In turbomachines, the transfer of energy between the rotor and the fluid does not—in theory—result in lateral forces on the rotor. In positive displacement machines, on the other hand, the transfer of energy between the moving components and the working fluid usually results in unbalanced pressure fields and forces. Muhammed and Childs (2013, “Rotordynamics of a Two-Phase Flow Twin Screw Pump,” ASME J. Eng. Gas Turbines Power, 135(6), p. 062502) developed a model to predict the dynamic forces in twin-screw pumps, showing that the helical screw shape generates hydraulic forces that oscillate at multiples of running speed. The work presented here attempts to validate the model of Muhammed and Childs (2013, “Rotordynamics of a Two-Phase Flow Twin Screw Pump,” ASME J. Eng. Gas Turbines Power, 135(6), p. 062502) using a clear-casing twin-screw pump. The pump runs in both single and multiphase conditions with exit pressure up to 300 kPa and a flow rate 0.6 l/s. The pump was instrumented with dynamic pressure probes across the axial length of the screw in two perpendicular directions to validate the dynamic model. Two proximity probes measured the dynamic rotor displacement at the outlet to validate the rotordynamics model and the hydrodynamic cyclic forces predicted by Muhammed and Childs (2013, “Rotordynamics of a Two-Phase Flow Twin Screw Pump,” ASME J. Eng. Gas Turbines Power, 135(6), p. 062502). The predictions were found to be in good agreement with the measurements. The amplitude of the dynamic pressure measurements in two perpendicular plans supported the main assumptions of the model (constant pressure inside the chambers and linear pressure drop across the screw lands). The predicted rotor orbits at the pump outlet in the middle of the rotor matched the experimental orbits closely. The spectrum of the response showed harmonics of the running speed as predicted by the model. The pump rotor's calculated critical speed was at 24.8 krpm, roughly 14 times the rotor's running speed of 1750 rpm. The measured and observed excitation frequencies extended out to nine times running speed, still well below the first critical speed. However, for longer twin-screw pumps running at higher speed, the coincidence of a higher-harmonic excitation frequency with the lightly damped first critical speed should be considered.
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September 2016
Research-Article
Vibration Modeling and Experimental Results of Two-Phase Twin-Screw Pump
Ameen Muhammed,
Ameen Muhammed
Artificial Lift Systems,
Baker Hughes, Inc.,
Claremore, OK 74017
e-mail: ameen.muhammed@bakerhughes.com
Baker Hughes, Inc.,
Claremore, OK 74017
e-mail: ameen.muhammed@bakerhughes.com
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Dara W. Childs
Dara W. Childs
Leland T. Jordan Professor of Mechanical
Engineering Turbomachinery Laboratory,
Texas A&M University,
College Station, TX 77843-3123
e-mail: dchilds@tamu.edu
Engineering Turbomachinery Laboratory,
Texas A&M University,
College Station, TX 77843-3123
e-mail: dchilds@tamu.edu
Search for other works by this author on:
Ameen Muhammed
Artificial Lift Systems,
Baker Hughes, Inc.,
Claremore, OK 74017
e-mail: ameen.muhammed@bakerhughes.com
Baker Hughes, Inc.,
Claremore, OK 74017
e-mail: ameen.muhammed@bakerhughes.com
Dara W. Childs
Leland T. Jordan Professor of Mechanical
Engineering Turbomachinery Laboratory,
Texas A&M University,
College Station, TX 77843-3123
e-mail: dchilds@tamu.edu
Engineering Turbomachinery Laboratory,
Texas A&M University,
College Station, TX 77843-3123
e-mail: dchilds@tamu.edu
1Corresponding author.
Contributed by the Turbomachinery Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received September 13, 2015; final manuscript received January 13, 2016; published online March 22, 2016. Editor: David Wisler.
J. Eng. Gas Turbines Power. Sep 2016, 138(9): 092601 (17 pages)
Published Online: March 22, 2016
Article history
Received:
September 13, 2015
Revised:
January 13, 2016
Citation
Muhammed, A., and Childs, D. W. (March 22, 2016). "Vibration Modeling and Experimental Results of Two-Phase Twin-Screw Pump." ASME. J. Eng. Gas Turbines Power. September 2016; 138(9): 092601. https://doi.org/10.1115/1.4032662
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