US3238872A - Shaped charge construction - Google Patents

Shaped charge construction Download PDF

Info

Publication number
US3238872A
US3238872A US343865A US34386564A US3238872A US 3238872 A US3238872 A US 3238872A US 343865 A US343865 A US 343865A US 34386564 A US34386564 A US 34386564A US 3238872 A US3238872 A US 3238872A
Authority
US
United States
Prior art keywords
case
shaped charge
cavity
detonation
explosive
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US343865A
Inventor
Zernow Louis
John L Squier
Lieberman Irving
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerojet Rocketdyne Inc
Original Assignee
Aerojet General Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aerojet General Corp filed Critical Aerojet General Corp
Priority to US343865A priority Critical patent/US3238872A/en
Application granted granted Critical
Publication of US3238872A publication Critical patent/US3238872A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E21EARTH DRILLING; MINING
    • E21BEARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B43/00Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
    • E21B43/11Perforators; Permeators
    • E21B43/116Gun or shaped-charge perforators
    • E21B43/117Shaped-charge perforators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/08Blasting cartridges, i.e. case and explosive with cavities in the charge, e.g. hollow-charge blasting cartridges

Definitions

  • This invention generally relates to improved explosive charges to be used for industrial purposes, and more particularly to improvements in confined explosive charges known as shaped charges.
  • Shaped charges generally include a charge of high explosive contained in a case between a hollow conical metal liner and the wall of the case, the liner beingv arranged With its rim secured around the open end of the case.
  • On detonation of the explosive practically all of the energy of the explosion is utilized in collapsing the liner into a jet of metal.
  • the jet of metal is driven axially out of the case at extremely high velocity enabling it to penetrate steel or to be driven deeply into the strata sur- -rounding a Well.
  • the described characteristic has caused shaped charges to be widely used in the oil well industry for rejuvenating a dry oil ⁇ well by perforating the oil well tubing and surrounding strata to increase the yield of oil in the area of the well.
  • Shaped charges of known construction although utilizing the greatest part of the energy derived from the detonation of the explosive, do permit some of the energy of the explosion to be Wasted in the vdeformation of the shaped charge case thereby.
  • an object of this invention to provide a shaped charge of improved construction, wherein the effective energy from the detonation of the explosive material in the shaped charge which is utilized by the shaped charge is increased to a degree not heretofore achieved "by shaped charges of known construction.
  • FIGURE 1 is a horizontal section through a conventional shaped charge suspended in a Well tubing
  • FIGURE 2 is a horizontal section through a shaped charge constructed in accordance with the .present invention
  • FIGURE 3 is a vertical section taiken along line 3 3 in FIGURE 2;
  • FIGURE 4 is a horizontal section through a perforator gun having a modified arrangement of the novel shaped charge of the invention mounted therein;
  • FIGURE 5 is a vertical section taken along line 5-5 in FIGURE 4 with the outer tube omitted.
  • FIGURE 1 a conventional conliguration of a shaped charge is shown which includes a cylindrical casing A -having a channel or groove B extending along the outer rear surface thereof, a central recess C in the inner rear surface of the casing A adjacent the channel B, and a liner D in the form of a hollow cone of metal positioned with its apex disposed toward the rear of the casing A and its open end secured to the casing A around the front end thereof.
  • Recess C is loaded before the liner D is positioned in ⁇ the casing A with a charge of sensitive booster explosive E, While a charge of high explosive F is disposed in the space within the casing A located :between the rear wall thereof and the liner D.
  • the ront end of the casing is closed by a cap G.
  • a length of Primacord H extends through the channel B, the Frimacord H including an explosive contained in a waterproof tube and provid-ing in eect a detonation wave which travels at a high rate of speed through the length of the cord.
  • Any suitable means such as a squib, not shown, may be provided to initiate detonation of the Primacord H.
  • the shaped charge shown in FIGURE l is illustrated in position for perforating an oil well tube I, the shaped charge being suspended at a desired depth by any suitable means, not shown.
  • the Primacord H is detonated which creates a detonation Wave that travels past the booster explosive charge E, detonating the latter which in turn detonates the charge of high explosive F.
  • the hollow conical liner D is shaped to guide or direct the greater part of the energy derived from the detonation of the high explosive F in an axial direction with respect to the liner D so as to effect melting of the liner D into a line jet of metal which travels at such speed through the front end of casing A as to t-raverse cap G and the wall of well tube I, and thereafter proceeds into the earth strata surrounding the tube I.
  • the improved shaped charge embodying the present invention will permit a smaller detonating charge to be used to effect a penetration equal in magnitude to that effected by a larger shaped charge of conventional construction.
  • a shaped charge case 26 is shown formed as a metallic casting which substantially fills the transverse crosssectional area of the pipe or tube 23 to be pierced or perforated.
  • the case 2li is provided with a cylindrical transverse cavity 21 and has a thickened metallic body wall 22 which resists deformation from the energy generated by the detonation of the high explosive to be contained within the case 20.
  • the thickened 'body wall 22 has a generally spherical outer surface which provides a maximum of additional metal thickness of the case 20 for use in the oil well tube 23 having a circular crosssection, as shown.
  • the increased thickness of the body Wall 22 retards the outward movement of the case 2l) upon detonation of the explosive charge contained therein, and serves to concentrate more of the energy which has been released by the detonation of the explosive charge upon the collapsible cone.
  • This concentration of the explosive energy on the collapsible cone serves to impart higher energies to the jet formed from the collapsing of the cone.
  • the other parts of the shaped charge such as the conical metallic liner 24, end cap 25, recess 26 lled With the booster explosive charge 26', and the channel or groove 27 for Primacord 2S are similar to the corresponding parts in FIGURE 1 and no further description thereof is believed to be necessary.
  • the high explosive positioned between the liner 24 and the case 20 is indicated at 3 28.
  • the shaped charge may be suspended in a desired area by a line connected to an eye 29 Welded to the case as indicated in FIGURE 3.
  • FIGURES 4 and 5 a modified form of the improved shaped charge in accordance with the present invention is shown, the modified shaped charge being intended for use in a pe-rforator gun.
  • a perforator gun may be used to form a number of perforations in a localized area. It would be desirable to use a perforator gun repeatedly, but heretofore, such guns have had a relatively short life.
  • the tubular body of a perforator gun has been characteristically susceptible to deformation caused by the ⁇ distortion of the cases of the shaped charges used therewith when the explosive material contained in the shaped charges was detonated, while the ports in the wall of the perforator gun through which the jets of metal from the detonated shaped charges issued were subjected to excessive wear because of inaccurate firing of the metal jets through the ports which often occurred.
  • the perforator gun comprises a thick cylindrical tube or wall 30 having a plurality of radial ports 31 (only one such port 31 being shown in FIGURES 4 and 5) through which the liquid metal jets from the shaped charge units 32 are to be fired.
  • a threaded bushing 33 is mounted in the port 31, the oute-r end of the bushing 33 being closed by a cap 33.
  • the bushing 33 serves to protect the surface of the cylindrical tube 30 bounding the port 31 and to accurately position the forward end of the spaced charge unit 32 corresponding thereto, it being understood that a plurality of spaced charge units 32 corresponding in number to the plurality of ports 31 in the cylindrical tube 30 are disposed along the length thereof.
  • a recess 34 is provided in the inner surface of the gun tube 30 and is aligned with the port 31. Recess 34 receives a stub 35 integral with the shaped charge unit 32 and extending radially outwardly from the rear portion thereof so as to accurately locate the Irear portion of the shaped charge unit 32 Within the cylindrical tube 30 of the perforator gun.
  • the shaped charge unit 32 has an end cap 36 provided with a frusto-conical outer portion converging toward the port 31, the end cap 36 serving as a spacer element between the remainder of the shaped charge unit 32 and the port 31 and having an outwardly convergent passage therethrough providing communication between the interior of the shaped charge unit 32 and the port 31.
  • the bushing 33 is screwed into port 31 so as to engage the forward end of the spacer element or end cap 36 and hold the stub 35 in recess 34.
  • the case of the shaped charge unit 32 is provided with a longitudinally extending passageway therethrough for receiving a length of Primacord 36', the passageway and the Primacord 36 extending therethrough being located slightly forward of the stub 35.
  • the Primacord 36 is in communication with a recess 37 which is provided in the rear portion of the case for the shaped charge unit 32, the recess 37 opening inwardly and containing a booster explosive charge 38.
  • the booster explosive charge 38 adjoins a charge of high explosive 39 which is received within the central transverse cavity formed in the case of the shaped charge unit 32.
  • the volume of the transverse cavity in the shaped charge unit 32 is maintained at a magnitude comparable to the volume of the transverse cavity 21 in the shaped charge unit of FIGURES 2 and 3 by providing a rearward frustoconical cavity portion therefor, the thickness of the wall of the case of the shaped charge unit 32 being maintained throughout the extent thereof.
  • a liner 42 comprising a hollow cone of metal with its apex disposed toward the rear of the case of the shaped charge unit 32 is secured to the case to retain the high explosive charge 39 in place.
  • a squib is diagrammatically shown at 40 for initiating detonation of the length of Primacord 36', the squib 40 being fired by electric energy directed thereto via electrical conductors or wires 41 which are connected to a suitable source of electrical power controlled by a switch, not shown, located at a remote station.
  • the Primacord 36 When the squib 40 is red, the Primacord 36 is ignited and burns explosively and progressively throughout its length detonating booster explosive charge 38 which in turn detonates the main charge of high explosive 39 causing liner 42 to be projected as a fine stream of molten metal at extremely high velocity outwardly through the bushing 33, so as to pierce the end cap 33 and the well tubing 43.
  • a shaped charge construction comprising (a) a shaped charge case having a forwardly opening transverse cavity provided therein,
  • said case being substantially spheroid in shape and having solid walls bounding said cavity, said solid walls having a cross-sectional thickness greatest at the point on said case intermediate the forward and rear ends thereof and progressively diminishing in thickness toward each of the forward and rear ends thereof, whereby said solid walls are of sufficient thickness to substantially prevent deformation of said case from the energy released by the detonation of said explosive material.
  • a shaped charge construction for insertion into a tubular member to form a perforation, said shaped charge construction comprising (a) a shaped charge case having a transverse cavity therein which is open at the forward end of the case,
  • said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of suilicient dimensions so as to enable said case to define a perimeter in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of the tubular member into which the shaped charge construction is adapted to be inserted, whereby deformation of the case upon detonation of said explosive material -is substantially prevented and greater energy from the detonation of the explosive material is concentrated on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
  • said case being substantially spheroid in shape and having solid walls bounding said cavity, said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse crosssectional thickness greatest at the point on said case intermediate the forward and rear ends thereof and progressively diminishing in thickness toward each of the forward and rear ends thereof, and
  • said case defining a circular perimeter in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular member, whereby deformation of the case upon detonation of said explosive material is substantially prevented and greater energy from the detonation of the explosive material is concentrated on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
  • said metallic liner being positioned to direct the energy of explosion from the detonation of said explosive material through the open end of said transverse cavity
  • said solid Walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of suicient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular member, whereby said tubular member acts to reinforce the walls of said case so as to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive material on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
  • said metallic liner being positioned to direct the energy of explosion from the detonation of said eX- plosive material through the open end of said transverse cavity
  • said shaped charge case having a rearwardly extending stub and being positioned in said tubular gun with said stub being received in the recess and with the open end of said transverse cavity being in registration with the port in said tubular gun,
  • said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of sufiicient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular gun to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive material on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom,
  • bushing means received by the port to protect the surface of said tubular gun bounding the port
  • a frusto-conical end lcap interposed between said case and said tubular gun with the smaller end of said end cap registering with said bushing means and the larger end of said end cap registering with the open end of said transverse cavity so that the jet of molten metal is directed through said bushing means, whereby said tubular gun may be repeatedly used without damage to the port.
  • said metallic liner being positioned to direct the energy of explosion from the detonation of said explosive material through the open end of said transverse cavity
  • said shaped charge case having a rearwardly extending stub and being positioned in said tubular gun with said stub being received in the recess and with the open end of said transverse cavity being in registration with the port in said tubular gun,
  • said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity o'f sufficient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular gun to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive ma-terial on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom,

Description

March 8, 1966 L. ZERNow ETAL 3,238,872
SHAPED CHARGE CONSTRUCTION Filed Feb. 1o, 1964 Figz 28 27 26 /NvE/vToR Louls zERNow mv UEBERMAN BY JoH .SQUIER United States Patent O ohio Filed Feb. 1o, 1964, ser. No. 343,865 6 Claims. (ci. 1oz-2a) This invention generally relates to improved explosive charges to be used for industrial purposes, and more particularly to improvements in confined explosive charges known as shaped charges.
Shaped charges generally include a charge of high explosive contained in a case between a hollow conical metal liner and the wall of the case, the liner beingv arranged With its rim secured around the open end of the case. On detonation of the explosive, practically all of the energy of the explosion is utilized in collapsing the liner into a jet of metal. The jet of metal is driven axially out of the case at extremely high velocity enabling it to penetrate steel or to be driven deeply into the strata sur- -rounding a Well. The described characteristic has caused shaped charges to be widely used in the oil well industry for rejuvenating a dry oil `well by perforating the oil well tubing and surrounding strata to increase the yield of oil in the area of the well. Shaped charges of known construction, although utilizing the greatest part of the energy derived from the detonation of the explosive, do permit some of the energy of the explosion to be Wasted in the vdeformation of the shaped charge case thereby.
It is, accordingly, an object of this invention to provide a shaped charge of improved construction, wherein the effective energy from the detonation of the explosive material in the shaped charge which is utilized by the shaped charge is increased to a degree not heretofore achieved "by shaped charges of known construction.
It is another object of the invention to provide an improved shaped charge case which will lengthen the useful life of shaped charge devices.
Other objects and many of the attendant advantages of this invention will be Ireadily appreciated as the same 'becomes 'better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:
FIGURE 1 is a horizontal section through a conventional shaped charge suspended in a Well tubing;
FIGURE 2 is a horizontal section through a shaped charge constructed in accordance with the .present invention;
FIGURE 3 is a vertical section taiken along line 3 3 in FIGURE 2;
FIGURE 4 is a horizontal section through a perforator gun having a modified arrangement of the novel shaped charge of the invention mounted therein; and
FIGURE 5 is a vertical section taken along line 5-5 in FIGURE 4 with the outer tube omitted.
Referring now to FIGURE 1, a conventional conliguration of a shaped charge is shown which includes a cylindrical casing A -having a channel or groove B extending along the outer rear surface thereof, a central recess C in the inner rear surface of the casing A adjacent the channel B, and a liner D in the form of a hollow cone of metal positioned with its apex disposed toward the rear of the casing A and its open end secured to the casing A around the front end thereof. Recess C is loaded before the liner D is positioned in `the casing A with a charge of sensitive booster explosive E, While a charge of high explosive F is disposed in the space within the casing A located :between the rear wall thereof and the liner D. The ront end of the casing is closed by a cap G.
3,238,872 Patented Mar. 8, 1956 A length of Primacord H extends through the channel B, the Frimacord H including an explosive contained in a waterproof tube and provid-ing in eect a detonation wave which travels at a high rate of speed through the length of the cord. Any suitable means such as a squib, not shown, may be provided to initiate detonation of the Primacord H. The shaped charge shown in FIGURE l is illustrated in position for perforating an oil well tube I, the shaped charge being suspended at a desired depth by any suitable means, not shown. When the shaped charge is to be fired, the Primacord H is detonated which creates a detonation Wave that travels past the booster explosive charge E, detonating the latter which in turn detonates the charge of high explosive F.
The hollow conical liner D is shaped to guide or direct the greater part of the energy derived from the detonation of the high explosive F in an axial direction with respect to the liner D so as to effect melting of the liner D into a line jet of metal which travels at such speed through the front end of casing A as to t-raverse cap G and the wall of well tube I, and thereafter proceeds into the earth strata surrounding the tube I.
While the greater part of the energy of the detonated explosive F is directed forwardly, a significant amount of energy is expended in tending to effect deformation of the casing A, and it is a particular function of the present invention to provide an improved shaped charge having a casing which resists such deformation. rI`he energy thus conserved is added to that acting axially and effects penetration of the strata to a greater depth. When greater depth penetration is not of major importance, the improved shaped charge embodying the present invention will permit a smaller detonating charge to be used to effect a penetration equal in magnitude to that effected by a larger shaped charge of conventional construction.
The improved performance of a shaped charge constructed in accordance with the present invention may result from various structural forms of the case, one of which is shown in FIGURES 2 and 3. `In these gures, a shaped charge case 26 is shown formed as a metallic casting which substantially fills the transverse crosssectional area of the pipe or tube 23 to be pierced or perforated. The case 2li is provided with a cylindrical transverse cavity 21 and has a thickened metallic body wall 22 which resists deformation from the energy generated by the detonation of the high explosive to be contained within the case 20. The thickened 'body wall 22 has a generally spherical outer surface which provides a maximum of additional metal thickness of the case 20 for use in the oil well tube 23 having a circular crosssection, as shown. The increased thickness of the body Wall 22 retards the outward movement of the case 2l) upon detonation of the explosive charge contained therein, and serves to concentrate more of the energy which has been released by the detonation of the explosive charge upon the collapsible cone. This concentration of the explosive energy on the collapsible cone serves to impart higher energies to the jet formed from the collapsing of the cone. These higher energies provide increased jet velocities which result in deeper and larger diameter penetrations into the surrounding material, Tests have indicated an `increase in excess of 25% in the depth of penetration effected by the use of the improved shaped charge.
The other parts of the shaped charge, such as the conical metallic liner 24, end cap 25, recess 26 lled With the booster explosive charge 26', and the channel or groove 27 for Primacord 2S are similar to the corresponding parts in FIGURE 1 and no further description thereof is believed to be necessary. The high explosive positioned between the liner 24 and the case 20 is indicated at 3 28. The shaped charge may be suspended in a desired area by a line connected to an eye 29 Welded to the case as indicated in FIGURE 3.
In FIGURES 4 and 5, a modified form of the improved shaped charge in accordance with the present invention is shown, the modified shaped charge being intended for use in a pe-rforator gun. A perforator gun may be used to form a number of perforations in a localized area. It would be desirable to use a perforator gun repeatedly, but heretofore, such guns have had a relatively short life. In the latter respect, the tubular body of a perforator gun has been characteristically susceptible to deformation caused by the `distortion of the cases of the shaped charges used therewith when the explosive material contained in the shaped charges was detonated, while the ports in the wall of the perforator gun through which the jets of metal from the detonated shaped charges issued were subjected to excessive wear because of inaccurate firing of the metal jets through the ports which often occurred. These defects are remedied by the construction now described.
The perforator gun comprises a thick cylindrical tube or wall 30 having a plurality of radial ports 31 (only one such port 31 being shown in FIGURES 4 and 5) through which the liquid metal jets from the shaped charge units 32 are to be fired. A threaded bushing 33 is mounted in the port 31, the oute-r end of the bushing 33 being closed by a cap 33. The bushing 33 serves to protect the surface of the cylindrical tube 30 bounding the port 31 and to accurately position the forward end of the spaced charge unit 32 corresponding thereto, it being understood that a plurality of spaced charge units 32 corresponding in number to the plurality of ports 31 in the cylindrical tube 30 are disposed along the length thereof. A recess 34 is provided in the inner surface of the gun tube 30 and is aligned with the port 31. Recess 34 receives a stub 35 integral with the shaped charge unit 32 and extending radially outwardly from the rear portion thereof so as to accurately locate the Irear portion of the shaped charge unit 32 Within the cylindrical tube 30 of the perforator gun.
The shaped charge unit 32 has an end cap 36 provided with a frusto-conical outer portion converging toward the port 31, the end cap 36 serving as a spacer element between the remainder of the shaped charge unit 32 and the port 31 and having an outwardly convergent passage therethrough providing communication between the interior of the shaped charge unit 32 and the port 31. The bushing 33 is screwed into port 31 so as to engage the forward end of the spacer element or end cap 36 and hold the stub 35 in recess 34. The case of the shaped charge unit 32 is provided with a longitudinally extending passageway therethrough for receiving a length of Primacord 36', the passageway and the Primacord 36 extending therethrough being located slightly forward of the stub 35. The Primacord 36 is in communication with a recess 37 which is provided in the rear portion of the case for the shaped charge unit 32, the recess 37 opening inwardly and containing a booster explosive charge 38. The booster explosive charge 38 adjoins a charge of high explosive 39 which is received within the central transverse cavity formed in the case of the shaped charge unit 32.
yIt will be noted that while the configuration of the transverse cavity in the case of the shaped charge unit 32 has been altered in the embodiment shown in FIGURES 4 and 5 from that illustrated in FIGURES 2 and 3, the volume of the transverse cavity in the shaped charge unit 32 is maintained at a magnitude comparable to the volume of the transverse cavity 21 in the shaped charge unit of FIGURES 2 and 3 by providing a rearward frustoconical cavity portion therefor, the thickness of the wall of the case of the shaped charge unit 32 being maintained throughout the extent thereof. A liner 42 comprising a hollow cone of metal with its apex disposed toward the rear of the case of the shaped charge unit 32 is secured to the case to retain the high explosive charge 39 in place.
CII
Maximum advantage is taken of the available space within the gun tube 30 through the use of the generally spherical case shown, although it will be understood that the case of the shaped charge unit 32 may take other forms, which may be similarly thickened in other geometric shapes. The added Wall thickness of the case of the shaped charge unit 32 serves to minimize damage to the gun tube 3i) due to greater retention of the energy of shock by the greater mass of metal in the case, and confinement of the blast effects arising from the detonation of the shaped charge unit 32, which results in a slower rate of expansion and fragments of lower velocity. The additional advantages previously stated with regard to the ernbodiment of FIGURES 2 and 3 of providing greater concentration of energy from t-he detonation of the explosive material in the shaped charge unit 32 and thus imparting greater energy to the liner 42 and the jet of molten metal formed therefrom are also realized in the embodiment of FIGURES 4 and 5 A squib is diagrammatically shown at 40 for initiating detonation of the length of Primacord 36', the squib 40 being fired by electric energy directed thereto via electrical conductors or wires 41 which are connected to a suitable source of electrical power controlled by a switch, not shown, located at a remote station.
When the squib 40 is red, the Primacord 36 is ignited and burns explosively and progressively throughout its length detonating booster explosive charge 38 which in turn detonates the main charge of high explosive 39 causing liner 42 to be projected as a fine stream of molten metal at extremely high velocity outwardly through the bushing 33, so as to pierce the end cap 33 and the well tubing 43.
In the case of a conventional perforating gun repeatedly fired with the usual form of shaped charges mounted therein, deformation of the shaped charge units causes slight but cumulative damage to the perforating gun at each firing thereof, and the accuracy of the path of the molten metal jets through the ports in the wall of the perforating gun is soon impaired to cause the gun wall around the ports to be worn away resulting in unsatisfactory performance. On the contrary, the positive suppression of deformation or distortion of the cases of shaped charge units constructed in accordance with the present invention insures long and satisfactory functioning of the perforator gun. The advantageous form of the shaped charge cases herein described may be readily and inexpensively produced by conventional casting procedures.
Preferred embodiments of the invention have been described and shown by way of illustration but should not be construed as necessarily limitative of the scope of the invention, since various modifications may be made by those skilled in the art without departing from the scope of the invention as defined by the appended claims.
We claim:
1. A shaped charge construction comprising (a) a shaped charge case having a forwardly opening transverse cavity provided therein,
(b) explosive material received in said cavity,
(c) a metallic liner secured to said case and closing off said cavity,
(d) means operably associated with said case to initiate detonation of said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal, and
(e) said case being substantially spheroid in shape and having solid walls bounding said cavity, said solid walls having a cross-sectional thickness greatest at the point on said case intermediate the forward and rear ends thereof and progressively diminishing in thickness toward each of the forward and rear ends thereof, whereby said solid walls are of sufficient thickness to substantially prevent deformation of said case from the energy released by the detonation of said explosive material.
2. A shaped charge construction for insertion into a tubular member to form a perforation, said shaped charge construction comprising (a) a shaped charge case having a transverse cavity therein which is open at the forward end of the case,
(b) explosive material received in said cavity,
(c) a metallic liner secured to said case and closing off said cavity to enclose said explosive material therein,
(d) means operably associated with said case for initiating detonation of:` said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal, and
(e) said case having solid walls bounding said cavity,
said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of suilicient dimensions so as to enable said case to define a perimeter in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of the tubular member into which the shaped charge construction is adapted to be inserted, whereby deformation of the case upon detonation of said explosive material -is substantially prevented and greater energy from the detonation of the explosive material is concentrated on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
3. In combination,
(a) an elongated cylindrical tubular member,
(b) a shaped charge case positioned in said tubular member and having a transverse cavity therein which is open at the forward end of the case,
(c) explosive material received in said cavity,
(d) a metallic liner secured to said case and closing off said cavity to enclose said explosive material therein,
(e) means operably associated with said case for initiating detonation of said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal,
(f) said case being substantially spheroid in shape and having solid walls bounding said cavity, said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse crosssectional thickness greatest at the point on said case intermediate the forward and rear ends thereof and progressively diminishing in thickness toward each of the forward and rear ends thereof, and
(g) said case defining a circular perimeter in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular member, whereby deformation of the case upon detonation of said explosive material is substantially prevented and greater energy from the detonation of the explosive material is concentrated on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
4. In combination,
(a) a tubular member having at least one port through the wall thereof,
(b) a shaped charge case having a transverse cavity therein which is open at the forward end of the case,
(c) explosive material received in said cavity,
(d) a metallic liner secured to said case and closing olf said cavity to enclose said explosive material therein,
(e) said metallic liner being positioned to direct the energy of explosion from the detonation of said explosive material through the open end of said transverse cavity,
(f) said shaped charge case being positioned in said tubular member with the open end of said transverse cavity being in registration with said port in said tubular member,
(g) means operably associated with said case for initiating detonation of said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal, and
(h) said case having solid walls bounding said cavity,
said solid Walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of suicient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular member, whereby said tubular member acts to reinforce the walls of said case so as to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive material on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom.
5. In combination,
(a) an elongated tubular perforator gun having at least one port through the wall thereof and an inwardly opening recess in the wall in oppositely disposed relation to the port,
(b) a shaped charge case having a transverse cavity therein which is open at the forward end of the case,
(c) explosive material received in said cavity,
(d) a metallic liner secured to said case -and closing off said cavity to enclose said explosive material therein,
(e) said metallic liner being positioned to direct the energy of explosion from the detonation of said eX- plosive material through the open end of said transverse cavity,
(f) said shaped charge case having a rearwardly extending stub and being positioned in said tubular gun with said stub being received in the recess and with the open end of said transverse cavity being in registration with the port in said tubular gun,
(g) means operably associated with said case for initiating detonation of said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal,
(h) said case having solid walls bounding said cavity,
said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity of sufiicient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular gun to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive material on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom,
(i) bushing means received by the port to protect the surface of said tubular gun bounding the port, and (j) a frusto-conical end lcap interposed between said case and said tubular gun with the smaller end of said end cap registering with said bushing means and the larger end of said end cap registering with the open end of said transverse cavity so that the jet of molten metal is directed through said bushing means, whereby said tubular gun may be repeatedly used without damage to the port.
6. In combination,
(a) an elongated tubular perforator gun having at least one port through the wall thereof and an inwardly opening recess in the Wall in oppositely disposed relation to the port,
(b) a shaped charge case having a transverse cavity therein which is open at the forward end of the case,
(c) explosive material received in said cavity,
(d) a metallic liner secured to said case and closing off said cavity to enclose said explosive material therein,
(e) said metallic liner being positioned to direct the energy of explosion from the detonation of said explosive material through the open end of said transverse cavity,
(f) said shaped charge case having a rearwardly extending stub and being positioned in said tubular gun with said stub being received in the recess and with the open end of said transverse cavity being in registration with the port in said tubular gun,
(g) means operably associated with said case for initiating detonation of said explosive material for forcing said metallic liner forwardly at high velocity in the form of a jet of molten metal,
(h) said case being substantially spheroid in shape and having solid walls bounding said cavity,
(i) said cavity tapering inwardly at the rear portion thereof to maintain a substantially equal transverse thickness of said solid walls from the forward end of said case to the rear end thereof,
(j) said solid walls having a transverse thickness substantially greater than the transverse thickness of said metallic liner and being provided with a transverse cross-sectional thickness along the cavity o'f sufficient dimensions so as to define a perimeter for said case in contiguous relation throughout at least a substantial portion of its entire extent with the internal surface of said tubular gun to substantially prevent deformation of said case upon detonation of said explosive material, thereby concentrating the energy from the detonation of said explosive ma-terial on said metallic liner to enhance the perforating effect of the jet of molten metal formed therefrom,
(k) bushing means received by the port to provide a protective liner for the surface of said tubular gun bounding the port, and
(l) a frusto-conical end Cap interposed between said case and said tubular gun to space the forward end of said case from said tubular gun with 'the larger base portion of said end cap 'conforming to the open end of said transverse cavity and the smaller top portion of said end cap conforming to said bushing means so that the jet of molten metal is directed through said bushing means, whereby said tubular gun may be repeatedly used without damage to the port.
References Cited by the Examiner UNITED STATES PATENTS 1,810,000 6/1931 Woodberry 10224 2,513,233 6/1950 Byers 102-24 2,742,857 4/ 1956 Turechek 102-20 2,765,739 10/1956 Mohaupt et al 102-20 2,925,775 2/1960 McKee 102-20 3,118,508 1/1964 Friedman et al. 102-24 OTHER REFERENCES Clark, G. B.: Studies of the Design of Shaped Explosive Charges and Their Effect in Breaking Concrete Blocks, AIME Technical Publication 2157, March 1947,
BENJAMIN A. BORCHELT, Primary Examiner.
V. R. PENDEGRASS, Assistant Examiner.

Claims (1)

1. A SHAPED CHARGE CONSTRUCTION COMPRISING (A) A SHAPED CHARGE CASE HAVING A FORWARDLY OPENING TRANSVERSE CAVITY PROVIDED THEREIN, (B) EXPLOSIVE MATERIAL RECEIVED IN SAID CAVITY, (C) A METALLIC LINEAR SECURED TO SAID CASE AND CLOSING OFF SAID CAVITY, (D) MEANS OPERABLY ASSOCIATED WITH SAID CASE TO INITIATE DETONATION OF SAID EXPLOSIVE MATERIAL FOR FORCING SAID METALLIC LINER FORWARDLY AT HIGH VELOCITY IN THE FORM OF A JET OF MOLTEN METAL, AND (E) SAID CASE BEING SUBSTANTIALLY SPHEROID IN SHAPE AND HAVING SOLID WALLS BOUNDING SAID CAVITY, SAID SOLID WALLS HAVING A CROSS-SECTIONAL THICKNESS GREATEST AT THE POINT ON SAID CASE INTERMEDIATE THE FORWARD AND REAR ENDS THEREOF AND PROGRESSIVELY DIMINISHING IN THICKNESS TOWARD EACH OF THE FORWARD AND REAR ENDS THEREOF, WHEREBY SAID SOLID WALLS ARE OF SUFFICIENT THICKNESS TO SUBSTANTIALLY PREVENT DEFORMATION OF SAID CASE FROM THE ENERGY RELEASED BY THE DETONATION OF SAID EXPLOSIVE MATERIAL.
US343865A 1964-02-10 1964-02-10 Shaped charge construction Expired - Lifetime US3238872A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US343865A US3238872A (en) 1964-02-10 1964-02-10 Shaped charge construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US343865A US3238872A (en) 1964-02-10 1964-02-10 Shaped charge construction

Publications (1)

Publication Number Publication Date
US3238872A true US3238872A (en) 1966-03-08

Family

ID=23348018

Family Applications (1)

Application Number Title Priority Date Filing Date
US343865A Expired - Lifetime US3238872A (en) 1964-02-10 1964-02-10 Shaped charge construction

Country Status (1)

Country Link
US (1) US3238872A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3323544A (en) * 1965-03-24 1967-06-06 Francis Gus Method and apparatus for draining liquid from containers
US3451339A (en) * 1964-03-03 1969-06-24 Tech De Rech Ind Et Mechanique Priming explosive devices
US4253523A (en) * 1979-03-26 1981-03-03 Ibsen Barrie G Method and apparatus for well perforation and fracturing operations
US4499830A (en) * 1981-06-29 1985-02-19 The United States Of America As Represented By The Secretary Of The Army High lethality warheads
US4502550A (en) * 1982-12-06 1985-03-05 Magnum Jet, Inc. Modular through-tubing casing gun
WO2007053190A2 (en) * 2005-06-01 2007-05-10 Baker Hughes Incorporated Low debris perforating gun system for oriented perforating
US20170328134A1 (en) * 2016-05-13 2017-11-16 Baker Hughes Incorporated System for Extended Use in High Temperature Wellbore
US10781773B2 (en) * 2015-11-04 2020-09-22 Northrop Grumman Innovation Systems, Inc. Solid rocket motors including flight termination systems, and related multi-stage solid rocket motor assemblies and methods

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1810000A (en) * 1921-06-07 1931-06-16 John H Woodberry Booster
US2513233A (en) * 1949-03-15 1950-06-27 Laud Stanley Byers Multiple jet blasting charge
US2742857A (en) * 1950-01-12 1956-04-24 Lane Wells Co Gun perforators
US2765739A (en) * 1951-01-26 1956-10-09 Welex Jet Services Inc Jet carrier sealing plug
US2925775A (en) * 1955-12-13 1960-02-23 Borg Warner Well casing perforator
US3118508A (en) * 1962-08-20 1964-01-21 Jersey Prod Res Co Drilling of off-vertical boreholes

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1810000A (en) * 1921-06-07 1931-06-16 John H Woodberry Booster
US2513233A (en) * 1949-03-15 1950-06-27 Laud Stanley Byers Multiple jet blasting charge
US2742857A (en) * 1950-01-12 1956-04-24 Lane Wells Co Gun perforators
US2765739A (en) * 1951-01-26 1956-10-09 Welex Jet Services Inc Jet carrier sealing plug
US2925775A (en) * 1955-12-13 1960-02-23 Borg Warner Well casing perforator
US3118508A (en) * 1962-08-20 1964-01-21 Jersey Prod Res Co Drilling of off-vertical boreholes

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451339A (en) * 1964-03-03 1969-06-24 Tech De Rech Ind Et Mechanique Priming explosive devices
US3323544A (en) * 1965-03-24 1967-06-06 Francis Gus Method and apparatus for draining liquid from containers
US4253523A (en) * 1979-03-26 1981-03-03 Ibsen Barrie G Method and apparatus for well perforation and fracturing operations
US4499830A (en) * 1981-06-29 1985-02-19 The United States Of America As Represented By The Secretary Of The Army High lethality warheads
US4502550A (en) * 1982-12-06 1985-03-05 Magnum Jet, Inc. Modular through-tubing casing gun
WO2007053190A2 (en) * 2005-06-01 2007-05-10 Baker Hughes Incorporated Low debris perforating gun system for oriented perforating
WO2007053190A3 (en) * 2005-06-01 2007-07-19 Baker Hughes Inc Low debris perforating gun system for oriented perforating
US10781773B2 (en) * 2015-11-04 2020-09-22 Northrop Grumman Innovation Systems, Inc. Solid rocket motors including flight termination systems, and related multi-stage solid rocket motor assemblies and methods
US20170328134A1 (en) * 2016-05-13 2017-11-16 Baker Hughes Incorporated System for Extended Use in High Temperature Wellbore

Similar Documents

Publication Publication Date Title
US2649046A (en) Explosive package
US2399211A (en) Method of perforating well casings
US4387773A (en) Shaped charge well perforator
US2708408A (en) Well perforating device
US4955939A (en) Shaped charge with explosively driven liquid follow through
US3750582A (en) Projectile with differential tandem shaped charges
US2946283A (en) Method and apparatus for perforating wellbores and casings
US4627353A (en) Shaped charge perforating apparatus
US3443518A (en) Multi-point ignition system for shaped charges
US3358780A (en) Cumulative shaped charges
US2796833A (en) Perforating devices
US3238872A (en) Shaped charge construction
US3190372A (en) Methods and apparatus for drilling bore holes
US3021784A (en) Shaped charge unit for well perforators
US2843041A (en) Deep perforation of subsurface formations
US4724767A (en) Shaped charge apparatus and method
GB1315179A (en) Mounting tubes in tube plates
US2974595A (en) Projectile
US4669384A (en) High temperature shaped charge perforating apparatus
US3269467A (en) Shaped charge apparatus
US3151556A (en) Metallic plug for stemming bore holes
US3292536A (en) Shaped explosive charges
US3268016A (en) Shaped charge apparatus
US3176613A (en) Shaped explosive charge
US3075462A (en) Combination projectile and shaped charge well perforating apparatus