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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.:
General Electric Company, Niskayuna, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1165137
Patent Number(s):
8,905,713
Application Number:
12/790,675
Assignee:
General Electric Company (Niskayuna, NY)
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 = {2014},
month = {12}
}

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Works referenced in this record:

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

  • Hada, Satoshi; Matsuura, Masaaki; Tsukagoshi, Keizo
  • Journal of High Temperature Society, Vol. 33, Issue 5
  • DOI: 10.7791/jhts.33.264