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Title: Hot gas path component for turbine system

Abstract

A hot gas path component for a turbine system is disclosed. The hot gas path component includes a shell and one or more porous media having an exterior surface and an interior surface and positioned adjacent the shell. The one or more porous media is configured to include varying permeability in one of an axial direction, a radial direction, an axial and a radial direction, an axial and a circumferential direction, a radial and a circumferential direction or an axial, a radial and a circumferential direction, the porous media is positioned adjacent the shell. The one or more porous media is further configured to control one of an axial, a radial, an axial and a radial, an axial and a circumferential, a radial and a circumferential or an axial, a radial and a circumferential flow of a cooling medium flowing therethrough.

Inventors:
; ;
Publication Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1489673
Patent Number(s):
10,100,666
Application Number:
13/853,556
Assignee:
General Electric Company (Schenectady, NY) NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2013 Mar 29
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Brzek, Brian Gene, Morgan, Victor John, and Lacy, Benjamin Paul. Hot gas path component for turbine system. United States: N. p., 2018. Web.
Brzek, Brian Gene, Morgan, Victor John, & Lacy, Benjamin Paul. Hot gas path component for turbine system. United States.
Brzek, Brian Gene, Morgan, Victor John, and Lacy, Benjamin Paul. Tue . "Hot gas path component for turbine system". United States. https://www.osti.gov/servlets/purl/1489673.
@article{osti_1489673,
title = {Hot gas path component for turbine system},
author = {Brzek, Brian Gene and Morgan, Victor John and Lacy, Benjamin Paul},
abstractNote = {A hot gas path component for a turbine system is disclosed. The hot gas path component includes a shell and one or more porous media having an exterior surface and an interior surface and positioned adjacent the shell. The one or more porous media is configured to include varying permeability in one of an axial direction, a radial direction, an axial and a radial direction, an axial and a circumferential direction, a radial and a circumferential direction or an axial, a radial and a circumferential direction, the porous media is positioned adjacent the shell. The one or more porous media is further configured to control one of an axial, a radial, an axial and a radial, an axial and a circumferential, a radial and a circumferential or an axial, a radial and a circumferential flow of a cooling medium flowing therethrough.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Oct 16 00:00:00 EDT 2018},
month = {Tue Oct 16 00:00:00 EDT 2018}
}

Patent:

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