发明名称 |
TURBO-ENGINE COMPONENT |
摘要 |
Disclosed is a turbo-engine component comprising a wall, the wall comprising a hot gas side surface and a coolant side surface. At least one coolant discharge duct is provided in said wall and opening out onto the hot gas side surface at a coolant discharge opening. A coolant flow direction is defined from the interior of the coolant discharge duct towards the discharge opening, the coolant discharge duct further being delimited by a delimiting surface thereof provided inside the wall. The coolant discharge duct has a first cross sectional direction and a second cross sectional direction. The coolant discharge duct is a blind cavity and is closed towards the coolant side surface, and further a dimension of the coolant discharge duct measured in the first cross sectional direction decreases in the coolant flow direction. |
申请公布号 |
US2017030200(A1) |
申请公布日期 |
2017.02.02 |
申请号 |
US201615223102 |
申请日期 |
2016.07.29 |
申请人 |
ANSALDO ENERGIA IP UK LIMITED |
发明人 |
KRÜCKELS Joerg;BRANDL Herbert |
分类号 |
F01D5/18;F01D9/02;F01D25/12 |
主分类号 |
F01D5/18 |
代理机构 |
|
代理人 |
|
主权项 |
1. A turbo-engine component comprising:
a wall, the wall having a hot gas side surface and a coolant side surface, wherein at least one coolant discharge duct is provided in said wall and opening out onto the hot gas side surface at a coolant discharge opening, a coolant flow direction being defined from an interior of the coolant discharge duct towards the discharge opening, the coolant discharge duct further being delimited by a delimiting surface thereof provided inside the wall, the coolant discharge duct having a first cross sectional direction and a second cross sectional direction, wherein the coolant discharge duct is a blind cavity and is closed towards the coolant side surface, and further a dimension of the coolant discharge duct measured in the first cross sectional direction decreases in the coolant flow direction. |
地址 |
London GB |