Turbine blade having a constant thickness airfoil skin
Patent
·
OSTI ID:1079403
A turbine blade is provided for a gas turbine comprising: a support structure comprising a base defining a root of the blade and a framework extending radially outwardly from the base, and an outer skin coupled to the support structure framework. The skin has a generally constant thickness along substantially the entire radial extent thereof. The framework and the skin define an airfoil of the blade.
- Research Organization:
- Siemens Energy, Inc. (Orlando, FL)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FC26-05NT42644
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- Patent Number(s):
- 8,292,583
- Application Number:
- 12/540,430
- OSTI ID:
- 1079403
- Country of Publication:
- United States
- Language:
- English
Transient Liquid Phase Bonding
|
journal | August 1992 |
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