Advanced cooling method for combustion turbine airfoil fillets
作者： Alexander Ralph Beeck , Robert Kenmer Scott
DOI:
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摘要: The present invention is directed to a hollow turbine airfoil having cooling system designed provide enhanced the fillet of airfoil. may include at least one channel, passing proximate fillet. A portion channel be positioned outer surface without breaching an vortex plate adjacent end wall inner and opening in fluid communication with chamber. also film that extend obliquely through
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