Influence of Channel Geometry and Flow Variables on Cyclone Cooling of Turbine Blades

被引:32
作者
Bruschewski, Martin [1 ]
Scherhag, Christian [1 ]
Schiffer, Heinz-Peter [1 ]
Grundmann, Sven [2 ]
机构
[1] Tech Univ Darmstadt, Inst Gas Turbines & Aerosp Prop, Petersenstr 30, D-64287 Darmstadt, Germany
[2] Univ Rostock, Inst Fluid Mech, D-18051 Rostock, Germany
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 2016年 / 138卷 / 06期
关键词
HEAT-TRANSFER ENHANCEMENT; MAGNETIC-RESONANCE; SWIRL; TURBULENCE; DECAY;
D O I
10.1115/1.4032363
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
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 S-0 = 3 and Re = 20; 000. 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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页数:10
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