EP 2581557 A2 20130417 - Hot gas path component for turbine system
Title (en)
Hot gas path component for turbine system
Title (de)
Heissgaskomponente für Turbinensystem
Title (fr)
Composant de partie chaude pour système de turbine
Publication
Application
Priority
US 201113271724 A 20111012
Abstract (en)
A hot gas path component (30) for a turbine system is disclosed. The hot gas path component (30) includes a shell (32) having an exterior surface (36) and an interior surface (38). The hot gas path component (30) further includes a porous medium (70) having an exterior surface (72) and an interior surface (74), the exterior surface (72) positioned adjacent to the interior surface (38) of the shell (32). The porous medium (70) is configured for flowing a cooling medium therethrough.
IPC 8 full level
F01D 5/18 (2006.01)
CPC (source: EP US)
F01D 5/183 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
EP 2581557 A2 20130417; CN 103046973 A 20130417; US 2013094971 A1 20130418
DOCDB simple family (application)
EP 12179575 A 20120807; CN 201210283962 A 20120810; US 201113271724 A 20111012