Inducer and Centrifugal Pump Contributions to the Rotordynamic Fluid Forces Acting on a Space Turbopump

Author:

Pace Giovanni1,Valentini Dario1,Pasini Angelo2,Torre Lucio3,Hadavandi Ruzbeh4,d'Agostino Luca2

Affiliation:

1. Sitael S.p.A., Via Gherardesca 5, Pisa 56121, Italy e-mail:

2. Department of Industrial and Civil Engineering, University of Pisa, Via Gerolamo Caruso 8, Pisa 56122, Italy e-mail:

3. GMYS-Space, Via di Broccoletto, Lucca 55100, Italy e-mail:

4. Sitael S.p.A., Via Gherardesca 5 Pisa 56121, Italy e-mail:

Abstract

The fluid-induced rotordynamic forces acting on a whirling space turbopump composed by an inducer and a radial impeller have been compared to the same forces measured on each single component of the turbomachine (i.e., on the inducer and on the radial impeller). The experimental campaign has been carried out in cold water at design and off-design conditions (80%, 100%, and 120% of the design flow rate) both in noncavitating (NC) and cavitating regimes. The paper illustrates the different trends of the rotordynamic forces on the axial and radial pumps and highlights their contributions on the overall turbomachine. At positive whirl ratios, the behavior of the inducer is dominant while, at negative ones, both the pumps show the same trends in such a way that the overall behavior is roughly the sum of each single component.

Funder

European Space Agency

Publisher

ASME International

Subject

Mechanical Engineering

Reference24 articles.

1. Rotordynamic Forces in Cavitating Inducers;ASME J. Fluids Eng.,1997

2. Internal Flows and Force Matrices in Axial Flow Inducers,1994

3. Experimental Investigation of the Effect of Cavitation on the Rotordynamic Forces on a Whirling Centrifugal Pump Impeller,1989

4. Rosenmann, W., 1965, “Experimental Investigations of Hydrodynamically Induced Shaft Forces With a Three Bladed Inducer,” ASME Symposium on Cavitation in Fluid Machinery, Chicago, IL, Nov. 7–11, pp. 172–195.https://ntrs.nasa.gov/search.jsp?R=19660038884

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