IP Library Granted Patent US 6,910,868
Granted Patent B2
US 6,910,868 · App. 10/624,632 · Granted Jun 28, 2005

Airfoil shape for a turbine bucket

Assignee: General Electric Company
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Quick Facts
Patent No.
US 6,910,868
App. No.
10/624,632
Granted
Jun 28, 2005
Kind
B2
Abstract

Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0 to 0.938 convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape. The X and Y distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of ±0.150 inches in directions normal to the surface of the airfoil.

Claims (21)

1. A turbine bucket including a bucket airfoil having an airfoil shape, said airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein the Z values are non-dimensional values from 0 to 0.938 convertible to Z distances in inches by multiplying the Z values by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define 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.

2. A turbine bucket according to claim 1 forming part of a third stage of a turbine.

3. A turbine bucket according to claim 1 wherein said airfoil shape lies in an envelope within ±0.150 inches in a direction normal to any airfoil surface location.

4. A turbine bucket according to claim 1 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

5. A turbine bucket including a bucket airfoil having an uncoated nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein the Z values are non-dimensional values from 0 to 0.938 convertible to Z distances in inches by multiplying the Z values by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each Z distance, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape, the X and Y values being scalable as a function of the same constant or number to provide a scaled-up or scaled-down airfoil.

6. A turbine bucket according to claim 5 forming part of a third stage of a turbine.

7. A turbine bucket according to claim 5 wherein said airfoil shape lies in an envelope within ±0.150 inches in a direction normal to any airfoil surface location.

8. A turbine bucket according to claim 5 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

9. A turbine comprising a turbine wheel having a plurality of buckets, each of said buckets including an airfoil having an airfoil shape, said airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein the Z values are non-dimensional values from 0 to 0.938 convertible to Z distances in inches by multiplying the Z values by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define the 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.

10. A turbine according to claim 9 wherein the turbine wheel comprises a third stage of the turbine.

11. A turbine according to claim 9 wherein the turbine wheel has 92 buckets and X represents a distance parallel to the turbine axis of rotation.

12. A turbine according to claim 9 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

13. A turbine according to claim 9 wherein the radial height between an axial centerline of said turbine wheel and a hub radius of each bucket airfoil at a leading edge thereof is 40.716 inches, the non-dimensionalized Z value at Z=0.000 starting at a radial height 41.891 inches from the axial centerline of the turbine wheel.

14. A turbine according to claim 13 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

15. A turbine comprising a turbine wheel having a plurality of buckets, each of said buckets including an airfoil having an uncoated nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein the Z values are non-dimensional values from 0 to 0.938 convertible to Z distances in inches by multiplying the Z values by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define 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, the X and Y distances being scalable as a function of the same constant or number to provide a scaled-up or scaled-down bucket airfoil.

16. A turbine according to claim 15 wherein the turbine wheel comprises a third stage of the turbine.

17. A turbine according to claim 15 wherein the turbine wheel has 92 buckets and X represents a distance parallel to the turbine axis of rotation.

18. A turbine according to claim 15 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

19. A turbine according to claim 15 wherein the radial height between an axial centerline of said turbine wheel and a hub radius of each bucket at a leading edge thereof is 40.716 inches, the non-dimensionalized Z value at 0.000 starting at a radial height 41.891 inches from the axial centerline of the turbine wheel.

20. A turbine according to claim 19 wherein the height of the airfoil from a value of Z=0 to a value of Z=0.938 is 15.146 inches.

21. A turbine according to claim 15 wherein the Z=0 coordinate value corresponds to 1.175 inches radially outwardly of an inlet hub radius of 40.716 inches at the leading edge of the airfoil.

Assignments (2)
CONFIRMATORY LICENSE Recorded May 23, 2018
From: GENERAL ELECTRIC GLOBAL RESEARCH CTR
To: UNITED STATES DEPARTMENT OF ENERGY
Reel/Frame 046222/0763 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 23, 2003
From: HYDE, SUSAN MARIE; BY, ROBERT ROMANY; TRESSLER, JUDD DODGE; SCHAEFFER, JON CONRAD; SIMS, CALVIN LEVY
To: GENERAL ELECTRIC COMPANY
Reel/Frame 014323/0402 →
Continuity (1)
Related Publication 20050019160A1 · Jan 27, 2005