Invention Grant
US09103217B2 Turbine blade tip with tip shelf diffuser holes 有权
涡轮叶片尖端,带有架子扩散孔

Turbine blade tip with tip shelf diffuser holes
Abstract:
A turbine blade having a tip including a tip shelf through which pass one or more diffuser cooling holes, the diffuser cooling holes directing the flow of cooling gas along the tip shelf, spreading the flow of cooling gas more evenly along the tip shelf and enhancing the formation of a curtain of cooling air along the tip shelf, leading to lower blade tip temperatures, reduced diversion of cooling air, and greater turbine blade life.
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