Drill strings are made of a series of drill pipes that are connected together. A drill bit is generally positioned at the lower end of the drill string to bore through the earth and create a well, enabling the recovery of hydrocarbons from subterranean reservoirs. Individual drill pipes typically have radially enlarged end connections, which allow for the drill pipes to be connected together, either end-to-end or using collars, to form the drill string. During drilling operations, the drill bit is rotated by rotating the drill string. The drill string is suspended from a drilling rig and is in tension, but in order to apply weight to cause the drill bit to bite into the earth, a bottom hole assembly is positioned just above the drill bit. The bottom hole assembly is, in effect, a number of weighted drill collars.
In extended-reach drilling, the drill bit can be several miles laterally displaced from the foot of the rig. In horizontal drilling, the bit follows an arcuate path and then drills a horizontal bore. In both extended-reach drilling and horizontal drilling, transmission of power from the rig to the drill bit may be hindered by frictional losses generated by contact between the enlarged, connected end portions of the drill pipes and the inner surface of the wellbore and/or casing that lines the wellbore.
To protect the drill string from abrasion against the side wall of the wellbore or casing, a drill pipe protector can be employed. Drill pipe protectors are typically elastomer elements that are clamped or otherwise secured to the outer diameter of the drill pipe. Such drill pipe protectors generally prevent the drill pipe from contacting inner surface of the casing or wellbore, thereby avoiding or at least mitigating frictional contact between the drill pipe body and the inner surface of the wellbore. Without a drill pipe protector, the drill string is subjected to shock and abrasion when the drill string comes into contact with the side wall of the wellbore or the casing.
Rotating drill pipe protectors have been implemented that allow for rotation between the drill pipe and the drill pipe protector, such that the drill pipe does not contact the wellbore when the rotating drill pipe is being rotated. Rotation of a drill string with respect to the rotating drill pipe protector may, however, create frictional torque on the drill string, even if to a lesser degree than the drill pipe directly engaging the casing/wellbore wall. Additionally, rotation of the drill string with respect to the rotating drill pipe protector may lead to wear and abrasions on the outer surface of the drill pipes of the drill string, and thus, may lead to a shorter life span of the drill pipe and/or the drill pipe protector.
Embodiments of the disclosure include an apparatus for reducing torque in a drill string that includes a clamp assembly having a first clamp segment and a second clamp segment, the first and second clamp segments each being generally arcuate and configured to connect together so as to secure the clamp assembly around an oilfield tubular and prevent the clamp assembly from axial and rotational movement relative to the oilfield tubular. The first and second clamp segments each include a first extension and a second extension, each of the first and second extensions having a tapered end that decreases in outer diameter as proceeding in an axial direction, so as to provide a conical guide surface. An outer sleeve is positioned around the clamp assembly, is configured to rotate with respect to the oilfield tubular and the clamp assembly, and is prevented from axial movement relative thereto.
Embodiments of the disclosure include a method, including securing a first clamp segment together with a second clamp segment and around a tubular, such that the first and second clamp segments resist axial and radial movement relative to the tubular. The first and second clamp segments each include first and second extensions, each of the first and second extensions having a tapered end. The method also includes positioning an outer sleeve around the first and second clamp segments. The outer sleeve is configured to rotate relative to the first and second clamp segments, and the outer sleeve is received axially between the tapered ends of the first clamp segment and axially between the tapered ends of the second clamp segment.
Embodiments of the disclosure include an apparatus for reducing torque in a drill string. The apparatus includes a clamp assembly including a first clamp segment and a second clamp segment, the first and second clamp segments each being generally arcuate and configured to connect together so as to secure the clamp assembly around an oilfield tubular and prevent the clamp assembly from axial and rotational movement relative to the oilfield tubular. The first and second clamp segments each include a first extension and a second extension, each of the first and second extensions having a tapered end that decreases in outer diameter as proceeding in an axial direction, so as to provide a conical guide surface. The first and second clamp segments each include at least one radial protrusion and at least two recesses. The clamp assembly further includes a plurality of lock inserts each having a tapered profile and configured to fit radially between the first clamp segment, the second clamp segment, or both and the oilfield tubular, so as to secure the clamp assembly to the oilfield tubular. The lock inserts each include a plurality of insert segments, and the first clamp segment and the second clamp segment each include a plurality of pockets on an inner surface thereof, the insert segments being configured to be positioned in the pockets between axially-extending walls of the first and second clamp segments. The apparatus also includes an outer sleeve positioned around the clamp assembly and including at least one radial protrusion configured to fit into the at least one recess of the first and second clamp segments, and at least one recess configured to receive the at least one protrusion of the first and second clamp segments, such that multiple load-transferring interfaces are formed between shoulder surfaces of the clamp assembly and shoulder surfaces of the outer sleeve. The outer sleeve is configured to rotate with respect to the oilfield tubular and the clamp assembly, and is prevented from axial movement relative thereto, wherein the first and second clamp segments each include a central body defining a recessed region, and the outer sleeve includes an inwardly-extending protrusion configured to be received at least partially into the recessed region, so as to retain an axial positioning of the outer sleeve relative to the clamp assembly.
The foregoing summary is intended merely to introduce a subset of the features more fully described of the following detailed description. Accordingly, this summary should not be considered limiting.
The accompanying drawing, which is incorporated in and constitutes a part of this specification, illustrates an embodiment of the present teachings and together with the description, serves to explain the principles of the present teachings. In the figures:
It should be noted that some details of the figure have been simplified and are drawn to facilitate understanding of the embodiments rather than to maintain strict structural accuracy, detail, and scale.
Reference will now be made in detail to embodiments of the present teachings, examples of which are illustrated in the accompanying drawing. In the drawings, like reference numerals have been used throughout to designate like elements, where convenient. The following description is merely a representative example of such teachings.
The torque reducer 100 may also include an outer sleeve 104, which may, as shown, be provided as a pair of sleeve segments 104A, 104B securable together using fasteners 104C (e.g., bolts). In other embodiments, the sleeve segments 104A, 104B may be otherwise connected together, such as by adhering, clamping, crimping, etc. In some embodiments, the sleeve segments 104A, 104B may be hinged on one circumferential side and removably coupled together (e.g., fastened) on the opposite circumferential side. It will be appreciated that any number of sleeve segments 104A, 104B may be employed. The combination of the sleeve segments 104A, 104B, are positioned entirely around the first and second clamp assemblies 106, 108, so as to fully envelope the clamp assemblies 106, 108.
The outer sleeve 104 may define a central, receiving region 105 and two end regions 107A, 107B. As shown, portions of the receiving region 105 and the end regions 107A, 107B may be defined in each of the sleeve segments 104A, 104B. The receiving region 105 may define an inner diameter that is larger than the inner diameter of the two end regions 107A, 107B. The receiving region 105 may be configured to receive the clamp assemblies 106, 108, while the end regions 107A, 107B may be configured to be received (e.g., directly) around the drill pipe 102 (or potentially with one or more other structures therebetween). Shoulders 109A, 109B may be defined at the transition between the end regions 107A, 107B and the clamp-receiving region 105. The shoulders 109A, 109B may be located on opposite axial sides of the clamp assemblies 106, 108 when the torque reducer 100 is assembled.
The inner diameter of the outer sleeve 104 in the clamp-receiving region 105 may be slightly larger than an outer diameter of the clamp assemblies 106, 108. The inner diameter of the end regions 107A, 107B may be slightly larger than the outer diameter of the drill pipe 102; however, the radial clearance between 107 and drill pipe 102 is greater than clearance between 105 and 106. Accordingly, the outer sleeve 104 may be rotatable relative to the clamp assemblies 106, 108 and the drill pipe 102, in a manner similar to a plain bearing. By contrast, the clamp assemblies 106, 108 may be secured in position on the drill pipe 102, and may thus rotate therewith, e.g., relative to the outer sleeve 104 and/or the surrounding wellbore (e.g., a stationary frame of reference). For example, the clamp assemblies 106, 108 may be configured to facilitate such relative rotation between the clamp assemblies 106, 108 and the outer sleeve 104 by providing a low-friction, wear-resistant engagement therebetween, as will be described in greater detail below.
Although
In the illustrated embodiment, each of the clamp segments 202, 204, 206, may include circumferential ends 202A, 202B, 204A, 204B, 206A, 206B, respectively (collectively referred to herein as circumferential ends 202A-206B). At least some of the circumferential ends 202A-206B may be configured to be pivotally coupled to one another, and some of the circumferential ends 202A-206B may be removably coupled together so as to allow the clamp assembly 200 to be received around and secured to the drill pipe 102 or another tubular.
For example, the circumferential end 202A of the first clamp segment 202 may be pivotally coupled to the circumferential end 206A of the intermediate clamp segment 206. The circumferential end 206B of the intermediate clamp segment 206 may be pivotally coupled to the circumferential end 204A of the second clamp segment 204. Once received around the drill pipe 102, for example, the circumferential end 202B of the first clamp segment 202 may be removably (and potentially adjustably and/or pivotally) connected to the circumferential end 204B of the second clamp segment 204, e.g., using bolts, as will be described in greater detail below.
The clamp segments 202-206 may each include one or more structural members (four are shown for each segment, e.g., 212, 214, 216, 218; collectively referred to herein as structural members 212-218), and one or more radial wear members (three are shown, e.g., 220, 222, 224; collectively referred to herein as radial wear members 220-224), which are also a part of the structure. The structural members 212-218 may be arcuate and made from a relatively strong (as compared to the radial wear members 220-224) material, such as steel, although other materials are contemplated. The radial wear members 220-224 may also be arcuate and may be made from a material providing a relatively low coefficient of friction (as compared to the structural members 212-218), such as brass, composite (e.g., a fiber-reinforced) material, plastic, or a combination thereof, although other materials are contemplated. Also, in some embodiments, the radial wear members 220-224 may be coated with a material to provide a relatively low coefficient of friction, in comparison to the main body thereof. In some embodiments, the structural members 212-218 may extend along a greater arc than the radial wear members 220-224, so as to provide for connection between the clamp segments 202-206. Further, the structural members 212-218 may be separated axially apart, and may be interleaved with the radial wear members 220-224 (i.e., the radial wear members 220-224 may each be positioned between two of the structural members 212-218).
The clamp segments 202-206 may each include arcuate axial wear members 230, 232, which may be positioned on opposite axial ends of the clamp segments 202-206 and connected to the end structural members 212, 218. The arcuate axial wear members 230, 232 may each include two or more recesses 234, 236, in which bolts 241 may be positioned. The recesses 234, 236 may be positioned between wear surfaces 233, 235, 237. The bolts 241 may extend through the assembly of axial wear members 230, 232, radial wear members 220-224, and structural members 212-218, so as to fasten the assembly together. The recesses 234, 236 may provide a pocket such that the bolt 241 ends are prevented from engaging adjacent surfaces, allowing for the low-friction material of the axial wear members 230, 232 (e.g., on the wear surfaces 233, 235, 237) to provide the axial extents of the clamp assembly 200 and thus engage axially adjacent structures, as will be described in greater detail below. It will be appreciated that the assembly 200 may be connected together in a variety of different ways, with the illustrated bolts 241 being just one among many contemplated. For example, in other embodiments, the wear members 220-224, 230, 232 may be connected via pins, dovetail geometry, bonding, etc.
The radial wear members 220-224, and potentially the axial wear members 230, 232 as well, may have a greater radial thickness than the structural members 212-218. For example, the radial wear members 220-224, the structural members 212-218, and the axial wear members 230, 232 may together define an inner surface 226 of each of the clamp assembly 200, which may be generally constant and configured to engage the drill pipe 102 (
As mentioned above, the circumferential end 206B of the intermediate clamp segment 206 may be pivotally coupled to the circumferential end 204A of the second clamp segment 204. In the illustrated embodiment, a plurality of links 240 may provide such pivotal coupling. For example, each of the plurality of links 240 may be positioned circumferentially adjacent to one of the radial wear members 220-224 and axially between two of the structural members 212-218. A pin may extend through the structural members 212-218 and the links 240 on each of the clamp segments 204, 206, thereby providing for a pivotal connection. The first segment 202 and the intermediate segment 204 may be similarly, pivotally coupled together with links.
In at least one embodiment, at least one of the clamp segments 202-206 may include a magnetic element configured to attract the at least one of the clamp segments 202-206 to the drill pipe 102 during installation. In some embodiments, the magnetic element may be integrated into (i.e., be a magnetized part of or embedded within) one or more of the structural members 212-218, radial wear members 220-224, and/or axial wear member 230, 232.
The outer surface of these clamp segments 202, 204 may be generally continuous in an axial direction, as shown (e.g., not including interleaved, axially-adjacent segments), and may be coated with a material providing a relatively low coefficient of friction so as to reduce friction between the clamp assembly outer surface and the inner surface of the outer sleeve during operation. This embodiment also includes the extension 275, extending from the lower (as viewed in the figure) axial end of the clamp segments 202, 204. The solid bodies of the clamp segments 202, 204 may extend, as a unitary piece from the extension 275 to the opposite axial end of the clamp assembly 200. In some embodiments, as shown, the extension 275 may form an integral part of the clamp segments 202, 204, and thus the solid body of the clamp segments 202, 204 may be considered to extend entirely between the axial ends of the clamp segment 202, 204.
For example, the fasteners 400 may be positioned between axially-adjacent structural members 212-218. The fasteners 400 may extend through pins 402 formed in the first clamp segment 202 and may be threaded into holes 404 provided in a corresponding location on the second clamp segment 204. As such, turning the fasteners 400 may serve to draw the first and second clamp segments 202, 204 closer together and reduce the overall circumference of the clamp assembly 106, thereby causing the clamp assembly 106 to grip the drill pipe 102. It will be appreciated that such adjustable and/or removable connection may be made using a variety of other structures, and that the clamp assembly 200 may include two or more sets of circumferential ends connected together in this manner.
Further, the shoulder 109A is closely proximal (e.g., potentially engaging) the axial wear member 230. Accordingly, when an axial load (e.g., to the left, in the illustration) is present, the shoulder 109A may engage the low-friction material of the axial wear member 230, thereby mitigating friction forces that would otherwise tend to impede relative rotation between the outer sleeve 104 and the clamp assembly 106. It will be appreciated that the interaction between the shoulder 109B (see
The method 800 may begin by positioning one or more clamp assemblies 106, 108 around a drill pipe 102, as at 802.
The method 800 may also include connecting together two circumferential ends 202B, 204B of clamp segments 202, 204 of the one or more clamp assemblies 106, 108, as at 804. As best shown in
The method 800 may also include positioning an outer sleeve 104 around an entirety of the one or more clamp assemblies 106, 108, such that the outer sleeve 104 is configured to rotate with respect to the drill pipe by sliding along radial and/or axial wear members of the one or more clamp assemblies, as at 808.
The medial shoulder 1000 may thus partition the clamp-receiving region 105 into two, smaller clamp-receiving portions 1005A, 1005B, each receiving one of the clamp assemblies 106, 108. The clamp-receiving portions 1005A, 1005B may have an axial length that is slightly larger than the axial length of the clamp assembly(ies) 106, 108 positioned therein, such that some amount of axial clearance is provided between the outer sleeve 104 and the clamp assemblies 106, 108. It will be appreciated that two or more clamp assemblies may be positioned in either or both of the clamp-receiving portions 1005A, 1005B. Moreover, it will be appreciated that the outer sleeve 104 may include more than one medial shoulder, and thus more than two clamp-receiving portions, each potentially including one or more clamp assemblies therein.
Referring again to the illustrated embodiment, when the first and second clamp assemblies 106, 108 rotate with respect to the outer sleeve 104 (as by rotation of the drill pipe 102), the axial wear member 232 of the first clamp assembly 106 and/or the axial wear member 230 of the second clamp assembly 108 may slide against the corresponding axially-facing surface 1002, 1004 of the medial shoulder 1000. Which (if any) of the clamp assemblies 106, 108 engages the shoulder 1000 may depend on a direction of an axial (e.g., drag) force incident on the outer sleeve 104.
As can also be seen in
The outer sleeve 104 may rotate relative to the drill pipe 102 and clamp assemblies 106, 108, while an inner surface of the end regions 107A, 107B thereof engages the extensions 1100, 1102. The extensions 1100, 1102 may thus be made of a low-friction, wear-resistant material, similar to or the same as, the axial wear members 230, 232. The extensions 1100, 1102 may be sized to extend all or a portion of the axial length of the end regions 107A, 107B, such that the axial ends of the extensions 1100, 1102 and the outer sleeve 104 are aligned. In other embodiments, the extensions 1100, 1102 may be shorter, and the ends thereof may be within the outer sleeve 104. In still other embodiments, such as, for example, the embodiment of
In the specific, illustrated embodiment, the extensions 1100, 1102 may each include an outboard shoulder 1104, 1106. The shoulders 1104, 1106 may be integral with the remainder of the extensions 1100, 1102, being formed by the extensions 1100, 1102 extending radially outward. The outboard shoulders 1104, 1106 may be formed so that the axial ends of the outer sleeve 104 may bear upon the outboard shoulders 1104, 1106 when an axial load is applied to the outer sleeve 104. Engagement of the outer sleeve 104 with the outboard shoulder(s) 1104, 1106 may be contemporaneous with rotation of the outer sleeve 104, and thus the outboard shoulders 1104, 1106 may provide for a relatively low-friction, wear-resistant interaction therebetween. An outer surface 1108, 1110 of the outboard shoulders 1104, 1106 may be tapered so as to provide a smooth transition from the drill pipe 102 outwards to the outer surface of the outer sleeve 104 as proceeding axially along the drill pipe 102.
Each of the clamp segments 202, 204 may each include a first extension 1404, 1406 and a second extension 1408, 1410, which extend in opposite axial directions from opposite axial ends of a central body 1412, 1414 of the clamp segments 202, 204, respectively. The extensions 1404-1410 may have a reduced thickness (radial dimension) in comparison to the central bodies 1412, 1414. Accordingly, axially-facing shoulders 1416A, 1416B, 1418A, 1418B may be defined at transitions between the extensions 1404-1410 and the central bodies 1412, 1414, e.g., where the extensions 1404-1410 meet the central body 1412, 1414. This may also be referred to as the central bodies 1412, 1414 and the extensions 1404-1410 together defining the shoulders 1416, 1418.
The outer sleeve 104 may be received around the segments 202, 204, such that an inner diameter surface thereof slides against an outer diameter surface of the segments 202, 204, as will be described in greater detail below. In particular, the outer sleeve 104 (including the two outer sleeve segments 104A, 104B, as mentioned above) may define a clamp-receiving region 105 therein, which is shaped (e.g., dimensioned) and/or otherwise configured to receive the central bodies 1412, 1414 of the clamp segments 202, 204. Further, the outer sleeve 104 may define first and second extension-receiving regions 1420, 1422 therein, on either axial side of the clamp-receiving region 105. The extension-receiving regions 1420, 1422 may be sized to receive the first extensions 1404, 1406 and the second extensions 1408, 1410, respectively. For example, the extension-receiving regions 1420, 1422 may have a smaller diameter than the clamp-receiving region 105. Axially-facing shoulders 1426, 1428 may be defined at a transition between the extension-receiving regions 1420, 1422 and the clamp-receiving region 105 (e.g., where the regions 1420, 1422 meet the clamp-receiving region 1411, which may also be referred to as the shoulders 1426, 1428 being defined therebetween). The shoulders 1426, 1428 may be sized, positioned, formed, or otherwise configured to slidingly engage the axially-facing shoulders 1416A, 1416B, 1418A, 1418B of the clamp assembly 200, respectively. The shoulder-to-shoulder engagement may provide a thrust-bearing function, transmitting axial loads on the outer sleeve 104 to the clamp assembly 200, and then to the drill pipe 102 via the gripping force.
In an embodiment, the inner clamp assembly 200 may be at least partially made from a through-hardened (or hardenable) alloy steel such as a chromium/molybdenum steel or a nickel/chromium/molybdenum steel, examples of which include AISI 4130, 4140, 4330, and 4340. In an embodiment, the outer radial surface of the clamp assembly 200 (e.g., provided cooperatively by the clamp segments 202, 204), which may be in contact with the inner surface of the outer sleeve 104, may be case-hardened using a process such as boriding, boronitriding, boronizing, or the like, which may produce a relatively low-friction and high surface hardness on the outer radial surface of the clamp assembly 200.
In an embodiment, the inner radial surface of the clamp assembly 200 (e.g., provided cooperatively by the clamp segments 202, 204) may be made at least partially of a bare, uncoated steel. The inner surface of the clamp assembly 200 may contact the drill pipe 102, and may thus not call for a low-friction interface therewith, as the clamp assembly 200 is generally configured, once attached to the drill pipe 102, to be immovable with respect thereto. As such, higher friction may be provided by the bare, uncoated steel of the inner surface of the clamp assembly 200 to maintain the axial and rotational holding force, so as to resist slippage. In some embodiments, non-marking grip coatings may be applied to the inner surface of the clamp assembly 200 to enhance friction between the clamp assembly 200 and the drill pipe 102. For example, a diamond nanoparticle embedded coating may be applied to the clamp assembly 200. The clamp assembly 200 may thus be formed with an outer surface having low friction and high hardness (e.g., harder than the inner surface of the outer sleeve 104) and an inner surface with high frictional characteristics.
The outer sleeve 104 may be made at least partially from a lower hardness steel than the casing into which the torque reducer 100 is run. The outer diameter surface of the outer sleeve 104 (e.g., as provided cooperatively by the sleeve segments 104A, 104B) may not be case-hardened, for example. The outer surface of the outer sleeve 104 having a lower hardness than the casing may avoid damage to interior of the casing. The inner surface of the outer sleeve 104 (e.g., as provided cooperatively by the sleeve segments 104A, 104B) may be case hardened, e.g., plasma nitrided. The case hardening of the inner surface of the outer sleeve 104 may be configured to produce a lower hardness than the hardness of the outer radial surface of the clamp assembly 200. Because the inner surface of the outer sleeve 104 slides against the relatively harder outer surface of the clamp assembly 200, the nitrided layer of the interior of the outer sleeve 104 may wear more quickly than does the boride hardened layer on the outer radial surface of the clamp assembly 200. Accordingly, the outer sleeve 104 is generally configured to be consumable or sacrificial, relative to the casing and the clamp assembly 200, as the wear of the components may generally occur in the outer sleeve 104, which is softer on the inside than the outer surface of the clamp assembly 200, and softer on the outside than the casing.
In this embodiment, the clamp assembly 106 includes enlarged extensions 1700, 1702 at either axial end of the clamp assembly 106. The clamp segments 202, 204 may each form half-cylindrical bodies (or another fraction, e.g., if there are more than two clamp segments). The outer sleeve 104 may be received around the clamp assembly 106, axially between the enlarged extensions 1700, 1702, such that axial forces incident on the outer sleeve 104 are transmitted to the clamp assembly 106 via engagement between inboard facing axial ends 1704, 1706 of the outer sleeve 104 and shoulder surfaces 1708, 1710 of the enlarged extensions 1700, 1702, as will be described in greater detail below.
Furthermore, at least a portion 1712, 1714 of each of the enlarged extensions 1700, 1702 may be tapered, as proceeding in an axial direction, away from one another, thereby providing a conical guide surface for the extensions 1700, 1702. In an embodiment, the enlarged extensions 1700, 1702 may be tapered into a relatively thin shoulder on the outboard side thereof. Since the clamp assembly 106 may be directly positioned on the tubular 102, this may provide a small shoulder profile for the torque reducer 100, which reduces the potential for the torque reducer 100 to catch on wellbore restrictions, other equipment, etc., while being moved in the well.
Referring specifically now to
The sleeve segment 104A may also include one or more protrusions alternating with one or more recesses. In particular, in this embodiment, the sleeve segment 104A includes three protrusions 1740, 1742, 1744 and two recesses 1746, 1748, with the recesses 1746, 1748 separating the protrusions 1740, 1742, 1744, and the protrusions 1740, 1742, 1744 representing areas of increased radial thickness, where the sleeve segment 104A extends radially inwards. The outer diameter surface 1750 of the outer sleeve 104 may be generally uniform. At least a portion 1745, 1747 of the protrusions 1740, 1744 may be tapered, such that ends 1749, 1751 of the protrusions 1740 are relatively small and, e.g., obscured from forming an exposed radial profile at the enlarged extensions 1700, 1702.
The clamp segment 204 may be substantially similar (e.g., the same as) the clamp segment 202, and the sleeve segment 104B may be substantially similar to (e.g., the same as) the sleeve segment 104A, such that, when assembled the internal profiles of recesses, protrusions, and shoulders discussed above are generally annular. More particularly, the recesses 1734, 1736, 1738 of the clamp assembly 106 may be sized and configured to receive the protrusions 1740, 1742, 1744 of the outer sleeve 104. Likewise, the recesses 1746, 1748 of the outer sleeve 104 may be sized and configured to receive the protrusions 1730, 1732 of the clamp assembly 106. The protrusions 1740, 1742, 1744 may engage and bear upon the protrusion 1730, 1732, and thereby transmit axial and radial loads thereto. The outboard-most protrusions 1740 and 1744 may also be able to bear against the enlarged extensions 1700, 1702, as noted above.
Accordingly, three load surfaces are provided between the outer sleeve 104 and the clamp assembly 106 to transmit force in either axial direction. That is, in the presence of downward axial loads, the protrusion 1740 bears upon the shoulder 1730, the protrusion 1742 bears upon the shoulder 1732, and the protrusion 1744 bears upon the enlarged extension 1702. The load engagements in the reverse axial direction (upwards), result in the protrusion 1744 bearing against the shoulder 1732, the protrusion 1742 bearing against the shoulder 1730, and the protrusion 1740 bearing against the enlarged extension 1700.
Referring again additionally to
As shown in
The pockets 2300-2304 may be wedge-shaped and may be positioned in the respective radially-enlarged portions of the clamp segments 202, 204, e.g., in the enlarged extensions 1700, 1702 and the shoulder 1730. In the illustrated embodiment, the pockets 2300, 2304 each define a single wedge, and the pocket 2302 defines two wedges, one tapering in each axial direction. Likewise, the inserts 2306-2312 may have a wedge-shaped exterior surface that is configured to slide along the inner surface of the wedge-shaped pockets 2300-2304. Accordingly, relative axial movement of the clamp segments 202, 204 and the inserts 2306-2312 may move the inserts 2306-2312 radially toward the tubular 102. Specifically, movement of the clamp segments 202, 204 downward drives the inserts 2306, 2308 into the tubular 102, while movement of the clamp segments 202, 204 upward drives the inserts 2310, 2312 into the tubular 102.
The inserts 2306-2312 may be sized such that, even in the farthest radially outward, or “retracted” position, the inserts 2306-2312 maintain a radial gap between the tubular 102 and the clamp segments 202, 204. In some cases, flexing, movement, etc., may permit part of one or both of the clamp segments 202, 204 to contact the tubular 102, but the inserts 2306-2312 may generally provide an annular radial gap between at least a portion of the clamp segments 202, 204 and the tubular 102. Thus, connecting the clamp segments 202, 204 together around the tubular 102 may provide an initial, radial-inward gripping force by compressing the inserts 2306-2312 between the clamp segments 202, 204 and the tubular 102. Axially-directed loads on the clamp segments 202, 204 may force the clamp segments 202, 204 in the axial direction, which in turn drives at least some of the inserts 2306-2312 into tighter gripping engagement with the tubular 102, thereby resisting displacement of the clamp assembly 106 relative to the tubular 102.
The clamp segment 204 may be substantially similar (e.g., the same). In this view, gripping surfaces 2400 of the inserts 2306-2312 are visible. The gripping surface 2400 is configured to engage the tubular 102 (e.g.,
As shown, the pockets 2300-2304 may each be partitioned into smaller, arcuate pockets, e.g., pockets 2402, 2404, 2406 as indicated for the pocket 2300. The inserts 2306-2312 may likewise be segmented into insert segments, e.g., insert segments 2408, 2410, 2412 for the insert 2302. Axially-extending shoulders 2414, 2416 are formed between adjacent pockets 2402-2408.
The insert segments 2408-2412 may be arcuate in shape, to match the curvature of the outer diameter surface of the tubular 102, and may be configured to bite into the tubular 102 when the clamp segments 202, 204 force the inserts 2306-2312 radially inwards. In at least some embodiments, at least a portion of the gripping surface 2400 may extend at least partially in an axial direction, providing a frictional contact surface with an axial component. When the gripping surface 2400 bites into the tubular 102, the gripping surface 2400 may be at least partially embedded into the tubular 102, and may thus provide transmission of axially and/or circumferentially-directed loads. In such embodiments, the gripping surface 2400 and inserts 2306-2312 may permit the clamp assembly 104 to resist rotation and axial movement with respect to the tubular 102.
The provision of arcuate insert segments 2408-2412 between the shoulders 2414, 2416 may provide for increased torque transmission between the insert segments 2408-2412 and the clamp segment 202, such that the clamp segment 202 resists rotation around the tubular 102, when the insert segments 2408-2412 are engaged with the tubular 102 (e.g.,
In at least some embodiments, the insert segments 2408-2412 may be initially held in place in the respective pockets 2402-2406 by a shearable member, e.g., a shear screw or pin, received through the clamp segment 202 and into connection with the insert segments 2408-2412. This may permit assembly of the clamp assembly 106 onto the tubular 102. The shearable member may yield under relatively low axial loads, releasing the inserts 2408-2412 to move between the extended and retracted positions. It will be appreciated that any one or more of the other inserts 2308, 2310 (e.g.,
The insert 2306 is configured to make contact with the tubular 102 when the clamp assembly 104 is initially installed onto the tubular. This arrangement provides an axial preload onto the insert 2306 such that the clamp assembly 104 is held stationary via the initial preload and frictional engagement with the tubular. Once an axial load is applied to the torque reducer 100, the torque reducer 100 may move incrementally, but the insert 2306 is held stationary due to the frictional engagement with the tubular. The incremental differential movement between the insert 2306 and the clamp assembly 104, combined with the tapered engagement surface between the insert 2306 and the clamp segments 202, 204 results in an increase in the radial compressive load between the insert 2306 and the clamp segments 202, 204. In at least some embodiments, when the clamp assembly 104 has been installed onto the tubular, the insert 2306 contacts of the tubular. Thus, the insert 2306 may provide a gap between the tubular and the clamp segments 202, 204, while the insert 2306 itself engages the tubular, e.g., at all times while installed.
As used herein, the terms “inner” and “outer”; “up” and “down”; “upper” and “lower”; “upward” and “downward”; “above” and “below”; “inward” and “outward”; “uphole” and “downhole”; and other like terms as used herein refer to relative positions to one another and are not intended to denote a particular direction or spatial orientation. The terms “couple,” “coupled,” “connect,” “connection,” “connected,” “in connection with,” and “connecting” refer to “in direct connection with” or “in connection with via one or more intermediate elements or members.”
While the present teachings have been illustrated with respect to one or more implementations, alterations and/or modifications may be made to the illustrated examples without departing from the spirit and scope of the appended claims. In addition, while a particular feature of the present teachings may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular function. Furthermore, to the extent that the terms “including,” “includes,” “having,” “has,” “with,” or variants thereof are used in either the detailed description and the claims, such terms are intended to be inclusive in a manner similar to the term “comprising.” Further, in the discussion and claims herein, the term “about” indicates that the value listed may be somewhat altered, as long as the alteration does not result in nonconformance of the process or structure to the illustrated embodiment.
Other embodiments of the present teachings will be apparent to those skilled in the art from consideration of the specification and practice of the present teachings disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the present teachings being indicated by the following claims.
This application is a continuation-in-part of U.S. patent application having Ser. No. 16/898,099, which was filed on Jun. 10, 2020 and is a continuation-in-part of U.S. patent application having Ser. No. 16/050,686, which was filed on Jul. 31, 2018 and claims priority to U.S. Provisional Patent application having Ser. No. 62/539,607, which was filed on Aug. 1, 2017. Each of these priority applications is incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
1889806 | Lamb et al. | Dec 1932 | A |
2813697 | Swart | Nov 1957 | A |
3397017 | Grant et al. | Aug 1968 | A |
3410613 | Kuus | Nov 1968 | A |
3667817 | Kellner | Jun 1972 | A |
4199011 | Kreft | Apr 1980 | A |
5069297 | Krueger et al. | Dec 1991 | A |
5579854 | Barry | Dec 1996 | A |
5692563 | Krueger et al. | Dec 1997 | A |
5711386 | Swietlik | Jan 1998 | A |
5810100 | Samford | Sep 1998 | A |
5901798 | Herrera et al. | May 1999 | A |
6032748 | DeBray et al. | Mar 2000 | A |
6250406 | Luke | Jun 2001 | B1 |
6739415 | Mitchell et al. | May 2004 | B2 |
6962205 | Lay, Jr. | Nov 2005 | B1 |
7025136 | Tulloch et al. | Apr 2006 | B2 |
7055631 | Mitchell et al. | Jun 2006 | B2 |
7159619 | Latiolais, Jr. | Jan 2007 | B2 |
7938202 | Mitchell et al. | May 2011 | B2 |
8511377 | Casassa et al. | Aug 2013 | B2 |
8668007 | Casassa et al. | Mar 2014 | B2 |
8863834 | Buytaert et al. | Oct 2014 | B2 |
8919450 | Cruz | Dec 2014 | B1 |
9109417 | Leiper et al. | Aug 2015 | B2 |
9115546 | Howlett | Aug 2015 | B2 |
9140391 | Pajak et al. | Sep 2015 | B2 |
9441772 | Pajak et al. | Sep 2016 | B2 |
9598913 | Buytaert et al. | Mar 2017 | B2 |
10294734 | Buytaert et al. | May 2019 | B2 |
10724305 | Smith | Jul 2020 | B2 |
10724308 | Smith | Jul 2020 | B2 |
11352840 | Smith | Jun 2022 | B2 |
20090308617 | Minto | Dec 2009 | A1 |
20150008042 | Buytaert et al. | Jan 2015 | A1 |
20170030151 | Lutgring et al. | Feb 2017 | A1 |
20200300047 | Smith et al. | Sep 2020 | A1 |
20210079740 | Baynham et al. | Mar 2021 | A1 |
Number | Date | Country |
---|---|---|
112761546 | May 2021 | CN |
3922808 | Dec 2021 | EP |
2595333 | Nov 2021 | GB |
98-40601 | Sep 1998 | WO |
2001059249 | Aug 2001 | WO |
Entry |
---|
International Search Report and Written Opinion dated Nov. 28, 2018, PCT Application No. PCT/US2018/044607, filed Jul. 31, 2018, pp. 1-19. |
Search and Examination Report dated Oct. 19, 2023, GB Application No. 2308404.9, 5 pages. |
Number | Date | Country | |
---|---|---|---|
20220298872 A1 | Sep 2022 | US |
Number | Date | Country | |
---|---|---|---|
62539607 | Aug 2017 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 16898099 | Jun 2020 | US |
Child | 17833032 | US | |
Parent | 16050686 | Jul 2018 | US |
Child | 17833032 | US |