This application claims the benefit under 35 U.S.C. ยง119 of the filing date of International Application No. PCT/US2013/040296, filed May 9, 2013.
This invention relates, in general, to equipment utilized and operations performed in conjunction with completing a subterranean well for hydrocarbon fluid production and, in particular, to a shaped charge perforating gun apparatus for generating perforations having variable penetration profiles.
Without limiting the scope of the present invention, its background will be described with reference to perforating a hydrocarbon bearing subterranean formation with a shaped charge perforating gun apparatus, as an example. After drilling a section of a subterranean wellbore that traverses a hydrocarbon bearing subterranean formation, individual lengths of metal tubulars are typically secured together to form a casing string that is positioned within the wellbore. This casing string increases the integrity of the wellbore and provides a path through which fluids from the formation may be produced to the surface. Conventionally, the casing string is cemented within the wellbore. To produce fluids into the casing string or to place addition cement behind the casing string, hydraulic openings or perforations must be made through the casing string and a distance into the formation.
Typically, these perforations are created by detonating a series of shaped charges located within one or more perforating guns that are deployed within the casing string to a position adjacent to the desired location. Conventionally, the perforating guns are formed from a closed, fluid-tight hollow carrier gun body adapted to be lowered into the wellbore on a conveyance such as wireline, coiled tubing, jointed tubing or the like. Disposed within the hollow carrier gun body is a charge holder that supports and positions the shaped charges in a selected spatial distribution. The shaped charges have conically constrained explosive material therein. A detonating cord that is used to detonate the shaped charges is positioned adjacent to the initiation ends of the shaped charges. The detonating cord can be activated electronically or mechanically when it is desired to firing the perforating guns.
In such closed, fluid-tight type gun bodies, the explosive jets produced upon detonation of the shaped charges must penetrate the hollow carrier gun body before penetrating the casing wall of the wellbore and the adjacent formation. To reduce the resistance produced by the hollow carrier gun body and increase the depth of perforation penetration into the formation, the perforating gun body may be provided with scallops or other radially reduced sections at the target regions through which the explosive jets pass. As such, the scallops in the hollow carrier gun body must be positioned in a spatial distribution that aligns with or corresponds to the spatial distribution of the shaped charges held within the gun body by the charge holder.
Once the perforating guns are deployed to the desired location, firing a conventional perforating gun results in perforations into the formation having substantially the same depth and entry hole dimensions. It has been found, however, that in certain operations, it may be desirable to generate perforations that do not have substantially the same depth and entry hole dimensions. A need has therefore arisen for a perforating gun apparatus that is operable to generate perforations having variable penetration profiles.
The present invention disclosed herein comprises a perforating gun apparatus operable to form perforations through the casing string and a distance into the formation. The perforating apparatus of the present invention is also operable to generate perforations having variable penetration profiles.
In one aspect, the present invention is directed to a perforating gun apparatus. The perforating gun apparatus includes a carrier gun body having a plurality of jet target regions. A first set of the jet target regions has a first resistance to jet penetration and a second set of the jet target regions has a second resistance to jet penetration. A charge holder is positioned within the carrier gun body. A plurality of shaped charges is supported by the charge holder. A first set of shaped charges is oriented to have discharge ends aligned with the first set of the jet target regions and a second set of shaped charges is oriented to have discharge ends aligned with the second set of the jet target regions such that firing the first set of shaped charges creates perforations having a first penetration profile and firing the second set of shaped charges creates perforations having a second penetration profile that is different from the first penetration profile.
In one embodiment, the first set of the jet target regions may have recesses of a first depth and the second set of the jet target regions may have recesses of a second depth. In this embodiment, the first depth may be at least 25 percent greater than the second depth. Alternatively, the first depth may be at least 50 percent greater than the second depth. In another embodiment, the first set of the jet target regions may have recesses including an insert of a first thickness and the second set of the jet target regions may have recesses including an insert of a second thickness. In this embodiment, the first thickness may be at least 50 percent greater than the second thickness. Alternatively, the first thickness may be at least 100 percent greater than the second thickness.
In a further embodiment, the first set of the jet target regions may have recesses including an insert of a first material and the second set of the jet target regions may have recesses including an insert of a second material. In this embodiment, the first material and the second material may be selected from the group consisting of ceramics, carbides, titanium and iron based alloys. The alloying constituents of the iron based alloys may be selected from the group consisting of boron, carbon, chromium, manganese, molybdenum, nickel, niobium, silicon, tungsten and vanadium. In the embodiments including inserts, the inserts may be coupled to the carrier gun body by a process selected from the group consisting of threading, brazing, adhering, thermal spraying and welding. In certain embodiments, the first penetration profile may include perforations having a greater depth than the second penetration profile. In other embodiments, the first penetration profile may include perforations having a greater entry hole diameter than the second penetration profile.
In another aspect, the present invention is directed to a perforating gun apparatus. The perforating gun apparatus includes a carrier gun body having a plurality of jet target regions. A first set of the jet target regions has recesses of a first depth that provide a first resistance to jet penetration and a second set of the jet target regions has recesses of a second depth that provide a second resistance to jet penetration. A charge holder is positioned within the carrier gun body. A plurality of shaped charges is supported by the charge holder. A first set of shaped charges is oriented to have discharge ends aligned with the first set of the jet target regions and a second set of shaped charges is oriented to have discharge ends aligned with the second set of the jet target regions such that firing the first set of shaped charges creates perforations having a first penetration profile and firing the second set of shaped charges creates perforations having a second penetration profile that is different from the first penetration profile.
In a further aspect, the present invention is directed to a perforating gun apparatus. The perforating gun apparatus includes a carrier gun body having a plurality of jet target regions. A first set of the jet target regions has recesses including an insert of a first thickness providing a first resistance to jet penetration and a second set of the jet target regions has recesses including an insert of a second thickness providing a second resistance to jet penetration. A charge holder is positioned within the carrier gun body. A plurality of shaped charges is supported by the charge holder. A first set of shaped charges is oriented to have discharge ends aligned with the first set of the jet target regions and a second set of shaped charges is oriented to have discharge ends aligned with the second set of the jet target regions such that firing the first set of shaped charges creates perforations having a first penetration profile and firing the second set of shaped charges creates perforations having a second penetration profile that is different from the first penetration profile.
In a yet another aspect, the present invention is directed to a perforating gun apparatus. The perforating gun apparatus includes a carrier gun body having a plurality of jet target regions. A first set of the jet target regions has recesses including an insert of a first material providing a first resistance to jet penetration and a second set of the jet target regions has recesses including an insert of a second material providing a second resistance to jet penetration. A charge holder is positioned within the carrier gun body. A plurality of shaped charges is supported by the charge holder. A first set of shaped charges is oriented to have discharge ends aligned with the first set of the jet target regions and a second set of shaped charges is oriented to have discharge ends aligned with the second set of the jet target regions such that firing the first set of shaped charges creates perforations having a first penetration profile and firing the second set of shaped charges creates perforations having a second penetration profile that is different from the first penetration profile.
For a more complete understanding of the features and advantages of the present invention, reference is now made to the detailed description of the invention along with the accompanying figures in which corresponding numerals in the different figures refer to corresponding parts and in which:
While the making and using of various embodiments of the present invention are discussed in detail below, it should be appreciated that the present invention provides many applicable inventive concepts, which can be embodied in a wide variety of specific contexts. The specific embodiments discussed herein are merely illustrative of specific ways to make and use the invention, and do not delimit the scope of the present invention.
Referring initially to
A wellbore 32 extends through the various earth strata including formation 14. A casing 34 is cemented within wellbore 32 by cement 36. Work string 30 includes various tools including shaped charge perforating gun apparatus 38 that is operable to generate perforations having variable penetration profiles. When it is desired to perforate the wellbore proximate formation 14, work string 30 is lowered through casing 34 until shaped charge perforating gun apparatus 38 is positioned adjacent to formation 14. Thereafter, shaped charge perforating gun apparatus 38 is fired such that the shaped charges form high speed jets that penetrate jet target regions of a carrier gun body 40 of perforating gun apparatus 38. In the illustrated embodiment, a first set of the jet target regions 42 has a first resistance to jet penetration and a second set of the jet target regions 44 has a second resistance to jet penetration. A first set of shaped charges is oriented to have discharge ends aligned with the first set of the jet target regions 42 and a second set of shaped charges is oriented to have discharge ends aligned with the second set of the jet target regions 44 such that firing the first set of shaped charges creates perforations 46 having a first penetration profile and firing the second set of shaped charges creates perforations 48 having a second penetration profile that is different from the first penetration profile. In the illustrated embodiment, perforations 46 having the first penetration profile are depicted as deep perforations having relatively narrow perforation tunnels and having relatively small entry hole diameters. Perforations 48 having the second penetration profile are depicted as shallow perforations having relatively wide perforation tunnels and having relatively large entry hole diameters. As such, upon detonation, the liners of the shaped charges form jets that pass through target regions 42, 44, casing 34, cement 36 and a depth into formation 14 forming perforations 46, 48 having variable penetration profiles.
Even though
Referring now to
The shaped charges 56 are retained within carrier gun body 52 by a charge holder 62 which, in the illustrated embodiment, includes an outer charge holder sleeve 64 and an inner charge holder sleeve 66. In this configuration, outer tube 64 supports the discharge ends of shaped charges 56, while inner tube 66 supports the initiation ends of shaped charges 56. Disposed within inner tube 66 is a detonator cord 70, such as a Primacord, which is used to detonate shaped charges 56. In the illustrated embodiment, the initiation ends of shaped charges 56 extend across the central longitudinal axis of perforating apparatus 50 allowing detonator cord 70 to connect to the high explosive within shaped charges 56 through an aperture defined at the apex of the housings of shaped charges 56.
Each of the shaped charges 56 is longitudinally and radially aligned with one of the recesses 54 in carrier gun body 52 when perforating apparatus 50 is fully assembled. In the illustrated embodiment, shaped charges 56 are arranged in a spiral pattern such that each shaped charge 56 is disposed on its own level or height. It should be understood by those skilled in the art, however, that alternate arrangements of shaped charges may be used, including cluster type designs wherein more than one shaped charge is at the same level, without departing from the principles of the present invention. As discussed below, various set of the recesses 54 of perforating gun apparatus 50 have different characteristics enabling substantially identical shaped charges 56 to create variable penetration profiles upon detonation. For example, in the illustrated embodiment, shaped charges 56 in an upper set of seven are each aligned with recesses 72 having a first depth (one being visible in
Due to the different depths of recesses 72, 74, 76, a different resistance through carrier gun body 52 is experienced by the various sets of shaped charges 56, respectively aligned with recesses 72, 74, 76. Due to the different resistance, shaped charges 56 aligned with recesses 72 will create different penetration profiles upon detonation than shaped charges 56 aligned with recesses 74. Likewise, shaped charges 56 aligned with recesses 74 will create different penetration profiles upon detonation than shaped charges 56 aligned with recesses 76. In addition, shaped charges 56 aligned with recesses 72 will create different penetration profiles upon detonation than shaped charges 56 aligned with recesses 76. For example, as shaped charges 56 aligned with recesses 72 encounter the thinnest target region, the perforations created therefrom will penetrate the greatest depth into the formation. Similarly, as shaped charges 56 aligned with recesses 74 encounter a thicker target region, the perforations created therefrom will penetrate to a lesser depth into the formation. Further, as shaped charges 56 aligned with recesses 76 encounter the thickest target region, the perforations created therefrom will penetrate the least depth into the formation. As such, perforating gun apparatus 50 of the present invention is operable to generate perforations having variable penetration profiles.
Referring now to
For example, as the shaped charges aligned with wall sections 108 encounter the thinnest target region, the perforations created therefrom will penetrate the greatest depth into the formation. Similarly, as the shaped charges aligned with wall sections 110 encounter a thicker target region, the perforations created therefrom will penetrate to a lesser depth into the formation. Further, as the shaped charges aligned with wall sections 112 encounter the thickest target region, the perforations created therefrom will penetrate the least depth into the formation. As such, perforating gun apparatus 100 of the present invention is operable to generate perforations having variable penetration profiles. As depicted in
Even though recesses 102, 104, 106 of carrier gun body 100 have been depicted and described as having particular depths and particular depths compared to one another, it should be understood by those skilled in the art that recesses having other depths and other depths compared to other recesses are possible and are considered to be within the scope of the present invention. For example, certain recesses in a carrier gun body 100 of the present invention may be described as having a first depth while other recesses in a carrier gun body 100 of the present invention may be described as having a second depth. Using this nomenclature, the depth comparison of the first depth to the second depth may be greater than 10 percent, greater than 25 percent, greater than 50 percent, greater than 100 percent, greater than 200 percent, greater than 400 percent and the like. What is important is that the difference in the depth of the recesses creates a difference in the resistance experienced by the jets created upon detonation of shaped charges aligned therewith, which results in different penetration profiles. Even though
Referring now to
In certain embodiments, the carrier gun body 120 may be formed from conventional steel. Inserts 128, 130 may be formed from any suitable material such as a ceramic material, a carbide material, a metal such as conventional steel, tool steel, titanium or an iron based alloy such as an iron alloyed with one or more alloying constituents selected from the group consisting of boron, carbon, chromium, iron, manganese, molybdenum, nickel, niobium, silicon, tungsten and vanadium. In one example, the weight percents of the alloying constituents are between about 0% and 4% boron, between about 0.1% and 8% carbon, between about 0.5% and 21% chromium, between about 55% and 95% iron, between about 0% and 3% manganese, between about 0.5% and 8% molybdenum, between about 0% and 5% nickel, between about 0% and 4% niobium, between about 0% and 2% silicon, between about 0% and 7% tungsten and between about 0% and 4% vanadium. In certain embodiments, inserts 128, 130 may be formed from a nanostructured material having nanosized features such as nanograined iron alloys including nanograined steels. As used herein, a nanostructured material will include materials having features from 1 to 500 nanometers and more preferably materials having features from 1 to 100 nanometers. Inserts 128, 130 may be coupled to carrier gun body 120 in any suitable manner including threading, brazing, adhering, thermal spraying, welding and the like.
Even though inserts 128, 130 have been depicted and described as having a particular thickness and a particular thickness compared to one another, it should be understood by those skilled in the art that inserts having other thicknesses and other thicknesses compared to other inserts are possible and are considered to be within the scope of the present invention. For example, certain inserts in a carrier gun body 120 of the present invention may be described as having a first thickness while other inserts in a carrier gun body 120 of the present invention may be described as having a second thickness. Using this nomenclature, the thickness comparison of the first thickness to the second thickness may be greater than 10 percent, greater than 25 percent, greater than 50 percent, greater than 100 percent, greater than 200 percent, greater than 400 percent and the like. What is important is that the difference in the thickness of the inserts creates a difference in the resistance experienced by the jets created upon detonation of shaped charges aligned therewith, which results in different penetration profiles.
Referring now to
Similar to inserts 128, 130 described above, inserts 148, 150, 152, 154 may be formed from any suitable material such as a ceramic material, a carbide material, a metal such as tool steel, titanium or an iron based alloy such as an iron alloyed with one or more alloying constituents selected from the group consisting of boron, carbon, chromium, iron, manganese, molybdenum, nickel, niobium, silicon, tungsten and vanadium. Also, as with inserts 128, 130 above, inserts 148, 150, 152, 154 may be coupled to carrier gun body 140 in any suitable manner including threading, brazing, adhering, thermal spraying, welding and the like.
Even though inserts 152, 154 and the combination of inserts 148, 150, have been depicted and described as having particular thicknesses and having particular thicknesses compared to one another, it should be understood by those skilled in the art that inserts having other thicknesses and other thicknesses compared to other inserts are possible and are considered to be within the scope of the present invention. What is important is that the difference in the materials of the inserts creates a difference in the resistance experienced by the jets created upon detonation of shaped charges aligned therewith, which results in different penetration profiles.
While this invention has been described with reference to illustrative embodiments, this description is not intended to be construed in a limiting sense. Various modifications and combinations of the illustrative embodiments as well as other embodiments of the invention will be apparent to persons skilled in the art upon reference to the description. It is, therefore, intended that the appended claims encompass any such modifications or embodiments.
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Number | Date | Country | |
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20140331852 A1 | Nov 2014 | US |