• 한국분무공학회지
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• 제4권3호
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• pp.8-14
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• 1999

The characteristics of the breakup process in supercritical spray is investigated during the injection of supercritical sulfur hexafluoride into dissimilar gases at supercritical pressures and subcritical temperature of the injected fluid. The visualization techniques used are backlighting and shadowgraph methods. The spray angles are measured and the breakup and mixing process are observed at near and supercritical conditions. The results show that spray angles are decreased with the in..ease of the ratio of density $(\frac{\rho_f}{\rho_g})$. At the supercritical temperature, the spray angles in atomization region are kept nearly constant such as the typical spray angle in gas injection. The mixing process is changed radically at the temperature where $\frac{d\rho}{dT}=\frac{1}{2}[\frac{d\rho}{dT}]_{max}$ at given pressure.

• 한국분말재료학회지
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• 제10권1호
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• pp.6-14
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• 2003

The purpose of the present study is to investigate the method decreasing debinding time as well as lowering operation condition than pure supercritical $CO_2$ debinding by using cosolvent or binary mixture of propane + $CO_2$. First method is to add cosolvent, such as n-hexane, DCM, methanol, 1-butanol, in supercritical $CO_2$. In case of adding cosolvent, we were found the addition of non-polar cosolvent (n-hexane) improves dramatically the binder removal rate (more than 2 times) compared with pure supercritical $CO_2$ debinding, second method is to use mixture of supercritical propane + $CO_2$, as solvent. In case of using mixture of supercritical propane + $CO_2$, the rate of debinding speeded up with increasing of pressure and concentration of propane at 348.15 K. It was found that addition of cosolvent (e.g., n-hexane, DCM) and binary mixture propane + $CO_2$ for supercritical solvent remarkably improved binder removal rate for the paraffin wax-based binder system, in comparison with using pure supercritical $CO_2$.

• 지구물리와물리탐사
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• 제7권1호
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• pp.25-32
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• 2004

We have carried out laboratory measurements of P-wave velocity and deformation strain during $CO_2$ injection into a porous sandstone sample, in dry and water-saturated conditions. The rock sample was cylindrical, with the axis normal to the bedding plane, and fluid injection was performed from one end. Using a piezoelectric transducer array system, we mapped fluid movement during injection of distilled water into dry sandstone, and of gaseous, liquid, and supercritical $CO_2$ into a water-saturated sample. The velocity changes caused by water injection ranged from $5.61\;to\;7.52\%$. The velocity changes caused by $CO_2$ injection are typically about $-6\%$, and about $-10\%$ for injection of supercritical $CO_2$, Such changes in velocity show that the seismic method may be useful in mapping $CO_2$ movement in the subsurface. Strain normal to the bedding plane was greater than strain parallel to the bedding plane during $CO_2$ injection; injection of supercritical $CO_2$ showed a particularly strong effect. Strain changes suggest the possibility of monitoring rock mass deformation by using borehole tiltmeters at geological sequestration sites. We also found differences associated with $CO_2$ phases in velocity and strain changes during injection.

• 한국분말재료학회지
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• 제21권6호
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• pp.407-414
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• 2014

The powder injection molding process having advantages in manufacturing three-dimensional precision parts essentially requires a debinding process before sintering to remove the binders used for preparing feedstock. In this study, powder injection molding of translucent alumina was performed, and carbon dioxide ($CO_2$) is used as a supercritical fluid that makes it possible to remove a large amount of binder, which is paraffin wax. The relationship between the optical property of translucent alumina and the debinding condition (temperature and pressure) of supercritical $CO_2$ was investigated. As temperature and pressure increased, extraction rate of the binder showed rising tendency and average grain size after sintering process was relatively fine. On the other hand, optical transmittance was reduced. As a result, the debinding condition at $50^{\circ}C$ and 20 MPa that represents the lowest extraction rate, $8.19{\times}10^{-3}m^2/sec$, corresponds to the largest grain size of $14.7{\mu}m$ and the highest optical transmittance of 45.2%.

• 청정기술
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• 제18권2호
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• pp.155-161
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• 2012

본 연구의 목적은 분말 사출성형 공정에서 초임계유체를 이용하여 사출성형체로부터 결합제를 효율적으로 제거하는 것이다. 두께 1~2 mm 정도의 얇은 성형체의 경우는 기존의 초임계 추출공정을 이용하여 초기부터 온도, 압력이 높은 조건에서도 아무런 결함 없이 단시간 내에 결합제를 제거할 수 있지만, 시편이 두꺼워질수록 초기에 균열이 발생하기 때문에 일정 공정조건에서는 한계가 있다. 따라서 초기에는 낮은 공정조건에서 시작하여 단계별로 온도와 압력을 상승시키는 초임계 가변 조건 탈지공정을 연구하였다. 두께 1~4 mm의 세라믹 사출성형체 시편을 사용하여 여러 가지 초임계 조건에서 탈지실험을 수행하여 두꺼운 세라믹 사출성형체에 균열이 생기지 않으면서 가장 추출수율이 높은 가변조건 공정의 초기조건을 설정하였다. 이렇게 설정한 초기조건을 시작으로 직경 10 mm, 두께 4 mm의 두꺼운 세라믹 사출성형체 시편을 온도 333.15~343.15 K, 압력 12~27 MPa, $CO_2$ 유량 0.5~1.0 L/min 범위에서 단계별로 상승시켜 최종적으로는 5시간동안 95% 이상의 파라핀 왁스 결합제를 제거할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.597-600
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• 2010

극저온 액체 질소 제트 유동의 아임계 및 초임계 특성을 파악하기 위한 실험을 수행하였다. 단일 제트 분사기를 고압 챔버 내에 장착하여 제트의 주위기체압력, 분사기 형상 및 유동 조건의 영향을 조사하였다. 실험 결과로부터 아임계 조건과 초임계 조건에서의 제트의 특성 변화를 관찰하였으며, 주위기체압력이 대기압일 경우 유동 내에 섭동이 발생함을 파악하였다. 분사기 형상에 따른 유동 변화 또한 파악하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.320-329
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• 2008

The influence of thermodynamic transition associated with transcritical nitrogen injection upon the flow structure was investigated to explore numerical simulation of the injectant dynamics of oxygen/hydrogen coaxial jet in liquid rocket engines. Single and coaxial nitrogen jets were treated by comparing the transcritical and perfect-gaseous conditions, wherein the numerical model was accommodative to the real-fluid thermodynamics and transport properties at supercritical pressures. The model was in the first place validated by comparing the results of transcritical nitrogen injection between calculations and available experiments. For a single jet under the transcritical condition, the nitrogen kept a relatively high density up to its pseudo-critical temperature inside the mixing layer, since it remains less expanding until heated up to its pseudo-critical temperature. Numerical analysis revealed that cryogenic jets exhibit strong dependence of specific enthalpy profile upon the associated density profile that are both dominated by turbulent thermal diffusion. In the numerical model, therefore, exact evaluation of turbulent heat fluxes becomes very important for simulating turbulent cryogenic jets under supercritical pressures. Concerning the coaxial jets due to transcritical/gaseous nitrogen injections, the density profile inside the mixing layer was again affected by the thermodynamic transition of nitrogen. However, hydrodynamic instability modes of the inner jet did not show significant differences by this thermodynamic transition, so that further study is needed for the mixing process downstream of the near injection position.

• 한국분말재료학회지
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• 제8권2호
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• pp.91-97
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• 2001

The conventional debinding process in metal injection molding is very long time-consuming and unfriendly environmental method. Especially, in such a case of injection molded parts from hard and fine metal powder, such as WC-Co, an extremely long period of time is necessary in the conventional slow binder removal process. On the other hand, supercritical debinding is thought to be the effective method which is appropriate to eliminate the aforementioned inconvenience in the prior art. The supercritical fluid has high diffusivity and density, it can penetrate quickly into the inside of the green metal bodies, and extract the binder. In this paper, super-critical debinding is compared with wicking debinding process. Wax-based binder system is used in this study. The binder removal rate in supercritical $CO_2$ have been measured at $65^{\circ}C$, 75$^{\circ}C$ in the pressure range from 20 MPa to 28 MPa. Pores and cracks in silver bodies after sintering were observed using SEM When the super-critical $CO_2$ debinding was carried out at 75$^{\circ}C$, almost all the wax (about 70 wt% of binder) was removed in 2 hours under 28 MPa and 2.5 hours under 25 MPa.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.124.1-124.1
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• 2005

• 한국추진공학회지
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• 제22권5호
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• pp.32-39
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• 2018

추진기관 연료의 주 성분으로 사용되는 액체 탄화수소 화합물의 초임계 분사 거동 특성을 분석하였다. 임계점의 차이가 있는 Decane과 Methylcyclohexane (MCH)를 실험 유체로 선정하였으며 Shadowgraphy 기법을 사용하였다. 아임계 조건의 동일한 인젝터 초기상태에서 Decane과 MCH는 서로 다른 거동을 보였다. 하지만 임계점 부근에서 증발엔탈피가 0에 가까워져 기화과정이 아닌 초임계 유체로의 상변화가 일어나고, 급격한 밀도변화가 없어 두 가지 유체 모두 분열이 발생하지 않았다.