• 제목/요약/키워드: cooling channel

검색결과 439건 처리시간 0.022초

터빈 기익 선단부에 설치된 냉각유로에서의 요철 배열에 따른 열전달 특성 (Heat Transfer Characteristics in a Leading Edge Cooling Channel of a Turbine Blade with Various Rib Arrangements)

  • 이동현;김경민;이동호;조형희
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.459-466
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    • 2005
  • The present study investigates the heat transfer characteristics of a triangular channel. Three different rib configurations are tested. The ribs are installed on two sides of the channel. The rib height (e) to channel hydraulic diameter is 0.079 and the rib-to-rib pitch (p) is 8 times of the rib height. The rotation number ranges from 0.0 to 0.1 while the Reynolds number is fixed at 10,000. The copper blocks with heaters are installed on the channel walls to measure the regionally averaged heat transfer coefficients. For the stationary $45^{\circ}$ and $135^{\circ}$ ribbed channels, a pair of counter rotating vortices is induced by the angled rib arrangements, and high heat transfer coefficients are obtained on the regions near the inner wall for the $45^{\circ}$ ribbed channel and near the leading edge for the $90^{\circ}$ ribbed channel. The heat transfer coefficients of angled ribbed channels are changed little with rotation, whereas those of the transverse ribbed channel are changed significantly with rotation.

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예연소기 헤드 및 냉각채널 시편 강도 시험 (Strength Experimets on Head and Cooling Channel Specimens of a Preburner)

  • 유재한;문인상;이수용
    • 한국추진공학회지
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    • 제15권2호
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    • pp.50-55
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    • 2011
  • 고성능 로켓엔진에 사용되는 다단연소싸이클의 주요 부품인 예연소기 개발 과정에서 브레이징 접합부를 모사하는 시편에 대한 강도 시험을 수행하고 유한 요소 해석 결과와 비교하였다. 진공 브레이징 되는 헤드의 산화제 분사기 및 진공 가압 브레이징되는 냉각채널 접합부를 모사할 수 있는 시편을 설계 및 제작하고 파단 시험을 수행하였다. 두 시편 모두 접합부가 아닌 모재에서 파단이 발생하였다. 그리고 해석을 통하여 예측된 파단 부위와 변형율이 시험 결과와 잘 일치하였다.

소형 액체로켓엔진용 예연소기 냉각채널 유동해석 (Numerical Study of the Cooling Channel of the Preburner for a Small Liquid Rocket Engine)

  • 문인상;신강창
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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    • pp.21-24
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    • 2010
  • 다단연소사이클 액체로켓엔진에 사용 가능한 예연소기의 냉각채널에 대한 해석연구를 진행하였다. 해석에 사용된 예연소기는 내부압력이 210 bar로서 한국형발사체에 사용되는 엔진이나 30톤급 엔진에 비해 매우 높으며 개방형 엔진의 가스발생기와는 달리 연소실 내부에서 산화제 과잉 연소를 하기 때문에 냉각방법이 까다롭고 또 그만큼 냉각채널의 역할이 매우 중요해진다. 이를 위해 매우 다양한 형상의 냉각채널이 고안되었고 이들의 유동해석을 실시하였다. 결과적으로 냉각채널의 차압을 목표 차압 아래로 달성할 수 있었다.

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케로신 연료 및 코킹에 대한 검토 (Review on Kerosene Fuel and Coking)

  • 이준서;안규복
    • 한국추진공학회지
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    • 제24권3호
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    • pp.81-124
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    • 2020
  • 액체산소/케로신 액체로켓엔진에서 케로신은 추진제일 뿐만 아니라 3,000 K 이상의 연소가스로부터 연소실 벽면을 보호하기 위한 냉각제 역할도 수행한다. 케로신은 냉각채널을 통과하면서 높은 온도에 노출되기 때문에 열과 관련한 화학반응이 일어나 탄소 과잉 고체가 침전되는 현상이 발생할 수 있다. 이러한 케로신의 열/유체 특성 시험 데이터는 재생냉각 연소실 설계에 필수적이다. 본 논문에서는 재생냉각채널과 케로신에 관련된 해외 연구를 조사하였다. 탄화수소 연료에 대한 전반적인 정보를 시작으로, 냉각채널 벽면에 발생하는 퇴적 현상, 이에 대한 원인/연구결과, 케로신 코킹 시험 장치/예방 방법 등을 체계적으로 정리하고자 하였다.

SMES용 kA급 초전도도체의 운전전류 특성 (Operating Current Characteristics of a kA Class Conductor for a SMES device)

  • 류경우;최병주;김해종;성기철
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 2003년도 학술대회 논문집
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    • pp.3-6
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    • 2003
  • We have developed a small-sized superconducting magnetic energy storage (SMES) device, which provides electric power with high quality to sensitive electric loads. In large magnets such as the SMES magnets the stability, which is determined by several factors, e.g. conductors cooling condition and operating current, magnets winding structure, is a crucial problem. The effect of the cooling condition, the copper ratio, and the conductor's size upon the recovery currents was investigated experimentally. The results indicate that the recovery current characteristics of the strands vary considerably according to their insulation method. In the fully insulated strands with a low copper ratio, the recovery current densities range from 10 to 20 % of their engineering critical current densities. The recovery current density of the 30-conductor with a cooling channel is about a factor of 1.8 higher than that without a cooling channel.

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엇갈린 V-형 리브가 부착된 냉각유로에서의 열유동 수치해석 (NUMERICAL SIMULATION OF FLOW AND HEAT TRANSFER IN A COOLING CHANNEL WITH STAGGERED V-SHAPED RIBS)

  • 명현국;김광용
    • 한국전산유체공학회지
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    • 제13권4호
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    • pp.107-113
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    • 2008
  • The present study numerically simulates the flow and heat transfer characteristics of rib-induced secondary flow in a square cooling channel with staggered V-shaped ribs, extruded on both walls. The rib pitch-to-height ratio (p/h) varies from 2.8 to 10 with the rib-height-to-hydraulic diameter ration (h/$D_h$)of 0.07 and the Reynolds number of 50,000. Shear stress transport (SST) turbulence model is used as a turbulence model. Computational results show that complex secondary flow patterns are generated in the channel due to the snaking flow in the streamwise direction for all tested cases. In the range of p/h=5 to 10 the staggered V-shaped rib gives about 3 times higher heat transfer augmentation than the reference smooth pipe with high heat transfer on both front side and the area around the leading edge of the ribs, while the former cases give about 18 times higher streamwise pressure drop than the latter ones. However, for the thermal performances, based on the equal pumping power condition, the case of p/h=2.8 gives the best result among three cases, mainly due to relatively low streamwise pressure drop, although it gives relatively low heat transfer augmentation.

Exergetic analysis for optimization of a rotating equilateral triangular cooling channel with staggered square ribs

  • Moon, Mi-Ae;Kim, Kwang-Yong
    • International Journal of Fluid Machinery and Systems
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    • 제9권3호
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    • pp.229-236
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    • 2016
  • Exergetic analysis was introduced in optimization of a rotating equilateral triangular internal cooling channel with staggered square ribs to maximize the net exergy gain. The objective function was defined as the net exergy gain considering the exergy gain by heat transfer and exergy losses by friction and heat transfer process. The flow field and heat transfer in the channel were analysed using three-dimensional Reynolds-averaged Navier-Stokes equations under the uniform temperature condition. Shear stress transport turbulence model has been selected as a turbulence closure through the turbulence model test. Computational results for the area-averaged Nusselt number were validated compared to the experimental data. Three design variables, i.e., the angle of rib, the rib pitch-to-hydraulic diameter ratio and the rib width-to-hydraulic diameter ratio, were selected for the optimization. The optimization was performed at Reynolds number, 20,000. Twenty-two design points were selected by Latin hypercube sampling, and the values of the objective function were evaluated by the RANS analysis at these points. Through optimization, the objective function value was improved by 22.6% compared to that of the reference geometry. Effects of the Reynolds number, rotation number, and buoyancy parameter on the heat transfer performance of the optimum design were also discussed.

엇갈린 V-형 리브가 부착된 냉각유로에서의 열유동 수치해석 (NUMERICAL SIMULATION OF FLOW AND HEAT TRANSFER IN COOLING CHANNEL WITH A STAGGERED V-SHAPED RIB)

  • 명현국;김광용
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.125-130
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    • 2008
  • The present study numerically simulates the flow and heat transfer characteristics of rib-induced secondary flow in a cooling channel with staggered V-shaped ribs, extruded on both walls. The rib pitch-to-height ratio (p/h) varies from 2.8 to 10 with the rib-height-to-hydraulic diameter ration ($h/D_h$) of 0.07 and the Reynolds number of 50,000. Shear stress transport (SST) turbulence model is used as a turbulence model. Computational results show that complex secondary flow patterns are generated in the duct due to the snaking flow in the streamwise direction for all tested cases. In the range of p/h=5 to 10 the staggered V-shaped rib gives about 3 times higher heat transfer augmentation than the reference smooth channel with high heat transfer on both front side and the area around the leading edge of the ribs, while the former cases give about 2.5 times higher streamwise pressure drop than the latter ones. Consequently, for the thermal performances, based on the equal pumping power condition, the staggered ones give about 2 times higher values than the latter ones with more uniform heat transfer distribution.

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대향류 핀삽입형 재생증발식 냉방기 연구 (Study on the Counterflow Regenerative Evaporative Cooler with Finned Channels)

  • 최봉수;홍희기;이대영
    • 설비공학논문집
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    • 제20권7호
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    • pp.447-454
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    • 2008
  • The regenerative evaporative cooler(REC) is to cool a stream of air using evaporative cooling effect without an increase in the humidity ratio. In the regenerative evaporative cooler, the air can be cooled down to a temperature lower than its inlet wet-bulb temperature. Besides the cooling performance, for practical application of the regenerative evaporative cooler, the compactness of the system is also a very important factor to be considered. In this respect, three different configurations, i.e., the flat plate type, the corrugated plate type, and the finned channel type are investigated and compared for the most compact configuration. The optimal structure of each configuration is obtained individually to minimize the volume for a given effectiveness within a limit of the pressure drop. Comparing the three optimal structures, the finned channel type is found to give the most compact structure among the considered configurations. The volume of the regenerative cooler can be reduced to 1/8 by adopting the finned channel type as compared to that of the flat plate type.