Method and apparatus for improved turbine bellyband rotor seal machining, installation and life

Patent metadata

Field	Value
Publication number	US-9273611-B2
Application number	US-201414337318-A
Country	US
Kind code	B2
Filing date	Jul 22, 2014
Priority date	Jul 22, 2014
Publication date	Mar 1, 2016
Grant date	Mar 1, 2016

Abstract

A method and apparatus for improved turbine bellyband rotor seal machining, installation and life are disclosed. A fixture is provided which can be temporarily attached to the turbine disks in a position straddling the gap between the disks, without destacking the turbine rotor. The fixture accepts power tools including a drill and a mill, and positions the power tools to drill and grind a rectangular slot into the disks, where the slot has the exact size and shape needed to receive an anti-rotation block which is integral to the replacement bellyband. Measuring tools are also provided which enable precise location of each of the four slots which must be machined in the disks. The resulting slots have a uniform size and shape, and are equally spaced around the circumference of the disk, thereby facilitating installation of the service bellyband from four identical segments.

First claim

What is claimed is:

1. A tool set for preparing two adjacent rotor disks in a gas turbine for installation of a bellyband rotor seal, said tool set comprising:
a machining fixture configured to cut a slot into the disks, said fixture comprising a body including a recessed pocket on a top surface and an opening through the body central to the pocket, a first drilling insert configured to fit in the pocket in the body, a second drilling insert configured to fit in the pocket in the body, a milling insert configured to fit into the pocket in the body, a pair of alignment pins protruding from a bottom surface of the body, and a pair of toggle bolts passing through the body and extending beyond the bottom surface of the body, where the machining fixture is mounted onto the disks using the alignment pins and the toggle bolts and the slot is cut using the first and second drilling inserts and the milling insert in sequence;
a half-circumference measurement band including a fitting at one end, where the fitting is sized to fit into the slot which has been cut into the disks, and the half-circumference measurement band is sized to extend halfway around a circumference of the disks; and
a quarter-circumference measurement band including a fitting at one end, where the fitting is sized to fit into the slot which has been cut into the disks, and the quarter-circumference measurement band is sized to extend one-quarter of a distance around the circumference of the disks.

2. The tool set of claim 1 wherein the machining fixture has a size which is small enough to enable the machining fixture to be used to cut the slot without destacking the disks from a rotor of the gas turbine.

3. The tool set of claim 1 wherein the bottom surface of the body of the machining fixture has a curvature which matches a curvature of an outer surface of the disks.

4. The tool set of claim 1 wherein the first drilling insert includes drill guides for drilling two smaller holes into each of the disks, where the smaller holes are located proximate to four corners of the slot.

5. The tool set of claim 1 wherein the second drilling insert includes drill guides for drilling one larger hole into each of the disks, where the larger holes overlap the smaller holes and an edge of the gap.

6. The tool set of claim 1 wherein the milling insert includes an air turbine cutting tool which follows a template to finish machining the slot after the smaller holes and the larger holes have been drilled.

7. The tool set of claim 1 wherein the pair of alignment pins are selected to have a size which fits in the gap with minimal clearance and are screwed onto the bottom surface of the body.

8. The tool set of claim 1 wherein each of the toggle bolts includes a toggle device which can be placed through the gap between the disks, rotated a quarter turn, and tightened against an inside surface of the disks.

9. The tool set of claim 1 wherein the half-circumference measurement band is used to determine a location of a second slot which is halfway around the disks from a first slot by taking an average of a first and second measurement, where the second measurement is made by wrapping the half-circumference measurement band around the disks in a direction opposite the first measurement.

10. The tool set of claim 9 wherein the quarter-circumference measurement band is used to determine a location of a third slot which is equidistant from the first and second slots by taking an average of a measurement from the first slot and a measurement from the second slot.

11. A tool for cutting a slot into two adjacent rotor disks in a gas turbine for installation of a bellyband rotor seal, said tool comprising:
a body including a recessed pocket on a top surface and an opening through the body central to the pocket, where a bottom surface of the body has a curvature which matches a curvature of an outer surface of the disks;
a first drilling insert configured to fit in the pocket in the body, where the first drilling insert includes four drill guide holes which are used to drill a first set of holes in the disks;
a second drilling insert configured to fit in the pocket in the body, where the second drilling insert includes two drill guide holes which are used to drill a second set of holes in the disks;
a milling insert configured to fit into the pocket in the body, where the milling insert includes an air turbine cutting tool which follows a template to finish machining the slot after the first and second set of holes have been drilled;
a pair of alignment pins protruding from a bottom surface of the body; and
a pair of toggle bolts passing through the body and extending beyond the bottom surface of the body, where the machining fixture is mounted onto the disks using the alignment pins and the toggle bolts and the slot is cut using the first and second drilling inserts and the milling insert in sequence.

12. The tool of claim 11 wherein the pair of alignment pins are selected to have a size which fits in a gap between the disks with minimal clearance and are screwed onto the bottom surface of the body.

13. The tool of claim 11 wherein each of the toggle bolts includes a toggle device which can be placed through a gap between the disks, rotated a quarter turn, and tightened against an inside surface of the disks.

14. The tool of claim 11 further comprising a measurement band including a fitting at one end, said fitting being sized to fit in a slot previously cut in the disks, said measurement band being sized to establish a location of a second slot in the disks relative to a first slot in the disks, where the location of the second slot is established as an average of two measurements taken in different directions.

15. A method for replacing a bellyband rotor seal in a gas turbine, said method comprising:
establishing a location of a first slot to be cut into two adjacent rotor disks in the gas turbine;
mounting a machining fixture onto the disks at the location of the first slot, where the fixture is mounted in a position straddling a gap between the disks;
machining the first slot into the disks using tools mounted to the machining fixture;
removing the fixture from the disks;
establishing a location of a second slot to be cut into the disks, where the second slot is to be located at a position on the disks which is 180 degrees from the location of the first slot, and where the location of the second slot is determined using a half-circumference measurement band which is fitted at one end into the first slot;
mounting the machining fixture onto the disks at the location of the second slot;
machining the second slot into the disks using the tools mounted to the machining fixture;
removing the fixture from the disks;
establishing a location of a third slot to be cut into the disks, where the third slot is to be located at a position on the disks which is 90 degrees from the locations of the first and second slots, and where the location of the third slot is determined using a quarter-circumference measurement band which is fitted at one end into either the first slot or the second slot;
mounting the machining fixture onto the disks at the location of the third slot;
machining the third slot into the disks using the tools mounted to the machining fixture;
removing the fixture from the disks;
establishing a location of a fourth slot to be cut into the disks, where the fourth slot is to be located at a position on the disks which is 180 degrees from the location of the third slot, and where the location of the fourth slot is determined using the half-circumference mea

Assignees

• Siemens Energy Inc

Inventors

• Bird Derek A
• Mitchell David J
• Olejarski Michael J

Classifications

• B23P6/002 Primary

  Repairing turbine components, e.g. moving or stationary blades, rotors, (B23P6/045 takes precedence) · CPC title

• F05D2230/80

  Repairing, retrofitting or upgrading methods · CPC title

• B23P13/02

  in which only the machining operations are important · CPC title

• B23B47/28

  Drill jigs for workpieces (equipment for setting or guiding the drill B23B49/00) · CPC title

• B23B49/00

  Measuring or gauging equipment on boring machines for positioning or guiding the drill; Devices for indicating failure of drills during boring; Centering devices for holes to be bored (marking-out equipment B25H7/00; measuring devices, gauges G01B) · CPC title