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Title: Articles which include chevron film cooling holes, and related processes

Abstract

An article is described, including an inner surface which can be exposed to a first fluid; an inlet; and an outer surface spaced from the inner surface, which can be exposed to a hotter second fluid. The article further includes at least one row or other pattern of passage holes. Each passage hole includes an inlet bore extending through the substrate from the inlet at the inner surface to a passage hole-exit proximate to the outer surface, with the inlet bore terminating in a chevron outlet adjacent the hole-exit. The chevron outlet includes a pair of wing troughs having a common surface region between them. The common surface region includes a valley which is adjacent the hole-exit; and a plateau adjacent the valley. The article can be an airfoil. Related methods for preparing the passage holes are also described.

Inventors:
;
Issue Date:
Research Org.:
GE Global Research, Niskayuna, New York (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1165137
Patent Number(s):
8905713
Application Number:
12/790,675
Assignee:
General Electric Company (Niskayuna, NY)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2010 May 28
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING

Citation Formats

Bunker, Ronald Scott, and Lacy, Benjamin Paul. Articles which include chevron film cooling holes, and related processes. United States: N. p., 2014. Web.
Bunker, Ronald Scott, & Lacy, Benjamin Paul. Articles which include chevron film cooling holes, and related processes. United States.
Bunker, Ronald Scott, and Lacy, Benjamin Paul. Tue . "Articles which include chevron film cooling holes, and related processes". United States. https://www.osti.gov/servlets/purl/1165137.
@article{osti_1165137,
title = {Articles which include chevron film cooling holes, and related processes},
author = {Bunker, Ronald Scott and Lacy, Benjamin Paul},
abstractNote = {An article is described, including an inner surface which can be exposed to a first fluid; an inlet; and an outer surface spaced from the inner surface, which can be exposed to a hotter second fluid. The article further includes at least one row or other pattern of passage holes. Each passage hole includes an inlet bore extending through the substrate from the inlet at the inner surface to a passage hole-exit proximate to the outer surface, with the inlet bore terminating in a chevron outlet adjacent the hole-exit. The chevron outlet includes a pair of wing troughs having a common surface region between them. The common surface region includes a valley which is adjacent the hole-exit; and a plateau adjacent the valley. The article can be an airfoil. Related methods for preparing the passage holes are also described.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Dec 09 00:00:00 EST 2014},
month = {Tue Dec 09 00:00:00 EST 2014}
}

Works referenced in this record:

Cross-flow film cooling passages
patent, March 1987


Coolant passages with full coverage film cooling slot
patent, May 1987


Method and apparatus for making diffused cooling holes in an airfoil
patent, February 1989


Cooled turbomachinery components
patent, November 1991


Film cooled components
patent, March 1992


Laser drilling of non-circular apertures
patent, March 1997


Device for recovering abrasives in water jet cutting systems
patent, November 1999


Method of producing a noncircular cooling bore
patent, October 2001


Method for forming shaped holes
patent, December 2001


Method of laser drilling a hole
patent, March 2004


Method of removing a coating from a substrate
patent, June 2005


Coated component with through-hole having improved surface finish
patent, June 2005


Apparatus and method for machining in confined spaces
patent, November 2005


Hot gas path component with mesh and turbulated cooling
patent, January 2006


Hot gas path component with mesh and dimpled cooling
patent, March 2007


Chevron film cooled wall
patent, February 2008


Combustor cooling with angled segmented surfaces
patent, May 2008


Momentum preserving film-cooling shaped holes
patent, August 2011


Film cooling hole for turbine airfoil
patent, November 2011


Method and apparatus for laser cutting a trench
patent, November 2012


Components with re-entrant shaped cooling channels and methods of manufacture
patent, March 2013


Methods of fabricating a coated component using multiple types of fillers
patent, September 2013


Method of forming a shaped hole
patent-application, May 2003


Cooled turbine component and cooled turbine blade
patent-application, June 2005


Chevron film cooled wall
patent-application, December 2005


High coverage cooling hole shape
patent-application, January 2008


Turbine Component
patent-application, November 2008


Development of High Performance Film Cooling of 1700 Degree C Class Gas Turbines [1700°C級ガスタービン高性能フィルム冷却の開発]
journal, January 2007


    Works referencing / citing this record:

    Components with microchannel cooling
    patent, March 2017


    Film cooling channel array with multiple metering portions
    patent, April 2016


    Components with microchannel cooling
    patent, February 2016


    Backstrike protection during machining of cooling features
    patent, February 2016