A circolimaçon positive displacement machine is driven by a limaçon mechanism, but the profiles of its rotor and housing are circular arcs. As such, its design models are different from those of the limaçon-to-limaçon machines, whose profiles are cut to the limaçon equations. For the benefit of the reader, the paper starts with a brief background on the general geometric aspects of the limaçon fluid processing technology. However, the focus is then turned to the circolimaçon machine, where its design parameters are introduced and geometric models are proposed to assist with the design process. Also, a computational inverse design model has been employed to work out a set of congruent geometric parameters to meet certain design requirements. Case studies are presented at the end of the paper to give the reader a numerical perspective on the design process of this class of positive displacement machines.
Skip Nav Destination
i.sultan@ballarat.edu.au
Article navigation
June 2008
Research Papers
A Geometric Design Model for the Circolimaçon Positive Displacement Machine
Ibrahim A. Sultan
Ibrahim A. Sultan
School of Science and Engineering,
i.sultan@ballarat.edu.au
The University of Ballarat
, P.O. Box 663, Ballarat, 3353 Victoria, Australia
Search for other works by this author on:
Ibrahim A. Sultan
School of Science and Engineering,
The University of Ballarat
, P.O. Box 663, Ballarat, 3353 Victoria, Australiai.sultan@ballarat.edu.au
J. Mech. Des. Jun 2008, 130(6): 062307 (8 pages)
Published Online: April 16, 2008
Article history
Received:
February 20, 2007
Revised:
June 13, 2007
Published:
April 16, 2008
Citation
Sultan, I. A. (April 16, 2008). "A Geometric Design Model for the Circolimaçon Positive Displacement Machine." ASME. J. Mech. Des. June 2008; 130(6): 062307. https://doi.org/10.1115/1.2901143
Download citation file:
Get Email Alerts
Cited By
Related Articles
The Tip Clearance Flow Resonance Behind Axial Compressor Nonsynchronous Vibration
J. Turbomach (October,2011)
Blade Tip Clearance Flow and Compressor Nonsynchronous Vibrations: The Jet Core Feedback Theory as the Coupling Mechanism
J. Turbomach (January,2009)
Nonuniform Flow in a Compressor Due to Asymmetric Tip Clearance
J. Turbomach (October,2000)
Modeling Shrouded Stator Cavity Flows in Axial-Flow Compressors
J. Turbomach (January,2000)
Related Proceedings Papers
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Introduction
Axial-Flow Compressors
Design of Rotor Time Constant Estimator and Sliding Mode Position Controller for Induction Machines
Proceedings of the 2010 International Conference on Mechanical, Industrial, and Manufacturing Technologies (MIMT 2010)