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

Patent ·
OSTI ID:1165137

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.

Research Organization:
GE Global Research, Niskayuna, New York (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Niskayuna, NY)
Patent Number(s):
8,905,713
Application Number:
12/790,675
OSTI ID:
1165137
Resource Relation:
Patent File Date: 2010 May 28
Country of Publication:
United States
Language:
English

References (39)

Method and apparatus for forming diffused cooling holes in an airfoil patent April 1980
Vortex generating flow passage design for increased film cooling effectiveness patent July 1985
Electrode for electrical discharge machining film cooling passages in an airfoil patent March 1987
Cross-flow film cooling passages patent March 1987
Coolant passages with full coverage film cooling slot patent May 1987
Method of fabricating film cooling slot in a hollow airfoil patent June 1987
Film cooling passages with step diffuser patent April 1988
Airfoil with diffused cooling holes and method and apparatus for making the same patent August 1988
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 for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture patent May 2001
Method of producing a noncircular cooling bore patent October 2001
Method for forming shaped holes patent December 2001
Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture patent May 2002
Process for drilling holes through a thermal barrier coating patent June 2003
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
Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method patent February 2013
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
Methods of manufacture for components with cooling channels 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

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