• 한국잠사곤충학회지
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• 제34권1호
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• pp.1-7
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• 1992

생식소동결로 누에 유전자원을 장기보존하기 위하여 생식소의 생식방법, 최적 동결속도 및 동해방지제, 동결매액의 과냉거점과 빙점, 생식소 동결시기 등, 생식소의 동결보존에 필요한 기초자료를 검토하여 다음의 결과를 얻었다. 1. 생식소 피다식 누에의 마취에 적합한 방법은 에칠에텔, 냉수침지, 저온접촉, 탄산가스 접촉 중 냉수에 10분간 침지처리하는 것이었다. 2. 누에난소를 동결함에 있어 그리세롤과 DMSO는 우수한 동결방지 효과를 보였으나 솔비톨은 부적합하였다. 3. 9-15%의 그리세롤을 첨가한 동결매액의 과냉거점과 빙점을 조사하여 잠열발생량을 2.0-4.5$^{\circ}C$로 억제할 수 있는 동결속도를 확인하였다. 4. 5령보다 4령누에에 난소를 이식하는 것이 난소생존 및 완성난형성 면에서 1.3-1.4배 유리하였다. 5. 동결난소를 이식받은 암나방을 수나방과 교미시켜 수정란을 얻었으며, 유전형질검정으로 이 수정난에서 발생한 차세대 누에가 동결난소에서 유래한 것임을 확인하였다. 6. 4령 또는 5령기에 동겨정소를 이식한 수나방과 교미한 정상 암나방 중 수정난을 산란한 것은 없었다.

• Journal of Advanced Marine Engineering and Technology
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• 제41권3호
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• pp.191-196
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• 2017

20세기에 대두된 HCFC나 CFC계의 냉매들의 환경에의 악영향을 극복하기 위하여 보다 환경 친화적인 이산화탄소와 같은 자연냉매에 대한 관심이 커지고 있다. 겨울철 대기의 열원을 이용하여 증발을 유도하는 이산화탄소 열펌프는 증발기의 온도가 높아 효율이 상대적으로 낮아지고, 130bar가 넘는 고압으로 인하여 열펌프 설비 부품들의 제작의 어려움이 따르게 된다. 본 연구는 보다 낮은 압력의 새로운 2단 팽창식 $CO_2$ 오토 캐스케이드 열펌프를 고안하여 이러한 단점들을 해소하고 보다 효율을 증가시키고자 하였다. 새로운 오토 캐스케이드 열펌프에 2단 팽창방식과 효과적인 냉각방식의 시스템 구성을 하여 혼합냉매인 $CO_2$ 와 R32를 적용하였다. 공정에 고압 70bar, 중간 팽창압은 25bar, 최종 저압은 10bar를 적용하여 해석한 결과, 현재의 오토 캐스케이드 열펌프 공정의 COP는 1.629이었으나, 개선된 중간 압력 25bar의 2단 팽창 오토 캐스케이드 공정은 2.332로 현재의 공정보다 43.15% 향상되었다. 또한 저압측 증발기의 온도도 $-10^{\circ}C$ 이하가 되어 찬 외기에도 증발이 용이하게 발생되는 공정이 되었다. 본 공정이 향후 $CO_2$ 열펌프의 성능계수를 보다 향상시키고 고압에 따른 부품 문제들의 해소에 기여할 수 있는 공정으로 분석되었다.

• Advances in aircraft and spacecraft science
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• 제4권1호
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• pp.37-52
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• 2017

Gas turbines operating in dusty or sandy environment polluted with micron-sized solid particles are highly prone to blade surface erosion damage in compressor stages and molten sand attack in the hot-sections of turbine stages. Commercial/Military fixed-wing aircraft engines and helicopter engines often have to operate over sandy terrains in the middle eastern countries or in volcanic zones; on the other hand gas turbines in marine applications are subjected to salt spray, while the coal-burning industrial power generation turbines are subjected to fly-ash. The presence of solid particles in the working fluid medium has an adverse effect on the durability of these engines as well as performance. Typical turbine blade damages include blade coating wear, sand glazing, Calcia-Magnesia-Alumina-Silicate (CMAS) attack, oxidation, plugged cooling holes, all of which can cause rapid performance deterioration including loss of aircraft. The focus of this research work is to simulate particle-surface kinetic interaction on typical turbomachinery material targets using non-linear dynamic impact analysis. The objective of this research is to understand the interfacial kinetic behaviors that can provide insights into the physics of particle interactions and to enable leap ahead technologies in material choices and to develop sand-phobic thermal barrier coatings for turbine blades. This paper outlines the research efforts at the U.S Army Research Laboratory to come up with novel turbine blade multifunctional protective coatings that are sand-phobic, sand impact wear resistant, as well as have very low thermal conductivity for improved performance of future gas turbine engines. The research scope includes development of protective coatings for both nickel-based super alloys and ceramic matrix composites.

• 한국전산유체공학회지
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• 제18권1호
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• pp.58-62
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• 2013

Personal Rapid Transit (PRT) is the emerging personal transport vehicle operating on the loop automatically. The PRT system utilize the electrical power from super capacity or battery, it is important to manage the power or energy. In this regards, the management of high temperature occurred by the operation of system is significantly important to prevent from serious damage of component. In this study, we studied the adequate shape of underbody which can reduce the heat accumulation by pickup coil and condenser using natural air cooling. We suggested the additional air pathway, air inlet and flow separator to decrease the temperature of the heat source components. It was found that suggested system can decrease the temperature of PRT under body by 16% during the static mode and by 10% during the running mode at 30km/h. It is expected that the findings of this study will feed into final design of newly built Korean PRT vehicle.

• Corrosion Science and Technology
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• 제9권5호
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• pp.187-195
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• 2010

Hyper duplex stainless steels have been developed in Korea for the purpose of application to the seawater system of Korean nuclear power plants. This system supplies seawater to cooling water heat exchanger tubes, related pipes and chlorine injection system. In normal operation, seawater is supplied to heat exchanger through the exit of circulating water pump headers, and the heat exchanged sea water is extracted to the discharge pipes in circulating water system connected to the circulating water discharge lines. The high flow velocity of some part of seawater system in nuclear power plants accelerates damages of components. Therefore, high strength and high corrosion resistant steels need to be applied for this environment. Hyper duplex stainless steel (27Cr-7.0Ni-2.5Mo-3.2W-0.35N) has been newly developed in Korea and is being improved for applying to nuclear power plants. In this study, the physical & mechanical properties and corrosion resistance of newly developed materials are quantitatively evaluated in comparative to commercial stainless steels in other countries. The properties of weld & HAZ (heat affected zone) are analyzed and the best compositions are suggested. The optimum conditions in welding process are derived for ensuring the volume fraction of ferrite(${\alpha}$) and austenite(${\gamma}$) in HAZ and controlling weld cracks. For applying these materials to the seawater heat exchanger, CCT and CPT in weldments are measured. As a result of all experiments, it was found that the newly developed hyper duplex stainless steel WREMBA has higher corrosion resistance and mechanical properties than those of super austenitic stainless steels including welded area. It is expected to be a promising material for seawater systems of Korean nuclear power plants.

• 한국수소및신에너지학회논문집
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• 제23권4호
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• pp.300-309
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• 2012

Long endurance is a key issue in the application of unmanned aerial vehicles. This study presents feasibility test results when fuel cell system as an alternative to the conventional engine is applied for the power of the UAV after the 150W fuel cell system is developed and packaged to the 1/4 scale super cub airplane. Fuel cell system is operated by dead-end method in the anode part and periodically purged to remove the water droplet in flow field during the operation. Oxygen in the air is supplied to the stack by the two air blowers. And fuel cell stack is water cooled by cooling circuit to dissipate the heat generated during the fuel cell operation. Weight balance is considered to integrate the stack and balance of plant (BOP) in package layout. In flight performance test, we demonstrated 4 times standalone take-off and landing. In the laboratory test simulating the flight condition to quantify the energy flow, the system is analyzed in detail. Sankey diagram shows that electric efficiency of the fuel cell system is 39.2%, heat loss 50.1%, parasitic loss 8.96%, and unreacted purged gas 1.67%, respectively compared to the total hydrogen input energy. Feasibility test results show that fuel cell system is high efficient and appropriate for the power of UAV.

• 한국결정학회지
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• 제9권1호
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• pp.30-38
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• 1998

주파수 무게센서를 장착한 자동직경제어 방식에 의해 Bi12GeO20 단결정을 쵸크랄스키법으로 육성하였다. 회전속도에 따른 계면모양의 변화를 관찰하기 위해, 회전속도를 변화시키면서 육성한 결과, 23-21rpm에서 평평한 계면이 형성되었다. Bi2O3의 휘발에 의한 화학 양론적 조성으로부터 이탈에 따른 Bi4Ge3O12의 생성과 이로 인한 색 변화를 관찰하기 위해, Bi2O3의 함량을 0.1-1mol% 보충한 결과, 0.3mol% 증발 보상을 하였을 때, 내포물이 적은 연한 갈색의 광학용 단결정을 육성할 수 있었다. 이러한 성장조건 하에서 직경 25mm x 길이 70mm 인 거의 일정한 직경을 갖는 단결정이 육성되었고 결함밀도는 103개/cm2를 나타내었다. XRD및 TEM에 의해 단결정의 우선 성장방향을 측정한 결과<110>이었다.

• 천문학회보
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• 제46권2호
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• pp.45.1-45.1
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• 2021

Horizon Run 5 (HR5) is a cosmological hydrodynamical simulation which captures the properties of the Universe on aGpc scale while achieving a resolution of 1kpc. This enormous dynamic range allows us to simultaneously capture the physics of the cosmic web on very large scales and account for the formation and evolution of dwarf galaxies on much smaller scales. On the back of a remarkable achievement of this, we have finished to run follow-up simulations which have 2 times larger volume than before and are expected to complementary to some limitations of previous HR simulations both for the study on the large scale features and the expansion history in a distant Universe. For these simulations, we consider the sub-grid physics of radiative heating/cooling, reionization, star formation, SN/AGN feedbacks, chemical evolution and the growth of super-massive blackholes. In order to do this project, we implemented a hybrid MPI-OpenMP version of the RAMSES code, 'RAMSES-OMP', which is specifically designed for modern many-core many thread parallel systems. These simulation successfully reproduce various observation result and provide a large amount of statistical samples of Lyman-alpha emitters and protoclusters which are important to understand the formation and expansion history of early universe. These are invaluable assets for the interpretation of current ΛCDM cosmology and current/upcoming deep surveys of the Universe, such as the world largest narrow band imaging survey, ODIN (One-hundred-square-degree Dark energy camera Imaging in Narrow band).

• 한국초전도ㆍ저온공학회논문지
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• 제25권4호
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• pp.70-74
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• 2023

The Small Punch Test (SPT) was developed to evaluate the softening and embrittlement of materials such as power plants and nuclear fusion reactors by taking samples in the field. Specimens used in the SPT are very thin and small disk-shaped compared to specimens for general tensile test, and thus have economic advantages in terms of miniaturization and repeatability of the test. The cryogenic SPT can also be miniaturized and has a significantly lower heat capacity than conventional universal test machines. This leads to reduced cooling and warm-up times. In this study, the cryogenic SPT was developed by modifying the existing room temperature SPT to be cooled by liquid nitrogen using a super bellows and a thermal insulation structure. Since the cryogenic SPT was first developed, basic experiments were conducted to verify the effectiveness of it. For the validation, aluminum alloy 6061- T6 specimens were tested for mechanical properties at room and cryogenic temperature. The results of the corrected tensile properties from the SPT experiment results were compared with known room temperature and cryogenic properties. Based on the correction results, the effectiveness of the cryogenic SPT test was confirmed, and the surface fracture characteristics of the material were analyzed using a 3d image scanner. In the future, we plan to conduct property evaluation according to the development of various alloy materials.

• 한국해안해양공학회지
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• 제18권4호
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• pp.329-337
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• 2006

삼천포 화력발전소에서 냉각수로 이용되고 방류되는 해수를 이용한 소수력 발전소가 삼천포 해역에 건설되고 있다. 본 연구에서는 소수력 발전소가 건설되는 지점, 즉 방류수로 및 방류해역의 흐름을 관측하고 흐름특성을 분석하였다. 방류수로의 흐름은 냉각수 방류량에 의한 영향이 지배적이며, 공간적으로는 냉각수가 합류되는 Weir 상류구간, 합류된 냉각수가 방류수로를 통하여 배출되는 Weir 하류구간, 방류해역으로 구분할 수 있다. Weir 상류 지점은 측면에서 유입되는 냉각수로 인하여 유량이 점차 증가하나, 수로의 폭이 증가하기 때문에 수위 변화가 미미한 지역이며, Weir 하류지점은 월류된 냉각수가 사류(super-critical flow)구간을 거쳐서 수리학적 도약으로 인한 강한 연직방향의 요동을 보이며 방류해역으로 이동하는 구간이다. 한편, 방류수에 의한 영향으로 외해방향으로의 해수흐름이 형성되나 유속은 조위의 승강운동에 크게 영향을 받는 것으로 파악되었다. 또한, 방류해역의 조위는 통영 검조소에 비하여 평균조차는 약 10% 크게 나타나고 있으며, 파랑전파에 의한 영향은 미미한 정도로 파악되었다.