Bucket for the last stage of a steam turbine
AssigneeGeneral Electric Company
InventorsJonathon E. Slepski, Andrey A. Chernobrovkin
Life of this patent
Estimating the term…
Abstract
A turbine bucket including a bucket airfoil having an airfoil shape is provided. The airfoil shape has a nominal profile according to the tables set forth in the specification. The X and Y coordinate are smoothly joined by an arc of radius R defining airfoil profile sections at each distance Z. The profile sections at the Z distances are joined smoothly with one another to form a complete airfoil shape.
Claims20
A turbine bucket including a bucket airfoil having an airfoil shape, said airfoil comprising a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z and arc coordinate R set forth in Tables 1-19 wherein the X, Y, Z and R distances are in inches, the X and Y coordinate values being smoothly joined by an arc of radius R defining airfoil profile sections at each distance Z, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
A turbine wheel comprising a plurality of buckets, each of said buckets including an airfoil having an airfoil shape, said airfoil comprising a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z and arc coordinate R set forth in Tables 1-19 wherein the X, Y, Z and R distances are in inches, the X and Y coordinate values being smoothly joined by an arc of radius R defining airfoil profile sections at each distance Z, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
A turbine comprising a turbine wheel having a plurality of buckets, each of said buckets including an airfoil comprising a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z and arc coordinate R set forth in Tables 1-19 wherein the X, Y, Z and R distances are in inches, the X and Y coordinate values being smoothly joined by an arc of radius R defining airfoil profile sections at each distance Z, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
Dependencies are inferred from the claim text.