发明名称 |
OUTER DIAMETER PLATFORM COOLING HOLE SYSTEM AND ASSEMBLY |
摘要 |
An airfoil component is described herein. The airfoil component may include an OD platform comprising a gaspath face and a non-gaspath face coupled together via a plurality of cooling holes. The airfoil component may include an airfoil extending in from the outer diameter platform. The plurality of cooling holes comprises a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil. |
申请公布号 |
US2016245093(A1) |
申请公布日期 |
2016.08.25 |
申请号 |
US201514627915 |
申请日期 |
2015.02.20 |
申请人 |
United Technologies Corporation |
发明人 |
Deibel Russell;Gleiner Matthew S. |
分类号 |
F01D5/18;F02C7/18;F02C3/04 |
主分类号 |
F01D5/18 |
代理机构 |
|
代理人 |
|
主权项 |
1. An airfoil component comprising:
an OD platform comprising:
a non-gaspath face; anda gaspath face coupled to the non-gaspath face via a plurality of cooling holes; and an airfoil extending from the outer diameter platform, wherein the plurality of cooling holes comprise a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil, wherein a plenum is formed adjacent to the non-gaspath face, wherein the plurality of cooling holes are coupled to the plenum. |
地址 |
Hartford CT US |