• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.12
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• pp.1293-1300
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• 2011

The configurations of the evaporator and condenser of a water chiller can be determined from the trade-off between the heat transfer area, which is related to the capital cost and the pressure drop, which is associated with the operational cost. In this study, the design of the water chiller focused on minimizing the water pressure drop of both condenser and evaporator for given cooling capacity and requirements. Commercial enhanced tubes were employed to simulate real-life conditions. The results of the present analysis were compared with those obtained by HTRI software for verifying them. The results indicated that a reduction in the water pressure drop, which is associated with the short length of a tube, can be effected by decreasing the number of tube passes and increasing the number of tubes and the tube diameter. However, using a large number of tubes with smaller diameters can reduce the capital cost because the tubes are short. The reduction of the capital cost is due to the fact that a small-diameter tube has low internal thermal resistance and hence contributes to a decrease in the overall thermal resistance per unit length.

• Journal of Advanced Marine Engineering and Technology
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• v.28 no.3
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• pp.397-404
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• 2004

냉각탑이란 석유화학플랜트, 철강플랜트 등과 같은 생산 공정이나 냉동기를 비롯한 각종 기계장치에서 발생된 열을 수냉식 열 교환장치에서 물로 직접 냉각시킬 때 공정유체의 열을 전달받아 데워진 물을 대기의 공기와 직접 접촉시켜 물의 증발 잠열을 이용하여 원하는 온도로 냉각시켜 주는 기계장치이다.(중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.189-192
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• 2004

Test Facility for hot firing test of small size liquid rocket engine has been developed to research the cooing characteristics of kerosene for cylinder part especially. Propellants for the tests are kerosene and liquid oxygen as fuel and oxidizer respectively and they are fed by gaseous nitrogen. The engine components used hot firing test except for cylinder are cooled by tap-water. Valves for supply of propellants and coolants are controlled by pneumatically. System control and data recording are conducted automatically.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.187-192
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• 2006

The combustion performance tests of a 30 tonf-class full-scale combustion chamber performed with water as a coolant were described. The combustion chamber has chamber pressure of 53bara and propellant flow mass rate of 90kg/s. Since it was first firing test for 30tonf-class combustion chamber using channel cooling, water coolant mass flow .ate of 35kg/s and 18kg/s were performed which correspond to 110% of kerosene design volume flow rate and equivalent cooling performance of kerosene. The test results are described and the results showed that the water cooling performance of this combustion chamber is sufficient and the firing test is feasible using the kerosene as a coolant.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.169-174
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• 2006

This paper is related to a design of high pressure sub-scale combustor with regenerative reeling. As a previous step for the evaluation of thermal heat flux, a similar combustor with cooling water was manufactured. Design conditions with high combustion efficiency and cooling performance were verified through the hot firing tests of the water-cooled high pressure combustor. Finally the regeneratively cooled high pressure combustor has been designed based on these data. After manufacturing it, its practical utility will be tested and verified through hot firing tests.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.3
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• pp.1-6
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• 2007

A 3-tonf-class high pressure sub-scale combustor was designed and manufactured to study the performance improvement of combustor. The combustor consists of a combustion chamber with film cooling, thermal barrier coating and water cooling channels to prevent thermal demage of the hardware and an injector head with 37 coaxial swirl injectors. Hot-firing tests were carried out at the design point with varying flow rate for film cooling. The test result revealed that the increase of film cooling flow rate decreases the combustion performance, but in the cases of similar film cooling flow rates, the combustion performance is dependent on the mixture ratio of main injector excluding the film cooling flow rate.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.1
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• pp.61-67
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• 2015

The cooling of hot exhaust gas is an important issue for the construction of combustor test facility. Water spray is an effective method for exhaust gas cooling due to its large latent heat in process of evaporation. In this study, 1-D analysis has been performed based on continuity, energy conservation, and saturated vapor property to understand water spray cooling of combustion gas. In the exhaust duct of combustor test facility, the injected water decreases combustion gas temperature, and evaporates in the combustion gas. However, some of the injected water is collected in the sump due to condensation. The evaporation of water helps combustion gas cooling, but causes pressure increase inside the exhaust duct due to increase of vapor pressure. These phenomena has been analyzed by 1-D modeling in this study. From 1-D analysis, the adequate mass flow rate of water spray to cool combustion gas and to avoid excessive pressure rise inside the exhaust duct has been decided.

• Proceedings of the Korean Radioactive Waste Society Conference
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• 2009.06a
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• pp.63-64
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• 2009

변환시설의 해체 시 발생한 해체폐기물은 2009년 현재까지 약 354톤이며, 이들 중 탱크, 배관, 반응기, 펌프류 동의 해체금속폐기물이 약 191톤으로 54% 를 차지하고 있다. 이들 해체금속폐기물은 제염 처리공정을 통하여 전량 자체처분폐기물로 전환시키는 것을 목표로 두고 있다. 이는 오염된 금속류를 효과적으로 제염한 다음 자체처분시킴으로서 방사성폐기물에 대한 처분비용을 저감할 수 있기 때문이다. 해체금속폐기물 중 스테인레스강 해체폐기물은 질산 용액을 사용한 초음파화학제염공정으로 제염한 후 자체처분폐기물로 53톤을 전환하였다. 탄소강 해체물의 경우 스팀제염공정으로 제염한 결과 제영 효율은 좋았으나 변환시설 가동 중 유지 보수를 위하여 페인팅을 하였던 해체물의 경우 페인트를 제거하지 않을 경우 스팀제염장치로는 제염이 안 되었다. 탄소강 해체금속폐기물은 약 117톤 발생하였으며, 이들 중 모터, 펌프 등을 제외한 제염 대상 폐기물은 약 80톤이며, 이들을 용융 제염 및 감용을 위하여 기초 연구를 수행한 결과를 바탕으로 약 180kg/batch 용량의 금속용융제염 설비를 제작 설치하여 탄소강 해체금속폐기물 용융제염 처리를 수행 중에 있다. 금속용융은 장치가 간단하고 폐기물 처리량이 비교적 적고 단속적인 운전에 매우 효과적인 고주파 유도로를 사용하였다. 용융장치는 고주파 발진장지와 용해로체로 구성된 고주파 유도설비와 냉각계통으로 구성된다. 고주파발진장치는 철제 200kg을 용해할 수 있는 용량을 갖추었으며, 실험 및 실제 처리 등 용해로체의 크기 변경이 필요할 경우에는 고주파발진기의 출력 주파수를 변경할 수 있게 하였다. 용융 장치의 발진기 부분의 입력전원은 3상, 440V, 60Hz 이며, 출력전원은 200kW, 출력주파수는 lkHz, 3kHz, 5kHz로 구성되어 있으며, 회당 180kg 의 폐기물을 용융할 시에는 3kHz로 고정하여 사용하였다. 용해로체 부분 중 고주파유도가열부는 heating coil 및 절연부로 구성되어 있고, 그 외 support frame과 lever로 구성되어 있다. 용해로체와 고주파 발진장치의 냉각을 위한 냉각설비는 냉각기와 냉매의 저장을 위한 저장조로 구성되어 있으며, 냉각기의 용량은 20RT 이다. 용융로체의 직경은 약 28cm로 크기가 큰 해체물의 장입이 어려워 작은 크기로 세절을 해야만 하며，용융로의 용량을 증가시킬 경우 해체물을 작은 크기로 세절하는 비용을 절감할 수 있을 것이다. 용융 중 시료 채취는 매 배치마다 수행하였으며, 그림3과 같은 시료 채취용 주형 틀에 국자모양의 채취기로 채취하였다. 해체물의 용융시 ingot를 생성하기 위해서 주형틀에 용융물을 장입하기 전 시료를 채취하였다 그림4는 생성된 ingot이며, 이들의 방사능 농도는 배치마다 차이는 있지만 최대 0.05 Bq/g 이하로 나타나 자체처분 폐기물로 전량 전환 가능하였다 그림5 는 해체물에 함유된 우라늄과 불순물을 제거한 슬래그로 방사능농도는 약 12Bq/g 으로 나타났으며, 이들의 발생량은 약 3wt% 정도로 폐기물 발생량이 작았다. 따라서 금속폐기물의 경우 용융제염으로 처리할 경우 폐기물 발생량을 최대로 줄일 수 있어 처리 효율이 기타 처리 공정보다 효율적인 것으로 판단된다.

• Korean Chemical Engineering Research
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• v.56 no.3
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• pp.388-403
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• 2018

We investigated design requirements of vent lines for Sodium-Water Reaction Pressure Relief System of Prototype Generation-IV Sodium-Cooled Fast Reactor. We developed design requirements of areas of the rupture disks of the steam generator, a diameter of the gas vent line of the sodium dump tank, a diameter of the gas vent line of the water dump tank, a diameter of the water dump line of the steam generator. With the design requirements, we calculated the time to vent fluid inside the steam generator and analyzed the transient pressure behavior, also evaluated the close pressure value of the isolation valve of the water dump line. Our results are expected to be used as basis information to design Sodium-Water Reaction Pressure Relief System of Prototype Generation IV Sodium-Cooled Fast Reactor.

• Aerospace Engineering and Technology
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• v.3 no.1
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• pp.197-204
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• 2004

A design of regenerative cooling system of 30 ton level thrust combustion chamber for ground test has been performed. The 1-D design code has been validated by comparing with the heat flux of the NAL calorimeter for high chamber pressure and water-cooling performance of the ECC engine of MOBIS. The present design code has been confirmed to predict accurately the heat flux and water-cooling performance for high chamber pressure condition. The maximum hot-gas-side wall temperature is predicted to be about 720 K without thermal barrier coating and the coolant-side wall temperature is less than the coking temperature of RP-1. The coolant temperature rises nearly 100 K with thermal barrier coating when Jet-A1 is used as coolant.