Not applicable.
Not applicable.
The present disclosure generally relates to a downhole bump barrel for use in a downhole artificial lift of the type that may be used to remove hydrocarbons from the ground. The disclosed elements and processes, however, may have applications outside the disclosed field and this description is not intended to limit the scope of the claimed subject matter in any way.
Downhole sucker-rod pumps are used in sucker-rod type artificial lift systems. Such systems conventionally include a number of different components including those illustrated in
In the example of
In the example of
During use movement of the movable assembly 11 within the stationary assemble 20 will result operation of a pump assemble in which: (a) a volume of production fluid is received within the barrel 24—through the plunger 13 and the traveling valve 12—during each typical downstroke and (b) a volume of production fluid is lifted through the annulus that will exist between the inner walls of the barrel 24 and the exterior of the movable assembly 11 during each typical upstroke. Thus, in the described system, production fluid will be received within, and move within, the interior space of the barrel 24 during each upstroke.
As those of ordinary skill in the art will appreciate, production fluid in a downhole well typically contains particles of various sizes (sand, for example), potentially corrosive materials; and or potentially abrading materials. As such, the interior of the barrel 24 is subject to harsh conditions tending to promote wear, abrasion and/or cracking. Such conditions can result in damage and/or deterioration of the material forming the barrel 24 resulting in failure of the artificial lift system 100, sub-optimum performance of the system 100, and/or undesired wear of the system 100.
The problem of undesired wear and/or corrosion of barrel surfaces has been long-standing within the relevant art and various approaches have been attempted to increase the wear/abrasion resistance of barrels. But to date, such attempts have been sub-optimal.
For example, it has been known to coat the inner surface of a barrel formed primarily from iron with a layer of chrome to increase the wear/abrasion of a barrel. One example of such an approach is reflected in
An alternate approach for that has been attempted to protect barrel surfaces within an artificial lift system involves the use of a NiCarb (or Ni-Carb) coating. One example of such an approach may be found in
A still further alternate approach—similar to that disclosed in U.S. Pat. No. 10,138,384—is reflected in
It is an object of the disclosure contained herein to overcome the described and other limitations of known approaches for enhancing the lifespan and operation of downhole pump barrels.
It is to be understood that the discussion above is provided for illustrative purposes only and is not intended to and does not limit the scope or subject matter of the appended or ultimately issued claims or those of any related patent application or patent. Thus, none of the appended claims, ultimately issued claims or claims of any related application or patent are to be limited by the above discussion or construed to address, include, or exclude each or any of the above-cited features or disadvantages merely because such were mentioned herein.
A brief non-limiting summary of one of the many possible embodiments of the inventions disclosed herein is a barrel for use in a sucker-rod pump assembly, comprising: a tubular core element comprising iron, the tubular core element defining an interior surface and a longitudinal axis; an interior layer formed on at least a portion of the interior surface, the interior layer including: a first region comprising Nickel Boride, wherein the thickness of the first region, when measured in a direction perpendicular to the longitudinal axis, is in the range of approximately 40 microns to 80 microns; and a second region substantially free of Boron, wherein the thickness of the second region, when measured in a direction perpendicular to the longitudinal axis, is in the range of approximately 1 micron to 40 microns; and wherein the second region is closer to the interior surface of the core element than the first region, when considered in a direction perpendicular to the longitudinal axis.
Additionally or alternately, the second region can consists of nickel plate.
None of these brief summaries of the inventions is intended to limit or otherwise affect the scope of what has been disclosed and enabled or the appended claims, and nothing stated in this Brief Summary of the Invention is intended as a definition of a claim term or phrase or as a disavowal or disclaimer of claim scope.
The following figures form part of the disclosure of inventions and are included to demonstrate further certain aspects of the inventions. The inventions may be better understood by reference to one or more of these figures in combination with the detailed description of certain embodiments presented herein in which:
While the inventions disclosed herein are susceptible to various modifications and alternative forms, only a few specific embodiments have been shown by way of example in the drawings and are described in more detail below. The figures and detailed descriptions of these embodiments are not intended to limit the breadth or scope of the inventive concepts or the appended claims in any manner. Rather, the figures and detailed written descriptions are provided to illustrate the inventive concepts to a person of ordinary skill in the art and to enable such person to make and use the inventive concepts illustrated and taught by the specific embodiments.
The Figures described above, and the written description of specific structures and functions below, are not presented to limit the scope of the inventions disclosed or the scope of the appended claims. Rather, the Figures and written description are provided to teach a person skilled in this art to make and use the inventions for which patent protection is sought.
A person of skill in this art having benefit of this disclosure will understand that the inventions are disclosed and taught herein by reference to specific embodiments, and that these specific embodiments are susceptible to numerous and various modifications and alternative forms without departing from the inventions we possess. For example, and not limitation, a person of skill in this art having benefit of this disclosure will understand that Figures and/or embodiments that use one or more common structures or elements, such as a structure or an element identified by a common reference number, are linked together for all purposes of supporting and enabling our inventions, and that such individual Figures or embodiments are not disparate disclosures. A person of skill in this art having benefit of this disclosure immediately will recognize and understand the various other embodiments of our inventions having one or more of the structures or elements illustrated and/or described in the various linked embodiments. In other words, not all possible embodiments of our inventions are described or illustrated in this application, and one or more of the claims to our inventions may not be directed to a specific, disclosed example. Nonetheless, a person of skill in this art having benefit of this disclosure will understand that the claims are fully supported by the entirety of this disclosure.
Those persons skilled in this art will appreciate that not all features of a commercial embodiment of the inventions are described or shown for the sake of clarity and understanding. Persons of skill in this art will also appreciate that the development of an actual commercial embodiment incorporating aspects of the present inventions will require numerous implementation-specific decisions to achieve the developer's ultimate goal for the commercial embodiment. Such implementation-specific decisions may include, and likely are not limited to, compliance with system-related, business-related, government-related, and other constraints, which may vary by specific implementation, location and from time to time. While a developer's efforts might be complex and time-consuming in an absolute sense, such efforts would be, nevertheless, a routine undertaking for those of skill in this art having benefit of this disclosure.
Further, the use of a singular term, such as, but not limited to, “a,” is not intended as limiting of the number of items. Also, the use of relational terms, such as, but not limited to, “top,” “bottom,” “left,” “right,” “upper,” “lower,” “down,” “up,” “side,” and the like are used in the written description for clarity in specific reference to the Figures and are not intended to limit the scope of the invention or the scope of what is claimed.
Reference throughout this disclosure to “one embodiment,” “an embodiment,” or similar language means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one of the many possible embodiments of the present inventions. The terms “including,” “comprising,” “having,” and variations thereof mean “including but not limited to” unless expressly specified otherwise. An enumerated listing of items does not imply that any or all of the items are mutually exclusive and/or mutually inclusive, unless expressly specified otherwise. The terms “a,” “an,” and “the” also refer to “one or more” unless expressly specified otherwise.
The description of elements in each Figure may refer to elements of proceeding Figures. Like numbers refer to like elements in all figures, including alternate embodiments of like elements.
Turning now to several descriptions, with reference to Figures, of particular embodiments incorporating one or more aspects of the disclosed inventions,
Referring first to
In the example of
In connection with the teachings of the present disclosure, once the Nickel containing layer 112 is formed on the core element 500, the layer 112 is exposed to a Boron containing mixture and subjected to a Boronization process (sometimes called a Boriding process). In this process Boron is diffused into a position of the exposed surface of the layer to a desired or predefined thickness. In exemplary embodiments the desired or predefined thickness is less than the original thickness of the layer 112 such that the result of the Boronization (or Boriding) process will be the creation of two regions within the layer 112, a first region 113 containing boron and a second region 112A substantially free of Boron. As reflected in the figure, in such an embodiment the second—substantially Boron free region 112A—will be closer to the core element 500 than the first region 113. The thickness of the Boron containing region can vary, but in some exemplary embodiments can be on the order of between about 40 microns to 80 microns.
In one exemplary embodiment, the Boron containing region of the layer 112 will comprise Nickel Boride (NiB).
As reflected in
Moreover, in the illustrated example, the both the region comprising Boron and the region substantially free of Boron will have a degree of corrosion resistance, wherein the degree of corrosion resistance of the region containing Boron will be less than the decree of corrosion resistance the region that is substantially free of Boron.
This structure, therefore, includes an outer hardened region 114 that will tend to protect the barrel from wear and deterioration, and an inner Nickel region 112 that can protect the core from corrosion. This is because the outer surface 114 will have a relative hardness that is significant and serves as a protective shield. However, because of its relative hardness, the outer region 114 can be brittle and subject to micro-cracking. Such micro-cracks, however, will not necessarily extend to the core element 500 because they will be halted by the relatively softer composition of the substantially Boron-free Nickel layer 112A. The substantially Boron-free nickel layer 112A can thus act as a barrier that can block any corrosive elements that may enter one of the micro-cracks within the outer layer 114, such as element 115 in
As reflected above, in the embodiment
In the example of
In the example of
In the example of
As reflected above, in the embodiment
In the example of
In the example of
In the example of
Many different manufacturing processes can be used to form a barrel for use in sucker rod assembly as discussed herein. One such process is depicted in
Referring to
After a period of time reflected by line 904, a step 906 can be performed in which a mixture containing Boron is applied to the Nickel plated tubular object. This step can be performed in various ways. For example, this step can involve the application of a Boron containing gas to all or part of the Nickel plated tubular object. For example, where only an interior portion of the Nickel plated tubular object is to be exposed to the Boron containing gas, the gas can be pumped through the interior region of the tubular object. As another example, this step can involve the placement of the tubular object into a fluid containing Boron or packing a particle-based material containing Boron about the tubular object. In still further embodiments, this step can involve the application of a Boron continuing paste to the portions of the tubular object to which boron is to be exposed.
In the example of
As will be appreciated, because the heating step 908 results in a diffusion of Boron into the Nickel layer, the specific physical surface characteristics of the exterior surface are not determinative of the extent to which Boron can be infused into the layer. As such, it is not critical that the steps 906 and/or 908 occur within a limited time period after the Nickel electroplating step. For example, embodiments are envisioned where the Nickel electroplating step occurs at one location at time, and the application and heating steps 906 and 908 (or one of the two) occur a period of time 904 after the conclusion of the electroplating step 902. More specifically, embodiments are envisioned in which the duration 904 exceeds 60 minutes. This ability to perform the application and/or heating steps 906/908 relatively long after the electroplating step 902 can be contrasted with the operations required to create a Chromed Nickel surface, which require that the chroming operation be performed relatively soon after the Nickel plating and/or that the Nickel plated layer be activated before the chroming operation. This ability permits the process depicted in
Following the heating step 908, the heated tubular object will be cooled at step 910.
Other and further embodiments utilizing one or more aspects of the inventions described above can be devised without departing from the spirit of Applicant's invention. Further, the various methods and embodiments of the methods of manufacture and assembly of the system, as well as location specifications, can be included in combination with each other to produce variations of the disclosed methods and embodiments. Discussion of singular elements can include plural elements and vice-versa.
The order of steps can occur in a variety of sequences unless otherwise specifically limited. The various steps described herein can be combined with other steps, interlineated with the stated steps, and/or split into multiple steps. Similarly, elements have been described functionally and can be embodied as separate components or can be combined into components having multiple functions.
The inventions have been described in the context of preferred and other embodiments and not every embodiment of the invention has been described. Obvious modifications and alterations to the described embodiments are available to those of ordinary skill in the art. The disclosed and undisclosed embodiments are not intended to limit or restrict the scope or applicability of the invention conceived of by the Applicants, but rather, in conformity with the patent laws, Applicants intend to protect fully all such modifications and improvements that come within the scope or range of equivalent of the following claims.
This application claims priority to U.S. Provisional Patent Application No. 63/520,028, filed on Aug. 16, 2023, the entire contents of which are incorporated herein for all purposes.
Number | Date | Country | |
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63520028 | Aug 2023 | US |