The design of an effective diffuser for a given last stage blade of an LP turbine is known to be highly dependent on the size and shape of the exhaust hood in which it is located. For retrofit steam turbines in particular, where a new last stage blade and diffuser are fitted into an existing exhaust hood, the shapes and sizes of the exhaust box have been seen to vary significantly from one contract to the next. An experimental parametric study of diffuser lips and exhaust hood configurations has been run on a model test turbine rig at GE Power to investigate the impact of various geometric parameters on the performance of the diffusers. Improved testing and post-processing methodologies means the diffuser performance has been obtained for a greater number of geometric configurations than was previously typically possible. The results of these experiments are compared with numerical calculations and confirm the accuracy of the standard in-house diffuser design tools. Key geometric parameters are identified from the test data and used to generate improved diffuser design guidelines.
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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:
978-0-7918-4986-6
PROCEEDINGS PAPER
Parametric Experimental and Numerical Study of LP Diffuser and Exhaust Hoods
Martin Claridge
Martin Claridge
GE Power, Rugby, UK
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Derek Taylor
GE Power, Rugby, UK
Gurnam Singh
GE Power, Rugby, UK
Phil Hemsley
GE Power, Rugby, UK
Martin Claridge
GE Power, Rugby, UK
Paper No:
GT2016-56640, V008T26A017; 10 pages
Published Online:
September 20, 2016
Citation
Taylor, D, Singh, G, Hemsley, P, & Claridge, M. "Parametric Experimental and Numerical Study of LP Diffuser and Exhaust Hoods." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 8: Microturbines, Turbochargers and Small Turbomachines; Steam Turbines. Seoul, South Korea. June 13–17, 2016. V008T26A017. ASME. https://doi.org/10.1115/GT2016-56640
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