Curved blade retention slot for turbine blade in a turbine disk

Patent metadata

Field	Value
Publication number	US-10273815-B2
Application number	US-201715498520-A
Country	US
Kind code	B2
Filing date	Apr 27, 2017
Priority date	Feb 26, 2008
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A method of forming a curved slot in a turbine disk includes the steps of forming a pre-slot in the turbine disk and finishing the pre-slot to form a slot that receives a portion of a turbine blade. The turbine disk including a first face, an opposing second face, and an outer perimeter surface extending between the first face and the opposing second face. The pre-slot includes a first curved wall and a second curved wall that each extend between the first face and the opposing second face. An intersection between the outer perimeter surface and each of the first curved wall and the second curved wall is defined by a curved line.

First claim

What is claimed is:

1. A turbine disk comprising:
a body portion including a first face that defines a first plane, an opposing second face that defines a second plane, and an outer circumferential surface extending between the first face and the opposing second face; and
a curved slot in the body portion that extends between the first face and the opposing second face, wherein the curved slot is defined by a first curved wall and a second curved wall, wherein the first curved wall and the second curved wall each extend between the first face and the opposing second face, and the curved slot receives a portion of a turbine blade, and wherein the first curved wall and the second curved wall have a center of curvature that is at a location outside an area between the first and second planes.

2. The turbine disk as recited in claim 1 wherein the curved slot defines an opening of the curved slot, and the opening is on an outer perimeter surface and is defined by a first curved line at a first intersection of the first curved wall and the outer circumferential surface and a second curved line at a second intersection of the second curved wall and the outer circumferential surface.

3. The turbine disk as recited in claim 2 wherein the first curved line and the second curved line are a portion of a circle.

4. The turbine disk as recited in claim 1 wherein a bottom wall is located between the first curved wall and the second curved wall.

5. The turbine disk as recited in claim 4 wherein an entirety of the first curved wall and an entirety of the second curved wall are substantially perpendicular to the bottom wall.

6. The turbine disk as recited in claim 1 wherein the curved slot includes a plurality of fingers and grooves.

7. The turbine disk as recited in claim 1 wherein a distance between the first curved wall and the second curved wall defines a width of the curved slot, and the width is constant for an entire curved distance of the curved slot.

8. The turbine disk as recited in claim 7 wherein the distance between the first curved wall and the second curved wall is constant along an entire height of the curved slot.

9. The turbine disk as recited in claim 1 , wherein the first curved wall and the second curved wall have the same center of curvature.

10. A turbine comprising:
a turbine disk including a body portion including a first face that defines a first plane, an opposing second face that defines a second plane, and an outer circumferential surface extending between the first face and the opposing second face, the turbine disk including a curved slot in the body portion that extends between the first face and the opposing second face, wherein the curved slot is defined by a first curved wall and a second curved wall, wherein the first curved wall and the second curved wall each extend between the first face and the opposing second face and have a center of curvature that is at a location outside an area between the first and second planes, and wherein the curved slot receives a portion of a turbine blade; and
a turbine blade having a curved base, wherein a curvature of the curved base of the turbine blade corresponds to a curvature of the first and second curved walls of the turbine disk, and the base of the turbine blade is received in the curved slot of the turbine disk.

11. The turbine as recited in claim 10 wherein the curved slot defines an opening of the curved slot, and the opening is on an outer perimeter surface and is defined by a first curved line at a first intersection of the first curved wall and the outer circumferential surface and a second curved line at a second intersection of the second curved wall and the outer circumferential surface.

12. The turbine as recited in claim 11 wherein the first curved line and the second curved line are a portion of a circle.

13. The turbine as recited in claim 10 wherein a bottom wall is located between the first curved wall and the second curved wall.

14. The turbine as recited in claim 13 wherein an entirety of the first curved wall and an entirety of the second curved wall are substantially perpendicular to the bottom wall.

15. The turbine as recited in claim 10 wherein the curved slot includes a plurality of fingers and grooves.

16. The turbine as recited in claim 10 wherein a distance between the first curved wall and the second curved wall defines a width of the curved slot, and the width is constant for an entire curved distance of the slot.

17. The turbine as recited in claim 16 wherein the distance between the first curved wall and the second curved wall is constant along an entire height of the curved slot.

18. The turbine as recited in claim 10 wherein the curved slot includes at least one finger and at least one groove and the curved base of the turbine blade includes at least one finger and at least one groove, wherein the at least one finger of the base of the turbine blade is received in the at least one groove of the curved slot and the at least one finger of the curved slot is received in the at least one groove of the base of the turbine blade.

19. The turbine as recited in claim 10 further including a plurality of slots and a plurality of turbine blades, wherein one of the plurality of turbine blades is received in each of the plurality of slots of the turbine disk.

20. The turbine as recited in claim 10 , wherein the first curved wall and the second curved wall have the same center of curvature.

Assignees

• United Technologies Corp

Inventors

• Guo Changsheng

Classifications

• F05D2240/30

  Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor · CPC title

• Y10T29/49336

  Blade making · CPC title

• F05D2250/71

  curved · CPC title

• F05D2220/32

  in gas turbines · CPC title

• B23C3/34

  Milling grooves of other forms, e.g. circumferential · CPC title