Apparatus and method for adjusting an inner casing of a turbomachine

Patent metadata

Field	Value
Publication number	US-9611759-B2
Application number	US-201414291070-A
Country	US
Kind code	B2
Filing date	May 30, 2014
Priority date	May 30, 2014
Publication date	Apr 4, 2017
Grant date	Apr 4, 2017

Abstract

A support assembly for externally adjusting an inner casing with respect to an outer casing for a turbomachine includes a carrier plate, a carrier block that is fixedly connected to the carrier plate, a restrictor block fixedly connected to the carrier plate, a rod coupled to the carrier plate, and a plate threadably connected to the rod. The carrier block includes an inclined side and a carrier side. The restrictor block includes a restrictor side and an inclined side. The restrictor side is generally oriented towards the carrier side. A vertical gap for receiving a support arm of an inner turbine casing is defined between the restrictor side and the carrier side. The plate may be rotated about the rod to cause simultaneous movement of the rod, the carrier plate, the carrier block and the restrictor block, thus adjusting the inner casing with respect to the outer casing.

First claim

What is claimed is:

1. A support assembly for externally adjusting an inner casing with respect to an outer casing for a turbomachine, comprising:
a carrier plate;
a carrier block fixedly connected to the carrier plate, the carrier block having an inclined side and a carrier side;
a restrictor block fixedly connected to the carrier plate, the restrictor block having a restrictor side and an inclined side, wherein the restrictor side is oriented towards the carrier side and a vertical gap is defined therebetween;
a rod coupled to the carrier plate; and
means for moving the rod, the carrier plate, the carrier block and the restrictor block threadably connected to the rod.

2. The support assembly as in claim 1 , wherein means for moving the rod, the carrier plate, the carrier block and the restrictor block comprises a lock plate threadably coupled to the rod.

3. The support assembly as in claim 1 , wherein the carrier side of the carrier block is configured to support a support arm of the inner turbine.

4. The support assembly as in claim 1 , further comprising a bushing for coupling the support assembly to the outer turbine casing, wherein the rod extends through the bushing and the rod is slideably coupled to the bushing.

5. The support assembly as in claim 4 , wherein the rod is configured to slide with respect to the bushing.

6. The support assembly as in claim 1 , further comprising a wear surface defined along at least a portion of the carrier side.

7. The support assembly as in claim 6 , wherein the wear surface is defined by at least one of a shim and a coating disposed along at least a portion of the carrier side.

8. The support assembly as in claim 1 , wherein a longitudinal axis of the rod extends substantially parallel to the inclined side of the carrier block and the inclined side of the restrictor block.

9. A turbine assembly, comprising:
an outer turbine casing, the outer turbine casing including a lower shelf having an inclined surface and an upper shelf having an inclined surface disposed along an inner surface of the outer turbine casing, the outer turbine casing further including an aperture extending through the outer casing between the lower shelf and the upper shelf;
an inner turbine casing at least partially surrounded by the outer turbine casing;
a support assembly for externally adjusting the inner turbine casing relative to the outer turbine casing, the support assembly including a carrier plate, a carrier block connected to the carrier plate, a restrictor block connected to the carrier plate, a rod connected to the carrier plate, the rod extending through the aperture of the outer turbine casing, and a lock plate threadably engaged with the rod outside of the outer turbine casing; and
wherein an inclined side of the carrier block is slideably engaged with the inclined surface of the lower shelf and an inclined side of the restrictor block is slideably engaged with the inclined surface of the upper shelf.

10. The turbine assembly as in claim 9 , wherein a longitudinal axis of the rod extends substantially parallel to the inclined side of the carrier block and the inclined side of the restrictor block.

11. The turbine assembly as in claim 9 , wherein the carrier plate, the carrier block, the restrictor block and the rod travel together when the lock plate is rotated.

12. The turbine assembly as in claim 9 , wherein the support assembly further comprises a bushing for coupling the support assembly to the outer turbine casing, wherein the rod extends through the bushing.

13. The turbine assembly as in claim 12 , wherein the rod is configured to slide with respect to the bushing as the lock plate is rotated.

14. The turbine assembly as in claim 9 , wherein the inner turbine casing further includes a support arm that extends radially outward from the inner turbine casing between the carrier block and the restrictor block, wherein a support surface of the support arm is engaged with a carrier side of the carrier block.

15. The turbine assembly as in claim 14 , further comprising a clearance gap defined between the support arm and a restrictor side of the restrictor block.

16. The turbine assembly as in claim 14 , further comprising a wear surface defined between the carrier side of the carrier block and the support surface of the support arm, wherein the wear surface is defined by at least one of a shim and a coating disposed along at least a portion of the carrier side.

17. The turbine assembly as in claim 9 , further comprising one or more bearings to facilitate relative movement between the support assembly and the outer turbine casing.

18. A method for adjusting an inner turbine casing with respect to an outer turbine casing, comprising:
providing an inner turbine casing including a support arm that includes a support surface;
providing an outer turbine casing including an aperture defined therethrough, wherein the outer turbine casing is radially outward from the inner turbine casing, wherein the outer turbine casing includes a lower shelf having an inclined surface and an upper shelf having an inclined surface; and
rotating a lock plate that is threadably connected to a rod of a support assembly coupled to the outer casing to simultaneously move a carrier plate, a carrier block that is slideably engaged with the inclined surface of the lower shelf and a restrictor block that is slideably engaged with the inclined surface of the restrictor block, wherein the rod extends through the aperture defined in the outer turbine casing and wherein the carrier block supports the support arm of the inner turbine casing.

19. The method as in claim 18 , further comprising rotating the lock plate about the rod to cause the carrier block to slide along the lower shelf and the restrictor block to slide along the upper shelf simultaneously to adjust a vertical position of the inner turbine casing with respect to the outer turbine casing.

20. The method as in claim 19 , wherein rotating the lock plate about the rod in a first rotational direction raises the inner turbine casing with respect to the outer turbine casing and rotating the lock plate about the rod in a second rotational direction lowers the inner turbine casing with respect to the outer turbine casing.

Assignees

• Gen Electric

Inventors

• Adaickalasamy James
• Akulu Pramod
• Black Kenneth Damon

Classifications

• F01D25/28 Primary

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2230/644

  for adjusting the position or the alignment, e.g. wedges or eccenters · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title