CLAPPER STYLE STOP VALVE SPHERICAL WASHER LAPPING TOOL

Abstract

A device and method to aid in lapping a spherical washer to a steam turbine component are provided. The device includes a drive head, the drive head made up of a drive cap and a hollow cylindrical portion projecting from the drive cap. The drive cap abuts a surface of the spherical washer. The cylindrical portion fits within and is concentric to an inner diameter of the spherical washer. The device also includes an expanding gasket including an outer diameter having a contour configured to fit a contour of an inner diameter of the spherical washer and an inner diameter slides onto the cylindrical portion such that the gasket and cylindrical portion are concentric. The drive head attaches to a drive unit which imparts a torque to lap the spherical washer with respect to a steam turbine component. The expanding gasket expands and holds the spherical washer during the lapping.

Claims

1. A method to lap a first turbine component to a second turbine component, comprising: applying a lapping compound to an outer surface of the first turbine component; preparing a device according to claim 1 for the lapping of the first component to the second component; positioning the device including the first component against the second turbine component such that the outer surface of the first turbine component abuts an inner surface of the second turbine component; attaching a drive unit to the drive head; imparting a torque by the drive unit to the device sufficient to lap the first turbine component to the second turbine component.

2. The method as claimed in claim 1, the preparing including: positioning an expanding gasket system over the outer diameter of the cylindrical portion of the drive head, positioning an inner diameter of the first turbine component over the outer diameter of the cylindrical portion adjacent to the gasket, and securing the expanding gasket system and the first component to the drive head.

3. The method as claimed in claim 2, the device further comprising: the expanding gasket tapered internally from each side on an inner diameter, and two plates, a first plate and a second plate, each tapered internally on an outer diameter such that the contour of each taper conforms to a taper of the gasket, the two plates disposed on opposite sides of the gasket with respect to a shaft axis, wherein the inner diameter of the expanding gasket and the inner diameters of the two plates slide over and are concentric with the cylindrical portion, wherein the first plate is disposed axially inward with respect to the drive head, and the second plate is disposed axially outward with respect to the drive head, wherein when the two plates are axially compressed towards one another such that the tapers of each plate abut the taper of the gasket, the gasket expands and grips the spherical washer without deformation.

4. The method as claimed in claim 3, further comprising attaching a tension bar assembly to the drive head, wherein the tension bar assembly applies a constant and consistent axial force during the lapping of the first turbine component to the second turbine component by thrusting the first turbine component against the second turbine component.

5. The method as claimed in claim 4, wherein the attaching includes inserting a first end of a tension shaft of the tension bar assembly into the hollow cylindrical portion of the drive head and latching the first end with a latching mechanism within the interior of the drive cap such that the first end is secured within the drive cap.

6. The method as claimed in claim 5, wherein the tension bar assembly includes a compression knob disposed at a second end of the tension shaft opposite the first end, wherein a tightening adjustment of the compression knob compresses a spring against the stop plate which then induces a constant axial tension along the device, the spring connecting the compression knob with the stop plate.

7. The method as claimed in claim 4, further comprising aligning the first turbine component to be concentric with the second turbine component.

8. The method as claimed in claim 7, wherein the aligning is accomplished by positioning a tension bushing over the outer diameter of the cylindrical portion of the drive head, wherein an inner diameter of the tension bushing slides over the outer diameter of the cylindrical portion of the drive head and abuts the plate disposed axially outward with respect to the drive head, and wherein the tension bushing aligns the device and the first component to be concentric with the second component.

9. The method as claimed in claim 1, wherein the first turbine component is a spherical washer and the second turbine component is a casing bushing of a stop valve assembly in a steam turbine engine.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0010] FIG. 1 illustrates an exploded view of a device to aid in lapping a spherical washer to a steam turbine component,

[0011] FIG. 2 illustrates a perspective view of the device secured to a spherical washer,

[0012] FIG. 3 illustrates a perspective view of the device including a tension bar assembly,

[0013] FIG. 4 illustrates a cross sectional view of the device secured within the valve casing,

[0014] FIG. 5 illustrates a perspective view of a latching mechanism,

[0015] FIG. 6 illustrates an exploded view of the latching mechanism and the drive cap,

[0016] FIG. 7 illustrates a perspective view of the device including a tension bar assembly attached to a drill, and

[0017] FIG. 8 illustrates a perspective view of the device within a clapper style stop valve.

DETAILED DESCRIPTION

[0018] To facilitate an understanding of embodiments, principles, and features of the present disclosure, they are explained hereinafter with reference to implementation in illustrative embodiments. Embodiments of the present disclosure, however, are not limited to use in the described systems or methods.

[0019] The components and materials described hereinafter as making up the various embodiments are intended to be illustrative and not restrictive. Many suitable components and materials that would perform the same or a similar function as the materials described herein are intended to be embraced within the scope of embodiments of the present disclosure.

[0020] Referring now to the figures, where the showings are for purposes of illustrating embodiments of the subject matter herein only and not for limiting the same, FIG. 1 illustrates an exploded view of a device 10 to aid in lapping a spherical washer 40 to another steam turbine component. The device 10 includes a drive head 20 which may be configured to attach to a drive unit in order to impart a torque sufficient to lap the two steam turbine components with respect to one another. Those skilled in the art would understand that the disclosed device may be employed in many other industrial systems as well as the embodiment including a steam turbine engine as discussed, for exemplary purposes, below.

[0021] As discussed above, a device 10 to aid in lapping a spherical washer 40 to another steam turbine component is desired. The proposed device 10, shown in FIG. 1, includes a drive head 20, the drive head 20 including a drive cap 22 and a hollow cylindrical portion 30 projecting from the drive cap 22. The cylindrical portion 30 may include threads 24 for securely attaching components onto the cylindrical portion 30.

[0022] A spherical washer 40 secured to the device 10 is illustrated in FIG. 2. The drive cap 20 is configured to abut the spherical washer 40. The cylindrical portion 30 fits within and is concentric to the inner diameter of the spherical washer 40. A fastener 60 may be used to secure the spherical washer 40 to the drive cap 22. A first alignment device 50, embodied in FIG. 2 as a bushing, may be used to properly align the device 10 and the spherical washer 40 with the steam turbine component. A driver portion 26 of the drive cap 22 opposite the projecting cylindrical portion 30 is configured to attach to a drive unit. The drive unit may impart a torque sufficient to lap the spherical washer 40 with respect to the steam turbine component.

[0023] In the embodiment described below, the steam turbine component is a stop valve casing bushing 210. A cross section of the casing bushing 210 within a steam turbine stop valve casing 240 may be seen in FIG. 4. The outer diameter of the spherical washer 40 may include a spherical contour that matches a corresponding spherical contour of the casing bushing 210. In the steam turbine, the casing bushing 210 abuts the stop valve casing 240 on its outer diameter and the steam turbine shaft on its inner diameter. The spherical contour of the casing bushing 210 may be an end surface 220 as seen in the embodiment of FIG. 4.

[0024] Referring back to FIG. 1, the device 10 may also include an expanding gasket system, including an expanding gasket 70 and two plates 80, one each disposed on opposite sides of the gasket 70 with respect to a longitudinal shaft axis 90. The outer diameter of the gasket 70 is configured to conform to a contour of the inner diameter of the spherical washer 40. The inner diameter of the gasket 70 may be tapered internally from both sides of the gasket such that a cross section of the gasket includes a V shape. The angle of incline for each taper on the inner diameter of the gasket 70 may be in the range of 45 to 60 degrees with respect to the longitudinal shaft axis 90. The expanding gasket 70 may comprise a rubber material such as a polyurethane material.

[0025] The two plates 80, a first plate and a second plate, one each disposed on opposite sides of the gasket 70 may be used to expand the gasket 70 when the two plates 80 are axially compressed towards one another into the inner diameter of the gasket 70. Each of the two plates 80 may be tapered internally on an outer diameter such that the contour of each taper conforms to the inner diameter taper of the gasket 70. When compressed together the tapers of the two plates 80 may abut and conform to the inner diameter taper of the gasket 70. In this way, the compression of the two plates 80 may be used to expand the gasket 70 and grip the spherical washer 40 without deforming the spherical washer 40. A deformed spherical washer could not be correctly lapped to its mating counterpart necessitating a replacement for the part and resulting in lost time and perhaps a longer shutdown time for the steam turbine.

[0026] FIG. 1 also illustrates the position of the gasket 70 and the two plates 80 with respect to the drive head 20 and the longitudinal shaft axis 90. The gasket 70 and the two plates 80 are configured to slide over the cylindrical portion 30 of the drive head 20 as well as to be concentric with the cylindrical portion 30. The first plate 80 may be disposed axially inward with respect to the drive head 20 and the second plate 80 may be disposed axially outward with respect to the drive head 20. The two plates 80 are free to slide axially along the cylindrical portion 30. When the fastener 60 is fastened, by perhaps screwing the fastener onto the threads of the cylindrical portion, the alignment device 50 pushes the plates axially together, expanding the gasket 70 and securing the gasket system 70, 80 to the drive cap 22.

[0027] A first alignment device 50, illustrated in FIG. 1, may also be configured to slide over the outer diameter of the cylindrical portion 30 of the drive head 20 and fit within the casing bushing 210 of the steam valve casing 240. The first alignment device 50 may be disposed adjacent to and axially outward from the second plate, with respect to the drive head 20. The first alignment device 50 may align the device 10 to be concentric with the casing bushing 210. Additionally, the alignment device 50 may act as a compression spacer for the expanding gasket 70 and the two plates 80 by providing an axial compression to the expanding gasket 70.

[0028] Referring now to FIG. 3, an embodiment of the device 10 is illustrated in which the device 10 further includes a tension bar assembly 100. The tension bar assembly 100 is configured to apply a constant and consistent force during the lapping of the spherical washer 40 to the steam turbine component by thrusting the spherical washer 40 against the steam turbine component, which in the exemplary embodiment the steam turbine component is the casing bushing 210.

[0029] The tension bar assembly 100 includes a tension shaft 110, which may be embodied as a cylindrical shaft. A first end of the tension shaft 110 fits within the cylindrical portion 30 of the drive head 20 and extends into the drive cap 22 where it is secured. The tension bar assembly 100 may also include a stop plate 120. The stop plate 120 is configured to abut a surface of a further steam turbine component so that a constant and consistent tension may be provided to the spherical washer 40 and the end surface 220, as seen in FIG. 4, of the casing bushing 210 while they are being lapped with respect to one another. A stop plate 120 abutting the surface of a support yoke 410 of the stop valve 400 may be seen in FIG. 8.

[0030] The tension bar assembly 100 may also include a compression knob 130 disposed at a second end of the tension shaft 110 opposite the first end. Both the compression knob 130 and the stop plate 120 may include a central hole such that an inner diameter of the compression knob 130 and stop plate 120 may be disposed onto the tension shaft 110 and positioned concentric to the tension shaft 110. The stop plate 120 and the compression knob 130 may be connected by a spring 140 so that the stop plate 120 may easily move relative to the tension shaft 110 and position the stop plate 120 so that it abuts the surface of the further steam turbine component. A tightening adjustment of the compression knob 130 compresses the spring 140 against the stop plate 120 which then induces a constant axial tension along the device 10 pulling the drive head 20 including the spherical washer 40 against the end surface 220 of the casing bushing 210. In this way, controlling the compression knob 130 enacts a constant controllable force between the spherical washer 40 against its mating component 220.

[0031] The tension bar assembly 100 may also include a second alignment device 150 having an inner diameter disposed onto the outer diameter of tension shaft 110 and an outer diameter abutting the inner diameter of the casing bushing 210. The second alignment device 150 allows the spherical washer 40 to be reliably lapped concentric to the end surface 220 of casing bushing 210. In the shown embodiment of FIG. 3, the second alignment device 150 is a tension bushing.

[0032] Referring back to FIG. 4, a cross sectional view of the device 10 secured to the spherical washer 40 is illustrated. Additionally, the device 10 is shown holding the spherical washer 40 against the casing bushing 210. In this configuration, the spherical washer 40 may be firmly held and aligned with the stop valve shaft axis 250 within stop valve casing 240 so that it may be lapped to the casing bushing 210. The end surface 220 of the casing bushing 210 may include a spherical surface 220. The spherical washer 40 includes a corresponding spherical surface that abuts the spherical surface of the casing bushing 210. A lapping process of the two surfaces allows the two surfaces to lie flush against one another so that a proper seal is formed between the two components 40, 210 such that steam will not leak out of the stop valve 400.

[0033] In the embodiment shown in FIG. 4, the first end of the tension shaft 110 of the tension bar assembly 100 is shown secured to the drive cap 22 using a latching mechanism 230. The latching mechanism 230 catches and holds the tension bar assembly 100.

[0034] The latching mechanism 230 comprises a catch piece as shown in FIGS. 5 and 6. FIG. 6 illustrates an exploded view of the catch piece and the drive cap 22 and indicates how the catch piece 230 may be installed into the drive cap 22. In this embodiment, the catch piece 230 slides down within an interior portion of the drive cap 22 and includes an opening 231 into which the first end of the tension shaft 110 may be inserted. Thus, the catch piece 230 catches and securely holds the first end of the tension shaft 110. Conversely, in order to release the first end of the tension shaft 110, the catch piece 230 may be depressed at its top surface, which lies flush with the top surface of the drive cap 22. Into the top surface of the catch piece 230, at least one through hole 232 is disposed into which a fastener 233 and a spring 234 may be inserted. The fasteners 233 secure the catch piece to the drive cap 22. The spring 234 enables the releasing functionality of the catch piece 230. Using the latching mechanism of the drive head 20 enables a quick latching/unlatching of the drive head 20 to/from the tension shaft assembly 100.

[0035] In the illustrated embodiment of FIG. 4, the two plates 80 are shown compressing the expanding gasket 70 such that the outer diameter of the gasket 70 abuts the inner diameter of the spherical washer 40 gripping the spherical washer 40 and radially holding it against the spherical end surface 220 of the casing bushing 210. The first alignment device 50, shown as a bushing in the illustrated embodiment, assists in compressing the expanding gasket system 70, 80. Additionally, the first alignment device 50 helps guide the expanding gasket 70 near the lapping area. A fastener, such as a nut, may be threaded onto threads of the cylindrical portion 30 securing the alignment device 50, the gasket 70 and two plates 80 to the drive head 20. A second alignment device 150 comprising a tension shaft bushing 150 is shown within and concentric to the casing bushing 210. The tension shaft bushing 150 slides onto the tension shaft 110 and helps the device 10 and the spherical washer 40 to maintain concentricity with the casing bushing 210. Maintaining concentricity between spherical washer 40 and the casing bushing 210 promotes a successful lapping of the two components and reduces the time the technician spends on the lapping process. If the components are not properly lapped to one another, one may need to re-lap the components leading to lost time and perhaps more downtime for the steam turbine engine.

[0036] The tension shaft bushing 150 may be locked into the tension shaft 110 of the tension bar assembly 100 using a locking mechanism. The locking mechanism may be embodied as a spring plunger. A spring plunger 260 may be used within each tension shaft bushing 150 to lock the tension shaft bushing 150 to the tension shaft 110. The spring plunger 260 may include a conical tip which fits a matching groove in the tension shaft 110 locking the tension shaft bushing 150 into the tension shaft 110. A break away force may be controlled by how much the spring plunger 260 is threaded into the tension shaft bushing 150. The spring plungers 260 may be radially threaded into the tension shaft 110. Thus, to install the tension bushings 150 onto the tension shaft 110, one may slide a tension shaft bushing 150 onto the tension shaft 110 and locate it onto a designated position using the locking mechanism. Multiple spring plungers 260 may be used and evenly spaced around the circumference of the bushing 150 in order to more securely lock the tension bushing 150 onto the tension shaft 110. For example, three spring plungers 260 may be spaced 120 degrees apart around the circumference of the tension bushing 150.

[0037] Referring now to FIG. 7, a perspective view of the device 10 including the tension bar assembly 100 is shown attached to a drive unit 300. In the embodiment of FIG. 8, the drive unit 300 is a drill. As described above the drive unit 300 imparts a torque to the device 10 that may be sufficient to lap the first turbine component to a second turbine component. The drive head 20 may include a driver portion 26 disposed at one end of the drive head 20 and configured to attach to the drive head 20. The driver portion 26 may include a hexagonal projection that will mate with a drill bit, for example, of the drive unit 300.

[0038] For illustrative purposes, FIG. 8 shows a perspective view of the device 10 within a clapper style stop valve 400 attached to the drill. From FIG. 8, one skilled in the art can see the scale of the device 10 and drill 300 within the stop valve 400 and the space constraints a technician may encounter when working within the stop valve 400 to lap the spherical washer 40 to the stop valve casing bushing 210.

[0039] Referring to FIGS. 1-8, a method to lap a first turbine component 40 to a second turbine component 210 is also provided. The method includes applying a lapping compound to an outer surface of the first turbine component 40. According to the method, a technician may then prepare the device 10, as described above, for a lapping procedure of the first turbine component 40 to the second turbine component 210 by positioning the expanding gasket system 70, 80 over the cylindrical portion 30 of the drive head 20. Additionally, an inner diameter of the first turbine component 40 may be positioned over the outer diameter of the cylindrical portion 30 adjacent to the gasket 70. Once the gasket system 70, 80 and the first turbine component 40 are secured onto the cylindrical portion 30 of the drive head 20, the device 10 including the first turbine component 40 may be positioned against the second turbine component 210 such that the outer surface of the first component 40 abuts and inner surface of the second turbine component 210. A drive unit 300 may then be attached to a driver portion 26 of the drive head 20.

[0040] The lapping procedure commences when the drive unit 300 imparts a torque to the device 10 sufficient to lap the first turbine component 40 to the second turbine component 210. During the lapping procedure, the first turbine component 40 rotates with respect to a stationary second component 210 lapping the first component 40 to the second component 210. The lapping procedure may be accomplished in less than 4 hours, a significant improvement from the 4 to 12 hours that the conventional procedures have taken.

[0041] In an embodiment, preparing the device 10 includes attaching a tension bar assembly 100, as described above, to the drive head 20. The tension bar assembly 100 applies a constant and consistent axial force during the lapping procedure of the first turbine component 40 to the second turbine component 210 by thrusting the first turbine component 40 against the second turbine component 210. The tension bar 110 is attached to the drive head 20 by inserting a first end of the tension shaft 110 into the hollow cylindrical portion 30 of the drive head 20. The device 10 is secured within the drive cap 22 by latching the first end with a latching mechanism 230 within the interior of the drive cap 22.

[0042] As described above, in order for the lapping procedure to be successful such that a proper seal may be formed between the two components 40, 210, the method may include aligning the first turbine component 40 to be concentric with the second turbine component 210. The aligning may be accomplished by positioning a tension bushing 50 over the outer diameter of the cylindrical portion 30 of the drive head 20. An inner diameter of the tension bushing 50 slides over the outer diameter of the cylindrical portion 30. The tension bushing 50 may align the device 10 and the first component 40 to be concentric with the second component 210.

[0043] In the described embodiment of the method, the first component is a spherical washer 40 and the second component is a casing bushing 210 of a stop valve assembly 240 in a steam turbine engine, however, one skilled in the art of turbomachinery would understand that other industrial components may be lapped to one another using the proposed device and method.

[0044] The disclosed device and method to lap a first turbine component to a second turbine component accomplishes the objective of firmly holding the spherical washer in order to lap it to the casing bushing within the stop valve assembly. By providing an alignment device, the tool may also align the device including the spherical washer with the casing bushing so that the lapping procedure produces good results. Additionally, using the provided tool reduces the time to lap the spherical washer to casing bushing at least by half and makes the lapping procedure less physically challenging for the technicians performing the procedure.

[0045] While embodiments of the present disclosure have been disclosed in exemplary forms, it will be apparent to those skilled in the art that many modifications, additions, and deletions can be made therein without departing from the spirit and scope of the invention and its equivalents, as set forth in the following claims.