• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
• /
• 2010.03b
• /
• pp.33-33
• /
• 2010

최근 개발된 식물성 절연유는 광유에 비해 약 3배 정도 점도가 높아 변압기 냉각에 상당한 영향을 주게 된다. 뿐만 아니라 식물유의 유동점은 $-20^{\circ}C$이하로 광유에 비해 높은 것이 단점이다. 온도가 낮을수록 점도가 급격히 높아질 뿐만 아니라 유동점에 도달할수록 응고되어 가기 때문에 겨울철에 변압기 부하가 낮거나, 교체 운전 초기에 냉각 특성 및 전기적 특성의 변화를 가져올 수 있다. 이에 따라 식물성 절연유를 유동점에 가까운 온도로 냉각한 후 절연파괴전압을 측정하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.31 no.8
• /
• pp.69-76
• /
• 2003

For stable combustion and safety of a structure of the propulsion system, a cooling system to the liquid rocket engine should be incorporated. In this study, Eulerian-Lagrangian scheme for two phase combustion, nongray radiation and soot formation effect, and film-wall interaction have been introduced to study the effect of film cooling. After briefly introducing the governing equation, combustion characteristics with change of wall temperature has been investigated by varying such parameters as fuel mass fraction for film cooling, diameter of the fuel droplet, overall mixture fraction of oxygen to fuel. Also, radiative heat flux is compared with the conductive one at the combustor wall.

• Journal of the KSME
• /
• v.31 no.4
• /
• pp.389-400
• /
• 1991

압정가공은 열간압정과 냉간압정으로 크게 나눌 수 있으며, 압정기와 피압정재의 종류에 따라 서도 분류한다. 열간압정에서는 알루미늄과 알루미늄합금을 제외하고는 종래에 오직 물만이 냉각겸 윤활제로 사용되어 왔다. 그러나 근년에 와서 열간압정에서도 윤활유를 사용하게 됨으 로서 롤(roll)의 수명연장, 전력소비량의 저감 및 사상(finishing) 강판의 표면품질향상등에 극히 유효하다는 것을 인식하게 되었다. 한편 냉각압정에서는 압정유를 사용해 온 것이 100년 가까이 되는 역사가 있고, 특히 과거 십 수년간에는 상당히 광범위하게 연구가 이루어져서, 많은 실적을 갖게 되었다. 예컨대, 석도원판으로 대표되는 박판압정에 있어서는 고속고압하에서 판의 형상 및 표면정쟁성 향상은 물론이고 저온(에너지 절감, 작업성 개선) 저농도사용(원단위감소)이 이루어 지고, 나아가 장수명(액의 오염이 적은 것)의 압정유가 개발되었다. 또한 마대강 압정에 있어 서는 고윤활이면서도 ECL(electric cleaning line)의 성략도 가능한 압정유 즉 밀크린시트(mill clean sheet) 압정유의 연구도 활발히 진행되고 있다. 압정유의 역할을 살펴보면 열간 또는 냉 간을 불문하고, 롤과 재료간의 감마작용이 주가 되지만 기타 실용적으로는 (1)냉각성 (2)판의 끝맺음(finishing)성 (3)선정선 (4)방장성,비부식성 (5) 내노화성 (6) 오일.스테인(oil stain) (7) 급 유성 (8)액관리성 (9)비수처리성 10) 안전위생 (11)경제성 등을 열거할 수 있다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.6 no.4
• /
• pp.1-6
• /
• 2002

A numerical heat transfer analysis and the structural analysis were performed for the design of sub-scale combustion chamber's coolant passage. The heat flux through the combustion chamber wall was estimated by 2-D heat transfer analysis of compressible hot gas and the result was applied as a thermal boundary condition of 3-D analysis. The heat flux estimated by the present method agreed well with the experimental correlation and proved to be insensitive to cooling condition. So the same thermal boundary condition was applied for various operating conditions. The maximum temperature of combustion chamber wall was predicted by 3-D analysis for single coolant passage and the result will be used for the development of a regeneratively cooled combustion chamber. Also estimated were the stress distribution and structural safety of coolant passage through the static structural analysis.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.13 no.3
• /
• pp.419-423
• /
• 1989

The laboratory quench method used in this study is based on plunging a silver cylinder heated to 800.deg. C in to mineral oil and vegetable at given temperature. Experimental apparatus and measuring method followed Korean Industrial Standard. Colling curves at the boundary of the cylinder measured by a silver-alumel thermocouple is recorded throughout the quenching period. Using the cooling curves, the coolingability of the quenching oils at various temperatures were compared and discussed.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.24 no.5
• /
• pp.1-12
• /
• 2020

In this paper, the heat transfer characteristics of Jet A-1, which is used as a coolant and fuel in a regeneratively cooled thrust chamber, were experimentally studied. By varying the applied current for heating the cooling channel, the simulated specimen diameter, the specimen outlet pressure and the coolant flow rate, the wall temperatures of the specimen and the Jet A-1 temperatures at the specimen inlet/outlet were measured. It was found that the specimen diameter and the flow rate were important factors for the characteristics of heat transfer and the outlet pressure did not affect the performance of heat transfer. The results of the heat transfer experiments were compared with the previous Nusselt number empirical equations and novel Nusselt number empirical equations were finally derived.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.34 no.10
• /
• pp.885-891
• /
• 2010

Thermal management is important for enhancing the performance and durability of polymer electrolyte membrane fuel cells (PEMFCs) and is taken into account in the design of PEMFCs. In general, cooling pates with circulating liquid coolant (water) are inserted between several unit cells to exhaust the reaction heat from PEMFCs. In this study, computational fluid dynamics (CFD) simulations were performed to characterize the uniform cooling performance of parallel multipass serpentine flow fields (MPSFFs) that were used as coolant flow channels in PEMFCs. The cooling performances of conventional serpentine and parallel flow fields were also evaluated for the purpose of comparison. The CFD results showed that the use of parallel MPSFFs can help reduce the temperature nonuniformity, and thus, can favorably enhance the performance and durability of PEMFCs.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.47 no.12
• /
• pp.881-889
• /
• 2019

The pre-swirl system is the device that minimizes energy loss of turbine cooling airflow from the stationary parts into rotating parts. In this paper, an off-design analysis was conducted for the ambient air temperature and turbine load conditions. The discharge coefficient was constant for ambient air temperature and turbine load. However, adiabatic effectiveness was increased. This is due to the volume flow rate. The volume flow rate was increased at higher ambient temperature and higher turbine load. It means that the volume of cooling air was increased and the cooling performance of the air was improved. Consequently, adiabatic effectiveness increased by 30.46% at 100% turbine load compared to 20% turbine load. And increased by 18.42% at 55℃ ambient air temperature compared to -20℃ ambient air temperature.

• Nuclear Engineering and Technology
• /
• v.20 no.1
• /
• pp.35-46
• /
• 1988

The prediction of clad surface temperatures is important to the design and the safety anlaysis of nuclear reactor. The accurate prediction requires the detailed knowledge of the flow structure and heat transfer, which is complicate due to anisotropic turbulent phenomena. A two-equation model including anisotropic eddy viscosity model is applied to forecast the velocity distribution. And the temperature field is calculated with uniform wall heat flux. The Galerkin's weighted residual finite element method has been used to calculate the turbulent quantities right up to the wall. The numerical results show good agreement with available data and that turbulence anisotropy strongly affects on the mean flow and thus the temperature field. And Nu-P/D correlation is established for sodium coolant in close-packed equilateral triangular bundle in the P/D range of 1.05 to 1.30.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.9 no.3
• /
• pp.35-41
• /
• 2001

In recent applications, map controlled thermostat has been adapted to optimize engine cooling system and vehicle cooling system. First of all, this strategy is focused on improving fuel consumption rate and reducing emissions, especially unburned hydrocarbon. The object can be obtained through controlling engine metal temperature by varying engine coolant temperature with engine load and speed. To achieve this goal, it is necessary to understand the characteristics of engine metal temperature and heat rejection rate to coolant. From the results of tested engines, it is obvious that fuel consumption rate has more dominant effect on engine metal temperatures than the corresponding engine power does. Also, Re-Nu relation which shows heat rejection rate to coolant in function of air-fuel mixture and engine specifications has been studied. Also, the empirical Re-Nu relation at full loaded engine was developed.