• 한국추진공학회지
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• 제7권1호
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• pp.10-17
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• 2003

액체 로켓의 추진제탱크 가압을 위해 사용되는 극저온 액체헬륨의 정상상태 및 천이상태 열유동 해석을 수치적으로 수행하였다 벽면에서의 단열 및 비단열 조건에 대한 정상 해석을 통하여 설계유량 및 설계유속을 만족시키는 헬륨 배관의 내경 및 압력손실, 온도변화 등을 조사하였으며 특히 단열조건에서도 헬륨의 온도는 주울-톰슨계수의 영향에 의해 증가하는 경향이 있음을 밝혀내었다. 그리고 국부적인 열유입 있을 경우에의 관내 헬륨의 온도 및 압력의 시간적 변화를 천이해석을 통하여 고찰하였으며 열유입부의 밀도 감소에 의한 열유입부 후단부의 속도 증가량을 예측하였다.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1997년도 춘계학술발표회논문집(1)
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• pp.489-494
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• 1997

A comparative transient analyses were performed for oxide and nitride cores or a large (3000 MWt), pool-type, liquid-metal-cooled reactor (LMR). The study was focused on three representative accident initiators with failure to scram : the unprotected loss-of-flow (ULOF), the unprotected transient overpower (UTOP), and the unprotected fast transient overpower (UFTOP). The margins to fuel melting and sodium boiling have been evaluated for these representative transients. The results show that there is an increase in safety margin with nitride core which maintains the physical dimensions of the oxide core.

• 한국분무공학회지
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• 제27권4호
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• pp.181-187
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• 2022

For carbon neutrality, direct-injection hydrogen engines are attracting attention as a future power source. It is essential to estimate the transient injection rate of hydrogen for the optimization of hydrogen injection in direct injection engines. However, conventional injection rate measurement techniques for liquid fuels based on the injection-induced fuel pressure change in a test section are difficult to be applied to gaseous fuels due to the compressibility of the gas and the sealing issue of the components. In this study, a momentum flux measurement technique is introduced to obtain the transient injection rate of gaseous fuels using a force sensor. The injection rate calculation models associated with the momentum flux measurement technique are presented first. Then, the volumetric injection rates are estimated based on the momentum flux data and the calculation models and compared with those measured by a volumetric flow rate meter. The results showed that the momentum flux measurement can detect the injection start and end timings and the transient and steady regimes of the fuel injection. However, the estimated volumetric injection rates showed a large difference from the measured injection rates. An alternative method is suggested that corrects the estimated injection rate results based on the measured mean volumetric flow rates.

• Journal of Welding and Joining
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• 제13권2호
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• pp.132-138
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• 1995

Rene80 superalloy was liquid phase diffusion bonded by using boron(B) as an insert material, where B has high diffusivity and higher melting point as an insert material. Bonding procedure and bonding mechanism of Rene80/B/Rene80 joint were investigated. As results, liquid metal was produced by solid state reaction between base metal and insert material on bonding zone. The liquid metal was produced preferentially at the grain boundary. Except for production of liquid metal, other bonding procedure was nearly same as TLP(Transient Liquid Phase) bonding. Bonding time, however, was reduced compared to prior result of TLP bonding. By bonding S.4ks at l453K, Ren80/B/Rene80 joint was isothermally solidified and homogenized where thickness of insert material was 7.5.mu.m.

• Journal of Welding and Joining
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• 제13권4호
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• pp.147-154
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• 1995

In order to study the bonding mechanism of Ni/B/Ni transient liquid phase bonding system, width of liquid layers were calculated, where in this system melting point of insert material(B) is higher than bonding temperature and melting point of base metal(Ni). Caclulated values were compared with experimental ones which were measured by bonding Ni/B/Ni system at 1433-1474K under vacuum atmosphere. As results, the width of initial liquid layer of Ni/B/Ni system was calculated as $W_{IL}$ = $W_{o}$[1 + {2.100..rho.$_{S/}$ ( $X_{3}$ + $X_{4}$)..rho.$_{Ni}$ }-.rho.$_{S/}$.rho. Ni/], and it was nearly same with experimental values. Maximum width of liquid layer, width of liquid layer during isothermal solidification and isothermal solidification time were calculated also.o.o.o.

• 대한기계학회논문집B
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• 제27권11호
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• pp.1572-1578
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• 2003

Particle Image Thermometry(PIT) with liquid crystal tracers is used for visualizing and analysis of the bubbly flow in a vertical temperature gradient. Quantitative data of the temperature were obtained by applying the color-image processing to a visualized image, and neural-network was applied to the color-to-temperature calibration. This paper describes the method, and presents the transient mixing temperature patterns of the bubbly flow.

• 마이크로전자및패키징학회지
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• 제28권2호
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• pp.71-79
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• 2021

본 연구에서는 고온 대응 EV (Electric Vehicle) 전력반도체 칩 접합용 Sn-Ni 페이스트의 제조 및 특성 평가 연구가 수행되었다. Sn-Ni 페이스트의 Sn과 Ni 함량에 따른 TLPS (Transient Liquid Phase Sintering) 접합부 미세 조직 변화 관찰 결과, Sn-20Ni (in wt.%)의 경우에는 Ni 분말의 부족, 그리고 Sn-50Ni의 경우에는 Ni 분말의 과다 포함에 따른 Ni 뭉침 현상이 관찰되었다. Sn-30Ni과 Sn-40Ni의 경우에는 TLPS 접합 공정 후 상대적으로 치밀한 접합부 단면 미세 구조 조직을 가짐을 확인하였다. TLPS 접합 공정 후 접합부 시편의 DSC 열 분석 결과로부터 TLPS 접합 공정 반응 동안 Sn과 Ni의 충분한 반응이 일어남을 확인하였으며, 접합 공정 후 접합부에는 Sn이 남아 있지 않음을 확인하였다. 추가적으로 공정 온도 변화에 따른 Sn-30Ni TLPS 접합부의 계면반응 및 기계적 강도 시험이 수행되었다. TLPS 접합 공정 후 접합부는 Ni-Sn 금속간화합물과 반응하고 남은 Ni 분말들로 구성되었으며, 접합 온도가 증가함에 따라 접합부 칩 전단강도는 증가하였다. 솔더링 온도와 유사한 270 ℃의 접합 온도에서 30분 동안의 TLPS 접합 공정 수행 후 약 30 MPa의 높은 칩 전단 강도 값을 얻었다.

• 설비공학논문집
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• 제10권4호
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• pp.495-507
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• 1998

The transient characteristics of a 4.0㎾ inverter driven heat pump was investigated by theoretical and experimental studies. The heat pump used in this study consists of a high side scroll compressor and $\Phi$7 compact heat exchangers with two capillary tubes. A series of tests was peformed to examine the transient characteristics of heat pump in heating and cooling mode when the operating speed was varied from 30Hz to 102Hz. One of the major issues that has not been addressed so far is transient characteristics during speed modulation. A cycle simulation model has been developed to predict the cycle performance under frequency rise-up conditions, and the results of theoretical study were compared with the results of experimental study. The theoretical model was driven from mass conservation and energy conservation equations to predict the operation points of refrigerant cycle and the performances at various operating speeds. For transient conditions, the simulated results are in good agreement with the experimental results within 10%. The transient cycle migration of the liquid state refrigerant causes a significant dynamic change in system. Thus, the migration of refrigerant is the most important factor whenever An experimental analysis is performed or A simulation model is developed.

• 한국의류학회지
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• 제25권1호
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• pp.61-70
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• 2001

As important factors determining human sensorial comfort, liquid moisture management and surface properties of heat resistant workwear materials were examined. To figure out liquid moisture management properties of the test materials, absorption capacity, rate of absorption, and evaporation properties were assessed. A modified GATS(Gravimetric Absorbency Testing System) was used to measure the liquid moisture accumulation associated with the wicking of liquid moisture from sweating skin. The GATS procedure measures demand wettability of materials to take up liquid in a direction perpendicular to the fabric surface and it was modified to incorporate a special test cell and cover to assess absorption behavior in the presence of evaporation. Fabric stiffness, smoothness, number and the length of surface fibers, and an estimate of the contact area between the skin and fabric surface were measured to characterize the mechanical and surface properties of the test materials. Also an estimate of the force with which a fabric clings to moist skin was made using as wet-cling index.

• 항공우주기술
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• 제4권2호
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• pp.142-152
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• 2005

액체로켓 엔진시스템 개발에 있어서 시동부터 정상상태까지의 시동특성은 안정된 시동의 재현성을 확보하여 신뢰도를 높이는 것과 과도상태의 시간을 단축하는 두 가지 목표를 만족하는 방향으로 전개된다고 할 수 있다. 특히 우리나라와 같이 액체로켓 엔진 개발의 초기단계에서는 엔진시스템 시험의 경험이 없어, 시동에서 정상상태까지 과연 어느 정도의 시간이 필요할 것인가에 대한 예측이 힘들 수밖에 없다. 본 연구에서는 터보펌프 공급식 액체로켓 엔진의 각 구성품의 모델을 구성하여 시동 과도 해석을 수행할 수 있는 프로그램을 완성하였다. 이 프로그램을 이용하여 25톤급 가스발생기 사이클 엔진에 대한 시동 특성을 조사하여 시동에서 정상상태에 이르는 시간을 계산하였으며, 비정상 상태의 엔진시스템의 동특성을 밝힐 수 있었다.