This invention relates in general to electrical submersible well pumps and in particular to thrust bearings for a centrifugal pump.
Centrifugal well pumps are commonly used for pumping oil and water from oil wells. The pumps have a large number of stages, each stage having a stationary diffuser and a rotating impeller. The rotating impellers exert a downward thrust as the fluid moves upward. Also, particularly at startup and when the fluid flow is nonuniform, the impellers may exert upward thrust. In the most common pump design, the impellers float freely on the shaft so that each impeller transfers downward thrust to one of the diffusers. A thrust washer or bearing is located between a portion of each impeller and the upstream diffuser to accommodate the downward thrust. Another thrust washer transfers downward thrust.
Some wells produce abrasive materials, such as sand, along with the oil. The abrasive material causes wear of the pump components, particularly in the areas where downward thrust and upward thrust are transferred. Tungsten carbide thrust bearings and bearing sleeves may be employed in these pumps to reduce wear. A number of designs for these components exist, but improvements are desirable.
The centrifugal pump stage of this invention has a stationary diffuser having a bore. A thrust bearing has an tubular portion that inserts into the bore. An external shoulder extends radially outward from the tubular portion and bears against a support surface formed in the bore of the diffuser for transmitting downward thrust from an upstream impeller to the diffuser. An internal shoulder extends inward from the tubular portion for transmitting upward thrust from a downstream impeller to the diffuser.
A thrust runner rotatably engages a downstream end of the thrust bearing for transmitting the downward thrust from the upstream impeller to the diffuser. The thrust runner has an upstream end with a greater surface area than a downstream end. The thrust bearing has a downstream end that has a radial width substantially equal to a difference between an outer diameter of the external shoulder less an inner diameter of the internal shoulder. The thrust bearing and thrust washer are preferably constructed of hard wear resistant materials, such as tungsten carbide.
Referring to
Pump 15 has a seal section 21 connected to its lower end. An electrical motor 23 connects to the lower end of seal section 21. Seal section 21 reduces a pressure differential between lubricant within motor 23 and the hydrostatic pressure in the well. An electrical power cable 24 extends downward from the surface to motor 23 for supplying power.
Referring to
Diffuser 27 has an axial bore with a lower portion 33a, a central portion 33b, and an upper portion 33c. The terms “upper” and “lower” are used herein for convenience only and not in a limiting manner. Lower portion 33a has the smallest diameter, while central portion 33b is intermediate in inner diameter, and upper portion 37c is a counterbore with the largest diameter. In this embodiment, central portion 33b has a greater length than either upper or lower portions 33a or 33b.
A shaft 35 extends rotatably through diffuser bore portions 33a, 33b and 33c for rotating impellers 29. A thrust bearing 37 is non-rotatably mounted in portions 33b and 33c, such as by an interference fit or other means. Thrust bearing 37 is a tubular member having a cylindrical base 43 and an external rim 39 on an upper end of base 43. External rim 39 has a side wall that is in contact with upper bore portion 33c. Preferably, thrust bearing 37 has an internal rim 41 that extends radially inward into close proximity, but not touching shaft 35. Internal rim 41 has an inner diameter that is smaller than an inner diameter of base 43, defining an upstream facing internal shoulder 42 at the intersection of internal rim 41 and base 43. Internal shoulder 42 is located in a plane perpendicular to the axis of shaft 35, thus extends radially inward from base 43.
Base 43 has an outer cylindrical surface that contacts central bore portion 33b. The outer diameter of base 43 is less than the outer diameter of external rim 39, defining an upstream facing external shoulder 45. External shoulder 45 is in a plane parallel with but axially offset from internal shoulder 42. Internal and external shoulders 42, 45 define a generally I-shaped configuration for the downstream portion of thrust bearing 37. External shoulder 45 is in contact with a downstream facing support shoulder 47 formed at the junction between central bore portion 33b and upper bore portion 33c. The inner cylindrical surface of base 43 has an inner diameter approximately the same as the inner diameter of lower bore portion 33a. The lower end of base 43 terminates a short distance above the intersection of lower bore portion 33a with central bore portion 33b in this embodiment. A shoulder is located at the intersection of lower bore portion 33a and central bore portion 33b, and the lower end of base 43 is spaced from this shoulder by a clearance. Internal and external shoulders 42, 45 are located much closer to the downstream end of thrust bearing 37 than the upstream end.
The upper end of thrust bearing 37 terminates substantially flush with the outlet of passages 31. A flat thrust face 48 is formed on the upper end of thrust bearing 37, extending from internal rim 41 to external rim 39. As shown in
Preferably, a cylindrical sleeve 51 locates between the inner diameter of thrust bearing base 43 and shaft 35. Sleeve 51 has an axial key slot 53 for receiving a key (not shown) to cause sleeve 51 to rotate with shaft 35. Sleeve 51 is free to move axially on shaft 35 a limited distance. The outer diameter of sleeve 51 is in sliding contact with the inner diameter of thrust bearing base 43. In this embodiment, the axial length of sleeve 51 is less than the axial length of thrust bearing base 43. As illustrated in
A thrust runner 57 has a downward facing smooth, flat thrust face 59 that engages thrust face 48 of thrust bearing 37. Thrust runner 57 has an exterior sidewall 61 that extends upward and inward from face 59. The exterior of sidewall 61 is a curved tapered surface in this embodiment, with a larger outer diameter at face 59 than at the upper end of thrust runner 57. The radial width and cross-sectional area of thrust runner face 59 is substantially the same as the radial width and cross-sectional area of thrust bearing face 48. The surface area of thrust runner face 59 is the same as the surface area of thrust bearing face 48 plus the area of grooves 49. An internal key slot 63 (
A downward extending impeller hub 65 of the adjacent downstream impeller 29 or a spacer (not shown) if used, contacts the upper end of thrust runner 61. The adjacent upstream impeller 29 has an upward extending hub 67 that fits within lower bore portion 33a and a small portion of thrust bearing base 43. Hub 67 of upstream impeller 29 contacts the lower end of sleeve 51. During normal operation, a clearance is located between the upper end of sleeve 51 and internal shoulder 42 of thrust bearing 37.
Thrust bearing 37, sleeve 51 and thrust runner 57 are constructed of a harder material than the material of diffusers 27 and impellers 29. Preferably, the material comprises a carbide, such as tungsten carbide.
In operation, motor 23 (
Under some circumstances, up thrust occurs, causing hub 67 of upstream impeller 29 to apply upward thrust to sleeve 51. Sleeve 51 moves upward into contact with internal shoulder 42. The upward force transfers from internal shoulder 42 through thrust bearing 37, diffuser 27 and into housing 25.
If desired, each stage could have one of the thrust bearings 37, thrust runners 57, and sleeve 51. Alternately, some of the stages could be of conventional type, not having a thrust runner, thrust bearing, or sleeve as described. Spacer sleeves between the impeller hubs of these conventional stages could transfer thrust downward to the next stage having a thrust runner and thrust bearing as described.
The invention has significant advantages. The thrust bearing provides transfers both downward and upward thrust to the diffuser. The thrust faces are considerably larger in cross-sectional area than the tubular portions of the thrust bearing and thrust runner.
While the invention has been shown in only one of its forms, it shoulder be apparent to those skilled in the art that it is not so limited but is susceptible to various changes without departing from the scope of the invention.
This application claims priority to provisional application 60/660,737, filed Mar. 11, 2005.
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Number | Date | Country | |
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20060204359 A1 | Sep 2006 | US |
Number | Date | Country | |
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60660737 | Mar 2005 | US |