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