The reduction of turbine blade-tip losses by means of passive tip injection was theoretically investigated. The analysis employed an analytical expression of the blade-tip discharge coefficient. The resulting blade-tip excitation forces (i. e. Thomas-Alford forces) were explicitly evaluated for unshrouded turbines with and without passive tip injection. It was found, that the Thomas-Alford coefficient for cross-force can substantially increase when the blade-tip gap was reduced. This observation can directly be explained on the basis of viscous flow effects through the gap, and it was in excellent agreement with available literature data. Due to passive tip injection, a slight decrease of the blade-tip excitation cross-force was obtained. The potential of the reduction of the cross-force due to passive tip injection was found to be comparable to the corresponding tip loss reduction.
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ASME 2015 International Mechanical Engineering Congress and Exposition
November 13–19, 2015
Houston, Texas, USA
Conference Sponsors:
- ASME
ISBN:
978-0-7918-5734-2
PROCEEDINGS PAPER
Reduction of Turbine Blade Tip Leakage Losses and Excitation Forces by Passive Tip Injection
Stefan aus der Wiesche,
Stefan aus der Wiesche
Muenster University of Applied Sciences, Steinfurt, Germany
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Maximilian Passmann,
Maximilian Passmann
Muenster University of Applied Sciences, Steinfurt, Germany
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Reinhard Willinger
Reinhard Willinger
Vienna University of Technology, Vienna, Austria
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Stefan aus der Wiesche
Muenster University of Applied Sciences, Steinfurt, Germany
Maximilian Passmann
Muenster University of Applied Sciences, Steinfurt, Germany
Reinhard Willinger
Vienna University of Technology, Vienna, Austria
Paper No:
IMECE2015-50120, V001T01A041; 9 pages
Published Online:
March 7, 2016
Citation
aus der Wiesche, S, Passmann, M, & Willinger, R. "Reduction of Turbine Blade Tip Leakage Losses and Excitation Forces by Passive Tip Injection." Proceedings of the ASME 2015 International Mechanical Engineering Congress and Exposition. Volume 1: Advances in Aerospace Technology. Houston, Texas, USA. November 13–19, 2015. V001T01A041. ASME. https://doi.org/10.1115/IMECE2015-50120
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