger are adopted to cover the wide temperature range and the refrigeration power is produced by turbo expander. The developed refrigeration system is successfully operated at its target temperature of 77 K. In experiments, all parameters such as pressure, temperature, mass flow rate and valve opening are measured to investigate characteristics during cool-down process and normal state. The difference between design and real operation is discussed with measured experimental data. At normal state of 77 K operation, the developed reverse-Brayton refrigeration system shows 1.83 kW at 68.2 K of cold-end temperature.

A Study on the System Safety Assessment of Aircraft (항공기 시스템의 안전성 평가에 관한 연구)

  • Lee, Kyung-Chol;Lee, Jong-Hee;Yi, Baeck-Jun;Yoo, Seung-Woo
    • Journal of Applied Reliability
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    • v.7 no.2
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    • pp.89-100
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    • 2007
  • For the certification of aircraft and part, it must be show the compliance with applicable requirements through system safety assessment. The safety assessment process should be planned and managed to provide the necessary assurance that all relevant failure conditions have been identified and that all significant combinations of failures which could cause those failure conditions have been considered. Complex systems, especially aircraft, should take into account any additional complexities and interdependencies which arise due to integration. In all cases involving integrated systems, the safety assessment process is of fundamental importance in establishing appropriate safety objectives for the system and determining that the implementation satisfies these objectives. This study review the safety assessment for the certification process of the aircraft engine system and analyze turbo-fan engine by fault analysis method for compliance with airworthiness requirement of aircraft engine system.

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A Study on CAD interfaced CAPP System for Turning Operation ( I ) : Automatic Feature Recognition and Process Selection (선삭공정에서 CAD 인터페이스된 자동공정계획시스템개발에 관한 연구( I ) : 형상특징의 자동인식과 공정선정)

  • Cho, Kyu-Kap;Kim, In-Ho
    • Journal of Korean Institute of Industrial Engineers
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    • v.17 no.2
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    • pp.1-16
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    • 1991
  • This paper deals with some critical activities of CAPP system such as generation of part description database, part feature recognition, process and operation selection, and sequencing method for turning operation of symmetric rotational parts. The part description database is generated by data conversion module from CAD data, and the part feature is recognized by using both pattern primitives and feature recognition rules. Machining processes and operations are selected based on machining surface features and its sequence is determined by rules acquired from process planning expert. AutoCAD is employed as CAD system and computer program is developed by using Turbo-C on IBM PC/AT compatible system.

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