Tandem seal adapter with integrated tracer material

Information

  • Patent Grant
  • 12084962
  • Patent Number
    12,084,962
  • Date Filed
    Monday, March 15, 2021
    3 years ago
  • Date Issued
    Tuesday, September 10, 2024
    4 months ago
  • Inventors
  • Original Assignees
    • DynaEnergetics Europe GmbH
  • Examiners
    • Gay; Jennifer H
    Agents
    • Womble Bond Dickinson (US) LLP
Abstract
A tandem seal adapter for a perforating gun assembly includes a housing having a first end adapted to be connected to a first perforating gun and a second end adapted to be connected to a second perforating gun. A port extends through a wall of the housing and is in communication with an interior of the first perforating gun. A tracer material is arranged in the port, and a retainer secures the tracer material in the port. Upon detonation of the first perforating gun, the retainer is displaced and the tracer material is expelled from the port by gas pressure produced by the detonation. A corresponding method of using a tandem seal adapter to disperse tracer material into a wellbore and a tool string employing such a tandem seal adapter are also provided.
Description
BACKGROUND

Hydrocarbons, such as fossil fuels (e.g., oil) and natural gas, are extracted from underground wellbores extending deeply below the surface using complex machinery and explosive devices. Once the wellbore is established by placement of casing pipes after drilling and cementing the casing pipe in place, wellbore tools are lowered into the wellbore, and positioned adjacent one or more hydrocarbon reservoirs in underground formations.


The wellbore tools used in oil and gas operations are often sent down a wellbore in tool strings which are comprised of multiple discrete wellbore tools, or modules, connected together to consolidate different or multiple wellbore operations into a single “run”, or process of sending wellbore tools downhole to perform one or more operations. This approach contributes to time and cost savings because preparing and deploying a wellbore tool into a wellbore and pumping, with fluid under hydraulic pressure, the wellbore tool to a particular location in a wellbore that may be a mile or more under the ground requires a great deal of time, energy, and manpower. Additional time, manpower, and costs are required to conduct the operation and remove the spent wellbore tool(s) from the wellbore.


Wellbore tools, or “downhole tools”, as known and/or according to this disclosure include, without limitation, perforating guns, puncher guns, logging tools, jet cutters, plugs, frac plugs, bridge plugs, setting tools, self-setting bridge plugs, self-setting frac plugs, mapping/positioning/orientating tools, bailer/dump bailer tools and ballistic tools. Many of these wellbore tools contain sensitive or powerful explosives because many wellbore tools are ballistically (i.e., explosively) actuated or perform ballistic operations within the wellbore. Additionally, certain wellbore tools may contain, among other things, sensitive electronic control components and connections within the wellbore tool that control various operations of the wellbore tool. Explosives, control systems, and other components of wellbore tools may be incredibly sensitive to conditions within the wellbore including the high pressures and temperatures, fluids, debris, etc. In addition, wellbore tools that have explosive activity may generate tremendous amounts of ballistic and gas pressures within the wellbore tool itself. Accordingly, to ensure the integrity and proper operation of wellbore tools connected together as part of the tool string, connections between adjacent wellbore tools within the tool string must not only connect adjacent wellbore tools in the tool string, they must, in many cases, seal internal components of the wellbore tools from the wellbore conditions and pressure isolate adjacent modules against ballistic forces.


A tandem seal adapter (TSA) is a known connector often used for accomplishing the functions of a connector as described above, and in particular for connecting adjacent perforating gun modules. A perforating gun is an exemplary, though not limiting, wellbore tool that may include many of the features and challenges described above. A perforating gun carries explosive charges/shaped charges into the wellbore to perform perforating operations by which the shaped charges are detonated in a manner that produces perforations in a surrounding geological hydrocarbon formation from which oil and gas may be recovered. Conventional perforating guns often include electric componentry to control positioning and detonation of the explosive charges.


Shaped charges typically serve to focus ballistic energy onto a target, thereby producing a round perforation hole (in the case of conical shaped charges) or a slot-shaped/linear perforation (in the case of slot shaped charges) in, for example, a steel casing pipe or tubing, a cement sheath and/or a surrounding geological formation. In order to make these perforations, shaped charges typically include an explosive/energetic material positioned in a cavity of a housing (i.e., a shaped charge case), with or without a liner positioned therein. It should be recognized that the case, casing or housing of the shaped charge is distinguished from the casing of the wellbore, which is placed in the wellbore after the drilling process and may be cemented in place in order to stabilize the borehole prior to perforating the surrounding formations. Often, the explosive materials positioned in the cavity of the shaped charge case are selected so that they have a high detonation velocity and pressure. When the shaped charges are initiated, the explosive material detonates and creates a detonation wave, which will generally cause the liner (when used) to collapse and be ejected/expelled from the shaped charge, thereby producing a forward moving perforating material jet that moves at a high velocity. The perforating jet travels through an open end of the shaped charge case which houses the explosive charge, and serves to pierce the perforating gun body, casing pipe or tubular and surrounding cement layer, and forms a cylindrical/conical tunnel in the surrounding target geological formation.


In order to confirm that the formation has been perforated and fractured efficiently and that hydrocarbons are being recovered, flow indicators are sometimes included in a perforating gun in an effort to release the flow indicators into the wellbore or formation upon detonation of one or more of the shaped charges in the perforating gun. Flow indicators, sometimes referred to as tracers, can also be used in the oil and gas industry in order to qualitatively or quantitatively gauge how fluid flows through the reservoir, as well as being a useful tool for estimating residual oil saturation.


Typical flow indicators are incorporated as part of a perforating gun housing or a shaped charge housed in the perforating gun housing and are purposed to flow in the wellbore fluid, up to the surface of the wellbore, so they can serve as an indicator that perforations have been formed in the wellbore and reached the formation. Such flow indicators may also serve to indicate where the flow is coming from and/or where fracturing has occurred. In typical prior art configurations, the perforation jet of a shaped charge pierces through a flow indicator material, or the charge itself includes a flow indicator. Because of this arrangement, the heat and/or energy generated upon detonation of the shaped charge potentially manipulates the flow indicator, which can lead to an inaccurate determination at the well site. The indicator material may become damaged from the sudden pressure impact or the extremely high temperature of the explosive force created upon detonation of the shaped charge. In addition, some indicator material may remain on the rim order edge of the gun scallop or on the casing hole and not reach the actual formation, which may be influence the accuracy of the flow indicator readings at the wellbore surface.


A general, exemplary connection between adjacent perforating gun modules connected by a TSA according to the prior art is shown in FIG. 1. The configuration of the assembly in FIG. 1 is a simplified and representative cross-sectional illustration intended to aid in the disclosure and without reference or limitation to any prior art design(s).


As shown in FIG. 1, the representative assembly 100 includes a first perforating gun 101 and a second perforating gun 102 connected by a TSA 50. Each of the first perforating gun 101 and the second perforating gun 102 includes a perforating gun body 30, 31 enclosing an interior portion 40, 41 of the perforating gun 101, 102 where internal components of each perforating gun 101, 102 may be housed. The TSA 50 is positioned between and extends respectively at opposing ends into a portion of the interior 40, 41 of each of the first perforating gun 101 and the second perforating gun 102. The TSA 50 is connected to each of the first perforating gun 101 and the second perforating gun 102 by threaded connections 42 between an external threaded portion of the TSA 50 and an internal threaded portion of the perforating gun body 30, 31. A central portion 80 of the TSA 50 is positioned between two sealing elements 12, such as o-rings, that provide a seal about a junction 81 between the respective gun bodies 30, 31 which abut when fully screwed onto the TSA 50. The TSA 50 includes a through-bore 82 allowing electrical relays to pass between adjacent perforating guns 101, 102, and such through—bore 82 is typically sealed to pressure seal the adjacent perforating guns 101, 102 from each other.


Accordingly, there is a need for a mechanism of deploying tracer material into a wellbore upon detonation of a shaped charge such that the tracer material is not manipulated by the shaped charge. The present invention overcomes the disadvantages of the prior art by removing the tracer material from a direct impact by the shaped charge.


BRIEF DESCRIPTION

Embodiments of the disclosure are associated with a tandem seal adapter for a perforating gun assembly. The tandem seal adapter includes a housing having a first end and a second end spaced apart from the first end. According to an aspect, the first end is adapted to be connected to a first perforating gun and the second end is adapted to be connected to a second perforating gun. A port extends through a wall of the housing, from an exterior of the housing to an interior of the housing. The port is configured to be in communication with an interior of the first perforating gun. According to an aspect, a tracer material is arranged in the port, and a retainer secures the tracer material in the port. Upon detonation of the first perforating gun, gas pressure generated by the detonation displaces the retainer and the tracer material is expelled from the port.


Embodiments of the disclosure may be associated with a method of using a tandem seal adapter for a perforating gun assembly to disperse tracer material into a wellbore. The method includes connecting at least a first perforating gun to a tandem seal adapter. A tracer material is positioned in a port which extends through a housing of the tandem seal adapter. According to an aspect, the port extending through a wall of the housing from an exterior of the housing to an interior of the housing and is in communication with an interior of a first perforating gun. The tracer material is secured in the port by a retainer. The method further includes detonating a shaped charge in the first perforating gun, which creates a pressure sufficient to displace the retainer and expel the tracer material out of the port and into the wellbore.


Further embodiments of the disclosure are associated with a tool string including a plurality of perforating guns. Each perforating gun of the plurality of perforating guns includes at least one shaped charge and a tandem seal adapter positioned between every two adjacent perforating guns of the plurality of perforating guns. According to an aspect, the tandem seal adapter includes a housing having a first end adapted to be connected to a first perforating gun of the plurality of perforating guns and a second end adapted to be connected to a second perforating gun of the plurality of perforating guns. A port extends through a wall of the housing from an exterior of the housing to an interior of the housing. The port is in communication with an interior of the first perforating gun and a tracer material is arranged in the port. According to an aspect, a retainer is poisoned in the port, such that the tracer material is secured in the port. Upon detonation of the first perforating gun, gas pressure produced by the detonation displaces the retainer and expels the tracer material from the port.





BRIEF DESCRIPTION OF THE DRAWINGS

A more particular description will be rendered by reference to exemplary embodiments that are illustrated in the accompanying figures. Understanding that these drawings depict exemplary embodiments and do not limit the scope of this disclosure, the exemplary embodiments will be described and explained with additional specificity and detail through the use of the accompanying drawings in which:



FIG. 1 is a cross-sectional view of a tandem seal adapter assembly, according to the prior art;



FIG. 2 is a perspective view of a tandem seal adapter, according to an embodiment;



FIG. 3A is a cross-sectional view of a tandem seal adapter, according to an embodiment;



FIG. 3B is a cross-sectional view of a tandem seal adapter, according to an embodiment;



FIG. 4 is a cross-sectional view of a tandem seal adapter, including a tracer material and a plug, according to an embodiment;



FIG. 5A is a perspective view of a tracer material and a plug, according to an embodiment;



FIG. 5B is a perspective view of a plug, according to an embodiment;



FIG. 6 is a cross-sectional view of a tandem seal adapter according to an embodiment; and



FIG. 7 is a cross-sectional view of a perforating gun connected to the tandem seal adapter of FIG. 6; and



FIG. 8 is a side view of a tool string including a plurality of perforating guns connected by a plurality of tandem seal adapters, according to an embodiment.





Various features, aspects, and advantages of the exemplary embodiments will become more apparent from the following detailed description, along with the accompanying drawings in which like numerals represent like components throughout the figures and detailed description. The various described features are not necessarily drawn to scale in the drawings but are drawn to emphasize specific features relevant to some embodiments.


DETAILED DESCRIPTION

The headings used herein are for organizational purposes only and are not meant to limit the scope of the disclosure or the claims.


Reference will now be made in detail to various embodiments. Each example is provided by way of explanation and is not meant as a limitation and does not constitute a definition of all possible embodiments.


Embodiments of the disclosure are associated with a tandem seal adapter/tracer sub assembly (TSA) 200. The TSA 200 is illustrated in FIG. 2. According to an aspect, the TSA 200 includes a housing 210 having a first end 212 and a second end 214 spaced apart from the first end 212. A rib 242 may extend around a circumference of the TSA 200, between at least a portion of the first end 212 and the second end 214. The first and second ends 212, 214 may each be adapted to be connected to a perforating gun assembly.


The TSA 200 is illustrated in further detail in FIG. 3A and FIG. 3B. As illustrated in FIG. 3A, the first and second end 212, 214 may be receivable within an interior portion of a perforation gun. It is contemplated that the first end 212 and the second end 214 may include a connecting element to connect the TSA 200 to adjacent perforating gun housings. According to an aspect, the connection element includes a threaded connection. FIG. 3B illustrates the first end 212 and the second end 214 of the TSA 200 including threads 215. The threads 215 may mechanically couple with corresponding threads of the adjacent perforating gun housings.


The TSA 200 may include a cavity 224 extending along a longitudinal direction Y1 of the housing 210, between the first end 212 and the second end 214. According to an aspect, the cavity 224 extends from the first end 212 to the second end 214. The cavity 224 may be configured to receive one or more electrical components to facilitate the transmission of an electrical signal between connected perforating gun assemblies.


According to an aspect and as further illustrated in FIGS. 3A-3B, the TSA 200 may further include a pathway 222 extending from the first end 212 of the housing 210. The pathway 222 may also extend along a longitudinal direction Y2 of the housing 210. According to an aspect, the pathway 222 extends parallel to and spaced apart from the cavity 224.


A port 216 extends through a wall 211 of the housing to the pathway 222. According to an aspect, the port 216 radially extends from the pathway 222. As illustrated in FIG. 3A, the port 216 may intersect the pathway 222. The pathway 222 connects the port 216 to the interior of a perforating gun connected to the first end 212 of the TSA 200 (FIG. 6). According to an aspect, the port 216 includes a first radial bore 228 and a second radial bore 229. The first radial bore 228 extends from the pathway 222, while the second radial bore 229 extends from the first radial bore 228 to an external surface 227 of the housing 210. According to an aspect and as illustrated in FIG. 3B, the second radial bore 229 has an inner diameter ID2 that is larger than the inner diameter ID1 of the first radial bore 228.


In a further aspect, the tandem seal adapter 200 may comprise a rib 242 extending radially from the wall 211 of the housing 210. The rib 242 may project from the external surface 227 of the housing 210, between the first end 212 and the second end 214 of the housing 210. According to an aspect the port 216 extends through a portion of the rib 242.



FIG. 4 illustrates the TSA 200 including a tracer material 218. The tracer material 218 is positioned in portion of the port 216. According to an aspect, the tracer material is positioned in the first radial bore 228 of the port 216, such that the tracer material 218 is adjacent the pathway 222. The tracer material 218 may be perpendicular to the pathway 222. According to an aspect, the tracer material 218 may include a solid material secured in the port. The tracer material 218 may be formed from a dissolvable material that, when exposed to wellbore fluids, dissolves and is detectable in the wellbore or formation fluid. When displaced from the port, the tracer material is exposed to the wellbore fluids and may be carried to the surface of the wellbore, via hydrocarbons or the wellbore fluids. According to an aspect, the tracer 218 includes at least one of a dissolvable material. According to an aspect, the tracer 218 includes a small insoluble radioactive plastic sphere, which can be employed to perform a tracer loss measurement in water injector wells. The sphere or a plurality of spheres is designed to have the same density as the injection fluid so that the sphere travels along with the fluid when it is placed into the flow stream of an injection well. Typically, the radioactive beads do not enter the actual formation, but rather remain on the rock face in an open-hole scenario (non-cased) or somewhere within the perforation channel in a cased hole scenario.


According to a further aspect and as illustrated in FIG. 4, a retainer/plug 220 is positioned in the port, adjacent the tracer material 218, thus retaining the tracer material 218 within the port 216. At least a portion of the retainer 220 may be exposed to the wellbore. In an embodiment, the portion of the retainer 220 exposed to the wellbore is configured to withstand the wellbore environment, so that prolonged exposures to the wellbore will not cause wear and tear of the retainer 220. The retainer 220 may be inserted into the port 216 from the external surface 227 of the housing 210. To ensure that no wellbore fluids enters the port 216, one or more sealing members 240 may be secured to the retainer and positioned in the port 216. The sealing members 240 may comprise O-rings or the like.


According to an aspect, the retainer 220 is at least temporarily secured within the port 216. The retainer 220 may be press fit into the port 216. As seen for instance in FIG. 5A and FIG. 5B, the retainer 220 includes a head portion 232 and a body portion 230 extending from the head portion 232. According to an aspect, the head portion 232 has an outer diameter OD1 that is larger than an outer diameter OD2 of the body portion 230. As seen, for instance in at least FIGS. 4 and 6, the body portion 230 may extend, at least partially, into the first radial bore 228 and the head portion 232 may extend within the second radial bore 229 of the port 216. The outer diameter OD1 of the head portion 232 may be selected so that the head portion 232 is too large to be received into the first radial bore 228. This helps to ensure proper assembly of the retainer 220 and may also help to ensure that the tracer material 218 is retained in the port 216.


The retainer 220 may be mechanically fastened in the port 216. According to an aspect and as illustrated in FIG. 5A, the body portion 230 includes one or more protrusions 231 that interact with an inner wall of the first radial bore 228. The protrusions 231 may facilitate the retention of the retainer 220 within the port 216. The protrusions 231 may be deformable so that they bend and flex in order for the body portion 230 to be positioned in the port 216 (FIG. 4 and FIG. 6). Alternatively and as illustrated in FIG. 5B, the body portion 230 includes a thread configured to interact with a threaded inner surface (not shown) of first radial bore 228 of the port 216. The head portion 232 may include a thread to interact with a threaded inner surface (not shown) of the second radial bore 229 of the port 216.


As shown in FIG. 6, an exemplary embodiment of a TSA 200 for a perforating gun assembly may include a housing 210 having a first end 212 adapted to be connected to a first perforating gun 213A and a second end 214 adapted to be connected to a second perforating gun 213B (FIG. 8). The TSA may be configured substantially as described hereinabove with respect to FIGS. 2-4, thus for purposes of convenience and not limitation, all of the various features of the TSA 200 are not repeated hereinbelow.


As illustrated in FIG. 6, the TSA 200 includes a port 216 extending through a wall 211 of the housing 210. The port 216 intersects with a pathway 222 extending from the first end of the housing 212 and in communication with an interior of the first perforating gun 213A. Upon detonation of one or more shaped charges (FIG. 7) secured within the interior of a housing of the perforating gun 213A, pressurized gas from the detonation travels along the pathway 222 towards the tracer material 218. The pressurized gas forces the tracer material 218 and the retainer 220 out of the port 216 and into the wellbore. While the retainer 220 is pressure resistant against pressures towards an interior of the housing 210, and is adapted to maintain a pressure rating of the first perforating gun 213A, the detonation of the shaped charges generates a pressure that is greater than the atmospheric pressure of the perforating gun 213A and that can displace and expel the tracer material 218 and the retainer 220 from the TSA 200. The pressure rating of the perforation gun may me about 20,000 psi, while the wellbore pressure is between about 5,000 psi and about 15,000 psi. Other housings connected with the perforating of the TSA 200, such as a frac plug or bridge plug, are configured to maintain a pressure differential of 10,000 psi. The retainer 220 is geometrically designed so that it only maintains pressure in one direction.


In use, when a perforating gun 213 connected to the TSA 200 is detonated (see, for example, FIG. 7), the interior space 217 of the perforating gun housing is in open communication with the path 222 of the TSA 200. Perforating guns, as understood by one of ordinary skill in the art, typically include a detonator 406 in communication with a detonating cord 404 and an internal gun feedthrough (e.g., an electrical feedthrough or through wire). The detonating cord 404 is connected to one or more shaped charges 402 secured within the interior 217 of a housing of the perforating gun 213. When a shaped charge 402 of a perforating gun 213 connected to the TSA 200 is detonated, a gas pressure is generated by the detonation of the shaped charge 402 of the perforating gun 213. This gas pressure moves into the path 222 and forces the retainer 220 to eject from the port 216 so that the tracer material 218 is exposed to the wellbore environment. The tracer material 218 will also be ejected into the wellbore, without any structural damage to the tracer material 218.


An exemplary embodiment of a method of using a TSA for a perforating gun assembly to disperse tracer material into a wellbore is also provided. FIG. 7 an example perforating gun assembly 300 including the TSA of FIGS. 2-4 and FIG. 6. The perforating gun assembly 300 includes a perforating gun 213A having one or more shaped charges 402 positioned therein. When more than one shaped charge 402 is included, the shaped charges 402 may be ballistically connected by a detonative device. The detonative device may include a booster, initiation pellets or a detonating cord. FIG. 6 illustrates the shaped charges 402 being connected by a detonating cord 404, which is connected to a detonator 406, as is known in the art.


The method includes connecting at least a first perforating gun 213 to a tandem seal adapter 200 (e.g., via a threaded connection 410), providing tracer material 218 in a port 216 which extends through a housing 210 of the tandem seal adapter 200. As described hereinabove, the port 216 extends through a wall 211 of the housing 210 from an exterior of the housing to an interior of the housing 210, and is in communication with an interior 217 of the first perforating gun 213A. A pathway 222 may extends from the first end 212 of the housing to the port 216 for connecting the port 216 to the interior 217 of the first perforating gun 213. The method may further include securing the tracer material 218 within the port 216 with a retainer 220. A shaped charge 402 in the first perforating gun 213A is detonated, which creates a pressure sufficient to displace the retainer 220 and expel the tracer material 218 from the TSA 200. According to an aspect, pressurized gas from the detonation may travel along the pathway 222 to the port 216, out of the port 216 and into the wellbore.


According to a further aspect, the method may further include providing a cavity 224 which extends within the housing 210 between the first end 212 and the second end 214, and pressure sealing the first perforating gun 213A from a second perforating gun 213B. The step of pressure sealing the first and second perforating guns 213A, 213B includes positioning a pressure bulkhead/bulkhead 226 within the cavity 224 of the TSA 200. The bulkhead 226 may include sealing elements, such as o-rings, to help to seal/isolate the components housed in the first perforating gun 213A from components housed in the second perforating gun 213B, as seen for instance in FIG. 8.


The bulkhead 226 may be configured as a rotatable bulkhead assembly. Such bulkhead assemblies are described in U.S. Pat. No. 9,784,549, commonly owned and assigned to DynaEnergetics Europe, which is incorporated herein by reference in its entirety. The bulkhead 226 includes a bulkhead body having a first end and a second end. A first electrically contactable bulkhead component such as a metal contact plug or the elongated pin, extends from the first end of the bulkhead body, and a second electrically contactable bulkhead component, such as a downhole facing pin, extends from the second end of the bulkhead body. One or more sealing elements, such as O-rings, extends around the bulkhead body. The o-ring/(s) may be compressively engage an inner surface of the cavity 224 of the TSA 200 so that a pressure seal is maintained between the first perforating gun 213A and the second perforating gun 213B.


According to an aspect, the bulkhead 226 is configured substantially as described and illustrated in U.S. Application Publication No. 2020/0217,635 published Jul. 9, 2020, which is incorporated herein by reference in its entirety. The bulkhead 226 may be configured as an electrical connector. According to an aspect, the electrical connector includes a connector body and a first electrical contact/pin provided at a first end of the connector body. The first electrical contact may be biased so as to rest at a first rest position if no external force is being applied to the first electrical contact. The first electrical contact may be structured so as to move from the first rest position to a first retracted position in response to an application of external force against the first electrical contact.


The method may also include features and functionality as discussed above in connection with the various embodiments of the TSA 200.


An exemplary embodiment of a tool string 500 may include a plurality of perforating guns 213A, 213B, 213C (collectively 213). As illustrated in FIG. 8, a TSA 200, configured substantially as described hereinabove, may be positioned between each adjacent perforating gun 213. Each perforating gun of the plurality of perforating guns 213 may include one or more shaped charges 402. The TSA 200 includes a housing 210 having a first end 212 adapted to be connected to a first of the connected perforating guns 213B and a second end 214 adapted to be connected to a second of the connected perforating guns 213C. A port 216 extends through a wall of the housing 210 from an exterior of the housing 210 to an interior of the housing 210, and is in communication with an interior 217 of the first of the connected perforating guns 213B. A tracer material 218 is arranged in the port 216, and a retainer 220 secures the tracer material 218 within the port 216. Upon detonation of the one or more shaped charges 402 within the perforating gun 213B (for example), the retainer 220 is displaced and the tracer material 218 is expelled from the port 216.


The tandem seal adapter 200 of the tool string 500 may also include the features and functionality as discussed above in connection with the various embodiments of the TSA 200 and method described hereinabove.


In embodiments which include a tool string 500 that includes multiple perforating guns connected to each other by TSAs 200, each TSA 200 may include a different type of tracer material in order to provide an indication as to which perforating zone was activated in the wellbore.


This disclosure, in various embodiments, configurations and aspects, includes components, methods, processes, systems, and/or apparatuses as depicted and described herein, including various embodiments, sub-combinations, and subsets thereof. This disclosure contemplates, in various embodiments, configurations and aspects, the actual or optional use or inclusion of, e.g., components or processes as may be well-known or understood in the art and consistent with this disclosure though not depicted and/or described herein.


The phrases “at least one”, “one or more”, and “and/or” are open-ended expressions that are both conjunctive and disjunctive in operation. For example, each of the expressions “at least one of A, B and C”, “at least one of A, B, or C”, “one or more of A, B, and C”, “one or more of A, B, or C” and “A, B, and/or C” means A alone, B alone, C alone, A and B together, A and C together, B and C together, or A, B and C together.


In this specification and the claims that follow, reference will be made to a number of terms that have the following meanings. The terms “a” (or “an”) and “the” refer to one or more of that entity, thereby including plural referents unless the context clearly dictates otherwise. As such, the terms “a” (or “an”), “one or more” and “at least one” can be used interchangeably herein. Furthermore, references to “one embodiment”, “some embodiments”, “an embodiment” and the like are not intended to be interpreted as excluding the existence of additional embodiments that also incorporate the recited features. Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term such as “about” is not to be limited to the precise value specified. In some instances, the approximating language may correspond to the precision of an instrument for measuring the value. Terms such as “first,” “second,” “upper,” “lower” etc. are used to identify one element from another, and unless otherwise specified are not meant to refer to a particular order or number of elements.


As used herein, the terms “may” and “may be” indicate a possibility of an occurrence within a set of circumstances; a possession of a specified property, characteristic or function; and/or qualify another verb by expressing one or more of an ability, capability, or possibility associated with the qualified verb. Accordingly, usage of “may” and “may be” indicates that a modified term is apparently appropriate, capable, or suitable for an indicated capacity, function, or usage, while taking into account that in some circumstances the modified term may sometimes not be appropriate, capable, or suitable. For example, in some circumstances an event or capacity can be expected, while in other circumstances the event or capacity cannot occur—this distinction is captured by the terms “may” and “may be.”


As used in the claims, the word “comprises” and its grammatical variants logically also subtend and include phrases of varying and differing extent such as for example, but not limited thereto, “consisting essentially of” and “consisting of.” Where necessary, ranges have been supplied, and those ranges are inclusive of all sub-ranges therebetween. It is to be expected that the appended claims should cover variations in the ranges except where this disclosure makes clear the use of a particular range in certain embodiments.


The terms “determine”, “calculate” and “compute,” and variations thereof, as used herein, are used interchangeably and include any type of methodology, process, mathematical operation or technique.


This disclosure is presented for purposes of illustration and description. This disclosure is not limited to the form or forms disclosed herein. In the Detailed Description of this disclosure, for example, various features of some exemplary embodiments are grouped together to representatively describe those and other contemplated embodiments, configurations, and aspects, to the extent that including in this disclosure a description of every potential embodiment, variant, and combination of features is not feasible. Thus, the features of the disclosed embodiments, configurations, and aspects may be combined in alternate embodiments, configurations, and aspects not expressly discussed above. For example, the features recited in the following claims lie in less than all features of a single disclosed embodiment, configuration, or aspect. Thus, the following claims are hereby incorporated into this Detailed Description, with each claim standing on its own as a separate embodiment of this disclosure.


Advances in science and technology may provide variations that are not necessarily express in the terminology of this disclosure although the claims would not necessarily exclude these variations.

Claims
  • 1. A tandem seal adapter comprising: a housing having a first end adapted to be connected to a first perforating gun and a second end adapted to be connected to a second perforating gun;a port extending through a wall of the housing from an exterior of the housing to an interior of the housing, wherein the port is configured to be in communication with an interior of the first perforating gun;a tracer material positioned in the port; anda retainer positioned in the port, adjacent the tracer material,wherein, upon detonation of the first perforating gun, the retainer is displaced and the tracer material is expelled from the port by gas pressure produced by the detonation.
  • 2. The tandem seal adapter of claim 1, further comprising: a pathway extending from the first end of the housing to the port, the pathway being in communication with the interior of the first perforating gun,wherein pressurized gas from the detonation travels along the pathway to the tracer material upon detonation of the first perforating gun.
  • 3. The tandem seal adapter of claim 2, further comprising: a cavity extending along a longitudinal axis of the housing, between the first end and the second end; anda bulkhead arranged in the cavity for pressure sealing the first perforating gun from the second perforating gun,wherein the pathway is parallel to and spaced apart from the cavity.
  • 4. The tandem seal adapter of claim 3, wherein the port extends in a radial direction from the pathway.
  • 5. The tandem seal adapter of claim 1, wherein the retainer comprises a plug inserted into the port from the exterior of the housing.
  • 6. The tandem seal adapter of claim 5, wherein the plug is press fit into the port.
  • 7. The tandem seal adapter claim 5, wherein: the port comprises a first radial bore which extends into the interior of the housing and which is partially fillable with the tracer material and a second radial bore which is larger than the first radial bore and which extends from the first radial bore towards the exterior of the housing; andthe plug comprises a body portion and a head portion, wherein the head portion has an outer diameter that is larger than an outer diameter of the body portion, and the body portion extends partially into the first radial bore and the head portion is positioned within the second radial bore.
  • 8. The tandem seal adapter of claim 7, wherein the body portion comprises one or more protrusions in engagement with an inner wall of the first radial bore.
  • 9. The tandem seal adapter of claim 7, further comprising: one or more sealing members secured to the body portion, where the one or more sealing members are configured for prevent wellbore fluids from entering the first radial bore.
  • 10. The tandem seal adapter of claim 1, further comprising: a rib extending radially from the wall of the housing, between the first end and the second end,wherein the port extends through a portion of the rib.
  • 11. The tandem seal adapter of claim 1, wherein the retainer is pressure resistant against pressures in a wellbore towards an interior of the housing and adapted to maintain a pressure rating of the first perforating gun.
  • 12. A method of using a tandem seal adapter for a perforating gun assembly to disperse tracer material into a wellbore, the method comprising: connecting at least a first perforating gun to a tandem seal adapter, wherein the tandem seal adapter comprises a first housing end,a second housing end,a port extending through a wall of the housing from an exterior of the housing to an interior of the housing,a tracer material positioned in the port, anda retainer positioned in the port, adjacent the tracer material;detonating a shaped charge positioned in the first perforating gun to create a detonating pressure; andusing the detonating pressure, displacing the retainer and expel the tracer material out of the port and into the wellbore.
  • 13. The method of claim 12, further comprising: providing a pathway extending from the first end of the housing to the port for connecting the port to the interior of the first perforating gun,wherein pressurized gas from the detonation travels along the pathway upon detonation of the first perforating gun.
  • 14. The method of claim 13, further comprising: providing a cavity which extends within the housing between the first end and the second end; andpressure sealing the first perforating gun from the second perforating gun via a bulkhead arranged in the cavity,wherein the pathway extends parallel to and spaced apart from the cavity.
  • 15. The method of claim 14, wherein the cavity extends along the longitudinal axis of the housing, andthe port extends in a radial direction from the pathway.
  • 16. The method of claim 12, wherein the retainer is press fit into the port.
  • 17. A tool string, comprising: a plurality of connected perforating guns, each of the connected perforating guns comprising at least one explosive charge;a tandem seal adapter connected between every two connected perforating guns of the plurality of connected perforating guns, wherein the tandem seal adapter comprises: a housing having a first end adapted to be connected to a first connected perforating gun of the plurality of connected perforating guns and a second end adapted to be connected to a second connected perforating gun of the plurality of connected perforating guns;a port extending through a wall of the housing from an exterior of the housing to an interior of the housing in communication with an interior of the first connected perforating gun of the plurality of connected perforating guns;a tracer material arranged in the port;a retainer for securing the tracer material in the port;wherein the retainer is displaced and the tracer material is expelled from the port upon detonation of the first connected perforating gun by gas pressure produced by the detonation.
  • 18. The tool string of claim 17, further comprising: a pathway extending from the first end of the housing to the port for connecting the port to the interior of the first connected perforating gun,wherein pressurized gas from the detonation travels along the pathway upon detonation of the first connected perforating gun.
  • 19. The tool string of claim 17, wherein the retainer comprises a plug inserted into the port from the exterior of the housing.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a national stage application of and claims priority to Patent Cooperation Treaty (PCT) Application No. PCT/EP2021/056507 filed Mar. 15, 2021, which claims the benefit of U.S. Provisional Application No. 62/990,165 filed on Mar. 16, 2020, each of which is incorporated herein and made a part hereof by reference for all purposes.

PCT Information
Filing Document Filing Date Country Kind
PCT/EP2021/056507 3/15/2021 WO
Publishing Document Publishing Date Country Kind
WO2021/185749 9/23/2021 WO A
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Related Publications (1)
Number Date Country
20230115055 A1 Apr 2023 US
Provisional Applications (1)
Number Date Country
62990165 Mar 2020 US