发明名称 |
GAS TURBINE ENGINE AIRFOIL TRAILING EDGE PASSAGE AND CORE FOR MAKING SAME |
摘要 |
An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes. |
申请公布号 |
US2015118064(A1) |
申请公布日期 |
2015.04.30 |
申请号 |
US201314390496 |
申请日期 |
2013.03.12 |
申请人 |
United Technologies Corporation |
发明人 |
Levine Jeffrey R.;Beattie Jeffrey S.;Staddon Malcolm C. |
分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
代理机构 |
|
代理人 |
|
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, a cooling passage extending in a radial direction from a root to a tip, and a trailing edge cooling passage interconnecting the cooling passage to the trailing edge, the trailing edge cooling passage including first and second pedestals of different sizes and arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes. |
地址 |
Hartford CT US |