发明名称 TURBINE ELEMENT, TURBINE ROTOR CORE UNIT AND METHOD FOR MANUFACTURING TURBINE BLADES
摘要 A turbine element airfoil (22) has a cooling passageway network with a slot extending from a trailing passageway toward the trailing edge (32). A number of discrete posts arranged in rows (130-146) span the slot between pressure and suction sidewall portions.
申请公布号 PL367008(A1) 申请公布日期 2004.10.18
申请号 PL20040367008 申请日期 2004.04.06
申请人 UNITED TECHNOLOGIES CORP 发明人 CUNHA FRANK J;DAHMER MATTHEW T
分类号 B23P15/04;B22C9/10;F01D5/18;F02C7/00 主分类号 B23P15/04
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