PERFORATING GUN FOR OIL AND GAS WELLS, AND SYSTEM AND METHOD FOR USING THE SAME

20210340846 · 2021-11-04

    Inventors

    Cpc classification

    International classification

    Abstract

    A perforating gun, system and method is provided. The perforating gun includes a body, a plurality of shaped charges, at least one initial propellant and may include an actuating mechanism. The plurality of shaped charges are mounted within the body, and each shaped charge has an amount of an explosive material. The actuating mechanism is in communication with each shaped charge and the at least one initial propellant. The actuating mechanism is configured to fire the at least one initial propellant before firing any of the plurality of shaped charges.

    Claims

    1. A perforating gun, comprising: a body; a plurality of shaped charges mounted within the body, each shaped charge having an amount of an explosive material; at least one initial propellant; and an actuating mechanism, in communication with each shaped charge and the at least one initial propellant, wherein the actuating mechanism is configured to fire the at least one initial propellant before firing any of the plurality of shaped charges.

    2. The perforating gun of claim 1, wherein the at least one initial propellant is a solid propellant.

    3. The perforating gun of claim 2, wherein the solid propellant includes at least one of potassium perchlorate, ammonium perchlorate, or barium perchlorate.

    4. The perforating gun of claim 1, wherein the body includes a first axial end and a second axial end disposed opposite the first axial end; and wherein the at least one initial propellant is configured to produce an amount of gas at an elevated pressure outside of the body upon being fired.

    5. The perforating gun of claim 4, wherein the amount of elevated pressure gas produced from the at least one propellant is produced in a direction from the second axial end toward the first axial end.

    6. The perforating gun of claim 1, wherein the body includes a first axial end and a second axial end disposed opposite the first axial end; and wherein the at least one initial propellant is disposed between the second axial end and the plurality of shaped charges.

    7. The perforating gun of claim 1, wherein the actuating mechanism is mechanically actuated.

    8. The perforating gun of claim 1, wherein the actuating mechanism is electrically actuated.

    9. A well casing perforation system for perforating a well casing within a subterranean well, the well casing containing a well fluid, and the well casing having an inner passage defined by an inner surface, comprising: a perforating gun having a body, a plurality of shaped charges mounted within the body, and at least one initial propellant, wherein the perforating gun has an exterior diameter proximate the plurality of shaped charges; and a controller configured to selectively cause the perforating gun to actuate when the perforating gun is disposed within the well casing, which actuation of the perforating gun includes first causing the at least one initial propellant to fire, and second causing the plurality of shaped charges to fire.

    10. The system of claim 9, wherein the perforating gun body includes a first axial end and a second axial end disposed opposite the first axial end; and wherein the at least one initial propellant is configured to produce an amount of gas at an elevated pressure outside of the body upon being fired.

    11. The system of claim 10, wherein the amount of elevated pressure gas produced from the at least one propellant is produced in a direction from the second axial end toward the first axial end.

    12. The system of claim 9, wherein the perforating gun includes a mechanically operated actuating mechanism, and the controller is configured to cause actuation of the perforating gun actuating mechanism.

    13. The system of claim 9, wherein the perforating gun includes an electrically operated actuating mechanism, and the controller is configured to cause actuation of the perforating gun actuating mechanism.

    14. A method of perforating a well casing within a subterranean well, the well casing containing a well fluid, and the well casing having an inner passage, the method comprising: providing a perforating gun having a body, a plurality of shaped charges mounted within the body, and at least one initial propellant, wherein the perforating gun body has an exterior surface proximate the plurality of shaped charges; disposing the perforating gun within the well casing inner passage at a position where a diameter of the body exterior surface is less than an inner diameter of the well casing inner passage, at which position an annular region is disposed around the perforating gun and between the perforating gun and the well casing, and the annular region is filled with said well fluid; driving the well fluid out of the annular region by firing the at least one initial propellant in a manner the maintains the well fluid out of the annular region for a period of time; and perforating the well casing by firing the plurality of shaped charges during the period of time in which the well fluid is maintained out of the annular region.

    15. The method of claim 14, wherein the perforating gun body includes a first axial end and a second axial end disposed opposite the first axial end, and the perforating gun is disposed within the well casing so that the second axial end is downhole of the first axial end; and wherein firing the at least one initial propellant drives the well fluid in a direction from the second axial end toward the first axial end.

    16. The method of claim 14, wherein the perforating gun includes a mechanically operated actuating mechanism, and the at least one initial propellant is fired by engaging the mechanically operated actuating mechanism.

    17. The method of claim 16, wherein the mechanically operated actuating mechanism is engaged by a drop bar impact.

    18. The method of claim 14, wherein the perforating gun includes an electrically operated actuating mechanism, and the at least one initial propellant is fired by engaging the electrically operated actuating mechanism.

    19. The method of claim 18, wherein the electrically operated actuating mechanism is engaged by a signal sent from a well control station.

    20. The method of claim 14, wherein the perforating gun includes a pressure operated actuating mechanism, and the at least one initial propellant is fired by subjecting the perforating gun to a predetermined first elevated pressure.

    21. The method of claim 20, wherein the plurality of shaped charges are fired by subjecting the perforating gun to a predetermined second elevated pressure, which second elevated pressure is greater than the first elevated pressure.

    Description

    BRIEF DESCRIPTION OF THE DRAWINGS

    [0033] The present disclosure is illustrated by way of example and not limited in the accompanying figures in which like reference numerals indicate similar elements. The drawing figures are not necessarily drawn to scale unless specifically indicated otherwise.

    [0034] FIG. 1 diagrammatically illustrates a prior art single stage perforating gun embodiment disposed within a well casing.

    [0035] FIG. 2 diagrammatically illustrates a prior art two stage perforating gun embodiment disposed within a well casing.

    [0036] FIG. 3 diagrammatically illustrates a prior art two stage perforating gun embodiment disposed within a well casing.

    [0037] FIG. 4 diagrammatically illustrates a prior art two stage perforating gun embodiment disposed within a well casing.

    [0038] FIG. 5 is a diagrammatic illustration of a subterranean well having a perforating gun and well control station.

    [0039] FIG. 6 diagrammatically illustrates a perforating gun embodiment disposed within a well casing according to the present disclosure in an unfired state.

    [0040] FIG. 7 diagrammatically illustrates a perforating gun embodiment disposed within a well casing according to the present disclosure in a fired state.

    [0041] FIG. 8 is a flow chart illustrating aspects of the present disclosure.

    DETAILED DESCRIPTION

    [0042] It is noted that various connections are set forth between elements in the following description and in the drawings (the contents of which are included in this disclosure by way of reference). It is noted that these connections are general and, unless specified otherwise, may be direct or indirect and that this specification is not intended to be limiting in this respect. A coupling between two or more entities may refer to a direct connection or an indirect connection. An indirect connection may incorporate one or more intervening entities or a space/gap between the entities that are being coupled to one another.

    [0043] An exemplary subterranean well is diagrammatically shown in FIG. 5 having a well casing 20 that extends into and within a subterranean formation 22. The well casing includes an inner passage 21 defined by an inner diameter surface 35 disposed at an inner diameter “WCID” (see FIG. 7). The subterranean formation 22 may be land based, or may be disposed at the floor of a body of water (e.g., an ocean). In some instances, a product such as cement 24 may be disposed contiguous with the well casing 20 and the subterranean formation 22 to secure the well casing 20 within the subterranean formation 22. The well may include a well head 26 disposed above the subterranean formation 22 and the well head 26 may be in communication with a well control station 28. A perforating gun 30 is shown disposed within the inner passage 21 of the well casing 20. Aspects of the present disclosure include a system for actuating one or more perforation guns 30 within a subterranean well, a perforating gun 30, and a well casing perforating system.

    [0044] Perforating guns 30 and associated apparatus can be utilized as part of an electric wireline perforating (“EWP”) system, or as part of a tubing conveyed perforating (“TCP”) system (shown in FIG. 5), or similar well systems. EWP systems utilize electrical signals to control downhole tooling including perforating guns. TCP systems, on the other hand, are often configured to use hydraulic pressure and/or mechanical force to control downhole tooling; e.g., to initiate a perforating gun 30. These type of systems may utilize sensors that provide information (e.g., pressure values, temperature values, time values, etc.) relating to downhole conditions, that can be used during the perforation of well casing 20 segments.

    [0045] Regardless of the type of system (e.g., EWP, TCP, or the like) utilized to operate a perforating gun 30, the well control station 28 may be configured to communicate with and control the various components of the well perforating system. The well control station 28 may be located at the subterranean well site, or may be located remote from the subterranean well site. The well control station 28 may include a controller 32, one or more input devices (e.g., a keyboard, a touch screen type HMI display, etc.), and with one or more output devices (e.g., a monitor screen, an HMI display, etc.). The controller 32 may be directly or indirectly in communication with various system components, including the perforating gun 30 or components utilized to actuate the perforating gun 30. The controller 32 may include any type of computer, computing device, computational circuit, CPU, processor, microprocessor, digital signal processor, co-processor, micro-controller, microcomputer, field programmable gate array, programmable logic device, state machine, logic circuitry, analog circuitry, digital circuitry, any combination thereof, or any type of processing circuit or logic device capable of executing a series of instructions that are stored in a memory device. The instructions stored in the memory device may represent logic instructions (e.g., commands), one or more algorithms, etc., for operating some or all of the system components, individually and/or collectively. The stored instructions are not limited to any particular form (e.g., program files, system data, buffers, drivers, utilities, system programs, etc.) provided they can be executed by the controller 32; e.g., by one or more processors included in the controller 32. The memory device may be a non-transitory computer readable storage medium configured to store instructions that when executed by the controller 32, cause the controller 32 to perform or cause the performance of certain functions or commands. The memory device may be a single memory device or a plurality of memory devices. The memory device may include a storage area network, network attached storage, as well as a disk drive, a read-only memory, random access memory, volatile memory, non-volatile memory, static memory, dynamic memory, flash memory, cache memory, and/or any device that stores digital information. Communications between the controller 32 and the various system components are not limited to any particular format, and may be via a hard-wired communication system, or via a wireless communication system, or any combination thereof.

    [0046] According to an aspect of the present disclosure, a perforating gun 30 is provided having a body 34 with a lengthwise extending axis 36 (see FIGS. 6 and 7). The body 34 has at least one outer radial surface 38 and has an inner passage 40 that extends lengthwise between a first axial end and a second axial end. In FIG. 5, the perforating gun 30 is shown as having a second axial end 41 that is downhole of a first axial end 43. In some perforating gun 30 embodiments, cap sections (not shown) may be used to enclose the inner passage 40 at each lengthwise end of the body.

    [0047] The perforating gun 30 includes a plurality of shaped charges 42 mounted within the body 34. Each shaped charge 42 may be disposed within a shaped charge cavity 44 disposed in the outer radial surface 38 of the body 34. The outer radial surface of the body 34 proximate the shaped charges 42 is shown as “ORSD” in FIG. 7. Each shaped charge 42 is directly or indirectly in communication with the inner passage 40. The shaped charges 42 may be positioned at a variety of axial and circumferential positions along the body 34 of the perforating gun 30. The present disclosure is not limited to any particular number of shaped charges 42, or the relative positioning of those shaped charges 42 on the body 34.

    [0048] Each shaped charge 42 includes an explosive material and a structure that is configured to produce, upon firing, a fluid jet 45 that extends radially outwardly (i.e., substantially perpendicular to the body lengthwise axis 36). The present disclosure is not limited to any particular shaped charge 42 configuration; e.g., a shaped charge 42 that includes an outer casing and a conical liner, with the explosive material sealed within the outer casing by the conical liner is an example of an acceptable shaped charge 42 configuration. Acceptable examples of explosive materials include, but are not limited to, Cyclotrimethylenetrinitramine, C3H6N606 (sometimes referred to as “Royal Demolition Explosive” or “RDX”), cyclotetramethylene-tetranitramine (sometimes referred to as “High Melting Explosive” or “HMX”), Hexanitrostilbene (sometimes referred to as “HNS” or “JD-X”), and 2,6-Bis(Picrylamino)-3,5-dinitropyridine (sometimes referred to as “PYX”). All of the plurality of shaped charges within the perforating gun 30 may have a uniform configuration, but that is not required.

    [0049] Perforating gun 30 shaped charges are known in the oil and gas field, and come in a variety of different configurations and types. The present disclosure may be used with a variety of different perforating gun shaped charges 42, and therefore is not limited to any particular type of perforating gun shaped charge 42.

    [0050] The present disclosure perforating gun 30 includes one or more initial propellants 46 that, upon firing, are operable to displace the well fluid 50 disposed in the annular region 48 surrounding the perforating gun 30. As will described below, the perforating gun 30 is configured and controlled so the initial propellant 46 is fired before the shaped charges 42 are fired. Upon firing, the initial propellant 46 produces an elevated pressure gas within the well casing 20 that drives the well fluid 50 within the annular region 48 away from the perforating gun 30 and therefore away from the shaped charges 42 incorporated into the perforating gun 30. Since the well casing 20 radially outside the perforating gun 30 is not yet perforated, the well fluid 50 in the annular region 48 travels within the well casing 20 away from the perforating gun 30. The displacement of the well fluid 50 from the annular region 48 creates a short-lived gas-gap 52 (e.g., see FIG. 7) in the annular region 48 between the perforating gun 30 and the well casing 20. Once the well fluid is temporarily displaced from the annular region 48, the shaped charge(s) 42 may be fired to perforate the well casing 20, the cement 24 disposed outside the well casing 20 (if present), and the subterranean formation 22 disposed radially outside of the perforating gun 30 without interference from well fluid 50 within the annular region 48. The perforating gun 30 may be configured with the one or more initial propellants 46 in any manner that permits the firing of the initial propellant 46 to displace the well fluid 50 in the annular region 48. The amount and/or type of initial propellant 46 is selected to provide sufficient force to displace the well fluid 50 in the annular region 48 for a period of time adequate for the shaped charges 42 to be fired with no well fluid 50 disposed within the annular region 48. As indicated above, solid propellants are a different material than the shaped charge explosive material; e.g., on a per weight basis, a solid propellant releases much less energy that the explosive material used in shaped charges, and that energy is produced substantially slower than the aforesaid explosive material (e.g., about 1,000 times slower). For the purpose of displacing the well fluid 50 in the annular region 48 for a period of time adequate for the shaped charges 42 to be fired, it is our experience that a solid type propellant can be used as an initial propellant. Non-limiting examples solid propellant types include potassium perchlorate, ammonium perchlorate, and barium perchlorate. The present disclosure is not limited to using any particular type of initial propellant 46, however. In some embodiments (as shown in FIG. 6), the initial propellant 46 may be aligned with the shaped charges 42. In some embodiments, the initial propellant 46 may be disposed on or in the perforating gun 30 at a position that will be downhole of the shaped charges 42 when the perforating gun 30 is located within the well casing 20 (e.g., disposed between the shaped charges 42 and a downhole axial end of the body 34), or configured to produce the elevated pressure downhole of the shaped charges 42, or more specifically configured to produce an elevated pressure gas at a position downhole of the shaped charges 42, which elevated pressure gas is produced in a direction traveling from the down hole axial end to the upper axial end of the perforating gun 30. Well fluid may be considered to be an incompressible fluid. Locating the initial propellant 46 at a position that will produce the motive force to displace the well fluid 50 in a direction toward the well head 26 facilitates the displacement of the annular region 48 well fluid 50.

    [0051] In some embodiments, the perforating gun 30 may include an actuating mechanism 54 (shown schematically in FIG. 6) configured to permit the one or more initial propellants 46 and the shaped charges 42 to fire in a predetermined manner; i.e., fire the initial propellant 46 first, and subsequently fire the shaped charges 42 in a period of time while the annular region 48 has been cleared of well fluid 50. The actuating mechanism may assume a variety of different configurations, and the present disclosure is not therefore limited to any particular actuating mechanism 54 configuration. As a first example, an actuating mechanism 54 within a perforating gun 30 may include a first electrical detonator that is in communication with the initial propellant(s) 46 and a second electrical detonator that is in communication with the shaped charges 42. A first control signal from the well control station 28 may cause the first electrical detonator to fire initial propellant(s) 46 and a second control signal sent subsequently from the well control station 28 may cause the second electrical detonator to fire the shaped charges 42. Alternatively, an actuating mechanism 54 within a perforating gun 30 may include a control module in communication with the aforesaid first and second electrical detonators. Once a control signal from the well control station 28 is received by the control module, the control module sends a signal to the first electrical detonator to fire the initial propellant(s) 46, and subsequently sends a second signal to the second electrical detonator to fire the shaped charges 42. As a further alternative, if the perforating gun 30 is mechanically actuated by a drop bar, the impact of the drop bar may cause actuating of the initial propellant 46, and actuate a delay mechanism (e.g., a fuse or other device) that is operable to fire the shaped charges 42 after a period of time. As yet another alternative, the initial propellant may be actuated by exposing the perforating gun 30 to a first pressure within the well casing 20, and the shaped charges 42 may be actuated by exposing the perforating gun 30 to a second higher pressure. For example, the perforating gun 30 may have a first actuator that operates once a first pressure rupture disk is burst, and a second actuator that operates once a second pressure rupture disk is burst, which second rupture disk is configured to rupture at a higher pressure than the first rupture disk; i.e., the second pressure is greater than the first pressure. Once the perforating gun is in the desired position within the well casing 20, the well fluid may be pressurized to reach the first pressure, thereby causing the first rupture disk to rupture and cause the first actuator to fire the initial propellant 46. The firing of the initial propellant 46 may create a locally elevated pressure within the well casing that is adequate to cause the second rupture disk to rupture and cause the second actuator to fire the shaped charges 42. In still further alternative embodiments, the actuating mechanism 54 may include hardware that sequentially fires the initial propellant 46 and then the shaped charges 42 using sensor input (e.g., temperature sensors, pressure sensors, etc.). The above actuating mechanism 54 example are provided to illustrate possible actuating mechanisms that may be used, and the present disclosure is not intended to be limited thereto. In addition, the actuating system that is used to fire the initial propellant 46 first, and subsequently fire the shaped charges 42 in a period of time while the annular region 48 has been cleared of well fluid 50, may be implemented entirely within the well control station 28, or may include elements disposed within both the perforating gun 30 and the well control station 28.

    [0052] During operation of the system, the perforating gun 30 is inserted into a well casing 20 to a desired downhole position for perforation. Once positioned, an operator may utilize the well control station 28 to actuate the perforating gun 30. Alternatively, in some embodiments the operator may need not use a well control station 28 to actuate the perforating gun 30; e.g., the perforating gun 30 may include sensors that cause actuation upon one or more parameters (e.g., temperature, pressure, time, etc.) being satisfied. Either way, once the perforating gun 30 is actuated, the actuating mechanism 54 of the perforating system operates to fire the one or more initial propellants 46. For a very short period of time after the initial propellants 46 are fired, the well fluid 50 displaced from the annular region 48 will remain displaced until pressures equalize within the well casing 20. This period of time may be referred to as the “displacement dwell time”. During this period of time, the actuating mechanism 54 operates to fire the shaped charges 42 (the shaped charges 42 may be fired together or in some predetermined order). Each shaped charge 42 produces a fluid jet 45 that passes through the standoff distance between the outer radial surface 38 of the perforating gun 30 and the inner diameter surface 35 of the well casing 20 (now devoid of well fluid 50), perforates the well casing 20, the cement 24 disposed outside the well casing 20 (if present), and extends into the subterranean formation 22. Hence, the impediment to the shaped charge fluid jet 45 caused by the well fluid 50 in the annular region 48 is eliminated. As a result, the entrance hole diameter (“EHD”) through the well casing 20 and cement 24 and the formation penetration (PEN) are improved. A well application in an unconsolidated subterranean formation 22 (which typically requires a secondary sand control system), benefits from a larger EHD in the well casing 20. A well application in a high-compressive strength formation (e.g., carbonate, shale, sand, etc.) benefits from both a larger EHD in the well casing 20 and a larger PEN. The present disclosure can be used to provide both a larger EHD and a deeper PEN for a given shaped charge 42.

    [0053] The present disclosure can provide other benefits as well. For example, a significant portion of the cost of a perforating gun 30 is related to the explosive material used in the shaped charges 42. The present disclosure eliminates the well fluid 50 impediment to the shaped charge fluid jet 45 during the perforation process. As a result, it may be possible to use less explosive material per shaped charge 42 and still form the same type perforation within the subterranean formation 22. Alternatively, it may be possible for a perforating gun 30 to have fewer shaped charges 42 per linear distance, and still get the same fracturing performance within the subterranean formation 22. As another example, U.S. Department of Transportation (USDOT) rules limit transportation of explosive materials on a cargo aircraft to no more than thirty-nine grams (39 gm) net explosive weight. Many legacy perforating guns require more than 39 gm net explosive weight to achieve a desirable perforating tunnel (EHD & PEN) downhole. In these cases, if air shipment of a perforating gun is required, then only a charter flight can be used, which greatly increases the cost and sometimes negatively affects availability. By improving the perforating gun performance by removing the well fluid 50 impediment, it may be possible to use less explosives to generate the same EHD and, PEN, thereby improving the transportation possibilities.

    [0054] A method of perforating a well casing within a subterranean well according to the present disclosure, which well casing contains a well fluid, and has an inner passage defined by an inner surface, may include the following: a) providing a perforating gun having a body, a plurality of shaped charges mounted within the body, at least one initial propellant, wherein the perforating gun has an exterior diameter proximate the plurality of shaped charges; b) disposing the perforating gun within the well casing at a position in the well casing where the exterior diameter is less than an inner diameter of the well casing inner passage, at which position an annular region is disposed around the perforating gun and annular region is filled with well fluid; c) driving the well fluid out of the annular region by firing the at least one initial propellant in a manner the maintains the well fluid out of the annular region for a period of time; and d) perforating the well casing by firing the plurality of shaped charges during the period of time in which the well fluid is maintained out of the annular region.

    [0055] In some embodiments of the present disclosure, a perforating gun 30 may include a secondary propellant that is configured similar to perforating guns described above. More specifically, the perforating gun may be configured to fire the secondary propellant after the shaped charges are fired, to produce an additional pressure even that can cause fracturing within the formation; i.e., an additional pressurization after the shaped charges are fired to physically change the formation perforation and thereby enhance fluid flow into the formation perforation and subsequently into the well casing.

    [0056] Aspects of the disclosure have been described in terms of illustrative embodiments thereof. Numerous other embodiments, modifications, and variations within the scope and spirit of the appended claims will occur to persons of ordinary skill in the art from a review of this disclosure. For example, one of ordinary skill in the art will appreciate that the steps described in conjunction with the illustrative figures may be performed in other than the recited order, and that one or more steps illustrated may be optional in accordance with aspects of the disclosure. One or more features described in connection with a first embodiment may be combined with one or more features of one or more additional embodiments.