Gas turbine including sealing band and anti-rotation device

Patent metadata

Field	Value
Publication number	US-9808889-B2
Application number	US-201414155585-A
Country	US
Kind code	B2
Filing date	Jan 15, 2014
Priority date	Jan 15, 2014
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

A turbine is provided comprising a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, at least one pair of adjacent rotatable disks defining an annular gap therebetween and having respective opposing sealing band receiving slots aligned with the annular gap A sealing band is located in the opposing receiving slots to seal the annular gap Disk engagement structure is defined in the pair of adjacent rotatable disks. A clip member is coupled to the sealing band and engaged with the pair of adjacent rotatable disks through the disk engagement structure The clip member may have an aperture extending only partially through the clip member for alignment with a hole in the sealing band for engagement with a tool To improve weld geometry, the clip member may have angled surfaces and notched areas, and the sealing band may have chamfered edges.

First claim

What is claimed is:

1. A turbine comprising:
a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, at least one pair of adjacent rotatable disks defining an annular gap therebetween and having respective opposing sealing band receiving slots aligned with the gap;
a sealing band located in said opposing sealing band receiving slots to seal said annular gap;
disk engagement structure defined in said pair of adjacent rotatable disks; and
a clip member coupled to said sealing band and in engagement with said pair of adjacent rotatable disks through said disk engagement structure, said clip member having an aperture extending only part way through said clip member and used during assembly of said clip member to said sealing band, said clip member restricting movement of said sealing band.

2. The turbine of claim 1 , further comprising:
band engagement structure comprising a pair of circumferentially aligned band notches in opposing edges of said sealing band.

3. The turbine of claim 1 , wherein said clip member comprises a U-shaped member having first and second legs and a center portion, said aperture being provided in said center portion.

4. The turbine of claim 3 , further comprising:
attachment structure affixing said legs of said U-shaped member to said sealing band.

5. The turbine of claim 4 , wherein said attachment structure comprises welded joints between said U-shaped member legs and said band.

6. The turbine of claim 5 , wherein said sealing band includes a hole located between axially spaced-apart first and second edges of said sealing band, said hole in said sealing band being generally aligned with said aperture in said clip member so as to allow a tool to pass through said sealing band hole and threadedly engage with said clip member aperture so as to retain said clip member in engagement with said sealing band during the formation of said welded joints between said U-shaped member legs and said sealing band.

7. The turbine of claim 5 , wherein prior to the formation of the welded joints, a first edge of said sealing band comprises a first chamfer and a second edge of said sealing band comprises a second chamfer, a first angle greater than about 50 degrees is defined by said first chamfer and an angled first surface of said first leg of said U-shaped member and a second angle greater than about 50 degrees is defined by said second chamfer and an angled second surface of said second leg of said U-shaped member.

8. The turbine of claim 7 , wherein prior to the formation of the welded joints, a first notched relief area is defined at an intersection of said first surface of said first leg of said U-shaped member and an engagement surface of said center portion of said U-shaped member and a second notched relief area is defined at an intersection of said second surface of said second leg of said U-shaped member and the engagement surface of said center portion of the U-shaped member.

9. The turbine of claim 7 , further comprising band engagement structure comprising first and second circumferentially aligned band notches in opposing edges of said sealing band, said first chamfer being defined in said first notch and said second chamfer being defined in said second notch.

10. A turbine comprising:
a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, at least one pair of adjacent rotatable disks defining an annular gap therebetween and having respective opposing sealing band receiving slots aligned with the gap;
a sealing band located in said opposing sealing band receiving slots to seal said annular gap, said sealing band comprising axially spaced-apart first and second edges;
disk engagement structure defined in said pair of adjacent rotatable disks; a clip member coupled to said sealing band and in engagement with said pair of adjacent rotatable disks through said disk engagement structure, said clip member comprising a U-shaped member having first and second legs and a center portion, said clip member restricting movement of said sealing band; and
welded joints affixing said legs of said U-shaped member to said sealing band,
wherein prior to said welded joints being formed, said first edge of said sealing band comprises a first chamfer and a first angle greater than about 50 degrees is defined by said first chamfer and an angled first surface of said first leg of said U-shaped member.

11. The turbine of claim 10 , wherein prior to said welded joints being formed, said second edge of said sealing band comprises a second chamfer and a second angle greater than about 50 degrees is defined by said second chamfer and an angled second surface of said second leg of said U-shaped member.

12. The turbine of claim 11 , wherein said first edge of said sealing band further comprises a third chamfer and said second edge of said sealing band further comprises a fourth chamfer, said first and third chamfers defining a first V-edge and said second and fourth chamfers defining a second V-edge.

13. The turbine of claim 12 , wherein each of said first and second V-edges define an angle falling within a range of from about 85 to about 95 degrees.

14. The turbine of claim 11 , wherein prior to said welded joints being formed, a first notched relief area is defined at an intersection of said first surface of said first leg of said U-shaped member leg and an engagement surface of said center portion of the U-shaped member and a second notched relief area is defined at an intersection of said second surface of said second leg of said U-shaped member leg and a band adjacent surface of said center portion of the U-shaped member.

15. A process for coupling a clip member to a sealing band located in opposing sealing band receiving slots of a pair of adjacent rotatable disks of a turbine, the clip comprising a U-shaped member having first and second legs and a center portion provided with an aperture extending only part way through the clip member, the sealing band comprising a hole located between axially spaced-apart first and second edges of the sealing band, the process comprising:
aligning the aperture in the U-shaped member center portion with the hole in the sealing band;
passing a tool through the sealing band hole;
threadedly engaging the tool with the U-shaped member aperture so as to retain said clip member in engagement with said sealing band; and
forming welded joints between the U-shaped member legs and the band.

16. The process of claim 15 , wherein prior to the formation of the welded joints, the first edge of the sealing band comprises a first chamfer and the second edge of the sealing band comprises a second chamfer, a first angle greater than about 50 degrees is defined by the first chamfer and an angled first surface of the first leg of the U-shaped member and a second angle greater than about 50 degrees is defined by the second chamfer and an angled second surface of the second leg of the U-shaped member.

17. The process of claim 16 , wherein prior to the formation of the welded joints, a first notched relief area is defined at an intersection of the first surface of the first leg of said U-shaped member and an engagement surface of the center portion of the U-shaped member and a second notched relief area is defined at an intersection of the second surface of the second leg of said U-shaped member and the engagement surface of the center portion of the U-shaped member.

Assignees

• Siemens Energy Inc

Inventors

• Mitchell David J
• Olejarski Michael J
• Muller Christopher J

Classifications

• B23K2101/001

  Turbines · CPC title

• B23K31/02 Primary

  relating to soldering or welding · CPC title

• F05D2230/232

  by welding · CPC title

• B23K33/004

  Filling of continuous seams · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title