Two-Phase Flow Modeling of Inducers

Author:

Harun Amrin F.1,Prado Mauricio G.2,Shirazi Siamack A.3,Doty Dale R.4

Affiliation:

1. INTEC Engineering, 15600 JFK Blvd, Suite 300, Houston, TX 77032

2. Department of Petroleum Engineering

3. Department of Mechanical Engineering

4. Department of Mathematics and Computer Science, University of Tulsa, 600 S. College Ave., Tulsa, OK 74104

Abstract

Inducers, which are classified as axial flow pumps with helical path blades, are used within rotary gas separators commonly used in electrical submersible pump installations. A two-phase flow model has been developed to study the inducer performance, focusing on head generation. The proposed model is based on a meridional flow solution technique and utilizes a two-fluid approach. The model indicates that head degradation due to gas presence is a function of flow pattern. The effect of flow pattern diminishes when the void fraction is greater than 15 percent since the centrifugal force dominates the interfacial drag force. In this case, the two-phase flow can be approximated as a homogeneous mixture. The model also suggests that a liquid displacement correction is needed when phase segregation occurs inside the inducer. The new model significantly improves the ability to predict separation efficiency of a rotary gas separator over existing models. Hydrocarbon-air and water-air experimental data were gathered to validate the new model.

Publisher

ASME International

Subject

Geochemistry and Petrology,Mechanical Engineering,Energy Engineering and Power Technology,Fuel Technology,Renewable Energy, Sustainability and the Environment

Reference38 articles.

1. Ross, C. C., and Banerian, G., 1956, “Some Aspects of High Suction Specific Speed Inducers,” Trans. ASME, 78(8), pp. 1715–1721.

2. Acosta, A. J., 1958, “An Experimental Study of Cavitating Inducers,” Proc. Second Symposium on Naval Hydrodynamics, Washington, D.C., pp. 553–557.

3. Rains, D. A. , 1958, “Head Flow Characteristics of Axial Flow Inducers,” Jet Propul., August, 557–558.

4. Lakshminarayana, B., 1974, “Experimental and Analytical Investigation of Flow Through a Rocket Pump Inducer,” NASA SP 304, Part II, pp. 690–731.

5. Lakshminarayana, B., 1978, “On the Shear Pumping Effect in Rocket Pump Inducers,” book chapter in Pump-Analysis, Design and Application, 1, Worthington Pump Inc., pp. 49–68.

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