Steam turbine drum nozzle having alignment feature, related assembly, steam turbine and storage medium

• US 10,287,903 B2
• Filed: 04/06/2016
• Issued: 05/14/2019
• Est. Priority Date: 04/06/2016
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Burdgick, Steven Sebastian, Delorenzo, Mark Richard
• Primary Examiner(s): Verdier, Christopher
• Assistant Examiner(s): Davis, Jason G
• Application Number:
  US15/092,090
• Publication Number:
  US 20170292391A1
• Time in Patent Office: 1,133 Days
• CPC Class Codes: F01D 9/041 using blades F01D5/148 takes precedence
• CPC Class Codes: F01D 9/042 fixing blades to stators fixing stator-rings in the casing or to each other F01D25/246
• CPC Class Codes: F05D 2220/31 in steam turbines
• CPC Class Codes: F05D 2230/20 essentially without removing material
• CPC Class Codes: F05D 2230/64 using positioning or alignment devices for aligning or centring, e.g. pins
• CPC Class Codes: F05D 2240/128 Nozzles

Abstract

Various embodiments include a steam turbine drum nozzle, along with a related assembly and steam turbine. Particular embodiments include a nozzle having: an airfoil; a radially inner sidewall coupled with a first end of the airfoil; and a radially outer sidewall coupled with a second end of the airfoil, the second end opposing the first end, wherein the radially outer sidewall includes: a first section radially outward of the airfoil; a thinned section coupled with the first section; and a second section coupled with the thinned section radially outward of the airfoil, the second section having a radially outer face and a circumferentially facing side abutting the radially outer face, wherein the second section includes a circumferentially extending slot, and wherein the second section includes a relief slot extending into a body of the second section from the circumferentially facing side.

Claims

1. A steam turbine drum nozzle comprising:

an airfoil;

a radially inner sidewall coupled with a first end of the airfoil; and

a radially outer sidewall coupled with a second end of the airfoil, the second end opposing the first end, wherein the radially outer sidewall includes;

a first section radially outward of the airfoil;

a thinned section coupled with the first section; and

a second section coupled with the thinned section radially outward of the airfoil, the second section having a radially outer face and a circumferentially facing side abutting the radially outer face,

wherein the second section includes a circumferentially extending slot,

wherein the second section includes a relief slot extending into a body of the second section from the circumferentially facing side, and

wherein the relief slot extends from an approximate axial midpoint on the circumferentially facing side to a location axially inboard of an axially facing surface of the second section.

2. The steam turbine drum nozzle of claim 1, wherein the first section includes a first set of axially extending protrusions, the thinned section is radially outward of the first set of axially extending protrusions, and the second section includes a second set of axially extending protrusions radially outward of the thinned section.

3. The steam turbine drum nozzle of claim 1, wherein the circumferentially extending slot extends substantially entirely through the second section at the radially outer face.

4. The steam turbine drum nozzle of claim 1, wherein the relief slot at least partially surrounds the circumferentially extending slot.

5. The steam turbine drum nozzle of claim 1, wherein the relief slot abuts the circumferentially extending slot.

6. The steam turbine drum nozzle of claim 1, wherein the relief slot extends from the circumferentially facing side into the second section at an angle of approximately between one degree and five degrees.

7. The steam turbine drum nozzle of claim 1, wherein the relief slot has a circumferentially facing surface and is configured to align the circumferentially facing surface of the relief slot with a horizontal joint surface of a drum nozzle ring, the horizontal joint surface of the drum nozzle ring being a plane on a circumferential end of one of two halves that form the drum nozzle ring.

8. The steam turbine drum nozzle of claim 7, wherein the alignment of the circumferentially facing surface of the relief slot with the horizontal joint surface of the drum nozzle ring includes the circumferentially facing surface of the relief slot being coplanar with the horizontal joint surface of the drum nozzle ring.

9. A steam turbine comprising:

a drum nozzle ring having a first circumferentially extending slot therein; and

a plurality of drum nozzles aligned within the first circumferentially extending slot, at least one of the plurality of drum nozzles including;

an airfoil;

a radially inner sidewall coupled with a first end of the airfoil; and

a radially outer sidewall coupled with a second end of the airfoil, the second end opposing the first end, wherein the radially outer sidewall includes;

a first section radially outward of the airfoil;

a thinned section coupled with the first section; and

a second section coupled with the thinned section radially outward of the airfoil, the second section having a radially outer face and a circumferentially facing side abutting the radially outer face,

wherein the second section includes a second circumferentially extending slot,

wherein the second section includes a relief slot extending into a body of the second section from the circumferentially facing side, and

wherein the relief slot extends from an approximate axial midpoint on the circumferentially facing side to a location axially inboard of an axially facing surface of the second section.

10. The steam turbine of claim 9, wherein the first section includes a first set of axially extending protrusions, the thinned section is radially outward of the first set of axially extending protrusions, and the second section includes a second set of axially extending protrusions radially outward of the thinned section.

11. The steam turbine of claim 9, wherein the second circumferentially extending slot extends substantially entirely through the second section at the radially outer face.

12. The steam turbine of claim 9, wherein the relief slot at least partially surrounds the second circumferentially extending slot.

13. The steam turbine of claim 9, wherein the relief slot abuts the second circumferentially extending slot.

14. The steam turbine of claim 9, wherein the relief slot extends from the circumferentially facing side into the second section at an angle of approximately between one degree and five degrees.

15. The steam turbine of claim 9, wherein the drum nozzle ring is at least partially contained within a stator section.

16. The steam turbine of claim 15, further comprising a rotor section at least partially surrounded by the stator section.

17. The steam turbine of claim 9, wherein the relief slot has a circumferentially facing surface and is configured to align the circumferentially facing surface of the relief slot with a horizontal joint surface of the drum nozzle ring, the horizontal joint surface of the drum nozzle ring being a plane on a circumferential end of one of two halves that form the drum nozzle ring.

18. The steam turbine of claim 17, wherein the alignment of the circumferentially facing surface of the relief slot with the horizontal joint surface of the drum nozzle ring includes the circumferentially facing surface of the relief slot being coplanar with the horizontal joint surface of the drum nozzle ring.