Hydrocarbon fluids such as oil and natural gas are obtained from a subterranean geologic formation, referred to as a reservoir, by drilling a well that penetrates the hydrocarbon-bearing formation. Once a wellbore is drilled, various forms of well completion components may be installed to control and enhance the efficiency of producing the various fluids from the reservoir. Additionally, perforating guns and shaped charges may be used to perforate the hydrocarbon-bearing formation for enhanced production of the reservoir fluids.
In general, a system and methodology are provided to facilitate controlled detonation of charges, e.g. shaped charges, in a cost-efficient manner. Electronics for controlling detonation of a pellet of explosive material are mounted on a structure, such as a circuit board. The pellet is operatively coupled with the electronics and positioned to extend outwardly from the circuit board or other suitable structure. Another explosive component is arranged across the pellet at a predetermined angle, e.g. a right angle, with respect to a longitudinal axis of the pellet. In well applications or other applications utilizing shaped charges, the explosive component may be coupled to the shaped charge via, for example, a detonator cord.
However, many modifications are possible without materially departing from the teachings of this disclosure. Accordingly, such modifications are intended to be included within the scope of this disclosure as defined in the claims.
Certain embodiments of the disclosure will hereafter be described with reference to the accompanying drawings, wherein like reference numerals denote like elements. It should be understood, however, that the accompanying figures illustrate the various implementations described herein and are not meant to limit the scope of various technologies described herein, and:
In the following description, numerous details are set forth to provide an understanding of some embodiments of the present disclosure. However, it will be understood by those of ordinary skill in the art that the system and/or methodology may be practiced without these details and that numerous variations or modifications from the described embodiments may be possible.
The disclosure herein generally involves a system and methodology which facilitate controlled detonation of charges in a cost-efficient manner. For example, the system and methodology may be used in well applications to initiate detonation of shaped charges for perforation of a surrounding geologic formation. According to an embodiment, electronics are mounted on a structure to control detonation of a pellet of explosive material. In various applications, the electronics are mounted on a planar structure which may be in the form of a circuit board, e.g. a printed circuit board. The pellet is operatively coupled with the electronics and positioned to extend outwardly from the planar structure. Another explosive component is arranged across the pellet at a predetermined angle, e.g. a right angle, with respect to a longitudinal axis of the pellet. The explosive component may be part of or coupled with a detonator cord which is routed to the shaped charges of a perforating gun.
The technique described herein provides a cost-effective detonator system in a space efficient package by utilizing angled interaction of ballistic/explosive components rather than perpendicularly mounted circuit boards. Due to space constraints, conventional detonators often are long and skinny and this configuration previously dictated that certain electronics be mounted at right angles with respect to each other. For example, the control electronics may be mounted on a printed circuit board positioned along an axis of the perforating gun and at a right angle with respect to the electronics of an exploding foil initiator (EFI). In these conventional systems, the control electronics and the EFI electronics may be mounted on separate printed circuit boards or on a flexible printed circuit board bent at 90 degrees. The plane of the EFI is thus perpendicular to the axis of the perforating gun for coupling with a detonator cord in a space efficient manner. However, the right angled connection between the control electronics on the printed circuit board and the electronics of the EFI is a relatively difficult and expensive connection to construct.
In embodiments described herein, the angled turn, e.g. the right angled turn, which facilitates ultimate connection with the detonator cord or other suitable detonator device is accomplished via a ballistic connection instead of the electronic connection. The control electronics are mounted on a planar structure, e.g. a printed circuit board, and operatively engaged with a first explosive component, e.g. an explosive pellet, which extends outwardly from the planar structure. A second explosive component is laid across the first explosive component to achieve the desired angle, e.g. right angle, for ultimate connection with the detonator cord (or other suitable detonator) in a space efficient manner. The angled construction of ballistic/explosive components provides a dependable and inexpensive detonation system for detonation of shaped charges and other types of charges.
Referring generally to
The shaped charges 32 may be coupled with a detonator cord 34 or other suitable detonator device routed through housing 30. Once the perforating gun 22 is at a desired location in wellbore 24, the detonator cord 34 may be selectively detonated to cause detonation of those shaped charges 32 which are coupled with the detonator cord. In the example illustrated, a detonation system 36 is coupled to the detonator cord 34 to initiate detonation of the detonator cord 34 which, in turn, detonates the shaped charge or charges 32.
Referring generally to
In the specific example illustrated in
As illustrated in
The first explosive component 48 also comprises an engagement surface 54 oriented for engagement with a second explosive component 56. The second explosive component 56 is arranged at a predetermined angle with respect to first explosive component 48 to create a space efficient configuration. In some applications, for example, the second explosive component 56 is engaged with the first explosive component 48 at approximately a right angle although other angles may be used in some applications. In various space-efficient types of embodiments, a longitudinal axis 58 of the second explosive component 56 is generally perpendicular with the longitudinal axis 52 of first explosive component 48 such that the second explosive component 56 is generally parallel with circuit board 42 and plane 50. The first explosive component/pellet 48 and the second explosive component 56 comprise suitable explosive materials, such as explosive materials known and available to those of ordinary skill in the art. An example of explosive material includes explosive material used in conventional boosters employed in the well perforation industry.
Depending on the application, the second explosive component 56 may have a variety of forms and configurations, including the generally cylindrical form illustrated in
In some applications, a transfer donor 62 may be engaged with booster 60 or directly with detonator cord 34 such that electronics 44 initiate the sequential detonation of first explosive component 48, e.g. pellet 48, transfer donor 62, booster 60, and/or detonator cord 34. In this example, the pellet 48 effectively fires straight into the transfer donor 62, and the transfer donor 62 fires straight into the booster 60 or detonator cord 34. The second explosive component 56 may be positioned adjacent to or coupled with detonator cord 34, as illustrated in
In the example illustrated, the explosive material 64 of booster 60 (or of both booster 60 and transfer donor 62) may be positioned in a sleeve 66. The sleeve 66 is sized to receive a booster plug 68 which has an expanded feature 70. In some applications, the sleeve 66 is formed of aluminum, but it also may be formed of other suitable materials. The expanded feature 70 may be constructed for receipt in a corresponding recess 72 in housing 38 so that the second explosive component 56 is securely oriented and held within housing 38.
Referring generally to
In this embodiment, the second explosive component 56 comprises an end 76 of detonator cord 34. The end 76 of detonator cord 34 is disposed across first explosive component/pellet 48 at a predetermined angle. For example, the axis 52 of the first explosive component 48 may be generally at a right angle with respect to circuit board 42, and the longitudinal axis 58 of the second explosive component 56 may be generally at a right angle with respect to first explosive component 48 and its longitudinal axis 52.
As illustrated in
As illustrated in
The curved surface 78 and corresponding curved surface 80 increase the ballistic transfer efficiency in many applications. However, other applications may utilize a flat or a substantially flat engagement surface 54 as with the embodiment illustrated in
The system 20, e.g. well system, may be used in a variety of applications, including numerous well perforation applications and other applications utilizing controlled detonation of shaped charges or other charges. For example, the detonation system 36 and a suitable overall system 20 may be used in well applications, mining applications, and various other applications which benefit from a controlled, dependable detonation. Depending on the specifics of a given application, the construction of the overall system 20 and detonation system 36 may vary. Additionally, the system 20 may be designed for use in many types of wells, including vertical wells and deviated, e.g. horizontal, wells. The wells may be drilled in a variety of formations with single or multiple production zones and with many different types of perforating gun systems constructed to form various types of perforations in the production zones of the geologic formation.
Depending on the application, the detonation system 36 may be constructed in several configurations. For example, the electronics 44 and supporting structure 40 may have a variety of sizes, components and configurations. Depending on the application, the electronics 44 may be controlled by signals sent downhole from a surface control system via various communication lines or wireless techniques. Additionally, the first explosive component 48 and the second explosive component 56 may be operatively engaged via a variety of techniques and components. For example, the components may be held in contact or near contact by housing 38 and/or by other mounting structures. The types of explosive material 64 and the configuration of that explosive material also may be adjusted according to the parameters of a given application. Similarly, the second explosive component 56 may have a variety of components, including boosters, transfer donors, detonator cord ends, and various combinations of these components and/or other suitable components.
Although a few embodiments of the disclosure have been described in detail above, those of ordinary skill in the art will readily appreciate that many modifications are possible without materially departing from the teachings of this disclosure. Accordingly, such modifications are intended to be included within the scope of this disclosure as defined in the claims.
The present document is based on and claims priority to U.S. Provisional Application Ser. No. 61/840,913 filed Jun. 28, 2013, incorporated herein by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/US2014/044282 | 6/26/2014 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2014/210275 | 12/31/2014 | WO | A |
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Number | Date | Country | |
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20160376879 A1 | Dec 2016 | US |
Number | Date | Country | |
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61840913 | Jun 2013 | US |