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US3054938A - Means and mode for depositing material by jet perforation - Google Patents

Means and mode for depositing material by jet perforation
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US3054938A
US3054938AUS854217AUS85421759AUS3054938AUS 3054938 AUS3054938 AUS 3054938AUS 854217 AUS854217 AUS 854217AUS 85421759 AUS85421759 AUS 85421759AUS 3054938 AUS3054938 AUS 3054938A
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jet
formation
charge
opening
explosive
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US854217A
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Lorrain D Meddick
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Dresser Industries Inc
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Dresser Industries Inc
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Sept. 18, 1962 l., D. MEDDICK MEANS AND MODE FOR DEPOSITING MATERIAL BY JET PERFORATION Original Filed June 5, 1956 2 Sheets-Sheet 1 an .l L.
0Q2/WN /t/E/CK INVENTOR.
.2 Yum BY a Sept. 18, 1962 L. D. MEDDICK MEANS .AND MODE FOR DEPOSITING MATERIAL BY JET PERFORATION Original Filed June 5, 1956 2 Sheets-Sheet 2 3 054,938 MEANS AND MODE FR DEPUSYHNG MATERIAL BY JET PERFRATIN Lorrain D. Meddicir, Houston, Tex., assigner to Dresser Industries, line., Dalias, Tex., a corporation of Delaware .Continuation of application Ser. No. 539,421, .lune 5, 1956. This application Nov. 9, 1959, Ser. No. 854,217 3 Ciaims. (Cl. 102-20) The present invention relates generally to well casing perforating, and particularly to a novel means and mode for introducing into an earth formation encircling a cased earth well, through the casing encircling cement, a corrosion-inducing or acidizing substance concurrently with perforation of the casing and formation of a hole or opening into the encircling earth formation. More specifically, the invention relates to a mode and means for concurrently perforating in situ a cemented well casing and depositing in the encircling earth formation a corrosioninducing substance or component thereof, through detonation of a suitably fabricated or compounded specially shaped charge of high explosive.
This application is a continuation of the copending application of Lorrain D. Meddick7 Serial No. 589,421 led June 5, 1956, now abandoned, for Means and Mode for Depositing Materials by let Perforation.
It is known in the prior art to perforate in situ cemented well casings my means including suitably shaped and positioned charges of highly explosive material. Such operations are conventionally termed shaped-charge perforating and involve the detonation of a suitably positioned explosive charge having a suitably formed depression or concavity therein, and which, when detonated, produces a high-velocity stream or jet of material capable of piercing steel well casing, cement and earth formation. It has been discovered that the earth formation thus breached by a high-velocity jet may be penetrated to a considerable distance beyond that region within which connate fluids may, and actually do, readily ow from the formation into the hole produced by the jet. The remainder of the penetrated extent of earth formation while actually of the general shape of a tapered hole, is sometimes found to be filled with semi-compacted formation material or debris which greatly impedes drainage of connate fluid into the produced hole. Since the primary purpose of perforating the casing and forming a hole extending into the encircling earth formation is to permit ready access of connate fluids into the well casing, it is desirable that the hole formed by the jet be free and open throughout its entire extent. The present invention aims to provide a mode and means whereby this plugging effect in the most distant reaches of the produced hole is greatly reduced and the compacted material there deposited is rendered loose, whereby flow of connate fluid into the well casing is greatly facilitated.
The principal aim of the invention is accomplished by incorporating in the material composing the jet which pierces the well casing and encircling formation, one or more substances which when deposited in the produced hole will produce an acidizing or other corrosive effect, either alone or in combination with connate or introduced lluids. The corrosion-inducing or acidizing material or substance has the eifect of softening, dissolving or loosening the cementing material by which the dis- 3,054,938 Patented Sept. 18, 1,962
crete particles of material compacted together in the outer reaches of the produced hole are held together. The freeing or loosening elfect thus produced in the outer end of the opening breached into the earth formation is operationally the equivalent of producing an opening of much greater effective depth. The corrosion-inducing or acidizing material to be deposited is carried into the opening substantially concurrently or simultaneously with the production of the opening by the high velocity jet or by the after jet. The substance to be thus deposited may comprise one or more liquid components and/ or one or more solid or granular components, which, when deposited in the opening or hole, either alone or in combination with fluids there present, or with each other, produce the desired loosening of the grain structureI of the plug in the end of the hole. The substances to lbe thus introduced into the hole substantially concurrently with its formation are, according to the invention, so disposed with relation to the substances producing and comprised in the jet as to be incorporated in the latter in one or the other of several related ways. These modes and the requisite structures for carrying them out will hereinafter be more fully explained.
As constructed heretofore, shaped charge casing-perforating devices have generally included a metallic shell or cone-like liner of copper or other similar metal or alloy nested in the depression or concavity of the explosive charge, the purpose of which shell or liner is to aid the high-Velocity jet to pierce or penetrate any nearby object in its path. It has been determined experimentally that in many instances a portion of this metallic shell is lodged within the opening produced in the well casing and formation, thus forming an obstruction impeding the ow of fluids into the well. The relative positioning and general shape of such a carrot or obstruction may Vary but is often such as to form a tightly litting plug. It is a subsidiary aim of the present invention to provide means whereby such obstruction or carrot is not produced, or if produced is soon corroded and thus removed from the opening in the casing or at least loosened to the extent of minimizing its impedance to fluid How.
ln view of the preceding stated considerations it is a primary object of the present invention to provide apparatus for producing a perforation in an earth well casing and concurrently therewith producing and acidizing a fluid-draining hole in the adjacent earth formation. lt is another object of the invention to provide means whereby a greater effective depth of penetration into an earth formation may be elfected with shaped charge explosive means.
Another object of the invention is to provide a mode for producing an earth-penetrating opening of greater effective depth outwardy through a cemented well casing.
Another object of the invention is the provision of means for enhancing the results secured by earth well casing perforating by shaped charge explosive means.
The preceding and other objects and advantages of the invention which will hereinafter be made more fully apparent are accomplished by the mode of the invention as practiced with apparatus according to the concepts thereof, a preferred form of which apparatus and modifications thereof is depicted in the several views of the accompanying drawings.
In the drawings:
FIGURE l is a diagrammatic view, partly in longitudinal section, of a portion of an earth well borehole which has been cased and cemented, the well borehole extending through a plurality of earth formations; and showing means according to the invention suspended in the borehole;
FIGURE 2 is a longitudinal view in vertical section through a portion of cased earth borehole in which is situated apparatus according to the present invention, and illustrating one shaped charge device positioned for operation and showing the effect produced by previous detonation of a similar device;
FIGURE 3 is a fragmentary view in sectional elevation to an enlarged scale of a portion of cased earth well borehole with the casing perforated and formation breached by a shaped charge explosive device; and
FIGURES 4 through 10 are longitudinal views in section through respective shaped charge devices having structural arrangements according to the present invention.
Referring now to the drawings and to FIGURE 1 in particular, there is shown an earth borehole penetratin-g earth formations 12, 14 and 16, the borehole having been cased with aconventional well casing 18 cemented in place along a portion of its length or extent bycement 20 suitably introduced into the annular space between the exterior of thecasing 18 and the borehole wall. The casing or borehole, as is conventional, may be substantially lled with fluid, or either or both may be unoccupied except for gases. Shown suspended at a desired location in the cased borehole by means of an electricconductor suspending cable 22, is a wellcasing perforating apparatus 24 hereinafter more fully described. The suspendingcable 22 may extend over aguide sheave 26 and be wound upon or unwound from conventional hoist drum means (not shown).Perforating apparatus 24 comprises acable head 24h in which theelectric cable conductor 22 is terminated, and the head may comprise or be terminated at its lower end by means for detonating a length of primacord by electric current conducted thereto throughcable 22. The perforating apparatus comprises atubular body section 24h connected in known manner tocable head 24h, and terminated at its lower end by a conventional bull plug 24s. This much of the apparatus, with the exception of shaped charge devices supported inbody section 24, may be conventional and is well known in the art, and will not hereinafter be more fully described.
Referring now to FIGURE 2, in which is depicted partially in sections, portions of perforatingapparatus 24 and fragmentary portions of a well casing and cement and adjacent earth formation, one unexploded shape charge `device 30 is shown in position for detonation. A hole 16a is shown, formed in the adjacent earth formation by detonation of a similar shaped charge device previously located as indicated in dotted outline. 'Ihe unexploded shaped charge device shown generally at 30` comprises an outer rigid body orshell 30s fitting in aninternal recess 24r formed in body 24b, and a charge aligner 30a iitting in a port opposed torecess 24r and adapted to maintain theshell 30s in proper position in body 24b. The shaped charge device also comprises a charge of explosive 30e suitably secured inshell 30s, and additional and unconventional means hereinafter more fully described. Suitably threaded in a transverse bore through the reduceddiameter base ofshell 30s is a length ofdetonable fuse 32 such as primacord, which extends to and is adapted to be detonated by conventional fuse-detonating means in or immediately belowcable head 24h, all as is well known in this art. Positioned in close proximity to thedetonable fuse 32 in the base ofshell 30s is a booster charge Stlb of high explosive adapted to be detonated by action offuse 32 and adapted in turn to detonate the explosive 30e comi prised in the specially shaped unit contained in the body ofshell 30s.
According to the concept of the present invention, the interior elements housed withinshell 30s may be constructed and arranged in a variety of different forms several of which are shown in longitudinal cross-section in FIGURES 4 through 9, whileshell 30s andaligner 30a may be as shown or of conventional form. The structure within shell 343s is so constructed and arranged as to provide, when detonated, a jet comprising one or more substances which, either alone or in combination with connate fluid and/or each other, will aid in deeper effective penetration of the formation by weighting the jet and/ or by inducing corrosion in the produced opening formed by the jet. Preferably the device is so constructed `and arranged that when detonated there is carried into the -produced opening with the jet one or more acidizing or corrosion-inducing elements or substances the penetration and corrosive effect being preferably aided by introducing into the jet a heavy substance of proper characteristics, such as, for example, mercury.
Referring now to FIGURE 4, the principal components of one type of shaped charge device according to the present invention, with the charge aligner removed, is shown in section.Shell 30s houses or includes thebooster charge 30b adjacent which a detonable fuse 32 (such as primacord) extends through a transverse bore in the base of the shell, as shown or as in conventional shaped charge construction. Also included inshell 30s is acharge 30e of high explosive having, at its face opposed to the booster charge 30h, a depression or concavity formed therein which is preferably of generally conical form, as indicated. Nested in theshell 30s and preferably but not necessarily in contact with theexplosive charge 30e, is a conical liner 301? of suitable metal such as copper, as is conventional practice. In certain forms of shaped charge devices -according to the present invention, this metallic liner 301? may be dispensed with or a substitute of a type hereinafter more fully explained may be employed. As is well known in the shaped charge devices arts, detonation of thecharge 30e at its base by booster charge 3017 results in creation of a high velocity detonation wave in the shapedexplosive charge 30e which proceeds generally forward through the charge and which, upon reaching the apex ofliner 30t, causes a forwardly progressing disintegration of the liner with possible partial vaporizing of the liner material resulting in the formation of a forwardly-directed, high velocity jet of gases and particulated and vaporized liner material. As is well known, such jet is capable of piercing a considerable thickness of steel or other resistant material.
In accordance with the concepts of the present invention there is included within the body member orshell 30s for transportation by and with the high-velocity jet produced by the explosive, one or more materials which, when transported into the opening produced by the jet, will produce a corroding effect such as, for example, an acidizing effect, in the opening. In the embodiment of apparatus depicted in section in FIGURE 4, there is incorporated inshell 30s in close proximity to cone-like liner 30t, a conelike hollow `sealedcapsule 34a in the interior of which is contained one or more ingredients designed to produce the corroding effect when injected into the produced opening. The material contained incapsule 34a may be an acid, or may be a material in granular or like form which, upon contact with fluid in the produced opening, will combine therewith to produce an acid or corrosive substance.Capsule 34a is made of material suitable to the purpose, and may be, for example, of glass, synthetic rubber, or the like, where the contained material is a free acid. Preferably the material of whichcapsule 34a is constructed is one which will be vaporized or substantially completely particulated by the explosion, and will be such as not to add materially to a cementing action of displaced particles of the formation pierced. It is evident that the material contained incapsule 34a will in large measure be picked up and incorporated in finely divided form into the produced jet and thereby injected into and through the openings produced in the casing and encircling cement, and carried into and deposited in the far reaches of the opening breached into the formation. The thus deposited material dissolves or otherwise weaken-s or destroys the cementing substances holding the grains of the formation material together. An important subsidiary effect of the material thus deposited in the breached hole or opening is that of corroding or dissolving any so-called carrot particles or other fragments of the shaped charge device which may `be lodged in the opening in the casing or formation and thus obstruct the :free ilow of fluids from the formation into the well.
Referring now to FIGURE 5, a modified form of structure is depicted in which the conical metal liner 3th is positioned with two capsules 34b and 34C between it and the explosive charge. Capsules 34h and 34C, which may be constructed in a manner similar to that above explained with respect tocapsule 34a, are each adapted to contain separated components which, when mixed together in the high velocity jet and transported into the breached opening are adapted to combine and produce the desired corrosive effect. While any desired combination of materials may be thus deposited in the breached opening, there may be cited as typical examples sodium hydroxide, potassium hydroxide, sulphur, sulphuric acid and hydrochloric acid.
Another means and mode of introducing into the jet stream material to be deposited in the breached opening is illustrated in FIGURE 6 wherein shell or liner Silt has suitably cemented to it a plurality of discrete capsules orbodies 34d consisting of or comprising materials to be deposited by the jet. It will be evident that the particles orcapsules 34d may, under some circumstances, be cemented or otherwise secured to the opposite surface of liner 3431*, thus being positioned between the liner andexplosive charge 30e. Capsules orbodies 34d may be capsules of mercury, acid, or other corrosion-inducing material, or may be suitable coated pellets of corrosiveagent constituents such as sodium hydroxide or potassium hydroxide, which wil combine with, for example, water in the opening, to provide a corrosive effect.
FIGURE 7 illustrates an additional form of means for introducing the material to be deposited in the breached opening, the structure there comprising a conventional liner Sllt and a specially-compounded shaped charge Stf of high explosive in which is incorporated or embedded dispersed discrete particles orcapsules 34e, each of which may consist of or comprise one or more of the substances to be injected into the produced opening by the jet. Alternatively, two or more types or sets of particles or capsules may be employed, each type or set comprising a material different from that of the other set; and such modification of the structure shown in FIGURE 7 is illustrated in FIGURE 8, wherein there is incorporated in the high explosive shaped charge a plurality of capsules or pellets 34]t comprising one material and a plurality of larger capsules or pellets 341' comprising a different material.
In FIGURE 9 there is depicted another modified form of shaped charge structure according to the invention, in which shell 30s is of supercially changed dimensions and liner Silt has cemented or otherwise suitably secured thereto on its inner face a plurality of pellets orcapsules 34k, and on the outside surface thereof a plurality of pellets or capsules 34m, pellets orcapsules 34k and pellets or capsules 34m containing or comprising either the same or similar materials, or alternatively, different materials. One of the materials contained in one of the sets of pellets or particles may contain or comprise a very heay metal, such as mercury, which may aid in producing the desired corrosive effect in the produced formation-penetrating hole or opening, and may concurrently aid the high velocity jet in producing a deeper penetration into the formation by weighting the jet. In particular, mercury may substantially weight the jet and corrode or soften, as by amalgamation, a copper or other soft-metal carrot lodged in the casing perforation or formation opening. It will be understood that such heavy metal or other jet-weighting material may be incorporated in other forms of apparatus herein depicted, as, for example, in capsule 34h illustrated in FIGURE 5. i
Additionally, and in accordance with the concept of the present invention, all possibility of the production of a carrot or other undesirable metallic fragment in the casing perforation or opening in the formation may be eliminated by forming the liner of a suitable non-metallic capsule filled with such heavy liquid metal as mercury. Such a liner or capsule is adapted to feed into the high velocity jet a stream or iiow of mercury to weight the jet for eifectively deep penetration of the encircling formation, without any possibility of production of a carrot at the casing perforation or in the encircling formation. A structure suitable for this mode of operation is depicted in FIGURE l0, in which a hollow, core-shaped capsule 3411 of, for example, glass, containing mercury, is depicted in close proximity to the highexplosive charge 30e whereby the liquid metal is picked up and entrained in the high velocity jet produced whencharge 30e is detonated.
It will be seen from the foregoing that there is provided by the invention a mode and means for providing effectively deeper and better penetration of an earth formation encircling a cased well borehole, by suitably incorporating into the high velocity jet produced by the detonation of a shaped charge of explosive, one or more substances which aid the jet in effectively penetrating the formation to a deeper extent and/ or depositing in the lower or outer reaches of the produced opening breached into the formation a corrosive material or a corrosioninducing material which is adapted to effectively attack soft-metal fragments and the cementitious material securing the grains of the formation together. It is evident that in the light of the present disclosure modifications of the mode and apparatus herein disclosed as exemplary will occur to those skilled in the art, and accordingly it is not desired to be limited to the specific details of the illustrative mode and apparatus, but what is claimed is:
l. An explosive perforating device comprising:
a detonable explosive shaped charge having a conical,
concave face;
a hollow, cone shaped capsule fitted against said conical face and including spaced apart conical Wall means forming a chamber therebetween, said chamber being disposed over substantially the entire area of said conical, concave face;
a body of liquid within said chamber to provide a layer of liquid over substantially the entire area of said conical, concave face; and
means for detonating said shaped charge.
2. An explosive perforating device comprising:
a detonable shaped charge having a conical, concave face;
a conical metal body composed principally of copper;
a hollow, cone shaped capsule fitting against said conical face and between said shaped charge and said metal body, said capsule including spaced apart conical wall means forming a chamber therebetween with said chamber being disposed over substantially the entire area of said conical, concave face;
a body of liquid reactive with copper within said chamber to provide a layer of such liquid over substantially the entire area of said conical, concave face; and means for detonating said shaped charge.
3,054,938 7 8 3. An explosive perforating device comprising: References Cited in the file of this patent a detonable shaped charge having a conical, concave UNITED STATES PATENTS face;
- 2 796 833 Sweetman June 25 1957 a conical metal body composed principally of copper tting against said face; 2,809,584 Moses Oct. 15, 1957 a hollow, cone shaped capsule tting within said conical body and including spaced apart conical Wall FORFIGN PATENTS ber being disposed over substantially the entire area 479,259 Canada Dec. 11, 1951 of said conical body; 10
OTHER REFERENCES Published Abstract Ian. 13, 1953, Class 102-20 of Doll application 78,333, published in 666 O.G. 599-600, Jan. 13, 1953.
a body of liquid reactive with copper Within said chamber to provide a layer of liquid over substantially the entire area of said conical, concave face; and
means for detonating said shaped charge.
US854217A1959-11-091959-11-09Means and mode for depositing material by jet perforationExpired - LifetimeUS3054938A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3135205A (en)*1959-03-031964-06-02Hycon Mfg CompanyCoruscative ballistic device
US3188955A (en)*1961-03-311965-06-15Western Co Of North AmericaExplosive charge assemblies
US3255347A (en)*1962-11-201966-06-07Halliburton CoSystem for determining fluid flow rate in boreholes
US3382800A (en)*1964-11-091968-05-14Navy UsaLinear-shaped charge chemical agent disseminator
US3404600A (en)*1966-09-201968-10-08Air Force UsaExplosive projector for projectiles
US3415321A (en)*1966-09-091968-12-10Dresser IndShaped charge perforating apparatus and method
US3566979A (en)*1968-12-261971-03-02Sun Oil CoFormation marking system
US3664262A (en)*1969-05-231972-05-23Us NavyReactive focusing warhead concept
US3675575A (en)*1969-05-231972-07-11Us NavyCoruscative shaped charge having improved jet characteristics
US4045356A (en)*1963-06-241977-08-30The Boeing CompanyFracturing agent
US4120701A (en)*1966-08-251978-10-17The United States Of America As Represented By The Secretary Of The ArmyReactant for steel
US20060266551A1 (en)*2005-05-252006-11-30Schlumberger Technology CorporationShaped Charges for Creating Enhanced Perforation Tunnel in a Well Formation
EP1918507A1 (en)*2006-10-312008-05-07Services Pétroliers SchlumbergerShaped charge comprising an acid
US20090114382A1 (en)*2007-09-072009-05-07Schlumberger Technology CorporationShaped charge for acidizing operations
US20090151948A1 (en)*2007-12-142009-06-18Schlumberger Technology CorporationDevice and method for reducing detonation gas pressure
US20110094406A1 (en)*2009-10-222011-04-28Schlumberger Technology CorporationDissolvable Material Application in Perforating
US20130180701A1 (en)*2012-01-182013-07-18Owen Oil ToolsSystem and method for enhanced wellbore perforations
US20160169639A1 (en)*2014-12-122016-06-16Schlumberger Technology CorporationComposite Shaped Charges

Citations (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CA479259A (en)*1951-12-11E.I. Du Pont De Nemours And CompanyTreatment of wells
US2796833A (en)*1952-05-101957-06-25William G SweetmanPerforating devices
US2809584A (en)*1953-04-011957-10-15Smith BernardConnector ring for two stage rockets

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CA479259A (en)*1951-12-11E.I. Du Pont De Nemours And CompanyTreatment of wells
US2796833A (en)*1952-05-101957-06-25William G SweetmanPerforating devices
US2809584A (en)*1953-04-011957-10-15Smith BernardConnector ring for two stage rockets

Cited By (31)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3135205A (en)*1959-03-031964-06-02Hycon Mfg CompanyCoruscative ballistic device
US3188955A (en)*1961-03-311965-06-15Western Co Of North AmericaExplosive charge assemblies
US3255347A (en)*1962-11-201966-06-07Halliburton CoSystem for determining fluid flow rate in boreholes
US4045356A (en)*1963-06-241977-08-30The Boeing CompanyFracturing agent
US3382800A (en)*1964-11-091968-05-14Navy UsaLinear-shaped charge chemical agent disseminator
US4120701A (en)*1966-08-251978-10-17The United States Of America As Represented By The Secretary Of The ArmyReactant for steel
US3415321A (en)*1966-09-091968-12-10Dresser IndShaped charge perforating apparatus and method
US3404600A (en)*1966-09-201968-10-08Air Force UsaExplosive projector for projectiles
US3566979A (en)*1968-12-261971-03-02Sun Oil CoFormation marking system
US3675575A (en)*1969-05-231972-07-11Us NavyCoruscative shaped charge having improved jet characteristics
US3664262A (en)*1969-05-231972-05-23Us NavyReactive focusing warhead concept
US20060266551A1 (en)*2005-05-252006-11-30Schlumberger Technology CorporationShaped Charges for Creating Enhanced Perforation Tunnel in a Well Formation
US8584772B2 (en)*2005-05-252013-11-19Schlumberger Technology CorporationShaped charges for creating enhanced perforation tunnel in a well formation
US7819064B2 (en)2006-10-312010-10-26Schlumberger Technology CorporationShaped charge and a perforating gun
EP1918507A1 (en)*2006-10-312008-05-07Services Pétroliers SchlumbergerShaped charge comprising an acid
US20080282924A1 (en)*2006-10-312008-11-20Richard SaengerShaped Charge and a Perforating Gun
US20090114382A1 (en)*2007-09-072009-05-07Schlumberger Technology CorporationShaped charge for acidizing operations
US7909115B2 (en)*2007-09-072011-03-22Schlumberger Technology CorporationMethod for perforating utilizing a shaped charge in acidizing operations
US20090151948A1 (en)*2007-12-142009-06-18Schlumberger Technology CorporationDevice and method for reducing detonation gas pressure
US7640986B2 (en)*2007-12-142010-01-05Schlumberger Technology CorporationDevice and method for reducing detonation gas pressure
US8677903B2 (en)2009-10-222014-03-25Schlumberger Technology CorporationDissolvable material application in perforating
US8342094B2 (en)*2009-10-222013-01-01Schlumberger Technology CorporationDissolvable material application in perforating
US20110094406A1 (en)*2009-10-222011-04-28Schlumberger Technology CorporationDissolvable Material Application in Perforating
US20140151046A1 (en)*2009-10-222014-06-05Schlumberger Technology CorporationDissolvable material application in perforating
US9671201B2 (en)*2009-10-222017-06-06Schlumberger Technology CorporationDissolvable material application in perforating
US20130180701A1 (en)*2012-01-182013-07-18Owen Oil ToolsSystem and method for enhanced wellbore perforations
US8919444B2 (en)*2012-01-182014-12-30Owen Oil Tools LpSystem and method for enhanced wellbore perforations
EP2805012A4 (en)*2012-01-182015-11-11Owen Oil Tools LpSystem and method for enhanced wellbore perforations
AU2013209503B2 (en)*2012-01-182017-02-02Owen Oil Tools LpSystem and method for enhanced wellbore perforations
US20160169639A1 (en)*2014-12-122016-06-16Schlumberger Technology CorporationComposite Shaped Charges
US9612095B2 (en)*2014-12-122017-04-04Schlumberger Technology CorporationComposite shaped charges

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