Belly band seal with anti-rotation structure

Patent metadata

Field	Value
Publication number	US-9845698-B2
Application number	US-201514748271-A
Country	US
Kind code	B2
Filing date	Jun 24, 2015
Priority date	Jun 24, 2015
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

A belly band seal for use in a multi-stage turbomachine having plural rotor disks includes a seal strip positionable in a space between a pair of arms defined by opposing portions of adjoining rotors. The seal strip includes opposite edges for locating in respective slots in end faces of said pair of arms. The belly band seal further includes an anti-rotation structure disposed on a radially inner surface of the seal strip. The anti-rotation structure is configured as a cantilever having a pivoted end fixed to the radially inner surface and a free end comprising a radially inwardly extending engagement member for removably positioning in a radial recess in one of the arms. The cantilever is configured so as to urge the engagement member toward the radial recess by spring action. The radial recess is configured to constrain a tangential movement of the engagement member upon being positioned therein.

First claim

What is claimed is:

1. A belly band seal for use in a turbomachine having a plurality of stages comprising plural rotor disks, and arms on opposed portions of adjoining rotor disks to define paired arms with a space therebetween, said paired arms comprising respective end faces including slots, the belly band seal comprising:
a seal strip for positioning in said space between said paired arms, the seal strip being in the shape of a segment of a ring having opposite edges for locating in respective slots of said paired arms and coaxial to the rotor disks;
an anti-rotation structure disposed on a radially inner surface of the seal strip, the anti-rotation structure being configured as a cantilever having a pivoted end fixed to the radially inner surface of the seal strip and a free end comprising a radially inwardly extending engagement member for removably positioning in a radial recess provided on one of the arms of the paired arms;
wherein the cantilever is rotatable about a pivot axis and is configured to be in a deflected state during assembly of the seal strip, and in a natural state when a final assembly position is reached;
wherein the cantilever is configured so as to urge the engagement member toward the radial recess by spring action upon reaching of the final assembly position, and
wherein the radial recess is configured to constrain a tangential movement of the engagement member upon being positioned therein.

2. The belly band seal according to claim 1 , wherein the anti-rotation structure and the seal strip are machined from a metal bar.

3. The belly band seal according to claim 1 , wherein the engagement member is a pin having a generally cylindrical shape.

4. The belly band seal according to claim 1 , wherein the engagement member has a bolted design comprising a hexagonal shape.

5. The belly band seal according to claim 1 , wherein the engagement member further comprises a verification pin that is configured to snap into a through-opening in the seal strip when the engagement member is properly positioned in the radial recess.

6. The belly band seal according to claim 5 , wherein upon snapping into the through-opening, the verification pin protrudes outwardly from a radially outer surface of the seal strip.

7. The belly band seal according to claim 6 , wherein the point of protrusion of the verification pin is located in the respective slot in the end face of said one of the arms.

8. The belly band seal according to claim 6 , wherein the point of protrusion of the verification pin is located in the space between the paired arms.

9. The belly band seal according to claim 1 , wherein the pivoted end of the cantilever comprises a region with reduced material defining a recess.

10. The belly band seal according to claim 1 , wherein the seal strip comprises a provision for attaching a temporary retaining structure to hold the cantilever in a deflected position to allow unobstructed movement of the belly band seal during its assembly, until a final assembly position is reached.

11. A multi-stage turbmomachine comprising:
a plurality of rotor disks, comprising arms on opposed portions of adjoining rotor disks that define paired arms with a space therebetween, said paired arms comprising respective end faces including slots;
a belly band seal comprising:
a seal strip positioned in said space between said paired arms, the seal strip being in the shape of a segment of a ring having opposite edges located in respective slots of said paired arms, wherein the ring is coaxial to the rotor disks;
an anti-rotation structure disposed on a radially inner surface of the seal strip, the anti-rotation structure being configured as a cantilever having a pivoted end fixed to the radially inner surface of the seal strip and a free end comprising a radially inwardly extending engagement member removably positioned in a radial recess provided on one of the arms of the paired arms;

wherein the cantilever is rotatable about a pivot axis and is configured to be in a deflected state during assembly of the seal strip, and in a natural state when a final assembly position is reached:
wherein the cantilever is configured so as to urge the engagement member toward the radial recess by spring action upon reaching of the final assembly position, and

wherein the radial recess is configured to constrain a tangential movement of the engagement member positioned therein.

12. The multi-stage turbomachine according to claim 11 , wherein the engagement member further comprises a verification pin snaps into a through-opening in the seal strip when the engagement member is properly positioned in the radial recess.

13. The multi-stage turbomachine according to claim 12 , wherein the verification pin protrudes outwardly from a radially outer surface of the seal strip.

14. The multi-stage turbomachine according to claim 13 , wherein the point of protrusion of the verification pin is located in the respective slot in the end face of said one of the arms.

15. The multi-stage turbomachine according to claim 13 , wherein the point of protrusion of the verification pin is located in the space between the pair of arms.

16. A method for assembling a belly band seal in a multi-stage turbomachine, the bellyband seal comprising a seal strip in the shape of a segment of a ring and an anti-rotation structure disposed on to a radially inner surface of the seal strip, the anti-rotation structure being configured as a cantilever having a pivoted end fixed to the radially inner surface of the seal strip and a free end comprising a radially inwardly extending engagement member, the method comprising:
arranging the belly band seal to cover an annular space between a pair of arms formed by opposed portions of adjoining rotor disks of the multi-stage turbomachine by positioning the seal strip such that opposite edges of the seal strip are located in respective slots of said pair of arms;
moving the seal strip along the slots in a circumferential direction until a final assembly position is reached wherein the engagement member is aligned with a radial recess in one of the arms of the pair of arms, wherein during the movement of the seal strip, the free end of the cantilever is deflected and held in position by a temporary retaining structure to allow unobstructed passage of the seal strip through the slots;
upon reaching the final assembly position, releasing the free end of the cantilever whereby the engagement member is urged towards the radial recess and held therein by spring action of the cantilever;
wherein the radial recess constrains a tangential movement of the engagement member positioned therein.

17. The method according to claim 16 , wherein the temporary retention structure is a pin which is removably supported in a pin-hole on the seal strip to hold the cantilever in the deflected position during the movement of the seal strip.

18. The method according to claim 16 , wherein the engagement member further comprises a verification pin that is configured to snap into a through-opening in the seal strip when the engagement member is properly positioned in the radial recess,
wherein the method further comprises verifying that the engagement member is properly positioned in the radial recess by inspecting if the verification pin has snapped into positioned into the through-opening in the seal strip.

19. The method according to claim 18 , wherein upon snapping into through-opening, the verification pin protrudes outwardly from a radially outer surface of the seal strip,
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Assignees

• Siemens Energy Inc

Inventors

• Brooks Robert T
• Gurao Manish S

Classifications

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F05D2240/55

  Seals · CPC title

• F05D2250/411

  in rotation · CPC title

• F01D11/005 Primary

  Sealing means between non relatively rotating elements · CPC title