Patent Grant
9689246
Embodiments of the present disclosure relate to stimulation devices for initiating energetic material in downhole applications. More particularly, embodiments of the present disclosure relate to stimulation devices including a housing having an energetic material disposed therein and an initiation system for igniting the energetic material in order to stimulate formations intersected by a wellbore and related methods.
Downhole stimulation techniques include high energy-based downhole stimulation techniques and propellant-based downhole stimulation techniques. Such downhole stimulation techniques generally are implemented to increase the effective surface area of producing formation material available for production of hydrocarbons resident in the formation by opening and enlarging cracks in the rock of the formation.
High energy-based downhole stimulation techniques generally employ the detonation of high energy explosive material within a wellbore. The resultant shockwave caused by detonation of the high energy explosive material in the wellbore may be employed to fracture a formation adjacent the wellbore.
Propellant-based downhole stimulation techniques generally employ tools having a circular cylinder housing filled with propellant grain, which may comprise a single volume or a plurality of propellant “sticks” in a housing. Such tools may include conventional propellant ignition systems that use pyrotechnic initiators or small rocket motors. When deployed in a wellbore adjacent a producing formation, the ignition systems will generally initiate a burn at one end of the propellant grain (i.e., a cigarette-type burn) that must propagate along the entire length of the propellant grain. As the propellant grain is initiated, gases from the burning propellant grain exit the housing through holes formed in the housing, entering the producing formation. The pressurized gas may be employed to fracture a formation, to perforate a formation when spatially directed through apertures in the housing against the wellbore wall, or to clean existing fractures or perforations in a formation made by other techniques.
Alternatively, the housing of the tool may include an axially extending bore through the center of the propellant grain and a detonation cord extending through the bore. When deployed in a wellbore adjacent a producing formation, the detonation cord will initiate a burn along the axially extending bore through the center of the propellant grain that will propagate generally radially through the ignited propellant grain. As the propellant grain is initiated, gases from the burning propellant grain exit the housing through preformed holes (which may be initially closed by a thinner housing wall, by a so-called “burst disk,” or by another covering structure to prevent propellant contamination by wellbore fluid) formed in the housing, entering the producing formation. The pressurized gas may be employed to fracture a formation, to perforate a formation when spatially directed through apertures in the housing against the wellbore wall, or to clean existing fractures or perforations in a formation made by other techniques.
U.S. Pat. No. 8,033,333 to Frazier et al., the disclosure of which is incorporated herein in its entirety by this reference, discloses such a propellant-based downhole stimulation device including a detonation cord. The downhole stimulation device includes a housing holding a propellant therein. A detonation cord is disposed in an axially extending bore through the center of the propellant. Initiation of the detonation cord ignites the propellant. Openings or holes in the housing, which are generally initially sealed, serve as passageways for the expelled gas from the ignited propellant to exit the housing into the wellbore.
However, conventional propellant ignition systems that use pyrotechnic initiators or small rocket motors generally provide initiation of the propellant housed therein over a period of ten to one hundred milliseconds. Such a relatively long ignition period as compared to a much shorter period of ignition of high explosive materials may not be desirable in some applications. Such a relatively long ignition period renders impractical and ineffective any contemplated use of the two types of stimulation devices in combination as the ignition of the propellant grain would start well after the detonation of the explosive materials. Thus, formation fractures opened by detonation of an explosive in the wellbore might partially or completely collapse before gas could emanate from a propellant-based stimulation tool to desirably extend and enlarge the fractures. Further, the relatively slower burn of the propellant grain traveling from one end of the propellant grain to the other opposing end also requires relatively more time to build the desired pressures in the housing of the tool. Such a relatively longer time domain to build pressure within the housing may also render impractical and ineffective any contemplated use of propellant-based and explosive-based stimulation devices in combination as the gases produced by combustion of the propellant grain would start exiting the housing well after the detonation of the explosive materials, again negating any potential benefit of deploying propellant-based stimulation tools in the same wellbore as explosive-based stimulation tools. Further, gases produced by combustion of the propellant grain in a conventional propellant-based stimulation tool employing preformed holes in the tool housing to exit gas generated within the tool will exit the tool at a relatively low pressure, reducing the potential benefit of fracture expansion.
Other conventional downhole stimulation devices including initiation systems including a detonation cord, such as those disclosed in U.S. Pat. No. 8,033,333, may not produce the desired pressures in the tool within the desired time domain when implemented in systems including both propellant-based and explosive-based stimulation. Further, the preformed openings in the housing may not allow the desired pressures to build in the housing of the tool as gases will start exiting the housing through the openings once the initial seals are breached. Further still, the initiation of the propellant grain along the bore formed in the propellant grain requires a reduction in overall propellant grain in the housing in order to form the bore, thereby, restricting the amount of propellant that is available in the housing to combust. Finally, the initiation of the propellant grain along the bore formed in the propellant grain may also require relatively more time to build the desired pressures in the housing of the tool as the bore within the propellant grain forms a void in the propellant grain that must be pressurized along with the remainder of the housing.
In some embodiments, the present disclosure comprises a downhole stimulation device including a housing having a first end, a second end, and a longitudinal axis extending between the first end and the second end, an energetic material disposed within the housing, and an initiator coupled to the housing at one of the first end and the second end. The initiator comprises a shaped charge for igniting the energetic material within the housing. The shaped charge is configured to produce a projectile to penetrate the energetic material in order to ignite the energetic material.
In some embodiments, the shaped charge is configured to produce the projectile to penetrate the energetic material along a majority of the housing from the first end to the second end of the housing.
In some embodiments, the energetic material entirely fills a cross-sectional area within the housing taken in a direction transverse to the longitudinal axis proximate to the initiator.
In other embodiments, the present disclosure comprises a downhole stimulation device including a cylindrical housing having a first end, a second end, and a longitudinal axis extending between the first end and the second end. A lateral outer surface of the cylindrical housing extending a direction transverse to the longitudinal axis of the housing comprises a continuous surface. The downhole stimulation device further includes an energetic material disposed within the cylindrical housing and an initiator coupled to the cylindrical housing at one of the first end and the second end. The initiator comprises a shaped charge for igniting the energetic material within the cylindrical housing.
In some embodiments, the energetic material entirely fills at least a majority of an inner portion of the cylindrical housing coincident with and surrounding a centerline of the cylindrical housing.
In further embodiments, the present disclosure comprises a downhole stimulation device including a cylindrical housing having a first end, a second end, a longitudinal axis extending between the first end and the second end, and an imperforate lateral outer surface. The downhole stimulation device further includes an energetic material disposed within the cylindrical housing and an initiator coupled to the cylindrical housing at one of the first end and the second end. The imperforate lateral outer surface of the housing is adapted to deform under internal pressure in the housing caused by gases produced by combustion of the energetic material in the cylindrical housing to form at least one aperture in the cylindrical housing to permit expulsion from the cylindrical housing of the gases produced by the combustion of the energetic material.
In yet other embodiments, the present disclosure comprises a method of operating a downhole stimulation device. The method includes disposing a stimulation device having an energetic material disposed within a housing of the stimulation device in a borehole, initiating the energetic material with a jet formed with a shaped charge by penetrating the energetic material with the jet to ignite the energetic material along a depth of the borehole, and burning the energetic material in a laterally extending direction transverse to the depth of the borehole.
In yet other embodiments, the present disclosure comprises a method of operating a downhole stimulation device. The method includes initiating an energetic material disposed within a housing of the stimulation device, burning the energetic material in a laterally extending direction transverse to a depth of a borehole in which the stimulation device is disposed, forming at least one aperture in the housing with internal pressure in the housing caused by gases produced by combustion of the energetic material, and producing at least one gas steam extending laterally from the housing formed by the gases produced by combustion of the energetic material.
The illustrations presented herein are not actual views of any particular stimulation device or component thereof, but are merely idealized, schematic representations that are employed to describe embodiments of the present disclosure.
In some embodiments, the present disclosure comprises a stimulation device including a housing filled with an energetic material (e.g., a propellant). The stimulation device further includes an initiation device comprising, for example, a shaped charge coupled to the housing of the stimulation device. The initiation device is configured to produce a jet of sufficiency high kinetic energy to travel through the energetic material in the housing longitudinally and ignite the energetic material to burn laterally outwardly. Ignition and burn of the energetic material generates high pressure combustion gases that exit the housing in order to stimulate one or more subterranean formations proximate the stimulation device in a subterranean wellbore.
In some embodiments, the energetic material may at least substantially fill the housing. For example, the energetic material may entirely fill the housing or may fill a majority of the length of the housing with the exception of one or more voids in the energetic material positioned at one or more axial ends of the of the housing.
In one embodiment, the energetic material may fill the portion of the housing proximate (e.g., coincident with and surrounding) a centerline of the housing.
In some embodiments, the lateral sides of the housing may be substantially continuous. For example, the housing may be formed to have a continuous lateral outer surface without any openings formed in the lateral outer surface.
Referring to
Stimulation device 100 may be deployed in a wellbore adjacent a producing formation by conventional techniques including, without limitation, wireline, tubing and coiled tubing. In some embodiments, formation stimulation may take the form of one or more of fracturing a target, pristine rock formation and restimulation of an existing producing well.
Stimulation device 100 comprises a housing 102. In some embodiments, the housing 102 may comprise a substantially cylindrical shape (e.g., having a cylindrical cross section). In some embodiments, the housing 102 may be formed from a material such as, for example, a metal (e.g., steel), a metal alloy (e.g., aluminum), a composite, or combinations thereof.
As depicted, the lateral side or sides of the housing 102 may be substantially continuous. For example, the housing 102 may have a continuous (e.g., uniform, monolithic) lateral portion 105 (e.g., a lateral outer surface extending in a direction transverse to (e.g., perpendicular to) and along a longitudinal axis L102 (e.g., centerline) of the housing 102) without any openings formed in the lateral portion 103. In embodiments where the housing 102 has a substantially cylindrical shape, the housing 102 may substantially consist of a barrel forming the lateral portion 103 and two end caps (e.g., first end 124 and second end 126) on either side of the barrel where the barrel has a continuous outer surface without any laterally extending openings formed therein.
An energetic material 104 (e.g., propellant grain) is disposed in the housing 102. The energetic material 104 may fill a majority of the housing 102. For example, the energetic material 104 substantially fills (e.g., entirely fills) one or more cross-sectional areas within the housing 102 taken in a direction transverse to (e.g., perpendicular to) and along the longitudinal axis L102 (e.g., centerline) of the housing 102. In such an embodiment, the one or more cross-sectional areas may be taken proximate (e.g., adjacent) an initiator element, discussed below. In some embodiments, the energetic material 104 may entirely fill the housing 102. In other embodiments, the energetic material 104 may fill a majority of the axial length of the housing 102 with the exception of one or more voids in the energetic material 104 positioned at one or more axial ends (e.g., first end 124 and second end 126) of the of the housing 102. In some embodiments, the energetic material 102 may fill the portion of the housing 102 proximate (e.g., coincident with and surrounding) the longitudinal axis L102 (e.g., centerline) of the housing 102.
In some embodiments, the energetic material 104 may be surrounded (e.g., laterally surrounded) by the housing 102 (e.g., the lateral portion 103 of the housing 102).
An initiator element (e.g., shaped charge 106) may be positioned proximate to the housing 102. For example, the shaped charge 106 may be coupled to (e.g., removably coupled) the housing 102 via a connection between the shaped charge 106 and a portion of the housing 102 (e.g., raised portion 103), such as, for example, threaded connection 108. In other embodiments, the connection between the shaped charge 106 and the housing 102 may comprise other suitable connections (e.g., a connection utilizing fasteners, an interference fit, quick connect/disconnect fittings, etc.). In some embodiments, as discussed below with regard to
The shaped charge 106 may include a case 110, an initiator 112, an explosive material 114, and one or more liners (e.g., a liner 116). In some embodiments, the liner 116 may comprises one or more materials, such as, for example, a metal (e.g., copper), a consolidated powdered metal (e.g., powdered copper, powdered copper and tungsten), a metal alloy (e.g., aluminum), a ceramic, a reactive material (e.g., aluminum/PTFE, nickel/aluminum, zirconium/epoxy, iron oxide/potassium perchlorate/fluropolymer), or combinations thereof.
In some embodiments, the configurations, shapes, and sizes of one or more of the case 110, explosive material 114, and liner 116 may be tailored to produce a desired projectile (e.g., the shape, width, speed, penetration depth, or combinations thereof of the projectile) for a specific application. For example, the case 110 may be formed in a shape such as a generally cylindrical tube or other suitable shapes in order to produce the desired shape of a projectile formed from the liner 116.
At least a portion of the case 110 may be filled with the explosive material 114. The explosive material 114 may be formed within the interior of the case 110 and may comprise an explosive material 114 such as polymer-bonded explosives (“PBX”), LX-14, C-4, OCTOL, trinitrotoluene (“TNT”); cyclo-1,3,5-trimethylene-2,4,6 trinitramine (“RDX”); cyclotetramethylene tetranitramine (“HMX”); hexanitrohexaazaisowurtzitane (“CL 20”); waxed RDX, HMX and/or CL-20; combinations thereof; or any other suitable explosive material. In some embodiments, the explosive material 114 may also be formed to have a countersunk recess in a forward surface of the explosive material 114 to receive the placement of a liner or liners 116.
The case 110 may also include a detonator such as the initiator 112 located, for example, at the rear surface of the case 110. The initiator 112 may comprise any known detonation device sufficient to detonate the explosive material 114 within the case 110 including, but not limited to, explosives such as pentaerythritol tetranitrate (“PETN”), PBXN-5, CH-6, blasting caps, and electronic detonators (e.g., exploding-bridgewire detonators (EBW), exploding foil initiators).
When the explosive material 114 in the shaped charge 106 is detonated by the initiator 112, the liner 116 is formed into a projectile (see, e.g., projectile 120 (
In some embodiments, the shaped charge 106 may be set at a selected standoff distance from the energetic material 104 within the housing 102 of the stimulation device 100. For example, the housing 102 of the stimulation device 100 may include a standoff structure 118 (e.g., a tube) positioned between the shaped charge 106 and the housing 102 to provide a selected distance (e.g., 0.5 inch (12.7 millimeters) to 2.0 inches (50.8 millimeters)) between the shaped charge 106 and the energetic material 104 within the housing 102.
The projectile 120 may travel (e.g., displace) through the energetic material 104 from a first end 124 of the housing 102 (e.g., a first axial end) toward (e.g., to or beyond) a second end 126 (e.g., a second axial end) of the housing 102 opposing the first end 124. In some embodiments, the projectile 120 may travel through the energetic material 104 along the longitudinal axis L102 (e.g., centerline) of the housing 102. It is noted that while the first and second ends 124, 126 of the housing 102 are shown as being substantially planar in
In some embodiments, projectile 120 may penetrate a majority of the length (e.g., the entire length) of the energetic material 104 along the longitudinal axis L102 of the housing 102 (e.g., a length of three feet (91.44 centimeters) or greater). For example, the projectile 120 may penetrate through the energetic material 104 from the first end 124 of the housing 102 to the second end 126. In some embodiments, the projectile 120 may penetrate a majority of the length of the energetic material 104 along the longitudinal axis L102 of the housing 102 (e.g., 80% or more, 90% or more, 95% or more, 100% of the length of the energetic material 104) without penetrating the housing 102 at the second end 126 (e.g., stopping short of the housing 102, contacting the housing 102 without forming an opening through the housing 102 to the exterior of the housing 102). Such an embodiment may enable the majority of the energetic material 104 to be ignited along the length of the energetic material 104 while keeping the housing 102 intact (e.g., sealed) at the second end 126. Further, such an embodiment may enable the use of other stimulation devices proximate (e.g., adjacent) the stimulation device 100 while reducing the probability that the shaped charge 102 will inadvertently penetrate the housing 102 and ignite an adjacent device in the tool string.
The projectile 120 may be in the form of a high velocity jet of hot particles (e.g., a high-energy jet of material of the liner 116). As the projectile 120 travels through the energetic material 104 the high velocity and hot particles of the projectile 120 transfer energy (e.g., via frictional heating) to the energetic material 104 as the projectile 120 penetrates the energetic material 104. The energy transferred to the energetic material 104 by the projectile 120 ignites the energetic material 104. In some embodiments, the pressure wave of the projectile 120 imparted to the energetic material 104 by initiation of the shaped charge 106 may also aid in ignition of the energetic material 104. For example, the high pressures created by ignition of the shaped charge 106 may fracture the energetic material 104 into multiple smaller pieces thereby increasing the surface area of burning energetic material 104, which may enhance gas generation rates.
As the projectile 120 travels through the energetic material 104, the projectile 120 at least partially initiates burn (e.g., deflagration) of the energetic material 104, generating combustion products in the form of high pressure gases. The projectile 120 enables a majority (e.g., an entirety) of the energetic material 104 along the length of the longitudinal axis L102 of the housing 102 to be initiated (e.g., directly initiated with the projectile 120 formed by the shaped charge 106). For example, the projectile 120 may substantially simultaneously (e.g., in less than one hundred microseconds (e.g., ten to one hundred microseconds)) ignite a majority (e.g., an entirety) of the energetic material 104 along the length of the longitudinal axis L102 of the housing 102. The initiated burn may then propagate laterally (e.g., radially, i.e., a substantially radial burn) through the volume of energetic material 104. For example, the propagation of the burn laterally through the volume of energetic material 104 may create a progressive burn where the reacting surface area of the burning energetic material 104 increases over time.
In other embodiments, the number and/or positioning of one or more initiator devices (e.g., shaped charges 106) and configuration of the housing 102 and energetic material 104 therein may be tailored for one or more types of burn. For example, various components of the stimulation device 100 may be selected to produce a progressive burn, neutral burn (where the reacting surface area of the energetic material 104 remains substantially constant over time), regressive burn (when the reacting surface area of the energetic material 104 decreases over time), or combinations thereof upon ignition.
In some embodiments, the housing 102 may be configured such the buildup of pressure within the housing 102 causes at least some of the apertures 128 in the housing 102 to form in a direction along (e.g., substantially parallel to) the length or depth of the borehole in which the stimulation device 100 is to be deployed. For example, the housing 102 may be configured such that the buildup of pressure within the housing 102 causes at least some of the apertures 128 in the housing 102 to form in along the length (e.g., along the longitudinal axis L102) of the housing 102. In embodiments where the stimulation device 100 has a cylindrical cross section, the housing 102 may be configured such that hoop stress in the cylindrical portion (e.g., the lateral portion 103) of the housing 102 forms the apertures 128 extending along the longitudinal axis L102) of the housing 102. In some embodiments, the housing 102 may be tailored to provide one or more apertures 128 at substantially predetermined locations by, for example, varying the wall thickness of the housing 102.
The gas streams 130 may pass through the apertures 128 in the housing 102 in a direction transverse to (e.g., perpendicular to) one or more of the length or depth of the borehole and the length (e.g., along the longitudinal axis L102) of the housing 102. In some embodiments, the stimulation device 100 may be configured to produce gas streams 130 around a substantial majority of the housing uniformly (e.g., 360° about the length of one or more of the borehole and of the housing 102), or directionally, such as, for example, in a 45° arc, a 90° arc, etc., transverse to (e.g., perpendicular to) one or more of the length or depth of the borehole and the length of the housing 102.
In embodiments of the present disclosure, propellant type, amount and burn rate may be adjusted to accommodate different geological conditions and provide different pressures and different pressure rise rates for maximum benefit. For example, the energetic material 104 may comprise ballistically-tailored propellant structures comprising two or more propellant grain that are formulated and configured to provide, for example, customizable burn types and rates, such as those disclosed in U.S. patent application Ser. No. 13/781,217 to Arrell Jr. et al., entitled “Method and Apparatus for Ballistic Tailoring of Propellant Structures and Operation Thereof for Downhole Stimulation,” the disclosure of which is incorporated herein in its entirety by this reference.
One or more energetic materials (e.g., propellants) suitable for implementation of embodiments of the present disclosure may include, without limitation, a material used as a solid rocket motor propellant, such as, for example, a propellant comprising a powdered metal fuel. Various examples of such energetic material and components thereof are described in Thakre et al., Solid Propellants, Rocket Propulsion, Volume 2, Encyclopedia of Aerospace Engineering, John Wiley & Sons, Ltd. 2010, the disclosure of which document is incorporated herein in its entirety by reference. The energetic material may be a class 4.1, 1.4 or 1.3 material, as defined by the United States Department of Transportation shipping classification, so that transportation restrictions are minimized. By way of example, the energetic material may include a polymer having at least one of a fuel and an oxidizer incorporated therein. The polymer may be an energetic polymer or a non-energetic polymer, such as glycidyl nitrate (GLYN), nitratomethylmethyloxetane (NMMO), glycidyl azide (GAP), diethyleneglycol triethyleneglycol nitraminodiacetic acid terpolymer (9DT-NIDA), bis(azidomethyl)-oxetane (BAMO), azidomethylmethyl-oxetane (AMMO), nitraminomethyl methyloxetane (NAMMO), bis(difluoroaminomethyl)oxetane (BFMO), difluoroaminomethylmethyloxetane (DFMO), copolymers thereof, cellulose acetate, cellulose acetate butyrate (CAB), nitrocellulose, polyamide (nylon), polyester, polyethylene, polypropylene, polystyrene, polycarbonate, a polyacrylate, a wax, a hydroxyl-terminated polybutadiene (HTPB), a hydroxyl-terminated poly-ether (HTPE), carboxyl-terminated polybutadiene (CTPB) and carboxyl-terminated polyether (CTPE), diaminoazoxy furazan (DAAF), 2,6-bis(picrylamino)-3,5-dinitropyridine (PYX), a polybutadiene acrylonitrile/acrylic acid copolymer binder (PBAN), polyvinyl chloride (PVC), ethylmethacrylate, acrylonitrile-butadiene-styrene (ABS), a fluoropolymer, polyvinyl alcohol (PVA), or combinations thereof. The polymer may function as a binder, within which the at least one of the fuel and oxidizer is dispersed. In one embodiment, the polymer is polyvinyl chloride.
The fuel may be a metal (e.g., a consolidated powdered metal), such as aluminum, nickel, magnesium, silicon, boron, beryllium, zirconium, hafnium, zinc, tungsten, molybdenum, copper, or titanium, or alloys mixtures or compounds thereof, such as aluminum hydride (AlH3), magnesium hydride (MgH2), or borane compounds (BH3). The metal may be used in powder form. In one embodiment, the metal is aluminum. The oxidizer may be an inorganic perchlorate, such as ammonium perchlorate or potassium perchlorate, or an inorganic nitrate, such as ammonium nitrate, sodium nitrate, or potassium nitrate. Other oxidizers may also be used, such as hydroxylammonium nitrate (HAN), ammonium dinitramide (ADN), hydrazinium nitroformate, a nitramine, such as cyclotetramethylene tetranitramine (HMX), cyclotrimethylene trinitramine (RDX), 2,4,6,8,10,12-hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane (CL-20 or HNIW), and/or 4,10-dinitro-2,6,8,12-tetraoxa-4,10-diazatetracyclo-[5.5.0.05,9.03,11]-dodecane (TEX). In one embodiment, the oxidizer is ammonium perchlorate. The energetic material may include additional components, such as at least one of a plasticizer, a bonding agent, a burn rate modifier, a ballistic modifier, a cure catalyst, an antioxidant, and a pot life extender, depending on the desired properties of the energetic material. These additional components are well known in the rocket motor art and, therefore, are not described in detail herein. The components of the energetic material may be combined by conventional techniques, which are not described in detail herein.
Energetic material for implementation of embodiments of the present disclosure may be selected to exhibit, for example, burn rates from about 0.1 in/sec (2.54 millimeters/sec) to about 4.0 in/sec (101.6 millimeters/sec) at 1,000 psi (6894.8 kilopascals) and an ambient temperature of about 70° F. (21.1° C.). Burn rates will vary, as known to those of ordinary skill in the art, with variance from the above pressure and temperature conditions before and during the energetic material burn.
The energetic material may be cast, extruded or machined from an energetic material formulation. Casting, extrusion and machining of energetic material formulations are each well known in the art and, therefore, are not described in detail herein.
In some embodiments, the cavity 207 (e.g., the centerline of the cavity 207) may be coextensive with the longitudinal axis L202 (e.g., centerline) of the housing 202.
In some embodiments, the cavity 207 may only extend through a minor portion of the energetic material 204 in the housing 202 along the longitudinal axis L202 of the housing 202.
In some embodiments, the shaped charge 206 may include a cap 210. The cap 210 may surround a portion of the housing 202 (e.g., raised lip 203) and the connection 208 between the shaped charge 206 and the housing 202 may be formed within the cap 210.
As above, in some embodiments, the shaped charge 206 may be set at a selected standoff from the energetic material 204 within the housing 202 of the stimulation device 200. For example, the housing 202 of the stimulation device 200 may include a standoff 218 (e.g., a tube) positioned between the shaped charge 206 and the housing 202 to provide a selected distance (e.g., 0.5 inch (12.7 millimeters) to 2.0 inches (50.8 millimeters)) between the shaped charge 206 and the energetic material 204 within the housing 202.
Embodiments of the present disclosure may provide stimulation devices that are more robust and effective than other similar stimulation devices. For example, stimulation devices in accordance with some embodiments of the present disclosure enable energetic material to fill the majority or entirety of the housing of the stimulation devices as opposed to stimulation devices that require a central bore formed through the energetic material to accommodate an initiator such as a detonation cord or small rocket igniter. Moreover, elimination of the central bore in some embodiments may reduce the cost and time required to manufacture the stimulation device. Embodiments of the disclosure thus enable deployment of a larger volume of energetic material in a stimulation tool of a given interior volume in comparison to conventional designs. For example, in some embodiments, the maximum amount of propellant capable of filing the housing may be used.
Further, a stimulation device employing an initiator device such as a shaped charge enables relatively faster and substantially simultaneous (i.e., within microseconds) ignition of the energetic material in the housing along a majority of or an entirety of the length of a stimulation tool as compared to conventional propellant initiators. Such a configuration enables a majority of the energetic material to be ignited along its length without rupturing and depressurizing the housing in the axial direction. Additionally, a stimulation device employing an initiator device such as a shaped charge may enable the production of a desired pressure within a desired time domain relatively faster than other conventional downhole stimulation devices employing an initiator such as a detonation cord.
For example, the stimulation device employing an initiator device such as a shaped charge may enable ignition of the energetic material in the housing in a similar time scale as the high explosives (e.g., approximately ten to one hundred microseconds) employed in conventional stimulation devices. Such a time scale may be beneficial when the stimulation device (e.g., a deflagrating stimulation device) is employed in a drill string with other stimulation devices employing high explosives such that the ignition and/or initial release of energy from the deflagrating stimulation device using an energetic material such as a propellant occurs substantially simultaneously as the detonation of the high explosive stimulation devices (e.g., immediately following the fracturing initially caused by the high explosives). In such a configuration, the formation proximate the borehole may be fractured a selected distance with one or more high explosive stimulation devices immediately followed (e.g., within microseconds) by additional opening of the fractures by one or more deflagrating stimulation devices.
Further, the stimulation device employing an initiator device such as a shaped charge may enable a relatively more reliable and effective ignition of the energetic material within the stimulation device as compared to conventional stimulation devices. For example, the projectile or jet formed by the shaped charge may enable enhanced ignition of the energetic material through one or both of frictional heating and through pressurization of the housing caused by initiation of the shaped charge. Such enhanced ignition may enable pressure to build relatively faster in the housing. Further, in embodiments where pressure within the housing deforms the housing to form an aperture therein (e.g., when the housing lacks initial, preformed apertures) the housing may allow greater pressure to build therein as compared to conventional stimulation devices including initial, preformed apertures. Such building pressure may further enhance ignition and increase the rate of burn of the energetic material as the pressure increases within the initially sealed housing.
Finally, a stimulation device employing a removable shaped charge enables the entire initiator device to be separated from the energetic material in the housing providing an explosive safe and arm (S&A) feature enabling safe handling and/or transportation of the stimulation device and facilitating compliance with government regulations relating to such transport, particularly air transport to offshore well sites.
While particular embodiments of the disclosure have been shown and described, numerous variations and alternate embodiments encompassed by the present disclosure will occur to those skilled in the art. Accordingly, the disclosure is only limited in scope by the appended claims and their legal equivalents.
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