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Title: Cooling arrangement for a gas turbine component

Abstract

A cooling arrangement (82) for a gas turbine engine component, the cooling arrangement (82) having a plurality of rows (92, 94, 96) of airfoils (98), wherein adjacent airfoils (98) within a row (92, 94, 96) define segments (110, 130, 140) of cooling channels (90), and wherein outlets (114, 134) of the segments (110, 130) in one row (92, 94) align aerodynamically with inlets (132, 142) of segments (130, 140) in an adjacent row (94, 96) to define continuous cooling channels (90) with non continuous walls (116, 120), each cooling channel (90) comprising a serpentine shape.

Inventors:
;
Publication Date:
Research Org.:
Siemens Aktiengesellschaft, Munich, DE (Europe)
Sponsoring Org.:
USDOE
OSTI Identifier:
1169639
Patent Number(s):
8,951,004
Application Number:
13/657,923
Assignee:
Siemens Aktiengesellschaft (Munich, DE) DOESC
DOE Contract Number:  
SC0001359
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Lee, Ching-Pang, and Heneveld, Benjamin E. Cooling arrangement for a gas turbine component. United States: N. p., 2015. Web.
Lee, Ching-Pang, & Heneveld, Benjamin E. Cooling arrangement for a gas turbine component. United States.
Lee, Ching-Pang, and Heneveld, Benjamin E. Tue . "Cooling arrangement for a gas turbine component". United States. doi:. https://www.osti.gov/servlets/purl/1169639.
@article{osti_1169639,
title = {Cooling arrangement for a gas turbine component},
author = {Lee, Ching-Pang and Heneveld, Benjamin E},
abstractNote = {A cooling arrangement (82) for a gas turbine engine component, the cooling arrangement (82) having a plurality of rows (92, 94, 96) of airfoils (98), wherein adjacent airfoils (98) within a row (92, 94, 96) define segments (110, 130, 140) of cooling channels (90), and wherein outlets (114, 134) of the segments (110, 130) in one row (92, 94) align aerodynamically with inlets (132, 142) of segments (130, 140) in an adjacent row (94, 96) to define continuous cooling channels (90) with non continuous walls (116, 120), each cooling channel (90) comprising a serpentine shape.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Feb 10 00:00:00 EST 2015},
month = {Tue Feb 10 00:00:00 EST 2015}
}

Patent:

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