• 제목/요약/키워드: Blade shape

검색결과 478건 처리시간 0.036초

Effect of Spacing between Layers and Shape of Segment on the Performance of Pattern Saw Blade

  • Park, Hee-Dong;Kim, Youn-Chul;Chang, Joon-Ho;Shin, Min-Hyo
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part2
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    • pp.1140-1141
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    • 2006
  • Diamond tools with several layers of diamond grits through thickness direction were tested by sawing. The saw blades with evenly distributed grits showed better cutting performance compared to the random distributed saw. At a given concentration of grits, as the spacing between layers was increased, the cutting performance was improved, and as decreased, it showed more tool life

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차세대 헬리콥터 로터용 탄성체베어링 소재 특성에 관한 실험적 연구 (An Experimental Study for Material Properties of Elastomer Bearing Using Next Genration Helicopter rotor system)

  • 정정교;김영석;박건록;김두훈;이명규;김덕관
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 춘계학술대회논문집
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    • pp.325-329
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    • 2003
  • Nowadays many peoples are using helicopter in various fields, not only military use but also common people applications such as air-measurement, photography, transportation of goods and persons, saving life and fire fighting etc. And it will be expected more popular than now. Most important part of helicopter to increasing performance and to reducing noise is rotor hub-system. Hub system consists of rotor-blade and rotor-hub. We participate to develop next-generation rotor hub system with elastomeric bearing, part of rotor hub. In this paper we introduce about the role and shape of elastomeric bearing in next-generation helicopter hub system. Then we study about bearing-material requirements and measuring methods. Finally we represent some experimental results.

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프로펠러 날개의 동적 구조해석 시스템 개발 (A Dynamic Structural Analysis System for Propeller Blades)

  • 노인식;이정렬;이현엽;이창섭
    • 대한조선학회논문집
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    • 제41권2호
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    • pp.114-120
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    • 2004
  • Propeller blades have complex airfoil section type geometry and the thickness is continuously varied to both its length and cord-wise direction. in the present research, the finite element analysis program PROSTEC (Propeller Stress Evaluation Code) is developed to calculate the structural responses of propeller blades in irregular ship wake field. To represent the curved and skewed geometry of propeller blades accurately, 20-node curved solid element using the quadratic shape function is adopted. Input data for the analysis including the geometry and pressure distribution of propeller blades can be generated automatically from the propeller design program. And to visualize the results of analysis on windows system conveniently, the post processor PROSTEC-POST is developed.

섬유상 분말로 제조된 배향성을 가진 $BaTiO_3$ 세라믹 (Oriented Barium Titanate Ceramics Made from Fiber State Powder)

  • 서용교;야나기다히로아끼
    • 한국세라믹학회지
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    • 제30권12호
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    • pp.1066-1070
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    • 1993
  • When looked upon as a polycrystalline, ceramics have two basic differences from a single crystal. One is that there exist grain boundaries, the other is that the crystal axes of each small crystal are arranged in random directions. But the crystal axes fo small crystals which compose ceramics may be made to have the tendency of being arranged in a specific direction. This is called that the crystal axes are oriented. The degree of the direction arrangement of the crystal axes is called orientation. In order to orient the crystal axes effectively, the fiberous barium titanates were made through KDC method and the ion exchange method. And then they were arranged through pressing, doctor blade, and syringe. As the result of Lotgering evaluation, the sample oriented through syringe showed the highest orientation. After sintering, though the most particles that had been fiberous shaped became global shape viewed through SEM, the orientation of the crystals was reinforced by means of sintering.

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석탄화력발전소 보일러 연소용 공기 제어알고리즘의 개발 (The Development of Boiler Combustion Air Control Algorithm for Coal-Fired Power Plant)

  • 임건표;이흥호
    • 전기학회논문지P
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    • 제61권4호
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    • pp.153-160
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    • 2012
  • This paper is written for the development of boiler combustion air control algorithm of coal-fired power plant by the steps of design, coding and test. The control algorithms were designed in the shape of cascade control for two parts of air master, forced draft fan pitch blade by standard function blocks. This control algorithms were coded to the control programs of distributed control systems under development. The simulator for coal-fired power plant was used in the test step and automatic control, sequence control and emergency stop tests were performed successfully like the tests of the actual power plant. The reliability will be obtained enough to apply to actual site if the total test has been completed in the state that all algorithms were linked mutually. It is expected that the project result will contribute to the safe operation of domestic power plant and the self-reliance of coal-fired power plant control technique.

리어가이더 시작각 변화가 횡류홴 성능에 미치는 영향 (Effects of Starting Angles of a Rearguider on the Performance of a Cross-Flow Fan)

  • 김형섭;김동원;윤태석;박성관;김윤제
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1981-1986
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    • 2004
  • A cross-flow fan relatively makes high dynamic pressure at low speed because a working fluid passes through an impeller blade twice and blades have a forward curved shape. Therefore, the performance of a cross-flow fan is influenced 25% by the impeller, 60% by the rearguider and the stabilizer, 15% by the heat exchanger. At the low flow rate, there exists a rapid pressure head reduction, a noise increase and an unsteady flow against a stabilizer and a rearguider. Moreover, it is difficult to analyze the reciprocal relations of the cross-flow fan because each parameter is independent. Numerical analyses are conducted with different starting angles of the rearguider. Two-dimensional, unsteady governing equations are solved, using FVM, PISO algorithm, sliding grid system and ${\kappa}-{\varepsilon}$ standard turbulence model.

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Turbine Impeller 형상이 유동특성에 미치는 영향에 관한 연구 (A Study on Effect of Flow Characteristics for Turbine Impeller Shape)

  • 전언찬;윤기호;강창훈
    • 한국기계가공학회지
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    • 제13권4호
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    • pp.36-43
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    • 2014
  • Recently, research has been conducted to develop the ORC (organic Rankine cycle), to recover waste heat from facilities such as industrial plants ultimately to create mechanical or electrical energy. The ORC system consists of a heat exchange, a condenser, a pump and a boiler. In this paper, 84 flow analyses were conducted with 21 cases and three variables, i.e., a number of large wings, a number of small wings, and RPMs. R245fa was used as a refrigerant. The flow cavitation phenomenon was investigated through a flow analysis, and a flow stream analysis was conducted.

CFD와 역설계를 이용한 교반기 Impeller 형상 해석에 관한 연구 (Study on the Industrial Agitator's Impeller Shape Analysis Using CFD and Reverse Engineering)

  • 김동균;배석태;박재현
    • 한국CDE학회논문집
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    • 제11권5호
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    • pp.359-364
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    • 2006
  • Industrial Agitators are used in various industrial fields where they are necessary to intimately mix two reactants in a short period of time. However, despite their widespread use, complex unsteady flow characteristics of industrial mixers are not systematically investigated. The present study aims for clarify unsteady flow characteristics induced by various impellers in agitator's tank. Impellers are Pitched blade turbine(PBT) types, Screw type and Rushton turbine type(RUT). In this study is numerical analysis of the Industrial agitator's Impeller types. The rotating speed of impellers fixed about 100RPM. Numerical analysis results show that differential flow characteristics of each type Impeller and Rushton turbine type(RUT) is suitable for mixing powder.

임펠러 직경비 및 리어가이더 형상변화가 횡류홴 성능에 미치는 실험적 연구 (Experimental Study on the Performance of a Cross-Flow Fan with Various Diameter Ratios of Impeller and Rearguider Shapes)

  • 김형섭;김동원;윤태석;박성관;김윤제
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.391-396
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    • 2003
  • A cross-flow fan relatively produces higher dynamic pressure at low speed because a working fluid passes through an impeller blade twice and blades have a forward curved shape. The performance of a cross-flow fan is influenced 25% by the impeller, 60% by the rearguider and the stabilizer, and 15% by the heat exchanger. At the low flow rate, there exist a rapid pressure head reduction, a noise increase and an unsteady flow against a stabilizer and a rearguider. The purpose of this study is to investigate the reciprocal relation among each parameter Experiments are conducted to study the effects of a rearguider and a diameter ratio of impeller on the performance analysis of a cross-flow fan. Comparing with the rearguider of radial type, the Archimedes type shows excellent results for various diameter ratios.

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실험계획법을 사용한 원심펌프 임펠러 최적설계 (Design Optimization of Centrifugal Pump Impeller Using DOE)

  • 김성;최영석;윤준용;김덕수
    • 한국유체기계학회 논문집
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    • 제11권3호
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    • pp.36-42
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    • 2008
  • In this paper, the performance characteristics of the impeller in a centrifugal pump were investigated using DOE(Design of Experiment) with commercial CFD software. Geometric parameters of vane plane development were defined with the meridional shape and frontal view of the impeller. The incidence angles and the exit blade angle were selected as main parameters using 2k factorial and the influences of selected design parameters were examined through the optimization process using RSM.