The air handling system for large diesel/gas engines such as those used on locomotive, marine, and power generation applications require turbochargers with a high reliability and with turbomachinery capable to adjust to different operating conditions and transient requirements. The usage of variable geometry turbocharging (VGT) provides flexibility to the air handling system but adds complexity, cost and reduces the reliability of the turbocharger in exchange for improved engine performance and transient response. For this reason, it was desirable to explore designs that could provide the variability required by the air handling system, without the efficiency penalty of a conventional waste gate and with as little added complexity as possible. The current work describes a new low-cost variable geometry turbine design to address these requirements. The new tandem nozzle concept proposed is applicable to both axial and radial turbines and has been designed using conventional one-dimensional models and two- three-dimensional computational fluid dynamics (CFD) methods. The concept has furthermore been validated experimentally on two different test rigs. In order to avoid the long lead times of procuring castings, the nozzle for the axial turbine was manufactured using new additive manufacturing techniques. Both the axial turbine and the radial turbine designs showed that the concept is capable to achieve a mass flow variability of more than 15% and provide a robust and cost-effective alternative to conventional VGT designs by significantly reducing the number of moveable parts.
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March 2019
Research-Article
Development of a New Low-Cost Tandem Variable Geometry Turbocharging Concept for Turbocharger Applications
Thomas Leonard,
Thomas Leonard
School of Mechanical and Aerospace Engineering,
Clean Energies Research
Centre in Sustainable Energy,
Queens University of Belfast,
Belfast 69126, UK
e-mail: tleonard06@qub.ac.uk
Clean Energies Research
Centre in Sustainable Energy,
Queens University of Belfast,
Belfast 69126, UK
e-mail: tleonard06@qub.ac.uk
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Stephen Spence
Stephen Spence
School of Mechanical and Aerospace Engineering,
Clean Energies Research Centre
in Sustainable Energy,,
Queens University of Belfast (QUB),
Belfast BT9 5AH, UK
e-mail: S.W.Spence@qub.ac.uk
Clean Energies Research Centre
in Sustainable Energy,,
Queens University of Belfast (QUB),
Belfast BT9 5AH, UK
e-mail: S.W.Spence@qub.ac.uk
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Rodrigo R. Erdmenger
Katya Menter
Rogier Giepman
Cathal Clancy
Aneesh Vadvadgi
Tom Lavertu
Thomas Leonard
School of Mechanical and Aerospace Engineering,
Clean Energies Research
Centre in Sustainable Energy,
Queens University of Belfast,
Belfast 69126, UK
e-mail: tleonard06@qub.ac.uk
Clean Energies Research
Centre in Sustainable Energy,
Queens University of Belfast,
Belfast 69126, UK
e-mail: tleonard06@qub.ac.uk
Stephen Spence
School of Mechanical and Aerospace Engineering,
Clean Energies Research Centre
in Sustainable Energy,,
Queens University of Belfast (QUB),
Belfast BT9 5AH, UK
e-mail: S.W.Spence@qub.ac.uk
Clean Energies Research Centre
in Sustainable Energy,,
Queens University of Belfast (QUB),
Belfast BT9 5AH, UK
e-mail: S.W.Spence@qub.ac.uk
1Present address: Dyson Ltd., Malmesbury BT9 5AH, UK.
2Present address: IHI Charging Systems International, Heidelberg 69126, Germany.
Manuscript received July 1, 2018; final manuscript received August 5, 2018; published online October 4, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Mar 2019, 141(3): 031006 (10 pages)
Published Online: October 4, 2018
Article history
Received:
July 1, 2018
Revised:
August 5, 2018
Citation
Erdmenger, R. R., Menter, K., Giepman, R., Clancy, C., Vadvadgi, A., Lavertu, T., Leonard, T., and Spence, S. (October 4, 2018). "Development of a New Low-Cost Tandem Variable Geometry Turbocharging Concept for Turbocharger Applications." ASME. J. Eng. Gas Turbines Power. March 2019; 141(3): 031006. https://doi.org/10.1115/1.4041279
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