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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.
Authors:
Publication Date:
OSTI Identifier:
1162125
Report Number(s):
8,870,537
13/942,782
DOE Contract Number:
FC26-05NT42644
Resource Type:
Patent
Research Org:
Mikro Systems, Inc., Charlottesville, VA (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING