发明名称 GAS TURBINE ENGINE AIRFOIL BAFFLE
摘要 An airfoil includes an airfoil wall having an exterior airfoil surface and an interior surface. The interior surface provides an airfoil cavity. A baffle is arranged in the airfoil cavity and provides a baffle wall having first and second portions spaced from one another on first and second sides. A tube interconnects the first and second portions and is configured to convey fluid through the tube between the first and second sides. The airfoil is cooled by supplying cooling fluid to a baffle arranged within an airfoil. The cooling fluid is passed through baffle cooling holes to a gap between the baffle and airfoil to cool an interior surface of the airfoil. A portion of cooling fluid is conveyed from one gap location to another gap through a tube in the baffle. Another portion of the cooling fluid is passed through film cooling holes in the airfoil.
申请公布号 US2013052008(A1) 申请公布日期 2013.02.28
申请号 US201113214429 申请日期 2011.08.22
申请人 SPANGLER BRANDON W. 发明人 SPANGLER BRANDON W.
分类号 F01D5/18 主分类号 F01D5/18
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