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US 2013/0094971 A1Published application
Hot gas path component for turbine system
AssigneeGeneral Electric Company
InventorsBenjamin Paul Lacy, Brian Gene Brzek, Rebecca Christine Malish
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Abstract
A hot gas path component for a turbine system is disclosed. The hot gas path component includes a shell having an exterior surface and an interior surface. The hot gas path component further includes a porous medium having an exterior surface and an interior surface, the exterior surface positioned adjacent to the interior surface of the shell. The porous medium is configured for flowing a cooling medium therethrough.
Claims20
A hot gas path component for a turbine system, comprising:
- a shell having an exterior surface and an interior surface;
- and
- a porous medium having an exterior surface and an interior surface, the exterior surface positioned adjacent to the interior surface of the shell, the porous medium configured for flowing a cooling medium therethrough.
A turbine system, comprising:
- a compressor;
- a turbine coupled to the compressor;
- and
- a plurality of hot gas path components disposed in at least one of the compressor or the turbine, at least one of the hot gas path components comprising:
- a shell having an exterior surface and an interior surface;
- and
- a porous medium having an exterior surface and an interior surface, the exterior surface positioned adjacent to the interior surface of the shell, the porous medium configured for flowing a cooling medium therethrough.
4 more elements
Dependencies are inferred from the claim text.