Abrasion-resistant thrust bearings for ESP pump

Abstract

A multistage centrifugal pump has a rotatable shaft, a plurality of pump stages and a thrust module. Each of the plurality of pump stages has an impeller connected to the rotatable shaft and a stationary diffuser. The thrust module has a thrust runner and a unitary thrust pad. The unitary thrust pad has an axial wear face adjacent the thrust runner and a radial wear surface adjacent the rotatable shaft. The axial wear face and radial wear surface are integrated as a unitary component. The unitary thrust pad is secured to a thrust pad support with threaded fasteners that are torqued to a predetermined extent.

Claims

1. A multistage centrifugal pump comprising: a rotatable shaft; a plurality of pump stages, wherein each of the plurality of pump stages comprises: an impeller connected to the rotatable shaft; and a stationary diffuser; and a thrust module, wherein the thrust module comprises: a thrust runner; a thrust pad support; and a unitary thrust pad, wherein the unitary thrust pad comprises: an axial wear face adjacent the thrust runner; a plurality of bolt recesses located along an outer circumference of the axial wear face; a radial wear surface adjacent the rotatable shaft; wherein the unitary thrust pad is secured to the thrust pad support with a plurality of threaded fasteners, wherein each of the plurality of threaded fasteners is located in a corresponding one of the plurality of bolt recesses; and wherein the axial wear face and radial wear surface are integrated as a unitary component.

2. The multistage centrifugal pump of claim 1, wherein the thrust module further comprises a shaft sleeve between the shaft and the radial wear surface of the unitary thrust pad.

3. An electric submersible pump configured to move fluids from a subterranean wellbore to the surface, the electric submersible pump comprising: a motor; and a pump driven by the motor and configured to push fluids from the wellbore to the surface, wherein the pump is a multistage centrifugal pump that comprises: a pump housing; a rotatable shaft; a plurality of pump stages, wherein each of the plurality of pump stages comprises: an impeller connected to the rotatable shaft; and a stationary diffuser; and a thrust module, wherein the thrust module comprises: a thrust runner; a thrust pad support; and a unitary thrust pad having an axial wear face adjacent the thrust runner, wherein the axial wear face is secured to the thrust pad support with a plurality of threaded fasteners.

4. The electric submersible pump of claim 3, wherein the thrust pad support is fixed in a stationary position within the pump housing.

5. The electric submersible pump of claim 3, wherein the unitary thrust pad further comprises a radial wear surface that surrounds the rotatable shaft.

6. The electric submersible pump of claim 5, wherein the thrust module further comprises a shaft sleeve positioned between the rotatable shaft and the radial wear surface of the unitary thrust pad.

7. The electric submersible pump of claim 6, wherein the axial wear face comprises a plurality of bolt recesses and wherein each of the plurality of threaded fasteners is located in a unique one of the plurality of bolt recesses.

8. The electric submersible pump of claim 7, wherein each of the plurality of bolt recesses is located at an outer circumference of the axial wear face.

9. The electric submersible pump of claim 3, further comprising a seal section disposed between the pump and the motor.

10. The electric submersible pump of claim 3, wherein the pump comprises a plurality of thrust modules.

11. The electric submersible pump of claim 3, wherein the thrust runner is connected to an impeller of one of the plurality of pump stages.

12. A thrust module for use in a multistage centrifugal pump that has a rotatable shaft, a pump housing, and a plurality of pump stages, wherein the thrust module comprises: a thrust runner; a thrust pad support; a unitary thrust pad, wherein the unitary thrust pad comprises: an axial wear face adjacent the thrust runner; a radial wear surface that directly engages the rotatable shaft; and means for securing the unitary thrust pad to the thrust pad support.

13. The thrust module of claim 12, wherein the axial wear face and radial wear surface are integrated as a unitary component.

14. The thrust module of claim 13, wherein the thrust module further comprises a shaft sleeve between the shaft and the radial wear surface of the unitary thrust pad, wherein the shaft sleeve directly engages the rotatable shaft.

15. The thrust module of claim 13, wherein the thrust pad support is fixed in location within the pump housing.

16. The thrust module of claim 12, wherein each of the plurality of pump stages includes an impeller and wherein the thrust runner is connected to an impeller in one of the plurality of pump stages.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a cross-sectional depiction of a PRIOR ART thrust module.

(2) FIG. 2 is a depiction of a submersible pumping system constructed in accordance with an exemplary embodiment.

(3) FIG. 3 is a cross-sectional depiction of a portion of the pump from the submersible pumping system of FIG. 2.

(4) FIG. 4 is a cross-sectional depiction of the thrust module from the pump of FIG. 3.

(5) FIG. 5 is a top view of the unitary thrust pad from the thrust module of FIG. 4.

WRITTEN DESCRIPTION

(6) FIG. 2 depicts a downhole pumping system 100 attached to production tubing 102. The pumping system 100 and production tubing are disposed in a wellbore 104, which is drilled for the production of a fluid such as water or petroleum. As used herein, the term “petroleum” refers broadly to all mineral hydrocarbons, such as crude oil, gas and combinations of oil and gas. The production tubing 102 connects the pumping system 100 to a wellhead 106 located on the surface. Although the pumping system 100 is well suited to recover petroleum products from a subterranean well, it will be understood that the present invention can also be used in other applications, including, but not limited to, dewatering and geothermal applications.

(7) The pumping system 100 includes a combination of a pump 108, a motor 110 and a seal section 112. The seal section 112 shields the motor 110 from wellbore fluids and accommodates the thermal expansion of lubricants within the motor 110. The motor 110 is provided with power from the surface by a power cable 114. The pump 108 is fitted with an intake section 116 to allow well fluids from the wellbore 104 to enter the pump 108, where the well fluid is forced to the surface through the production tubing 102. It will also be appreciated that the pumping system 100 may be deployed in surface-mounted applications, which may include, for example, the transfer of fluids between storage facilities, the removal of liquid on surface drainage jobs, the withdrawal of liquids from subterranean formations and the injection of fluids into subterranean wells.

(8) Although the pumping system 100 is depicted in a conventional “vertical” orientation, it will be appreciated that preferred embodiments of the pumping system 100 can also be installed in horizontal, deviated, or other non-vertical installations. As used in this disclosure, the use of the terms “upper” and “lower” should not be construed as limiting the preferred embodiments to a vertical orientation of the pumping system 100. Instead, as used in this disclosure, the terms “upper” and “lower” are analogous to “downstream” and “upstream,” respectively. The terms “downstream” and “upstream” are relative positional references that are based on the movement of fluid through the pump 108.

(9) Turning to FIG. 3, shown therein is a cross-sectional view of a portion of the pump 108. The pump 108 includes a pump housing 118, one or more turbomachinery stages 120 and a shaft 122. Each of stages 120 includes a diffuser 124 and an impeller 126. Each impeller 126 is connected to the shaft 122 through a keyed connection such that the impellers 126 rotate with the shaft 122. The keyed connection permits a limited amount of axial movement between the impellers 126 and the shaft 122. Each of the diffusers 124 is held in a stationary position within the pump housing 118 by a compressive load or bolted connection. In this way, the shaft 122 and impellers 126 rotate within the stationary diffusers 124. Multiple stages 120 may be grouped together in “modules” for functional and control purposes. A single pump 108 may include a plurality of modules of impellers 126 and diffusers 124.

(10) The pump 108 further includes a thrust module 128. Generally, the thrust module 128 offsets axial thrust loads imparted in upstream and downstream directions through the pump 108, while also providing radial support to the shaft 122. The pump 108 may include a plurality of thrust modules 128 interspersed between the modules of stages 120. In some embodiments, the pump 108 may include a thrust module 128 between each module consisting of 5-10 stages 120. In other embodiments, it may be desirable to install the thrust modules 128 between each stage 120 or at greater intervals within the pump 108.

(11) Turning to FIG. 4, shown therein is a cross-sectional depiction of the thrust module 128. The thrust module 128 includes a thrust bearing 130 that has a thrust runner 132 and a unitary thrust pad 134. The thrust runner 132 is configured for rotation with the shaft 122 and can be connected to a downstream impeller 126. The unitary thrust pad 134 includes an axial wear face 136 opposite the thrust runner 132 and a cylindrical, radial wear surface 138 proximate the shaft 122. The axial wear face 136 is configured for contact with the thrust runner 132. The radial wear surface 138 is configured to directly engage the shaft 122, or an intermediate shaft sleeve 140, as depicted in FIG. 4.

(12) Thus, unlike prior art thrust bearings that include separate axial and radial load surfaces, the unitary thrust pad 134 provides a single component that isolates axial loads produced by the pump stages 120 and provides radial support for the shaft 122. Combining the axial wear face 136 and the radial wear surface 138 into a single component ensures the perpendicularity of these features during manufacture rather than during assembly of individual components. Additionally, integrating the radial wear surface 138 into the unitary thrust pad 134 eliminates the need to separately secure the radial wear surface 138 against rotation or displacement. The thrust runner 132 and unitary thrust pad 134 are both designed for extended contact and are constructed from durable, wear-resistant materials. In some applications, the thrust runner 132 and unitary thrust pad 134 are manufactured from hardened carbide materials.

(13) Referring now also to FIG. 5, the unitary thrust pad 134 is connected to a thrust pad support 142, which is located in a stationary manner within the pump housing 118. The thrust pad support 142 can be constructed from metal alloys that are softer and more ductile than the thrust runner 132 and unitary thrust pad 134. The unitary thrust pad 134 is secured to the thrust pad support 142 with threaded fasteners 144. The axial wear face 136 includes bolt recesses 146 that permit the threaded fasteners 144 to be countersunk below the upper surface of the axial wear face 136 when the threaded fasteners 144 are fully engaged with the thrust pad support 142.

(14) In exemplary embodiments, the bolt recesses 146 extend to the outer circumference of the axial wear face 136. The placement of the bolt recesses 146 in this position discourages the accumulation of sand and other particles from the bolt recesses 146 and the axial wear face 136. Unlike the prior art use of pins or stakes, the threaded fasteners 144 not only prevent the unitary thrust pad 134 from rotating during use, but also fasten the unitary thrust pad 134 to the thrust pad support 142 so that adhesives and other bonding mechanisms are not required. When properly torqued, the threaded fasteners 144 will reliably secure the unitary thrust pad 134 to the thrust pad support 142 over a wide temperature range. This presents a significant advantage over the established practice of using pins and adhesives to secure the wear surfaces within a thrust module.

(15) It is to be understood that even though numerous characteristics and advantages of various embodiments of the present invention have been set forth in the foregoing description, together with details of the structure and functions of various embodiments of the invention, this disclosure is illustrative only, and changes may be made in detail, especially in matters of structure and arrangement of parts within the principles of the present invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed. It will be appreciated by those skilled in the art that the teachings of the present invention can be applied to other systems without departing from the scope and spirit of the present invention.