• Title/Summary/Keyword: 가스냉각

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An Investigation of Angled Discrete Rib-Turbulators for Cooling Enhancement of Gas Turbine Blades (가스 터빈 블레이드 냉각 성능 향상을 위한 경사요철의 단락 효과)

  • Wu, Seong-Je;Lee, Sei-Young;Cho, Hyung-Hee
    • Proceedings of the KSME Conference
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    • 2001.06d
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    • pp.782-789
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    • 2001
  • Local heat/mass transfer and friction loss in a square duct roughened with various types of continuous and discrete rib turbulators are investigated. The combined effects of the gap flows of the discrete ribs and the secondary flows are examined for the purpose of the reduction of thermally weak regions and the promotion of the uniformity of heat/mass transfer distributions as well as the augmentation of average heat/mass transfer. The rib-to-rib pitch to the rib height ratio (p/e) of 8 and the rib angles of 90 and 60 deg are selected with $e/D_{h}=0.08$. The vortical structure of the secondary flows induced by the parallel angled arrays are quite distinct from that induced by the cross angled arrays. This distinction influences on heat/mass transfer and friction loss in all the tested cases. The gap flows of the discrete ribs reduce the strength of the secondary flows but promote local turbulence and flow mixing. As a result, the fairly uniform heat/mass transfer distributions are obtained with two row gaps.

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Development of X-ray Image Processing Technology for Nondestructive Measurement of the Coating Thickness in the Simulated TRISO-coated Fuel Particle (모의 TRISO 핵연료입자 코팅층 두께 비파괴 측정을 위한 X-선 영상처리기술 개발)

  • Kim Woong-Ki;Lee Young-Woo;Park Ji-Yeon;Ra Sung-Woong
    • Proceedings of the Korea Information Processing Society Conference
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    • 2006.05a
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    • pp.669-672
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    • 2006
  • 고온가스냉각 원자로에서는 고온 안정성 및 핵분열생성물 차단 성능이 우수한 TRISO(tri-tsotropic) 핵연료를 사용하고 있다. TRISO 핵연료 입자는 직경이 약 1 mm인 구 형태로 입자의 중심에는 직경 $0.5{\mu}m$의 핵연료 커널(kernel)이 포함되며 커널 외곽을 코팅 층이 에워싸고 있다. 이 코팅 층은 완충(buffer) PyC(pyrolytic carbon) 층, 내부 PyC 층, SiC 층, 그리고 외부 PyC 층으로 구성되어 있다. 각 코팅 층의 두께는 수십${\sim}$${\mu}m$ 범위이며, 본 연구에서는 각 코팅 층의 두께를 비파괴적으로 측정하기 위하여 마이크로포커스 X-선 발생장치와 고해상도 X-선 평판(flat panel) 검출기로 구성된 정밀한 X-선 래디오그래피 장치를 구성하고, $UO_2$ 핵물질 대신에 $ZrO_2$를 커널로 사용한 모의 TRISO 핵연료 입자에 대한 래디오그래피 영상을 획득한 후 디지털 영상처리기술을 이용하여 코팅 층 사이의 경계선이 구분 가능하도록 영상을 개선하고 디지털 영상처리 알고리즘을 개발하여 코팅 층의 두께를 측정하였다.

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The heat transfer characteristics of supercritical $CO_2$ in a horizontal tube (수평관내 $CO_2$의 초임계 영역내 열전달에 관한 연구)

  • Oh Hoo-Kyu;Lee Dong-Geon;Son Chang-Hyo
    • Journal of Advanced Marine Engineering and Technology
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    • v.29 no.5
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    • pp.526-532
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    • 2005
  • The cooling heat transfer coefficient of $CO_2$(R-744) in a horizontal tube was investigated experimentally. The experiments were conducted without oil in a closed refrigerant loop which was driven by a magnetic gear pump. The main components of the refrigerant loop are a receiver, a variable-speed pump. a mass flow meter. a pre-heater and gas cooler(test section). The test section consists of a smooth, horizontal stainless steel tube of 7.75 mm inner diameter. The experiments were conducted at mass flux of 200 to $400\;kg/m^{2}s$ and the inlet cooling pressure of 7.5 MPa to 10.0 MPa. The variation of heat transfer coefficient tends to decrease as cooling pressure of $CO_2$ increases. The heat transfer coefficient with respect to mass flux increases as mass flux increases. The pressure drop of $CO_2$ in the gas cooler shows a relatively good agreement with that predicted by Blasius's correlation. The local heat transfer coefficient of $CO_2$ agrees well with the correlation by Bringer-Smith.

An Experimental Study on Transient Heat Transfer Characteristics of Gas Turbine Cooled Vane by Using Liquid Crystal Thermography (가스터빈 냉각 베인에서 감온액정을 이용한 과도적 열전달 특성에 관한 실험적 연구)

  • Suh Nam-Kyu;Chang Tae-Hyun
    • Journal of Advanced Marine Engineering and Technology
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    • v.30 no.1
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    • pp.22-29
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    • 2006
  • Gas turbine engine among Principal internal combustion engines has been mainly applied as an aero and industrial Power plant. In order to increase its thermal efficiency. it has been raised their pressure ratio of compressor and the turbine inlet temperature. To operate above the limit temperature of turbine material, turbine nozzle vanes should be cooled. For this the cooling air is bled from the compressor section of 9as turbine. Meanwhile, to keep high thermal efficiency of 9as turbine, turbine vanes are to be cooled by using small cooling air Therefore, the complex cooling passages are requested to be designed and evaluated the effectiveness of vane cooling by measuring turbine vane temperature. But it is very difficult or impossible for us to measure local turbine temperatures at actual temperature When local heat transfer coefficients are known these can be calculated, therefore this study has been investigated on obtaining these coefficients of turbine vane at room temperature using TLC.

A Fundamental Study on Sea Water Freezing Behavior in a Rectangular Vessel Cooled from Below (구형용기의 하부면 냉각에 의한 해수 동결거동의 기초적 연구)

  • 김명준;길병래;김명환
    • Journal of Advanced Marine Engineering and Technology
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    • v.21 no.5
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    • pp.564-570
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    • 1997
  • The most important factor for the desalination system is the fresh water production cost dependent upon the possible energy source which should be obtained easily and with low price. Recently in Korea the demand of LNG, as a cheap and clean energy which does not cause an environmental problem, has sharply been increased. In general, LNG is storaged in a tank as a liquid state below -162 'C. When it is serviced, however, the LNG absorbs energy from a heating source and transforms to the gaseous state with high pressure. During this process a huge amount of cold energy accumulated in LNG is wasted. This waste cold energy can be utilized for producing fresh water from sea water using a sea water freezing desalination system. In order to develop a sea water freezing desalination system and to establish its design technique, a qualitative and quantitative data regarding the freezing behavior of sea water is needed in advance. The goal of this study, therefore, are to reveal the freezing mechanism of sea water, to measure the freezing rate, and to investigate the freezing heat-transfer characteristics. The experimental results help to provide a general understanding of the sea water freezing behavior in a Rectangular vessel cooled from below.

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Fabrication and Characterization of Silicon Devices for Flow Measurement (II) (흐름측정용 실리콘 소자의 제작 및 특성 평가 (II))

  • Ju, B.K.;Ko, C.G.;Kim, C.J.;Tchah, K.H.;Oh, M.H.
    • Journal of Sensor Science and Technology
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    • v.3 no.1
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    • pp.12-18
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    • 1994
  • In this study, we fabricated and characterized a calorimetric-type flow sensing element using a micromachined silicon substrate. The cooling and heating effects resulted from the gas flow were measured by two temperature sensors located at both sides of the heating resistor, and the insulator diaphragm was employed as a substrate in order to improve thermal isolation. The sensor generated $0{\sim}378.4mV$ output signal under 10V bridge-applied voltage when the nitrogen gas was passed on the sensor surface having a mass flow rate of $0{\sim}0.25grs/min$, and reached to the stable operating condition within 10 seconds.

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A Thermodynamic Study on Suction Cooling-Steam Injected Gas Turbine Cycle (吸氣冷却-蒸氣噴射 가스터빈 사이클에 관한 열역학적 연구)

  • 박종구;양옥룡
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.1
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    • pp.77-86
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    • 1992
  • This paper discusses the thermodynamic study on the suction cooling-steam injected gas turbine cycle. The aim of this study is to improve the thermal efficiency and the specific output by steam injection produced by the waste heat from the waste heat recovery boiler and by cooling compressor inlet air by an ammonia absorption-type suction cooling system. The operating region of this newly devised cycle depends upon the pinch point limit and the outlet temperature of refrigerator. The higher steam injection ratio and the lower the evaporating temperature of refrigerant allow the higher thermal efficiency and the specific output. The optimum pressure ratios and the steam injection ratios for the maximum thermal efficiency and the specific output can be found. It is evident that this cycle considered as one of the most effective methods which can obtain the higher thermal efficiency and the specific output comparing with the conventional simple cycle and steam injected gas turbine cycle.

Determination of Enthalpy in the 150kW Arc-Jet (150kW 아크제트 유동의 엔탈피 결정)

  • Na, Jae Jeong;Lee, Jeong Min
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.7
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    • pp.547-551
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    • 2013
  • Mass averaged and core enthalpy in the arc jet flow are obtained experimentally. The experiment is made for the 150kW Huels type arc-jet applying the test condition for the research of gasturbine engine injection cooling technique. The mass averaged enthalpy value determined by the sonic throat method is 5.5MJ/kg. The core enthalpy value determined by the heat transfer rate method is 14.3MJ/kg. Based on result of experiment, the ratio of the core to mass averaged enthalpies is 2.6.

The Measurement of Total Acid Number in Transformer Oils using Simple Analytical Equipment (간이측정기구를 이용한 변압기 절연유 전산가 측정)

  • Nam, Chang-Hyun;Kim, Seok-Boon;Park, Hyun-Joo;Hwang, Seon-Jin
    • Proceedings of the KIEE Conference
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    • 2008.11a
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    • pp.397-399
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    • 2008
  • 발 변전설비 중 중요한 설비의 하나로 손꼽히는 변압기는 운전 중 신뢰성 확보가 관건이라 할 수 있다. 최근 안정적 전력공급에 대한 요구가 증대됨에 따라 변압기 이상진단 기술지원 요청이 매년 증가하고 있으며, 특히 절연과 냉각작용이 주기능인 전기절연유의 자체 품질관리는 변압기 예방진단을 위해 시행하고 있는 유중가스분석 못지않게 중요하다. 이에 전력연구원에서는 1999년 전산가 간이측정 기구를 개발하여 별도의 분석의뢰 없이 현장에서 바로 측정하여 절연유의 품질관리에 적용할 수 있도록 한 바 있다. 본 논문은 2008년 1월부터 4개월간 12개 전력관리처에 배분하여 66kV이상 급 모든 변압기의 전산가 현장측정을 완료하고 이에 대한 적용결과와 현장적용성을 검토하였다.

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A study on the Influence Affected on Injection Molding Product by Vacuum Degree (진공도가 사출성형제품에 미치는 영향에 관한 연구)

  • 이은종;신남호
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.4 no.3
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    • pp.183-188
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    • 2003
  • Non-molding and welding line happen by the assembly of gas at the connector terminal. There is not good phenomenon of burr by increasing the over injection pressure, the temperatures of die and resin to prevent from them. Therefore, the connector mold to apply the vacuum molding system is developed in this study. The vacuum pressure is controlled systematically with the optimum conditions in the important ingredients of injection molding that are the temperatures of melting resin and die and cooling condition. The badness in charging is cleared by making a vacuum to non-charging part of the deep bottom part of each cavity. And the vacuum system to reduce the cycle time is applied as the study envelopment of molding work. So, the good product and the productivity improvement can be obtained in this study.

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