发明名称 Gas turbine engine airfoil with dirt purge feature and core for making same
摘要 An airfoil includes a body. The body includes leading and trailing edges adjoining pressure and suction sides to provide an exterior airfoil surface. First and second cooling passages extend in a radial direction from a root to a tip. The first cooling passage includes a tip flag passage that is radially inboard from the tip and extends in a chord-wise direction to a first end that penetrates the trailing edge. The second cooling passage includes a second end terminates adjacent the tip flag passage and a dirt purge passage interconnects the second end to the tip flag passage. A core for making the airfoil is also disclosed.
申请公布号 US9279331(B2) 申请公布日期 2016.03.08
申请号 US201213453137 申请日期 2012.04.23
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Levine Jeffrey R.;Beattie Jeffrey S.
分类号 F01D5/18 主分类号 F01D5/18
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. An airfoil comprising: a body including leading and trailing edges adjoining pressure and suction sides to provide an exterior airfoil surface, first and second cooling passages extending in a radial direction from a root to a tip, the first cooling passage including a tip flag passage radially inboard from the tip and extending in a chord-wise direction to a first end that penetrates the trailing edge, the second cooling passage including a second end terminating adjacent the tip flag passage, and a dirt purge passage interconnecting the second end to the tip flag passage.
地址 Hartford CT US