Near-wall serpentine cooled turbine airfoil
Patent
·
OSTI ID:1162125
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.
- Research Organization:
- Mikro Systems, Inc., Charlottesville, VA (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FC26-05NT42644
- Assignee:
- Mikro Systems, Inc. (Charlottesville, VA)
- Patent Number(s):
- 8,870,537
- Application Number:
- 13/942,782
- OSTI ID:
- 1162125
- Resource Relation:
- Patent File Date: 2013 Jul 16
- Country of Publication:
- United States
- Language:
- English
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