Bucket dovetail bridge member and method for eliminating thermal bowing of steam turbine rotors

• US 6,558,118 B1
• Filed: 11/01/2001
• Issued: 05/06/2003
• Est. Priority Date: 11/01/2001
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Turnquist, Norman Arnold, Wolfe, Christopher Edward, Burnett, Mark Edward, Caruso, David Alan, Baily, Frederick George, Brisson, Bruce William
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): McAleenan, James M
• Application Number:
  US09/985,183
• Publication Number:
  US 20030082049A1
• Time in Patent Office: 551 Days
• Field of Search: 415/173.7, 415/174.2, 415/174.5, 415/231, 415/173.3, 415/173.5, 415/173.4, 415/174.4, 415/176, 415/178, 415/230
• US Class Current: 415/173.7
• CPC Class Codes: F01D 11/003 by packing rings; Mechanical seals
• CPC Class Codes: F01D 11/02 by non-contact sealings, e.g. of labyrinth type for sealing space between rotor blade tips and stator F01D11/08
• CPC Class Codes: F05D 2240/56 Brush seals

Abstract

A steam turbine has a rotor mounting axially spaced rotor wheels having male dovetails for mounting a plurality of axially spaced buckets having female dovetails. A plurality of arcuate bridging members extend axially between the axially adjacent bucket dovetails at locations spaced radially outwardly of the surface of the rotor shaft. A diaphragm in radial opposition to the bridging member mounts a brush seal having bristles engaging the bridging member. The bridging member carries backup labyrinth seal teeth for sealing with the diaphragm. The friction generated by contact between the brush seal bristles and bridging members lies radially outwardly of the rotor whereby non-uniform distribution of heat about the rotor surface due to frictional contact with the brush seal is avoided, with consequent avoidance of rotor bowing.

Claims

1. A steam turbine comprising:

a rotatable component including a rotor shaft carrying axially adjacent bucket rows and a non-rotatable component about said rotatable component, said rotor shaft having a shaft surface;

a bridging member extending generally axially between said adjacent bucket rows at a location spaced radially outwardly of said shaft surface and mounted for rotation with said rotatable component, said bridging member engaging said adjacent bucket rows; and

a brush seal carried by said non-rotatable component for sealing engagement with said bridging member.

2. A turbine according to claim 1 wherein said non-rotatable component has a diaphragm with an inner web spaced radially outwards of said rotor shaft surface and said bridging member, said brush seal extending between said web and said bridging member.

3. A turbine according to claim 1 including a labyrinth seal having at least one tooth extending between said non-rotating component and said bridging member and spaced generally radially from said shaft surface.

4. A turbine according to claim 1 wherein said rotatable component includes a plurality of buckets having bucket dovetails for connection with complementary dovetails on a wheel of said rotatable component, said bridging member extending axially between and being connected to said bucket dovetails.

5. A turbine according to claim 4 including tongue-and-groove connections between the bridging member and the bucket dovetails.

6. A turbine according to claim 4 wherein said bridging member and portions of the rotatable and non-rotatable components define at least one wheelspace void radially inwardly of said bridging member.

7. A turbine according to claim 1 including a labyrinth seal having at least one tooth extending between said non-rotatable component and said bridging member and spaced generally radially from said rotor shaft surface, said labyrinth seal tooth being carried by said bridging member and extending radially outwardly toward said rotatable component.

8. A turbine according to claim 7 including a plurality of axially spaced labyrinth seal teeth carried by said bridging member and extending radially outwardly toward said non-rotatable component.

9. A turbine according to claim 7 wherein said bridging member and portions of the rotatable and non-rotatable components define at least one wheelspace void radially inwardly of said bridging member, said brush seal lying in contact with said bridging member at an axial location therealong in radial alignment with said void.

10. A turbine according to claim 9 including a plurality of axially spaced labyrinth seal teeth carried by said bridging member and extending radially outwardly toward said non-rotatable component.

11. A turbine according to claim 1 wherein said bridging member comprises a plurality of bridging elements arranged in an annular array about and in spaced relation to said shaft, said rotatable component including a plurality of buckets having bucket dovetails for connection with complementary dovetails on a wheel of said rotatable component, said bridging member extending between and being connected to said bucket dovetails.

12. A turbine according to claim 11 wherein each said bridging element has a circumferential extent in excess of the circumferential extent of the bucket dovetails.

13. A turbine according to claim 12 wherein each said bridging member has a circumferential extent of about 1.5 bucket pitches of the bucket dovetail.

14. A turbine according to claim 4 wherein said rotatable shaft includes a generally annular rim extending generally radially outwardly from said shaft surface and a fastening element between said rim and said bridging member connecting said rim and said bridging member to one another at a location intermediate axial end edges of said bridging member.

15. In a steam turbine having a rotatable component including a rotor shaft having a rotor shaft surface and a non-rotatable component about the rotatable component carrying a brush seal for sealing engagement with the rotatable component, a method of substantially eliminating bowing of the rotor resulting from circumferential non-uniform distribution of heat about the rotor shaft surface due to frictional contact between the brush seal and the rotatable component, comprising the step of inhibiting circumferential non-uniform heat transfer to the rotor shaft surface generated by frictional contact between the rotatable component and the brush seal by extending a bridging member between axially spaced bucket dovetails at a location radially outwardly of said rotor shaft, engaging said bridging member with said bucket rows and engaging the brush seal against the bridging member.

16. A method according to claim 15 including providing at least one labyrinth tooth on the bridging member for sealing with the non-rotatable component.

17. A method according to claim 15 including providing a rim projecting radially outwardly from the shaft surface between male dovetails for the buckets and mounting the bridging member on the rim.

18. A method according to claim 15 including mounting a plurality of bridging members between axially adjacent buckets at a radial location defining at least one void between said bridging member and the shaft radially inwardly of said bridging member.

19. A method according to claim 15 including securing axially opposite end edges of said bridging member to axially adjacent bucket dovetails by a tongue-and-groove connection.

20. A method according to claim 15 wherein the rotatable component includes axially spaced wheels having male dovetails and the bucket dovetails are configured for tangential entry along the male dovetails and including the step of disposing a plurality of bridging members in a tangential direction between the bucket dovetails to stack the bridging members against one another in a tangential direction.