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Title: Near-wall serpentine cooled turbine airfoil

A serpentine coolant flow path is formed by inner walls in a cavity between pressure and suction side walls of a turbine airfoil, the cavity partitioned by one or more transverse partitions into a plurality of continuous serpentine cooling flow streams each having a respective coolant inlet.
Inventors:
Issue Date:
OSTI Identifier:
1162125
Assignee:
Mikro Systems, Inc. (Charlottesville, VA) NETL
Patent Number(s):
8,870,537
Application Number:
13/942,782
Contract Number:
FC26-05NT42644
Resource Relation:
Patent File Date: 2013 Jul 16
Research Org:
Mikro Systems, Inc., Charlottesville, VA (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

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