Gas turbine including belly band seal anti-rotation device

Patent metadata

Field	Value
Publication number	US-9334738-B2
Application number	US-201213657900-A
Country	US
Kind code	B2
Filing date	Oct 23, 2012
Priority date	Oct 23, 2012
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

A sealing band is located in opposing sealing band receiving slots of adjacent turbine disks to seal an annular gap therebetween. A through hole is defined in one of the disks, wherein the through hole defines a longitudinal hole axis and extends to the sealing band receiving slot in the disk. At least one engagement feature is defined on the disk and extends laterally of the through hole, perpendicular to the longitudinal hole axis. A pin member extends through the hole and is positioned within the sealing band receiving slot passing through an opening in the sealing band for resisting movement of the sealing band relative to the disk. The pin member includes a laterally extending cooperating feature positioned in engagement with the engagement feature for retaining the pin within the opening in the sealing band.

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 annular gap;
a sealing band located in the opposing sealing band receiving slots to seal the annular gap;
a through hole defined in at least one of said disks, said through hole defining a longitudinal hole axis and extending to said sealing band receiving slot in said at least one disk;
at least one engagement feature on said at least one disk extending laterally of said through hole, perpendicular to said longitudinal hole axis;
a pin member extending through said through hole and positioned within said sealing band receiving slot passing through an opening in said sealing band for resisting movement of said sealing band relative to said at least one disk, said pin member including a laterally extending cooperating feature positioned in engagement with said at least one engagement feature for retaining said pin member within said opening in said sealing band; and
wherein said opening in said sealing band includes a notch formed in an edge of said sealing band, and said pin member includes a radially inner end located within said notch in said sealing band.

2. The turbine of claim 1 , wherein said laterally extending cooperating feature comprises a pair of tabs extending from laterally opposing sides of said radially inner end of said pin member, and said at least one engagement feature including a surface within said sealing band receiving slot in said at least one of said disks, extending laterally from said through hole, perpendicular to said longitudinal hole axis, for engagement with said pair of tabs.

3. The turbine of claim 2 , wherein said through hole includes a pair of opposing laterally extending lobe areas for permitting passage of said pair of tabs therethrough.

4. The turbine of claim 3 , wherein said pin member includes a radially outer end, opposite said radially inner end, having outwardly deformed portions extending into said pair of opposing laterally extending lobe areas for preventing rotation of said pin member within said through hole.

5. The turbine of claim 1 , wherein said at least one engagement feature and said laterally extending cooperating feature comprise threaded portions on said each of said through hole and said pin member, respectively.

6. The turbine of claim 1 , wherein said pin member includes a radially outer end, opposite said radially inner end, and including a blind hole extending into said radially outer end.

7. The turbine of claim 6 , wherein said through hole includes at least one laterally extending lobe area, and a circumferential wall defining said blind hole in said pin member defines at least one outwardly deformed portion extending into said at least one laterally extending lobe area for preventing rotation of said pin member within said through hole.

8. A turbine comprising:
a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, each rotatable disk including a radially outwardly facing side, 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, said sealing band receiving slots each including opposing outer and inner radially facing slot surfaces;
a sealing band located in the opposing sealing band receiving slots to seal the annular gap;
a through hole defined in at least one of said disks, extending from said radially outwardly facing side through said outer radially facing slot surface, said through hole defining a longitudinal hole axis and extending through only an outer portion of said at least one of said disks from said radially outwardly facing side to one of said sealing band receiving slots in said at least one of said disks;
at least one engagement feature on said at least one of said disks extending laterally of said through hole, perpendicular to said longitudinal hole axis;
a pin member extending through said through hole and positioned through an opening in said sealing band, said pin member including a laterally extending cooperating feature positioned in engagement with said at least one engagement feature for preventing radial outward movement of said pin member out of said through hole and said pin member including a radially inner end located adjacent said inner radially facing slot surface of said one of said sealing band receiving slots;
wherein said at least one engagement feature is located radially outward of said one of said sealing band receiving slots.

9. The turbine of claim 8 , wherein said laterally extending cooperating feature comprises a pair of tabs extending from laterally opposing sides of said radially inner end of said pin member, and said at least one engagement feature including a surface within said one of said sealing band receiving slots in said at least one of said disks, extending laterally from said through hole, perpendicular to said longitudinal hole axis, for engagement with said pair of tabs.

10. The turbine of claim 9 , wherein said at least one engagement feature for engaging said pair of tabs is defined by said outer radially facing slot surface.

11. The turbine of claim 9 , wherein said through hole includes a pair of opposing laterally extending lobe areas for permitting passage of said pair of tabs therethrough.

12. The turbine of claim 11 , wherein said pair of opposing laterally extending lobe areas comprise generally semi-circular areas extending laterally outwardly from a wall defining said through hole.

13. The turbine of claim 11 , wherein said pin member includes a radially outer end, opposite said radially inner end, having outwardly deformed portions extending into said pair of opposing laterally extending lobe areas for preventing rotation of said pin member within said through hole.

14. The turbine of claim 8 , wherein rotation of said pin member about said longitudinal hole axis positions said laterally extending cooperating feature into engagement with said at least one engagement feature.

15. The turbine of claim 14 , wherein said at least one engagement feature is defined by a screw thread and said laterally extending cooperating feature is defined by a screw thread engaged with said screw thread of said at least one engagement feature.

16. The turbine of claim 8 , wherein said pin member includes a radially outer end, opposite said radially inner end, and including a blind hole extending into said radially outer end.

17. The turbine of claim 16 , wherein said through hole includes at least one laterally extending lobe area, and a circumferential wall defining said blind hole in said pin member defines at least one outwardly deformed portion extending into said at least one laterally extending lobe area for preventing rotation of said pin member within said through hole.

18. The turbine of claim 16 , including a slot formed in a bottom surface of the blind hole for engagement with a tool to rotate the pin member within the through hole.

19. A turbine comprising:
a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, each rotatable disk including a radially outwardly facing side, at least one pair of adjacent rotatable disks defining an annular gap therebetween and having respective opposing sealing band receiving slots aligned with the ann

Assignees

• Nereim Brian D
• Kendall Rebecca L
• Sane Piyush
• Siemens Ag

Inventors

• Nereim Brian D
• Kendall Rebecca L
• Sane Piyush

Classifications

• F01D11/00

  Preventing or minimising internal leakage of working-fluid, e.g. between stages (sealings in general F16J {; sealing arrangements for transition ducts of combustor cans F01D9/023}) · CPC title

• F01D11/003 Primary

  by packing rings; Mechanical seals · CPC title

• F01D5/06 Primary

  Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections {(F01D5/022, F01D5/023 take precedence)} · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title