• 한국유체기계학회 논문집
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• 제9권3호
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• pp.14-21
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• 2006

Leakage reduction through annular type seals of turbomachinery is necessary for enhancing their efficiency and the precise prediction method of seal leakage is needed. The analysis based on Bulk-flow concept has been mainly used in predicting seal leakage. However, full Navier-Stokes Equations with turbulent model derived in the seal flow passage have to be solved for improving the prediction of seal leakage. FLUENT 6 which is commercial CFD(Computational Fluid Dynamics) code based on FVM(Finite Volume Method) and SIMPLE algorism has been used to analyze leakage of various non-contact-type seals in this presentation. Comparing with the results of Bulk-flow model analysis and experiment, the result of CFD analysis shows good agreement with that of existing theoretical analysis for the incompressible grooved seal and compressive plain and staggered seal. The CFD analysis also shows improvement on the leakage prediction of the incompressible plain seal and compressive see-through-type labyrinth seal.

• Tribology and Lubricants
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• 제25권3호
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• pp.150-156
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• 2009

Precise leakage prediction for annular type seals of turbomachinery is necessary for enhancing their efficiency and various prediction methods have been developed. As the seal passage is designed intricately, the analysis based on Bulk-flow concept which has been mainly used in predicting seal leakage is limited. In order to improve the seal leakage prediction, full Navier-Stokes Equations with turbulent model derived in the seal flow passage have to be solved. In this study, 3D CFD (Computational Fluid Dynamics) analysis has been performed for predicting leakage of various non-contact type anular seals using FLUENT. Compared to the results by Bulk-flow model analysis, experiment, and 2D CFD analysis, the result of 3D CFD analysis shows improvement in predicting seal leakage, especially for the parallel grooved pump seal.

• 한국유체기계학회 논문집
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• 제18권1호
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• pp.44-50
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• 2015

Labyrinth seals are commonly used in various kinds of turbomachinery to reduce leakage flow. In the present 3D CFD analysis of see-through-type labyrinth air seal, the methodology of determining leakage and rotordynamic coefficients is suggested with the relative coordinate system for steady-state simulation. The leakage flow and rotordynamic forces predicted by using different solvers and turbulent models of FLUENT are compared with the results of the existing bulk-flow analysis code LABYSEAL.FOR and experiment. The present CFD result of direct stiffness(K) shows only improvement in prediction. The results of leakage and rotordynamic coefficients as well as computing time are sensitive against the used solver and turbulent model.

• 공업화학
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• 제10권2호
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• pp.310-318
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• 1999

공기분리 PSA 공정설계에 적용할 물질전달계수를 구하기 위하여 흡착탑을 통과하는 질소와 산소의 농도에 대한 동적파과곡선을 실험적으로 측정하였다. 그 결과를 전산모사에 의한 파과곡선과 비교하여 벌크흐름 중의 물질전달속도를 예측하였다. 전산모사에서 흡착은 coupled Langmuir isotherm을 따른다고 보았으며, 물질전달은 LDF 모델에 의해 표현된다고 가정하였다. 실험과 이론의 비교를 통해 얻은 물질전달계수는 유속에는 거의 영향을 받지 않았으나 압력 조건에 따라 민감한 변화를 보였다. 이를 통해 물질전달저항이 거대기공 확산영역에 있음을 예측할 수 있었으며, 물질전달계수를 압력변화에 대해 지수함수의 형태로 표현하였다. 질소나 산소 단일 성분에 대해서 얻은 물질전달계수는 질소와 산소 혼합 벌크기체의 파과곡선에 적용했을 경우에도 5% 이하의 오차로 잘 일치함을 보여주었다.

• 한국유체기계학회 논문집
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• 제16권3호
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• pp.26-31
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• 2013

In present 3D CFD study, the method for determining leakage and rotordynamic coefficients of a plain-gas seal is suggested by using the relative coordinate system for steady-state simulation. In order to find the effect of pre-swirl speed at seal inlet, pre-swirl velocity is included as a parameter. Present analysis is verified by comparison with results acquired from Bulk-flow analysis code and published experimental results. The results of 3D CFD rotordynamic coefficients of direct stiffness(K) and cross-coupled stiffness(k) show improvements in prediction. As pre-swirl speed at seal inlet increases, k also increases to destabilize system. However, pre-swirl speed at seal inlet does not show sensitivity to the leakage and rotordynamic coefficients of K and damping(C).

• Tribology and Lubricants
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• 제26권1호
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• pp.37-43
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• 2010

Precise prediction of rotordynamic coefficients for annular type seal of turbomachinery is necessary for enhancing their vibrational stability and various prediction methods have been developed. As the seal passage is designed complicatedly, the analysis based on Bulk-flow concept which has been mainly used in predicting seal dynamics is limited. In order to improve the seal rotordynamic prediction, full Navier-Stokes Equations with turbulent model derived in the seal flow passage have to be solved. In this study, 3D CFD(Computational Fluid Dynamics) analysis has been performed for predicting rotordynamic coefficients of non-contact type annular plain seal using FLUENT. Comparing with the results of Bulk-flow model analysis, the result of 3D CFD analysis shows good agreement.

• 멤브레인
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• 제6권2호
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• pp.86-95
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• 1996

본 연구에서는1축 회전판형 한외여과막 모듈의 순수 투과율 예측모델과 기름 에멀션의 분리 특성 및 투과율 예측모델을 유도하였다. 1축 RDM은 한외여과막(UOP사, 직경 0.22m)으로 제작된 회전판막을 장착하여 $25^{\circ}C$에서 압력, 각속도($\omega$), 농도 변화에 따라 분리특성을 조사하였다. 회전판막의 각속도가 0에서 52.36rad/s로 증가할수록 회전판내 유체가 받는 원심력에 의한 압력 강하와 분리막 표면의 미끄럼 흐름에 의한 압력 강하로 순수 투과율은 최대 각속도에서 3.9% 감소하였다. 원심력과 미끄럼 흐름에 의한 압력 강하는 선속도(${\omega}r$)의 자승에 비례하였다. 회전판의 각속도가 52.36에서 2.62rad/s로 감소할 때 5% 절삭유의 투과율은 30.16% 감소하였고 농도가 낮을수록 막회전과 투과율에 미치는 영향은 적었다. 절삭유의 투과율(J; $kg/m^{2} \cdot s$)은 회전에 의한 압력 강하를 고려한 유효압력차($\Delta P_{T}$ ; Pa), 벌크농도($C_{B}$; %), 선속도($\omega$r; m/s) 등에 영향을 받으며 실험 결과에 저항 모델을 적용하여 다음과 같은 식을 유도하였다.