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 |