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Title: Turbine component and methods of making and cooling a turbine component

Abstract

A turbine component includes a root and an airfoil extending from the root to a tip opposite the root. The airfoil forms a leading edge and a trailing edge portion extending to a trailing edge. Radial cooling channels in the trailing edge portion of the airfoil permit radial flow of a cooling fluid through the trailing edge portion. Each radial cooling channel has a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface. A method of making a turbine component and a method of cooling a turbine component are also disclosed.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1600268
Patent Number(s):
10,472,973
Application Number:
15/174,271
Assignee:
General Electric Company (Schenectady, NY)
DOE Contract Number:  
FE0024006
Resource Type:
Patent
Resource Relation:
Patent File Date: 06/06/2016
Country of Publication:
United States
Language:
English
Subject:
36 MATERIALS SCIENCE; 33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, and Hafner, Matthew Troy. Turbine component and methods of making and cooling a turbine component. United States: N. p., 2019. Web.
Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, & Hafner, Matthew Troy. Turbine component and methods of making and cooling a turbine component. United States.
Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, and Hafner, Matthew Troy. Tue . "Turbine component and methods of making and cooling a turbine component". United States. https://www.osti.gov/servlets/purl/1600268.
@article{osti_1600268,
title = {Turbine component and methods of making and cooling a turbine component},
author = {Dutta, Sandip and Zhang, James and Itzel, Gary Michael and Delvaux, John McConnell and Hafner, Matthew Troy},
abstractNote = {A turbine component includes a root and an airfoil extending from the root to a tip opposite the root. The airfoil forms a leading edge and a trailing edge portion extending to a trailing edge. Radial cooling channels in the trailing edge portion of the airfoil permit radial flow of a cooling fluid through the trailing edge portion. Each radial cooling channel has a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface. A method of making a turbine component and a method of cooling a turbine component are also disclosed.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {11}
}

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Works referenced in this record:

Turbine bucket profile yielding improved throat
patent, May 2016


Turbine blades made from multiple single crystal cast superalloy segments
patent, December 2001


Ceramic composite vane with metallic substructure
patent, February 2003


Internally cooled airfoil
patent, September 1993