Market requests for higher performance fans and legal requirements to meet minimum efficiency grades drive industrial fan designers for tunnel and metro applications to study or re-think stall control solutions. This paper, therefore, focuses on how anti-stall rings work and provides a robust and fast numerical methodology to evaluate and improve their efficiency and effectiveness. Here we present a numerical study validated against available experiments on the fitting of an anti-stall ring on an axial fan for tunnel and metro operations. The study synthetizes the effects of the anti-stall ring with an actuator disk coupled to a frozen rotor model for the fan, significantly reducing the computational load required and validating the methodology. Such approach can be implemented to easily derive fan performance with different geometries of the anti-stall ring plenum as well as its fins.
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ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
June 13–17, 2016
Seoul, South Korea
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4968-2
PROCEEDINGS PAPER
Modelling of Axial Fan and Anti-Stall Ring on a Virtual Test Rig for Air Performance Evaluation
Tommaso Bonanni,
Tommaso Bonanni
Sapienza University of Rome, Rome, Italy
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Alessandro Corsini,
Alessandro Corsini
Sapienza University of Rome, Rome, Italy
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Giovanni Delibra,
Giovanni Delibra
Sapienza University of Rome, Rome, Italy
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David Volponi,
David Volponi
Sapienza University of Rome, Rome, Italy
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Anthony G. Sheard
Anthony G. Sheard
AGS Consulting LLC, Atlanta, GA
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Tommaso Bonanni
Sapienza University of Rome, Rome, Italy
Alessandro Corsini
Sapienza University of Rome, Rome, Italy
Giovanni Delibra
Sapienza University of Rome, Rome, Italy
David Volponi
Sapienza University of Rome, Rome, Italy
Anthony G. Sheard
AGS Consulting LLC, Atlanta, GA
Paper No:
GT2016-56862, V001T09A005; 10 pages
Published Online:
September 20, 2016
Citation
Bonanni, T, Corsini, A, Delibra, G, Volponi, D, & Sheard, AG. "Modelling of Axial Fan and Anti-Stall Ring on a Virtual Test Rig for Air Performance Evaluation." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 1: Aircraft Engine; Fans and Blowers; Marine. Seoul, South Korea. June 13–17, 2016. V001T09A005. ASME. https://doi.org/10.1115/GT2016-56862
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