Perforating gun assembly having seal element of tandem seal adapter and coupling of housing intersecting with a common plane perpendicular to longitudinal axis

Information

  • Patent Grant
  • 11788389
  • Patent Number
    11,788,389
  • Date Filed
    Friday, April 2, 2021
    3 years ago
  • Date Issued
    Tuesday, October 17, 2023
    a year ago
Abstract
A perforating gun assembly may include a first housing extending along a longitudinal axis and a tandem seal adapter (TSA). The first housing may include a coupling provided at a first end of the first housing. The TSA may include a TSA body and a seal element provided on an outer surface of the TSA body. At least part of the TSA may be positioned inside the first housing such that the seal element and the coupling intersect with a common plane that is perpendicular to the longitudinal axis.
Description
FIELD

A perforation gun system is generally described. More particularly, various perforation gun components that can be modularly assembled into a perforation gun system, the assembled perforated gun system itself, a perforation gun system kit, and a method for assembling a perforation gun system are generally described.


BACKGROUND

Perforation gun systems are used in well bore perforating in the oil and natural gas industries to tie a bore hole with a storage horizon within which a storage reservoir of oil or natural gas is located.


A typical perforation gun system consists of an outer gun carrier, arranged in the interior of which there are perforators-usually hollow or projectile charges—that shoot radially outwards through the gun carrier after detonation. Penetration holes remain in the gun carrier after the shot.


In order to initiate the perforators, there is a detonating cord leading through the gun carrier that is coupled to a detonator.


Different perforating scenarios often require different phasing and density of charges or gun lengths. Moreover, it is sometimes desirable that the perforators shooting radially outwards from the gun carrier be oriented in different directions along the length of the barrel. Therefore, phasing may be required between different guns along the length.


Onsite assembly of perforation gun systems may also be problematic under certain conditions as there are certain safety hazards inherent to the assembly of perforation guns due to the explosive nature of certain of its sub-components, including the detonator and the detonating cord.


There is thus a need for a perforation gun system, which by virtue of its design and components would be able to address at least one of the above-mentioned needs or overcome or at least minimize at least one of the above-mentioned drawbacks.


SUMMARY

An exemplary embodiment of a perforating gun assembly may include a first housing extending along a longitudinal axis and a tandem seal adapter (TSA). The first housing may include a coupling provided at a first end of the first housing. The TSA may include a TSA body and a seal element provided on an outer surface of the TSA body. At least part of the TSA may be positioned inside the first housing such that the seal element and the coupling intersect with a common plane that is perpendicular to the longitudinal axis.


An exemplary embodiment of a perforating gun assembly may include a first housing extending in an axial direction and a tandem seal adapter (TSA). The first housing may include a coupling provided at a first end of the first housing. The TSA may include a TSA body and a seal element provided on an outer surface of the TSA body. At least part of the TSA may be inserted into the first end of the first housing such that a position of the seal element in the axial direction overlaps with a position of the coupling in the axial direction.


A wellbore tool string may include a first perforating gun, a second perforating gun, and a tandem seal adapter (TSA). The first perforating gun may include a first housing extending along a longitudinal axis. The second perforating gun may include a second housing extending along the longitudinal axis. The TSA may include a TSA body and a seal element provided on an outer surface of the TSA body. The first perforating gun and the second perforating gun may be coupled to each other at a coupling region. The TSA may be positioned inside the first housing and inside the second housing such that the seal element and the coupling region intersect with a common plane that is perpendicular to the longitudinal axis.





BRIEF DESCRIPTION OF THE DRAWINGS

These and other objects and advantages will become apparent upon reading the detailed description and upon referring to specific embodiments thereof that are illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments and are not therefore to be considered to be limiting of its scope, 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 side cut view of a perforation gun system according to an embodiment;



FIG. 2 is a side view of a top connector, bottom connector and stackable charge holders of a perforation gun system in accordance with another embodiment;



FIG. 3 is a side view of a top connector, bottom connector and stackable charge holders of a perforation gun system in accordance with another embodiment;



FIG. 4 is a front perspective view of a bottom connector in accordance with an embodiment;



FIG. 5 is a rear perspective view of the bottom connector shown in FIG. 4;



FIG. 6 is a front view of a stackable charge holder in accordance with an embodiment;



FIG. 7 is a front perspective view of the stackable charge holder shown in FIG. 6;



FIG. 8 is a rear perspective view of the stackable charge holder shown in FIG. 6;



FIG. 9 is a bottom view of the stackable charge holder shown in FIG. 6;



FIG. 10 is a top view of the stackable charge holder shown in FIG. 6;



FIG. 11 is a bottom view of a half-portion of a top connector in accordance with an embodiment;



FIG. 12 is a side view of the half-portion of the top connector shown in FIG. 11;



FIG. 13 is a top perspective view of the half-portion of the top connector shown in FIG. 11;



FIG. 14 is a bottom perspective view of the half-portion of the top connector shown in FIG. 11;



FIG. 15 is a perspective view of a top connector in accordance with an embodiment;



FIG. 16 is a front end view of the top connector shown in FIG. 15;



FIG. 17 is a rear end view of the top connector shown in FIG. 15;



FIG. 18 is a rear perspective view of the top connector shown in FIG. 15;



FIG. 19 is an enlarged detailed side cut view of a portion of the perforation gun system including a bulkhead and stackable charge holders shown in FIG. 1;



FIG. 20 is a perspective view of a bottom sub of a gun system in accordance with an embodiment;



FIG. 21 is a side view of a gun carrier of a gun system in accordance with an embodiment;



FIG. 22 is a side cut view of the gun carrier shown in FIG. 21;



FIG. 23 is a side view of a top sub of a gun system in accordance with an embodiment;



FIG. 24 is a side cut view of the top sub shown in FIG. 23;



FIG. 25 is a side view of a tandem seal adapter of a gun system in accordance with an embodiment;



FIG. 26 is a perspective view of the tandem seal adapter shown in FIG. 25;



FIG. 27 is a perspective view of a detonator in accordance with an embodiment;



FIG. 28 is a detailed perspective view of the detonator shown in FIG. 27;



FIG. 29 is another detailed perspective view of the detonator shown in FIG. 27;



FIG. 30 is another detailed perspective view of the detonator shown in FIG. 27;



FIG. 31 is another detailed perspective view of the detonator shown in FIG. 27, with a crimp sleeve;



FIG. 32 is a detailed side view of a tandem seal adapter and detonator in accordance with another embodiment;



FIG. 33 is a side cut view of a portion of a perforation gun system illustrating the configuration of the top sub in accordance with another embodiment;



FIG. 34 is a side cut view of a portion of a perforation gun system illustrating the configuration of the bottom sub in accordance with another embodiment; and



FIGS. 35A and 35B are electrical schematic views of a detonator and of wiring within a perforated gun system in accordance with another embodiment.





DETAILED DESCRIPTION

In the following description and accompanying FIGS., the same numerical references refer to similar elements throughout the FIGS. and text. Furthermore, for the sake of simplicity and clarity, namely so as not to unduly burden the FIGS. with several reference numbers, only certain FIGS. have been provided with reference numbers, and components and features of the embodiments illustrated in other FIGS. can be easily inferred therefrom. The embodiments, geometrical configurations, and/or dimensions shown in the FIGS. are for exemplification purposes only. Various features, aspects and advantages of the embodiments will become more apparent from the following detailed description.


Moreover, although some of the embodiments were primarily designed for well bore perforating, for example, they may also be used in other perforating scenarios or in other fields, as apparent to a person skilled in the art. For this reason, expressions such as “gun system”, etc., as used herein should not be taken as to be limiting, and includes all other kinds of materials, objects and/or purposes with which the various embodiments could be used and may be useful. Each example or embodiment are provided by way of explanation, and is not meant as a limitation and does not constitute a definition of all possible embodiments.


In addition, although some of the embodiments are illustrated in the accompanying drawings comprise various components and although the embodiment of the adjustment system as shown consists of certain geometrical configurations as explained and illustrated herein, not all of these components and geometries are essential and thus should not be taken in their restrictive sense, i.e. should not be taken as to limit the scope. It is to be understood, as also apparent to a person skilled in the art, that other suitable components and cooperations thereinbetween, as well as other suitable geometrical configurations may be used for the adjustment systems, and corresponding parts, according to various embodiments, as briefly explained and as can easily be inferred herefrom by a person skilled in the art, without departing from the scope.


Referring to FIGS. 1 to 3, an object is to provide a perforation gun system 10 having an outer gun carrier 12. The gun system 10 includes a top connector 14. At least one stackable charge holder 16 is provided for centralizing a single shaped charge 18 within the gun carrier 12. A detonation cord 20 is connected to the top connector 14 and to each stackable charge holder 16.


The gun system 10 includes at least one bottom connector 22 for terminating the detonation cord 20 in the gun system. As better shown in FIG. 2, it is also possible that the bottom connector 22 double as or serve the function of a spacer 24 for spacing a plurality of stackable charge holders 16.


In an embodiment, the gun system also includes a detonator 26 energetically coupled to the detonation cord 20.


As better shown in FIGS. 4 to 18, each of the top connector 14, stackable charge holder 16 and bottom connector 22 includes a rotation coupling 30 for providing a selectable clocking rotation between each of the above-mentioned components. As seen, for instance, in FIGS. 4-5 and 7-9, the rotation coupling 30 includes a first rotation coupling 30a and a second rotation coupling 30b.


Hence, a user can build multiple configurations of gun systems using various combinations of basic components. A first of these basic components includes a top connector. Another basic component is a single charge holder that centralizes a single shaped charge. The holder is adapted to be stacked and configured into 0, 30, 60, up to 360 degrees or any other combination of these phases for any specified length. Another basic component is a bottom connector that terminates the detonation cord in the gun. The bottom connector may carry as well an electrical connection therethrough. The bottom connector may also double as an imperial measurement stackable spacer to provide any gun shot density up to, for example, 6 shots per foot. Alternately, another bottom connector may be provided or configured to double as a metric measurement stackable spacer to provide any gun shot density up to, for example, 20 shots per meter. Another basic component includes a push-in detonator that does not use wires to make necessary connections. The push-in detonator may uses spring-loaded connectors, thus replacing any required wires and crimping.


Therefore, within the self-centralizing charge holder system, any number of spacers can be used with any number of holders for any specific metric or imperial shot density, phase and length gun system.


In an embodiment, only two pipe wrenches are required for assembly on site of the gun system, as no other tools are required.


In an embodiment, the top connector 14 provides energetic coupling between the detonator and detonating cord.


In an embodiment, each of the top connector 14, stackable charge holder 16 and bottom connector 22 are configured to receive electrical connections therethrough.


In an embodiment, all connections are made by connectors, such as spring-loaded connectors, instead of wires, with the exception of the through wire that goes from the top connector 14 to the bottom connector 22, whose ends are connectors.


In an embodiment, components of the assembly may include molded parts, which may also be manufactured to house the wiring integrally, through, for instance, overmolding, to encase the wiring and all connectors within an injection molded part. For example, the charge holder 16 could be overmolded to include the through wire.


In an embodiment, and as shown in FIGS. 4 and 5, each bottom connector 22 includes a cylindrical body 220 comprising a first base 222 and a second base 224. The pins 50 outwardly extend from the first base 222, and the sockets 52 at least partially extend into the second base 224. As illustrated in FIGS. 4 and 5, each socket 52 is spaced apart from an adjacent socket and each pin 50 is spaced apart from an adjacent pin. The cylindrical body 220 may include a plurality of alternating v-shaped channels 221 and v-shaped walls 223. The v-shaped channels partially extend from the first base 222 towards the second base 224, and the v-shaped walls 223 extend from the second base 224 to the first base 222. At least one of the pins 50 of the rotation coupling 30 extend from one of the v-shaped walls 223. According to an aspect, when the bottom connector includes the first rotation coupling 30a and the second rotation coupling 30b, the cylindrical body 220 extends therebetween. The bottom connector 22 includes a plurality of fins/wings 32 radially extending from the body 220. The wings 32 are configured for axially locking each bottom connector against a snap ring 54, or an equivalent retainment mechanism to keep the charge holder 16 from sliding out of the bottom of carrier 12 as it is handled, (shown on FIG. 1). According to an aspect, and as illustrated in FIG. 19, the bottom connector 22 may be recessed into a recess 49 formed in the tandem seal adapter 48. The bottom connector 22 from a first gun assembly can accommodate or house an electrical connection through a bulkhead assembly 58 to the top connector 14 of a second or subsequent gun assembly, as seen for instance in FIG. 19. The top and bottom connector, as well as the spacer, in an embodiment, are made of 15% glass fiber reinforced, injection molding PA6 grade material, commercially available from BASF under its ULTRAMID® brand, and can provide a positive snap connection for any configuration or reconfiguration. As better shown in FIG. 5, a terminating means structure 34 is provided to facilitate terminating of the detonation cord. The structure 34 may be formed in the first base 222. The snap ring 54 is preinstalled on the bottom of the carrier 12. The assembly can thus shoulder up to the snap ring 54 via the bottom connector fins 32.


In an embodiment and as shown in FIGS. 6 to 10, each stackable charge holder 16 includes a charge receiving structure for receiving a single shaped charge, and a plurality of projections 40 extending from the charge receiving structure. The projections 40 may rest against an inner surface 13 or diameter of the gun carrier 12 (as shown in FIG. 1) and thereby centralizing the shaped charge therewithin. The charge receiving structure may include a pair of arms 44, and each projection 40 may extend from at least one of the arms 44. A pair 42 of the plurality of projections 40 may also be configured for capturing the detonation cord (not shown) traversing each stackable charge holder 16. The pair 42 of the plurality of projections are also used for centralizing the shaped charge within an inner surface of the gun carrier. According to an aspect, the stackable charge holder 15 includes a first base 222 and a second base 224 spaced apart from the first base 222. The arms 44 extend between the first and second bases 222, 224. According to an aspect, the pins 50 outwardly extend from the first base 222, and the sockets 52 at least partially extend into the second base 224. Each pin is spaced apart from an adjacent pin, and each socket 52 is spaced apart from an adjacent socket.


In an embodiment, as shown in FIGS. 11 to 18, the top connector 14 includes a first end 242, a second end 244, and a coupler 246 formed at the first end 242. The top connector 14 may be configured for providing energetic coupling between the detonator 26 and a detonation cord. According to an aspect and as illustrated in FIGS. 11 and 14, an elongated opening 247 extends from the second end 244, adjacent the coupler 246, towards the first end 242. The elongated opening 247 is flanked by side walls 248 that provide the energetic coupling between the detonator 26 and the detonation cord 20. A rotation coupling 30 is formed at the second end 244. The rotation coupling includes at least one of a plurality of pins 50 and a plurality of sockets 52. According to an aspect, the top connector 14 includes at least one directional locking fin 46. Although the use of directional locking fins is described, other methods of directional locking may be used, in order to eliminate a top snap ring that would otherwise be used to lock the assembly. As better shown in FIG. 19, the locking fins 46 are engageable with corresponding complementarily-shaped structures 47 housed within the carrier 12, upon a rotation of the top connector 14, to lock the position of the top connector along the length of the carrier 12.


In an embodiment, as better shown in FIG. 19, the bottom connector 22 on one end and the top connector 14 on the other end abuts/connects to the bulkhead assembly 58. The tandem seal adapter 48 is configured to seal the inner components within the carrier 12 from the outside environment, using sealing means 60 (shown herein as o-rings). Thus, the tandem seal adapter 48 seals the gun assemblies from each other along with the bulkhead 58, and transmits a ground wire to the carrier 12. Hence, the top connector 14 and bulkhead 58 accommodate electrical and ballistic transfer to the charges of the next gun assembly for as many gun assembly units as required, each gun assembly unit having all the components of a gun assembly.


In an embodiment, the tandem seal adapter 48 is a two-part tandem seal adapter (not shown) that fully contains the bulkhead assembly 58 (comprised of multiple small parts as shown, for instance, in FIG. 19) and that is reversible such that it has no direction of installation.


In an embodiment and as better shown in FIGS. 27-31 and 35A, the detonator assembly 26 includes a detonator head 100, a detonator body 102 and a plurality of detonator wires 104, including a through wire 106, a signal-in wire 108 and a ground wire 110. The through wire 106 traverses from the top to the bottom of the perforating gun system 10, making a connection at each charge holder 16. The detonator head 100 further includes a through wire connector element 112 connected to the through wire 106 (not shown), a ground contact element 114 for connecting the ground wire 110 to the tandem seal adapter (also not shown), through ground springs 116, and a bulkhead connector element 118 for connecting the signal-in wire 108 to the bulkhead assembly 58 (also not shown). Different insulating elements 120A, 120B are also provided in the detonator head 100 for the purpose of insulating the detonator head 100 and detonator wires 104 from surrounding components. As better shown in FIG. 31, a crimp sleeve 122 can be provided to cover the detonator head 100 and body 102, thus resulting in a more robust assembly. The above configuration allows the detonator to be installed with minimal tooling and wire connections.


In an embodiment as shown in FIGS. 32, 33 and 35B illustrate a connection of the above-described detonator assembly 26 to the tandem seal adapter 48 and a pressure bulkhead 124. The bulkhead 124 includes spring connector end interfaces comprising contact pins 126A, 126B, linked to coil springs 128A, 128B. This dual spring pin connector assembly including the bulkhead 124 and coil springs 128A, 128B is positioned within the tandem seal adapter 48 extending from a conductor slug 130 to the bulkhead connector element. The dual spring pin connector assembly is connected to the through wire 106 of the detonator assembly 26.


In an embodiment and as better shown in FIGS. 11 to 18, the top connector 14 may have a split design to simplify manufacturing and aid in assembly. By “split design” what is meant is that the top connector 14 can be formed of two halves—a top half 15A and a bottom half 15B. A plurality of securing mechanisms 241 may be provided to couple the top half 15A to the bottom half 15B. As better shown in FIG. 15 or 18, the top connector 14 may also include a blind hole 45 to contain or house the detonation cord, thus eliminating the need for crimping the detonation cord during assembly.


In an embodiment and as shown for example in FIGS. 4 to 18, the rotation coupling 30 may either include a plurality of pins 50 (FIG. 5) symmetrically arranged about a central axis of the rotation coupling 30, or a plurality of sockets 52 (FIG. 4) symmetrically arranged about the central axis of the rotation coupling 30 and configured to engage the plurality of pins 50 of an adjacent rotation coupling 30. The pins each include a first end 51a, and a second end 51b opposite the first end 51a. According to an aspect, the second end 51b is wider than the first end 51a.


In another embodiment, the rotation coupling 30 may either include a polygon-shaped protrusion, or a polygon-shaped recess configured to engage the polygon-shaped protrusion of an adjacent rotation coupling. The polygon can be 12-sided for example for 30 degree increments.


In another embodiment, the top and bottom subs work with off the shelf running/setting tools as would be understood by one of ordinary skill in the art.


In one embodiment and as shown in FIG. 33, the top sub 72 facilitates use of an off the shelf quick change assembly 140 to enable electrical signals from the surface, as well as to adapt perforating gun system to mechanically run with conventional downhole equipment. The quick change assembly 140 may include a threaded adapter 143 to set an offset distance between an electrical connector 142 and the contact pin 126B extending from the bulkhead assembly 58. In one embodiment and as shown in FIG. 34, the bottom sub 70 may be configured as a sealing plug shoot adapter (SPSA) to be used specifically with this embodiment. The SPSA may receive an off the shelf quick change assembly 140 (not shown) and insulator 150 that communicates with a firing head threaded below it (not shown). A setting tool (not shown) may run on the bottom side of the perforating gun.


In an embodiment, final assembly of the tool string requires only two pipe wrenches. No tools are required to install the detonator or any electrical connections.


An object is to also provide a perforation gun system kit having the basic component parts described above and capable of being assembled within an outer gun carrier.


In an embodiment, a method for assembling a perforation gun system is provided, to which a certain number of optional steps may be provided. The steps for assembling the gun system for transport include the steps of:


providing a perforation gun system kit having component parts capable of being assembled within an outer gun carrier (element 12 in FIGS. 1, 21 and 22), the kit comprising a combination of:

    • a top connector;
    • at least one stackable charge holder for centralizing a single shaped charge within the gun carrier;
    • a detonation cord connectable to the top connector and to each stackable charge holder;
    • at least one bottom connector adapted for terminating the detonation cord in the gun system and adapted for doubling as a spacer for spacing a plurality of stackable charge holders; and
    • a detonator energetically couplable to the detonation cord,


wherein each of the top connector, at least one stackable charge holder and at least one bottom connector comprise a coupling having a plurality of rotational degrees of freedom for providing a selectable rotation between each of the top connector, at least one stackable charge holder and at least one bottom connector;


assembling a plurality of the stackable charge holders in a predetermined phase to form a first gun assembly;


running the detonation cord into a bottommost bottom connector;


assembling the bottommost bottom connector onto the assembled plurality of stackable charge holders;


running a through wire between the bottommost bottom connector and the top connector, so that the through wire goes from the top connector to the bottom connector;


clicking the detonation cord into recesses formed in capturing projections, the capturing projections being provided in each of the charge holders;


running the detonation cord into the top connector;


cutting the detonating cord, if the detonating cord is not precut a predetermined length; and


installing charges into each of the charge holders.


In an embodiment, the method further includes, prior to transport, the steps of:


pushing assembled components together to engage all pin connections therebetween; and


carrying out a continuity test to ensure complete connectivity of the detonating chord.


In an embodiment, on location, to complete the assembly, the method further comprises the steps of


threading on the previously assembled components a bottom sub (element 70 on FIGS. 1 and 20);


installing and connecting the detonator;


pushing in a tandem seal adapter with o-rings onto the first gun assembly;


pushing in a bulkhead (element 58 in FIG. 19) onto the tandem seal adapter, if the bulkhead and the tandem seal adapter are not pre-assembled;


threading a subsequent gun assembly onto the first gun assembly or threading a top sub (element 72 in FIGS. 1, 23 and 24) onto a topmost assembled gun assembly, for connection to a quick change assembly.


Of course, the scope of the perforation gun system, various perforation gun components, the perforation gun system kit, and the method for assembling a perforation gun system should not be limited by the various embodiments set forth herein, but should be given the broadest interpretation consistent with the description as a whole. The components and methods described and illustrated are not limited to the specific embodiments described herein, but rather, features illustrated or described as part of one embodiment can be used on or in conjunction with other embodiments to yield yet a further embodiment. Further, steps described in the method may be utilized independently and separately from other steps described herein. Numerous modifications and variations could be made to the above-described embodiments without departing from the scope of the FIGS. and claims, as apparent to a person skilled in the art.


In this specification and the claims that follow, reference will be made to a number of terms that have the following meanings. The singular forms “a,” “an” and “the” include plural referents unless the context clearly dictates otherwise. Further, reference to “top,” “bottom,” “front,” “rear,” and the like are made merely to differentiate parts and are not necessarily determinative of direction. Similarly, terms such as “first,” “second,” 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.”


Advances in science and technology may make equivalents and substitutions possible that are not now contemplated by reason of the imprecision of language; these variations should be covered by the appended claims. This written description uses examples to disclose the perforation gun system, various perforation gun components, the perforation gun system kit, and the method for assembling a perforation gun system, including the best mode, and also to enable any person of ordinary skill in the art to practice same, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the perforation gun system, various perforation gun components, the perforation gun system kit, and the method for assembling a perforation gun system is defined by the claims, and may include other examples that occur to those of ordinary skill in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.

Claims
  • 1. A wellbore tool string comprising: a first perforating gun having a first gun carrier extending along a longitudinal axis;a first shaped charge carrier provided within the first gun carrier, the first shaped charge carrier configured for receiving a first shaped charge;a second perforating gun having a second gun carrier extending along the longitudinal axis;a second shaped charge carrier provided within the second gun carrier, the second shaped charge carrier configured for receiving a second charge;a tandem seal adapter (TSA) in sealing engagement with the first gun carrier, the TSA comprising: a TSA body and a first seal element provided on an outer surface of the TSA body;a bore extending through the TSA body; anda bulkhead provided within the bore and configured to provide electrical connectivity through the bore, the bulkhead comprising: an outer body provided within the bore and having a bulkhead surface perpendicular to the longitudinal axis in contact with the TSA, wherein the outer body is non-conductive; andan electrical contact assembly extending through the outer body, the electrical contact assembly comprising a first electrical contact provided at a first end of the outer body; wherein:the first perforating gun and the second perforating gun are coupled to each other at a coupling region;the first gun carrier comprises first threads formed on the first gun carrier at a first end of the first gun carrier;the second gun carrier comprises second threads formed on the second gun carrier at a first end of the second gun carrier;the first threads are engaged with the second threads in the coupling region; andthe TSA is positioned inside the first gun carrier and inside the second gun carrier such that the first seal element, the first threads, and the second threads intersect with a common plane that is perpendicular to the longitudinal axis.
  • 2. The wellbore tool string of claim 1, wherein the electrical contact assembly further comprises: a second electrical contact provided at a second end of the outer body;wherein the first electrical contact is in electrical communication with the second electrical contact.
  • 3. The wellbore tool string of claim 2, further comprising: a first gun electrical contact provided within the first gun carrier; anda second gun electrical contact provided within the second gun carrier; whereinthe first electrical contact is configured to make wireless electrical contact with the first gun electrical contact; andthe second electrical contact is configured to make wireless electrical contact with the second gun electrical contact.
  • 4. The wellbore tool string of claim 2, wherein the second electrical contact is coaxial with the first electrical contact, the bore, and the TSA body.
  • 5. The wellbore tool string of claim 1, wherein: the first gun carrier contacts a first surface of the TSA body; andthe first end of the second gun carrier contacts a second surface of the TSA body.
  • 6. The wellbore tool string of claim 1, wherein: a TSA maximum outer diameter of the TSA is smaller than a first gun carrier maximum outer diameter of the first gun carrier; andthe TSA maximum outer diameter is smaller than a second gun carrier maximum outer diameter of the second gun carrier.
  • 7. The wellbore tool string of claim 1, wherein: the first seal element is provided to a first side in an axial direction relative to a TSA maximum outer diameter region; anda second seal element is provided on the outer surface of the TSA body to a second side in the axial direction relative to the TSA maximum outer diameter region opposite the first side.
  • 8. The wellbore tool string of claim 1, further comprising a conductive contact provided within the first gun carrier; wherein a surface of the electrical contact assembly that is non-parallel to the longitudinal axis is in wireless electrical contact with the conductive contact.
  • 9. The wellbore tool string of claim 1, wherein the TSA body is formed of a singular, monolithic piece of material.
  • 10. The wellbore tool string of claim 1, wherein the tandem seal adapter is in sealing engagement with the second gun carrier.
  • 11. The wellbore tool string of claim 1, wherein the TSA comprises: a TSA maximum radius portion; whereina portion of the first carrier abuts the TSA maximum radius portion; anda portion of the second carrier abuts the TSA maximum radius portion.
  • 12. The wellbore tool string of claim 1, wherein the TSA comprises: a first TSA region having a first TSA outer diameter;a second TSA region having a second TSA outer diameter, the second TSA outer diameter being larger than the first TSA outer diameter;a third TSA region having a third TSA outer diameter, the third TSA outer diameter being smaller than the second TSA outer diameter;a first shoulder surface extending from an outer surface of the first TSA region to an outer surface of the second TSA region; anda second shoulder surface extending from an outer surface of the third TSA region to the outer surface of the second TSA region; whereinthe second TSA region is disposed between the first TSA region and the third TSA region in the axial direction;a portion of the first carrier abuts the first shoulder surface; anda portion of the second carrier abuts the second shoulder surface.
  • 13. The wellbore a portion of the bore overlapping in the axial direction with an entirety of the TSA body having an outer diameter equal to a maximum outer diameter of the TSA body has a constant bore diameter.
  • 14. The wellbore tool string of claim 1, wherein an axial position of a portion of a maximum outer diameter region of the TSA body overlaps with the bulkhead in an axial direction.
  • 15. The wellbore tool string of claim 1, wherein a line from any point within the bore to any point radially outward from the TSA body overlapping in the axial direction with the TSA body intersects the TSA body.
  • 16. The wellbore tool string of claim 1, further comprising a sealing contact between the bulkhead and the TSA body.
  • 17. The wellbore tool string of claim 1, further comprising a first detonator provided within the first gun carrier, wherein the first detonator is in electrical communication with the electrical contact assembly.
  • 18. The wellbore tool string of claim 17, wherein the first detonator is in wireless electrical contact with the electrical contact assembly.
  • 19. The wellbore tool string of claim 1, further comprising: a first top connector provided within the first gun carrier;a first bottom connector provided within the second gun carrier;a second top connector provided within the second gun carrier;a second bottom connector provided within the second gun carrier;wherein the TSA is positioned between the first top connector and the second bottom connector.
  • 20. The wellbore tool string of claim 1, wherein the electrical contact assembly is spring-loaded.
Priority Claims (1)
Number Date Country Kind
2821506 Jul 2013 CA national
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 17/007,574 filed Aug. 31, 2020, which is a continuation of U.S. patent application Ser. No. 16/809,729 filed Mar. 5, 2020, which is a continuation of U.S. patent application Ser. No. 16/585,790 filed Sep. 27, 2019 (now U.S. Pat. No. 10,844,697 issued Nov. 24, 2020), which is a continuation of U.S. patent application Ser. No. 16/359,540 filed Mar. 20, 2019 (now U.S. Pat. No. 10,472,938 issued Nov. 12, 2019), which is a continuation of U.S. patent application Ser. No. 15/920,812 filed Mar. 14, 2018, which is a continuation of U.S. patent application Ser. No. 15/617,344 filed Jun. 8, 2017 (now U.S. Pat. No. 10,429,161 issued Oct. 1, 2019) which is a divisional patent application of U.S. patent application Ser. No. 15/287,309 filed Oct. 6, 2016 (now U.S. Pat. No. 9,702,680 issued Jul. 11, 2017), which is a divisional patent application of U.S. patent application Ser. No. 14/904,788 filed Jan. 13, 2016 (now U.S. Pat. No. 9,494,021 issued Nov. 15, 2016), which is a U.S. national stage entry of PCT Application No. PCT/CA2014/050673 filed Jul. 16, 2014, which claims priority to Canadian Patent Application No. 2,821,506 filed Jul. 18, 2013, each of which is incorporated herein by reference in its entirety. U.S. patent application Ser. No. 16/809,729 is also a continuation of U.S. application Ser. No. 15/920,800 filed Mar. 14, 2018, which is incorporated herein by reference in its entirety.

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OSO Perforating, LLC; Exhibit A3 U.S. Pat. No. 7,901,247 to Ring vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 4, 2021; 19 pages.
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Schlumberger Technology Corporation; Defendant's Preliminary Invalidity Contentions; dated Aug. 19, 2021; 213 pages.
Schlumberger Technology Corporation; Exhibit A-01 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over WO20190148009; dated Aug. 19, 2021; 267 pages.
Schlumberger Technology Corporation; Exhibit A-02 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over U.S. Pat. No. 4,598,775; dated Aug. 19, 2021; 178 pages.
Schlumberger Technology Corporation; Exhibit A-03 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over U.S. Pat. No. 4,753,301; dated Aug. 19, 2021; 178 pages.
Schlumberger Technology Corporation; Exhibit A-04 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over U.S. Pat. No. 10,746,003; dated Aug. 19, 2021; 186 pages.
Schlumberger Technology Corporation; Exhibit A-05 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over WO2017/024266; dated Aug. 19, 2021; 247 pages.
Schlumberger Technology Corporation; Exhibit A-06 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over U.S. Pat. No. 4,479,556; dated Aug. 19, 2021; 250 pages.
Schlumberger Technology Corporation; Exhibit A-07 to Defendant's Preliminary Invalidity Contentions Invalidity of U.S. Pat. No. 10,844,696 over US2017/0145798; dated Aug. 19, 2021; 279 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A14 U.S. Patent Application No. 2010/0065302 to Nesbitt vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 15 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A15 U.S. Pat. No. 3,173,992 to Boop vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 17 pages.
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Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A17 U.S. Pat. No. 3,387,533 to Runkel vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 16 pages.
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Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A19 U.S. Pat. No. 7,762,331 to Goodman vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 28 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A2 U.S. Pat. No. 3,582,251 to Burke, et al. vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 15 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A20 U.S. Patent Application No. 2012/0199352 to Lanclos vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 24 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A21 “3.12-in Frac Gun” Publication and 3.12-in Frac Gun System, both by Schlumberger vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 26 pages.
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Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A23 Amit Govil, “Selective Perforation: A Game Changer in Perforating Technology—Case Study,” 2012 European and West African Perforating Symposium vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 17 pages.
Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Exhibit A24 Schlumberger SafeJet System vs. Asserted Claims of U.S. Pat. No. 10,844,697; dated Aug. 30, 2021; 26 pages.
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Hunting Titan, Inc.; Defendant's Answer, Affirmative Defenses, and Counterclaims to Plaintiffs' Second Amended Complaint for Civil Action No. 4:20-cv-02123; dated Sep. 10, 2021; 77 pages.
Hunting Titan, Inc.; Defendant's Responsive Claim Construction Brief for Civil Action No. 4:20-cv-02123; dated Oct. 1, 2021; 31 pages.
Hunting Titan, Inc.; Defendant's Supplemental Brief on Claim Construction; dated Nov. 5, 2021; 9 pages.
Hunting Titan, Inc; Petitioner's Sur-Reply on Patent Owner's Motion to Amend for IPR No. 2018-00600; dated Apr. 11, 2019; 17 pages.
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Nextier Completion Solutions Inc.; Defendant NexTier Completion Solution Inc.'s Opening Claim Construction Brief; dated Oct. 18, 2021; 26 pages.
Nextier Completion Solutions Inc.; Defendant Nextier Completion Solutions Inc.'s First Amended Answer and Counterclaims to Plaintiffs' First Amended Complaint for Civil Action No. 6:20-CV-01201; dated Jun. 28, 2021; 17 pages.
Nextier Completion Solutions Inc.; Defendant's Preliminary Invalidity Contentions for Civil Action No. 6:20-cv-01201-ADA; dated Aug. 30, 2021; 21 pages.
Nextier Completion Solutions Inc.; Exhibit A-1 BakerHughes Select-Fire; dated Aug. 30, 2021; 33 pages.
Nextier Completion Solutions Inc.; Exhibit A-10 U.S. Pat. No. 7,762,331 to Goodman; dated Aug. 30, 2021; 4 pages.
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Nextier Completion Solutions Inc.; Exhibit A-12 U.S. Appl. No. 61/819,196 to Harrigan et al.; dated Aug. 30, 2021; 26 pages.
Nextier Completion Solutions Inc.; Exhibit A-13 U.S. Pat. No. 9,874,083 to Logan; dated Aug. 30, 2021; 18 pages.
Nextier Completion Solutions Inc.; Exhibit A-14 New Select-Fire System; dated Aug. 30, 2021; 33 pages.
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Nextier Completion Solutions Inc.; Exhibit A-16 U.S. Appl. No. 61/733,129 to Rogman dated Aug. 30, 2021; 55 pages.
Nextier Completion Solutions Inc.; Exhibit A-17 U.S. Pat. No. 8,387,533 to Runkel; dated Aug. 30, 2021; 5 pages.
Nextier Completion Solutions Inc.; Exhibit A-18 Schlumberger SafeJet; dated Aug. 30, 2021; 13 pages.
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G&H Diversified Manufacturing, LP; Redated Petition for Post Grant Review for PGR2021-00078; dated May 10, 2021; 20 pages.
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GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit A U.S. Pat. No. 10,844,697 vs Castel; dated Aug. 30, 2021; 88 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit B U.S. Pat. No. 10,844,697 vs Goodman; dated Aug. 30, 2021; 36 pages.
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GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit G U.S. Pat. No. 10,844,697 vs Bickford; dated Aug. 30, 2021; 7 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit H U.S. Pat. No. 10,844,697 vs Black; dated Aug. 30, 2021; 33 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit I U.S. Pat. No. 10,844,697 vs Rogman; dated Aug. 30, 2021; 59 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit J U.S. Pat. No. 10,844,697 vs Burton; dated Aug. 30, 2021; 57 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit K U.S. Pat. No. 10,844,697 vs Borgfeld; dated Aug. 30, 2021; 36 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit L U.S. Pat. No. 10,844,697 vs Boop '383; dated Aug. 30, 2021; 24 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit M U.S. Pat. No. 10,844,697 vs Boop '992; dated Aug. 30, 2021; 14 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit N U.S. Pat. No. 10,844,697 vs Deere; dated Aug. 30, 2021; 14 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit O U.S. Pat. No. 10,844,697 vs Harrigan Provisional; dated Aug. 30, 2021; 26 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit P U.S. Pat. No. 10,844,697 vs Burke '251; dated Aug. 30, 2021; 7 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit Q U.S. Pat. No. 10,844,697 vs Runkel; dated Aug. 30, 2021; 7 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit R U.S. Pat. No. 10,844,697 vs Tassaroli; dated Aug. 30, 2021; 10 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit S U.S. Pat. No. 10,844,697 vs Harrigan '048; dated Aug. 30, 2021; 7 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit T U.S. Pat. No. 10,844,697 vs Select-Fire System; dated Aug. 30, 2021; 36 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit U U.S. Pat. No. 10,844,697 vs New Select-Fire System; dated Aug. 30, 2021; 37 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit V U.S. Pat. No. 10,844,697 vs EWAPS; dated Aug. 30, 2021; 17 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; Exhibit W U.S. Pat. No. 10,844,697 vs SafeJet System; dated Aug. 30, 2021; 17 pages.
GR Energy Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; GR Energy's Preliminary Invalidity Contentions for Civil Action No. 6:21-cv-00085-ADA; dated Aug. 30, 2021; 18 pages.
GR Energy Services Operating GP LLC, GR Energy Services Management, LP and GR Energy Services, LLC; GR Energy's Opening Claim Construction Brief; dated Oct. 18, 2021; 23 pages.
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Horizontal Wireline Services, LLC and Allied Wireline Services, LLC; Defendants' Opening Claim Construction Brief; dated Oct. 18, 2021; 27 pages.
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Canadian Intellectual Property Office; Office Action for CA Application No. 3,070,118; dated Nov. 17, 2021; 3 pages.
Schlumberger; Lina Pradilla, Wireline Efficiency in Unconventional Plays—The Argentinean Experience, including excerpted image from slide 13; dated 2013; 16 pages http://www.perforators.org/wp-content/uploads/2015/10/SLAP_47_Wireline_Efficiency_Unconventional_Plays.pdf.
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United States District Court for the Northern District of Texas Dallas Division; Memorandum Opinion and Order in Civil Action No. 3:21-cv-00188-M; Mar. 23, 2022; 35 pages (order is redacted to protect confidential informatlon; redacted order has not yet been led by the Court).
United States District Court for the Northern District of Texas Dallas Division; Memorandum Opinion and Order in Civil Action No. 3:21-cv-00192-M; Mar. 23, 2022; 34 pages (order is redacted to protect confidential informatlon; redacted order has not yet been led by the Court).
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Hunting Titan, Inc.; Defendant Hunting Titan, Inc.'s Opposed Motion for Leave to Amend Invalidity Contentions for Civil Action No. 4:20-cv-02123; dated Nov. 19, 2021; 17 pages.
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Hunting Titan, Inc.; Defendant Preliminary Invalidity Contentions for Civil Action No. 4:20-cv-02123; dated Aug. 6, 2021; 52 pages.
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Hunting Titan, Inc.; Exhibit 2 to Defendant Hunting Titan, Inc.'s Opposed Motion for Leave to Amend Invalidity Contentions for Civil Action No. 4:20-cv-02123; dated Nov. 19, 2021; 33 pages.
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Related Publications (1)
Number Date Country
20210222526 A1 Jul 2021 US
Divisions (2)
Number Date Country
Parent 15287309 Oct 2016 US
Child 15617344 US
Parent 14904788 US
Child 15287309 US
Continuations (6)
Number Date Country
Parent 17007574 Aug 2020 US
Child 17221219 US
Parent 16809729 Mar 2020 US
Child 17007574 US
Parent 16585790 Sep 2019 US
Child 16809729 US
Parent 16359540 Mar 2019 US
Child 16585790 US
Parent 15920812 Mar 2018 US
Child 16359540 US
Parent 15617344 Jun 2017 US
Child 15920812 US