A study examining the internal cooling of turbine blades by swirling flow is presented. The sensitivity of swirling flow is investigated with regard to Reynolds number, swirl intensity, and the common geometric features of blade-cooling ducts. The flow system consists of a straight and round channel that is attached to a swirl generator with tangential inlets. Different orifices and 180-deg bends are employed as channel outlets. The experiments were carried out with magnetic resonance velocimetry (MRV) for which water was used as flow medium. As the main outcome, it was found that the investigated flows are highly sensitive to the conditions at the channel outlet. However, it was also discovered that for some outlet geometries the flow field remains the same. The associated flow features a favorable topology for heat transfer; the majority of mass is transported in the annular region close to the channel walls. Together with its high robustness, it is regarded as an applicable flow type for the internal cooling of turbine blades. A large eddy simulation (LES) was conducted to analyze the heat transfer characteristic of the associated flow for and . The simulation showed an averaged Nusselt number increase of factor 4.7 compared to fully developed flow. However, a pressure loss increase of factor 43 must be considered as well.
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June 2016
Research-Article
Influence of Channel Geometry and Flow Variables on Cyclone Cooling of Turbine Blades
Martin Bruschewski,
Martin Bruschewski
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
e-mail: bruschewski@glr.tu-darmstadt.de
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
e-mail: bruschewski@glr.tu-darmstadt.de
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Christian Scherhag,
Christian Scherhag
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
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Heinz-Peter Schiffer,
Heinz-Peter Schiffer
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
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Sven Grundmann
Sven Grundmann
Institute of Fluid Mechanics,
University of Rostock,
Rostock 18051, Germany
University of Rostock,
Rostock 18051, Germany
Search for other works by this author on:
Martin Bruschewski
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
e-mail: bruschewski@glr.tu-darmstadt.de
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
e-mail: bruschewski@glr.tu-darmstadt.de
Christian Scherhag
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
Heinz-Peter Schiffer
Institute of Gas Turbines
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
and Aerospace Propulsion,
Technische Universität Darmstadt,
Darmstadt 64287, Germany
Sven Grundmann
Institute of Fluid Mechanics,
University of Rostock,
Rostock 18051, Germany
University of Rostock,
Rostock 18051, Germany
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received November 16, 2015; final manuscript received December 11, 2015; published online February 9, 2016. Editor: Kenneth C. Hall.
J. Turbomach. Jun 2016, 138(6): 061005 (10 pages)
Published Online: February 9, 2016
Article history
Received:
November 16, 2015
Revised:
December 11, 2015
Citation
Bruschewski, M., Scherhag, C., Schiffer, H., and Grundmann, S. (February 9, 2016). "Influence of Channel Geometry and Flow Variables on Cyclone Cooling of Turbine Blades." ASME. J. Turbomach. June 2016; 138(6): 061005. https://doi.org/10.1115/1.4032363
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