Second Stage Turbine Bucket Airfoil.
Abstract
The second-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.
- Inventors:
-
- (Simpsonville, SC)
- (Clifton Park, NY)
- (Maineville, OH)
- Issue Date:
- Research Org.:
- GENERAL ELECTRIC CO
- OSTI Identifier:
- 879729
- Patent Number(s):
- 6,558,122
- Application Number:
- 09/987433
- Assignee:
- General Electric Company (Schenectady, NY) NETL
- DOE Contract Number:
- FC21-95MC31176
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Xu, Liming, Ahmadi, Majid, Humanchuk, David John, Moretto, Nicholas, and Delehanty, Richard Edward. Second Stage Turbine Bucket Airfoil.. United States: N. p., 2003.
Web.
Xu, Liming, Ahmadi, Majid, Humanchuk, David John, Moretto, Nicholas, & Delehanty, Richard Edward. Second Stage Turbine Bucket Airfoil.. United States.
Xu, Liming, Ahmadi, Majid, Humanchuk, David John, Moretto, Nicholas, and Delehanty, Richard Edward. Tue .
"Second Stage Turbine Bucket Airfoil.". United States. https://www.osti.gov/servlets/purl/879729.
@article{osti_879729,
title = {Second Stage Turbine Bucket Airfoil.},
author = {Xu, Liming and Ahmadi, Majid and Humanchuk, David John and Moretto, Nicholas and Delehanty, Richard Edward},
abstractNote = {The second-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2003},
month = {5}
}
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