发明名称 AIRFOIL COOLING CIRCUITS
摘要 An airfoil includes leading and trailing edges; first and second sides extending from the leading edge to the trailing edge, each side having an exterior surface; a core passage located between the first and second sides and the leading and trailing edges; and a wall structure located between the core passage and the exterior surface of the first side. The wall structure includes a plurality of cooling fluid inlets communicating with the core passage for receiving cooling fluid from the core passage, a plurality of cooling fluid outlets on the exterior surface of the first side for expelling cooling fluid and forming a cooling film along the exterior surface of the first side, and a plurality of cooling passages communicating with the plurality of cooling fluid inlets and the plurality of cooling fluid outlets. At least a portion of one cooling passage extends between adjacent cooling fluid outlets.
申请公布号 WO2014018138(A2) 申请公布日期 2014.01.30
申请号 WO2013US37302 申请日期 2013.04.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HUDSON, ERIC A.;PROPHETER-HINCKLEY, TRACY A.;QUACH, SAN;DEVORE, MATTHEW A.
分类号 F01D5/18;F01D5/14;F02C7/00 主分类号 F01D5/18
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