US3327630A - Vented shaped charge case - Google Patents
Vented shaped charge case Download PDFInfo
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- US3327630A US3327630A US532605A US53260566A US3327630A US 3327630 A US3327630 A US 3327630A US 532605 A US532605 A US 532605A US 53260566 A US53260566 A US 53260566A US 3327630 A US3327630 A US 3327630A
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- case
- container
- shaped charge
- cover
- shaped
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- 239000007789 gas Substances 0.000 claims description 26
- 238000013022 venting Methods 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 8
- 230000013011 mating Effects 0.000 description 9
- 238000007789 sealing Methods 0.000 description 9
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 239000002360 explosive Substances 0.000 description 6
- 239000012530 fluid Substances 0.000 description 4
- 239000007788 liquid Substances 0.000 description 3
- 230000035508 accumulation Effects 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 2
- 238000005474 detonation Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000008188 pellet Substances 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000012466 permeate Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 210000004907 gland Anatomy 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 210000002445 nipple Anatomy 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/08—Blasting cartridges, i.e. case and explosive with cavities in the charge, e.g. hollow-charge blasting cartridges
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B43/00—Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
- E21B43/11—Perforators; Permeators
- E21B43/116—Gun or shaped-charge perforators
- E21B43/117—Shaped-charge perforators
Definitions
- this invention relates to shaped charges; and, more particularly, to means for safely relieving hazardous accumulations of gases under pressure from within unfired encapsulated shaped charges as they are being removed from a well bore.
- encapsulated shaped charge One of the most commonly used perforating devices employed today for perforating wells is the so-called encapsulated shaped charge.
- Such encapsulated shaped charges are typically comprised of a hollow container in which a shaped explosive and liner are mounted, with a cover fluidly sealing the forward end of the container.
- the charges are customarily linked together as shown in Patent No. 3,100,443 or mounted either on a so-cal led strip carrier (such as described in Patent No. 3,048,101) or between a spaced pair of fairly stiff, but somewhat flexible, support members (such as those in Patent No. 3,282,213).
- Cast aluminum is one of the more popular materials used for fabricating such shaped charge cases since it is easily machined and less expensive than most other materials as well as leaves only minimum amounts of debris in a well upon detonation of the charges. Those skilled in the art do appreciate, however, that most cast aluminum alloys are more or less gas-pervious. Thus, as an aluminum shaped charge case is lowered either into a ga-filled well bore or into one containing liquids with gases in solution, the high well bore pressures will slowly force gases through the walls of the case which, of course, is initially at atmospheric pressure.
- the upper end of the production tubing is typically capped with a so-called lubricator assembly which includes an exposed upright pipe having a pressure-sealing gland at its upper end adapted to tightly seal around a suspension cable and suitable valving 'at its lower end to permit the introduction and removal of cable-suspended tools into and out of the well.
- a so-called lubricator assembly which includes an exposed upright pipe having a pressure-sealing gland at its upper end adapted to tightly seal around a suspension cable and suitable valving 'at its lower end to permit the introduction and removal of cable-suspended tools into and out of the well.
- the lubricator pressure must be bled-off more rapidly than could possibly be afforded to decompress the unfired shaped charges.
- the pressure exterior of the unfired shaped charges will be reduced much faster than the accumulated gases can possibly permeate back through the aluminum cases.
- This rapid depressuring will usually cause one or more of the caps to be displaced as far as the clearance between the shaped charges and internal wall of the lubricator will permit.
- the obvious hazard of removing a tightly stuck perforator with live charges and detonators from a lubricator needs no description to be fully appreciated.
- a hollow shaped charge case formed of gas-pervious material with means that are selectively operable for venting accumulated gases from within the case whenever the differential between the interior pressure and the ambient pressure exterior of the case is sufiicient to actuate the venting means.
- an otherwise conventional shaped charge case is provided with venting means for releasing accumulated gases from within the case should it be necessary to retrieve the shaped charge from a Well bore before detonating it.
- the venting means include one or more passages through the case and sealing means that fluidly seal the passages against entrance of fluids into the case but which open in response to a higher pressure within the case to release any accumulated gases therefrom.
- FIG. 1 is a partially cross-sectioned view of a shaped charge enclosed within a case of a gas-pervious material and arranged in accordance with the present invention
- FIG. 2 is a plan view of the forward end of the container shown in FIG. 1;
- FIG. 3 is a plan view similar to FIG. 2, but showing an alternate embodiment of a container arranged in accordance with the present invention.
- FIG. 4 is a partially cross-sectioned view similar to FIG. 1, but showing still another embodiment of the present invention.
- an encapsulated shaped charge 11 is shown comprised of a two-part case 11 of a gas-pervious material, such as aluminum or the like, and having a dished cover 12 snugly fitted over the forward portion 13 of a generally cylindrical hollow container 14 in which a preformed explosive pellet 15 is disposed.
- the cover 12 and container 14 together the cover is counterbored, at 16, for receiving the forward portion 13 of the container.
- the forward end of the explosive pellet 15 is formed in a generally conical, forwardly diverging, coaxial hollow that receives a complementarily shaped metal liner 17.
- a booster explosive 18 is received within a shallow axial recess 19 formed in the internal surface of the rear wall 20 of the container 14.
- a spaced pair of rearwardly extending longitudinal lugs 21 are provided for securing a det-onating cord 22 against the external surface of the rear Wall of the container 14 immediately opposite to the booster explosive 18.
- One or more sets of longitudinally spaced lateral lugs 23 and 24 are provided on opposite sides of the container 14 and spaced to the rear of a circumferential flange 25 around the central portion of the container to define grooves for receiving a support 26.
- venting means 27 in accordance with the present invention.
- the venting means 27 include a circumferential groove 28 defined by the forward face 29 of the container flange 25 and the rearward marginal face .30 of the cover 12.
- Longitudinal grooves 31 are extended along the exterior surface of the forward container portion 13 from between the forward flange face 29 to transverse notches 32 across the forward face 33 of the forward container portion.
- a rearwardly directed circumferential skirt 35 of a reduced external diameter may be provided around the rear marginal face 30 of the cover 12 so as to substantially cover the longitudinal grooves 31 as shown in FIG. 1. It will be recognized, however, that even though the circumferential skirt 35 is over the longitudinal grooves 31, there will be slight annular clearance, as at 36, between the rearwardmost edge of the skirt and the forward face 29 of the container flange 25.
- FIG. 3 an alternate embodiment is shown of a container 11' that is otherwise similar to that shown in FIGS. 1 and 2, with the same reference numerals being used but with prime marks to designate equivalent portions.
- the longitudinal grooves 31 may be substituted by flats 31' formed tangentially across the exterior surface of the forward container portion 13 and meeting the transverse slots 32. These flats 31', of course, will provide sufficient clearance between the mating surfaces of the cover (not shown) and container 14'.
- FIG. 4 an alternate embodiment is shown of still another shaped charge 10 that is otherwise similar to that shown in FIGS. 1-3, but with double prime marks denoting equivalent elements.
- this alternate embodirnent however, the previously described passages, such as the grooves 31 or flats 31 along the external surfaces of the forward container portions 13 and 13, are replaced by similarly arranged passages, such as flats or longitudinal grooves 31", in the internal mating surface of the cover 12".
- the shaped charge 10" is otherwise the same as that in FIGS. l-3.
- the O-rings 34-34" will fluidly seal the passage means (31-32, 31-32 or 31"-32") to prevent entrance of fluids from the well bore into the interior of the shaped charge cases 11-11.
- gases can and will gradually permeate through the permeable metal of the cases 11-11 and slowly accumulate therein. The pressure of these gases will, of course, be whatever the ambient fluid pressure is around the shaped charges 10-10. Should the shaped charges 10-10 be detonated in the expected manner, the presence of gases therein will not materially affect the performance of the shaped charge.
- This release may occur several times during the ascent of the shaped charges 1(1-10.
- a suflicient quantity of these trapped gases will have been vented from the interior of the cases 11-11" to prevent the displacement of the covers 12-12" relative to the containers 14-14".
- the venting means 27- 27" will have operated one or more times to release accumulated gases from the cases 11-11".
- the present invention has provided new and improved means for preventing entrapped gases within a shaped charge case from displacing the cover relative to the container before the pressure differential between the interior and exterior of a shaped charge case has reached an excessive magnitude otherwise suflficient to displace the cover relative to the container.
- a shaped charge may be safely withdrawn from a well bore with its cover still firmly in position.
- Shaped charge apparatus comprising: a hollow case having at least a portion of a gas-pervious material; shaped charge means in said case; means sealingly enclosing said shaped charge means within said case; and venting means for releasing accumulated gases from within the enclosed interior of said case whenever the pressure exterior of said case is lower than that in said enclosed intrior.
- said case includes a cover and a container adapted to be joined together and wherein said gas-venting means include resilient sealing means fluidly sealing said cover and container to one another at their junction.
- gas-venting means further include passage means between the interior of said case and said junction of said cover and container.
- said case includes a container and a cover having complementarily-fitting portions adapted to be joined together along mating surfaces and each defining an opposed marginal surface, and wherein said gas-venting means include resilient sealing means fluidly sealed between said marginal surfaces around said complementarily-fitting portions.
- gas-venting means further include passage means between the interior of said case and the enclosed space between said resilient sealing means and said complementarily-fitting portions.
- Shaped charge apparatus comprising: a hollow case adapted to sealingly enclose an explosive charge and including a cover and a container of a gas-pervious material, said container having a peripheral flange providing a forwardly-directed marginal surface and a cylindrical portion forward of said peripheral flange, said cover having a rearwardly-directed marginal surface defining the entrance of a cylindrical bore therein adapted to receive said forward container portion, said forward container portion and cylindrical bore having complementary mating surfaces adapted for snugly inter-fitting said cover and container to one another; and passage means along one of said mating surfaces adapted for providing communication between the interior of said case and the space between said marginal surfaces when said cover is fitted onto said container.
- the apparaus of claim 9 further including shaped charge means in said case; and resilient sealing means in said space and sealingly engaged with each of said opposed surfaces exterior of said passage means.
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- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Mining & Mineral Resources (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Environmental & Geological Engineering (AREA)
- Fluid Mechanics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
June 27, 1967 w T. BELL 3,32
VENTED SHAPED CHARGE CASE Filed March 8, 1966 I BY z Arro/r/v United States Patent O 3,327,630 VENTED SHAPED CHARGE CASE William T. Bell, Houston, Tex., assignor to Schlumberger Technology Corporation, Houston, Tex., a corporation of Texas Filed Mar. 8, 1966, Ser. No. 532,605 12 Claims. (Cl. 10224) ABSTRACT OF THE DISCLOSURE This disclosure describes various means by which gases that may have entered a fluidly sealed but gas-pervious shaped charge container can be safely vented therefrom without danger should the shaped charge be returned to the surface without being detonated.
Accordingly, as will subsequently become apparent, this invention relates to shaped charges; and, more particularly, to means for safely relieving hazardous accumulations of gases under pressure from within unfired encapsulated shaped charges as they are being removed from a well bore.
One of the most commonly used perforating devices employed today for perforating wells is the so-called encapsulated shaped charge. Such encapsulated shaped charges are typically comprised of a hollow container in which a shaped explosive and liner are mounted, with a cover fluidly sealing the forward end of the container. The charges are customarily linked together as shown in Patent No. 3,100,443 or mounted either on a so-cal led strip carrier (such as described in Patent No. 3,048,101) or between a spaced pair of fairly stiff, but somewhat flexible, support members (such as those in Patent No. 3,282,213). Once they are mounted and all connections made, the shaped charges are lowered into a well bore from an electrical cable and positioned adjacent to a particular interval of formations. Then, once they are calculated to be correctly positioned, the shaped charges are detonated to produce the desired perforations through the casing and cement sheath therearound.
Cast aluminum is one of the more popular materials used for fabricating such shaped charge cases since it is easily machined and less expensive than most other materials as well as leaves only minimum amounts of debris in a well upon detonation of the charges. Those skilled in the art do appreciate, however, that most cast aluminum alloys are more or less gas-pervious. Thus, as an aluminum shaped charge case is lowered either into a ga-filled well bore or into one containing liquids with gases in solution, the high well bore pressures will slowly force gases through the walls of the case which, of course, is initially at atmospheric pressure.
This accumulation of gases normally poses no particular problem so long as the shaped charge is detonated in the usual manner. It is not too uncommon, however, for some malfunction, as for example a defect in the detonating system, to prevent detonation of one or more of the shaped charges. It will be appreciated, however, that although the exterior ambient pressure in a well with liquid decreases as the unfired shaped charges are withdrawn from a well bore, the gases filling the interior of the cases will not escape as readily as they entered. Since time does not usually permit the unfired charges to be removed as slowly as they Were lowered into a well, the interior of the cases will instead usually remain at a fairly high pressure that may be in the order of several hundreds or even thousands of pounds/square inch as the shaped charges are raised. Thus, as the shaped charges near the surface, it is not at all uncommon for the pressure differential from their interiors to the exterior to become sufliciently high to displace the cover of the cases at least partially, if not entirely, off of the containers.
Where the perforating apparatus must be withdrawn through narrow confines, such as a small tubing string or a seating nipple, one or more covers may have been displaced sufficiently to prevent the further passage of the apparatus. In addition to many other obvious disadvantages, such an occurrence, of course, requires a time-consuming fishing operation which, if unsuccessful, could necessitate the abandonment of a substantial portion of the perforating apparatus in the well Ibore. This, is, of course, neither desired nor wanted. Similarly, even if the gas-filled shaped charges are eventually recovered with the caps in place, they still present an obvious hazard to those conducting the operation.
Where a perforating operation is conducted in a gas well under pressure, the upper end of the production tubing is typically capped with a so-called lubricator assembly which includes an exposed upright pipe having a pressure-sealing gland at its upper end adapted to tightly seal around a suspension cable and suitable valving 'at its lower end to permit the introduction and removal of cable-suspended tools into and out of the well. Thus, when perforating apparatus is being removed from such a well with live charges, the apparatus is first pulled up into the lubricator and the valves therebelow closed.
It is, of course, then necessary to bleed-oh the gas pressure in the lubricator before the perforating apparatus can be removed.
In such instances, to save time, the lubricator pressure must be bled-off more rapidly than could possibly be afforded to decompress the unfired shaped charges. Thus, the pressure exterior of the unfired shaped charges will be reduced much faster than the accumulated gases can possibly permeate back through the aluminum cases. This rapid depressuring will usually cause one or more of the caps to be displaced as far as the clearance between the shaped charges and internal wall of the lubricator will permit. The obvious hazard of removing a tightly stuck perforator with live charges and detonators from a lubricator needs no description to be fully appreciated.
Accordingly, it is an object of the present invention to provide means for releasing accumulated gases at high pressure from within encapsulated shaped charges as they are being withdrawn from a well bore.
This and other objects of the present invention are obtained by providing a hollow shaped charge case formed of gas-pervious material with means that are selectively operable for venting accumulated gases from within the case whenever the differential between the interior pressure and the ambient pressure exterior of the case is sufiicient to actuate the venting means. In one manner of accomplishing this, an otherwise conventional shaped charge case is provided with venting means for releasing accumulated gases from within the case should it be necessary to retrieve the shaped charge from a Well bore before detonating it. The venting means include one or more passages through the case and sealing means that fluidly seal the passages against entrance of fluids into the case but which open in response to a higher pressure within the case to release any accumulated gases therefrom.
The novel features of the present invention are set forth with particularity in the appended claims. The present invention, both as to its organization and manner of operation together with further objects and advantages thereof, may best be understood by way of illustration and example of certain embodiments when taken in conjunction with the accompanying drawings, in which:
FIG. 1 is a partially cross-sectioned view of a shaped charge enclosed within a case of a gas-pervious material and arranged in accordance with the present invention;
FIG. 2 is a plan view of the forward end of the container shown in FIG. 1;
FIG. 3 is a plan view similar to FIG. 2, but showing an alternate embodiment of a container arranged in accordance with the present invention; and
FIG. 4 is a partially cross-sectioned view similar to FIG. 1, but showing still another embodiment of the present invention.
Turning now to FIG. 1, in one embodiment of the present invention, an encapsulated shaped charge 11) is shown comprised of a two-part case 11 of a gas-pervious material, such as aluminum or the like, and having a dished cover 12 snugly fitted over the forward portion 13 of a generally cylindrical hollow container 14 in which a preformed explosive pellet 15 is disposed. To secure the cover 12 and container 14 together, the cover is counterbored, at 16, for receiving the forward portion 13 of the container. By suitably dimensioning the mating portions to provide, for example, an interference fit, the
As is typical, the forward end of the explosive pellet 15 is formed in a generally conical, forwardly diverging, coaxial hollow that receives a complementarily shaped metal liner 17. A booster explosive 18 is received within a shallow axial recess 19 formed in the internal surface of the rear wall 20 of the container 14. A spaced pair of rearwardly extending longitudinal lugs 21 are provided for securing a det-onating cord 22 against the external surface of the rear Wall of the container 14 immediately opposite to the booster explosive 18. One or more sets of longitudinally spaced lateral lugs 23 and 24 are provided on opposite sides of the container 14 and spaced to the rear of a circumferential flange 25 around the central portion of the container to define grooves for receiving a support 26.
The case 11, which is otherwise conventional, is provided with venting means 27 in accordance with the present invention. The venting means 27 include a circumferential groove 28 defined by the forward face 29 of the container flange 25 and the rearward marginal face .30 of the cover 12. Longitudinal grooves 31 are extended along the exterior surface of the forward container portion 13 from between the forward flange face 29 to transverse notches 32 across the forward face 33 of the forward container portion.
Thus, it will be seen that although the cover 12 is tightly fitted over the forward container portion 13, direct communicaiton is provided through the passages 31 and 32 between the interior of the case 11 and the circumferential groove 28. By fitting resilient sealing means, such as an O-ring 34, into the circumferential groove 28, it will be appreciated that a greater external fluid pressure will urge the O-ring tightly against the opposed faces 29 and as well as the longitudinal surface therebetween. On the other hand, should there be a greater internal pressure within the case 11 than that outside, such a greater internal pressure will displace the O-ring 34 radially outwardly a sufficient distance to bleed-off any trapped pressure.
If it is preferred, a rearwardly directed circumferential skirt 35 of a reduced external diameter may be provided around the rear marginal face 30 of the cover 12 so as to substantially cover the longitudinal grooves 31 as shown in FIG. 1. It will be recognized, however, that even though the circumferential skirt 35 is over the longitudinal grooves 31, there will be slight annular clearance, as at 36, between the rearwardmost edge of the skirt and the forward face 29 of the container flange 25.
Turning now to FIG. 3, an alternate embodiment is shown of a container 11' that is otherwise similar to that shown in FIGS. 1 and 2, with the same reference numerals being used but with prime marks to designate equivalent portions. In this alternate embodiment, the longitudinal grooves 31 may be substituted by flats 31' formed tangentially across the exterior surface of the forward container portion 13 and meeting the transverse slots 32. These flats 31', of course, will provide sufficient clearance between the mating surfaces of the cover (not shown) and container 14'.
Turning now to FIG. 4, an alternate embodiment is shown of still another shaped charge 10 that is otherwise similar to that shown in FIGS. 1-3, but with double prime marks denoting equivalent elements. In this alternate embodirnent, however, the previously described passages, such as the grooves 31 or flats 31 along the external surfaces of the forward container portions 13 and 13, are replaced by similarly arranged passages, such as flats or longitudinal grooves 31", in the internal mating surface of the cover 12". The shaped charge 10" is otherwise the same as that in FIGS. l-3.
Accordingly, it will be appreciated that whenever one of the shaped charges 10-16" as shown in FIGS. 1-4 is lowered into a well bore, the O-rings 34-34" will fluidly seal the passage means (31-32, 31-32 or 31"-32") to prevent entrance of fluids from the well bore into the interior of the shaped charge cases 11-11. As previously described, as the shaped charges 10-10" are lowered into the well bore, gases can and will gradually permeate through the permeable metal of the cases 11-11 and slowly accumulate therein. The pressure of these gases will, of course, be whatever the ambient fluid pressure is around the shaped charges 10-10. Should the shaped charges 10-10 be detonated in the expected manner, the presence of gases therein will not materially affect the performance of the shaped charge.
Should it be necessary, however, to retrieve one of the shaped charges 111-111" from a well bore containing liquid without its having been detonated, the exterior ambient pressure around the shaped charge will diminish as it is raised. Inasmuch as accumulated gases within the shaped charge cases 11-11 cannot readily escape, however, the pressure differential between the interior of the case and their exterior will gradually increase, Then, once this pressure differential has reached an amount sufficient to expand the O-rings 34-34", the O-ring will be displaced radially outwardly at least a distance sufiicient to uncover the outer end of the passage means (31-32, 31'32' or 31"-32") and release at least a portion of the accumulated gases.
This release may occur several times during the ascent of the shaped charges 1(1-10. Thus, by the time that the shaped charges 10-10" have reached the surface, a suflicient quantity of these trapped gases will have been vented from the interior of the cases 11-11" to prevent the displacement of the covers 12-12" relative to the containers 14-14". Similarly, where the well bore is filled with high pressure gases, as the pressure in the aforementioned lubricator is relieved, the venting means 27- 27" will have operated one or more times to release accumulated gases from the cases 11-11".
Accordingly, it will be appreciated that the present invention has provided new and improved means for preventing entrapped gases within a shaped charge case from displacing the cover relative to the container before the pressure differential between the interior and exterior of a shaped charge case has reached an excessive magnitude otherwise suflficient to displace the cover relative to the container. In this manner, by venting off any accumulated gases whenever the pressure differential reaches a magnitude less than that necessary to displace the cover, a shaped charge may be safely withdrawn from a well bore with its cover still firmly in position.
While particular embodiments of the present invention have been shown and described, it is apparent that changes and modifications may be made without departing from this invention in its broader aspects; and, therefore, the aim in the appended claims is to cover all such changes and modifications as fall within the true spirit and scope of this invention.
What is claimed is:
1. Shaped charge apparatus comprising: a hollow case having at least a portion of a gas-pervious material; shaped charge means in said case; means sealingly enclosing said shaped charge means within said case; and venting means for releasing accumulated gases from within the enclosed interior of said case whenever the pressure exterior of said case is lower than that in said enclosed intrior.
2. The apparatus of claim 1 wherein said case includes a cover and a container adapted to be joined together and wherein said gas-venting means include resilient sealing means fluidly sealing said cover and container to one another at their junction.
3. The apparatus of claim 2 wherein said gas-venting means further include passage means between the interior of said case and said junction of said cover and container.
4. The apparatus of claim 1 wherein said case includes a container and a cover having complementarily-fitting portions adapted to be joined together along mating surfaces and each defining an opposed marginal surface, and wherein said gas-venting means include resilient sealing means fluidly sealed between said marginal surfaces around said complementarily-fitting portions.
5. The apparatus of claim 4 wherein said gas-venting means further include passage means between the interior of said case and the enclosed space between said resilient sealing means and said complementarily-fitting portions.
6. The apparatus of claim 5 wherein said passage means extend along a mating surface of one of said complementarily-fitting portions.
7. The apparatus of claim 5 wherein said passage means extend along the mating surface of said cover portion.
8. The apparatus of claim 5 wherein said passage means extend along the mating surface of said container portion.
9. Shaped charge apparatus comprising: a hollow case adapted to sealingly enclose an explosive charge and including a cover and a container of a gas-pervious material, said container having a peripheral flange providing a forwardly-directed marginal surface and a cylindrical portion forward of said peripheral flange, said cover having a rearwardly-directed marginal surface defining the entrance of a cylindrical bore therein adapted to receive said forward container portion, said forward container portion and cylindrical bore having complementary mating surfaces adapted for snugly inter-fitting said cover and container to one another; and passage means along one of said mating surfaces adapted for providing communication between the interior of said case and the space between said marginal surfaces when said cover is fitted onto said container.
10. The apparatus of claim 9 wherein said cover and container are of cast aluminum.
11. The apparaus of claim 9 further including shaped charge means in said case; and resilient sealing means in said space and sealingly engaged with each of said opposed surfaces exterior of said passage means.
12. The apparatus of claim 11 wherein said cover and container are of cast aluminum.
References Cited UNITED STATES PATENTS 2,891,477 6/1959 Swanson 10220 X 2,984,307 5/1961 Barnes 10220 X 3,040,659 6/1962 McCullough 102-20 BENJAMIN A. BORCHELT, Primary Examiner. V. R. PENDEGRASS, Assistant Examiner.
Claims (1)
1. SHAPED CHARGE APPARATUS COMPRISING: A HOLLOW CASE HAVING AT LEAST A PORTION OF A GAS-PERVIOUS MATERIAL; SHAPED CHARGE MEANS IN SAID CASE; MEANS SEALINGLY ENCLOSING SAID SHAPED CHARGE MEANS WITHIN SAID CASE; AND VENTING MEANS FOR RELEASING ACCUMULATED GASES FROM WITHIN THE ENCLOSED INTERIOR OF SAID CASE WHENEVER THE PRESSURE EXTERIOR OF SAID CASE IS LOWER THAN THAT IN SAID ENCLOSED INTERIOR.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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US532605A US3327630A (en) | 1966-03-08 | 1966-03-08 | Vented shaped charge case |
FR97960A FR1527006A (en) | 1966-03-08 | 1967-03-08 | Advanced training in shaped charges |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US532605A US3327630A (en) | 1966-03-08 | 1966-03-08 | Vented shaped charge case |
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US3327630A true US3327630A (en) | 1967-06-27 |
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Application Number | Title | Priority Date | Filing Date |
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US532605A Expired - Lifetime US3327630A (en) | 1966-03-08 | 1966-03-08 | Vented shaped charge case |
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US (1) | US3327630A (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3636875A (en) * | 1970-06-29 | 1972-01-25 | Schlumberger Technology Corp | Shaped charge devices for wire carriers |
US3965993A (en) * | 1974-09-20 | 1976-06-29 | Schlumberger Technology Corporation | Well bore perforating apparatus |
US3991836A (en) * | 1974-09-20 | 1976-11-16 | Schlumberger Technology Corporation | Well bore perforating apparatus |
FR2370257A1 (en) * | 1976-10-01 | 1978-06-02 | Brown Andrew | EXCAVATION CHARGE CASE |
US4280407A (en) * | 1979-05-21 | 1981-07-28 | C-I-L Inc. | Explosive package assembly |
US4510870A (en) * | 1981-07-27 | 1985-04-16 | The United States Of America As Represented By The Secretary Of The Army | Charge liner construction and method |
US4784061A (en) * | 1987-10-05 | 1988-11-15 | Halliburton Company | Capsule charge locking device |
US4817531A (en) * | 1987-10-05 | 1989-04-04 | Jet Research Center, Inc. | Capsule charge retaining device |
US4881445A (en) * | 1988-09-29 | 1989-11-21 | Goex, Inc. | Shaped charge |
EP0352947A2 (en) * | 1988-07-14 | 1990-01-31 | Halliburton Company | Apparatus and method for retaining a charge in a well perforator |
US6098707A (en) * | 1998-04-24 | 2000-08-08 | The Ensign-Bickford Company | Perforation gun for well casing |
WO2001058832A2 (en) * | 2000-02-03 | 2001-08-16 | Schlumberger Technolgy Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
US20050235859A1 (en) * | 2004-04-08 | 2005-10-27 | Baker Hughes, Incorporated | Low Debris perforating gun system for oriented perforating |
US20080307951A1 (en) * | 2007-06-13 | 2008-12-18 | Baker Hughes Incorporated | Safety vent device |
US20150292306A1 (en) * | 2014-04-15 | 2015-10-15 | Hunting Titan, Inc. | Venting System for a Shaped Charge in the Event of Deflagration |
US9459080B2 (en) | 2013-03-15 | 2016-10-04 | Hunting Titan, Inc. | Venting system for a jet cutter in the event of deflagration |
US10954760B2 (en) * | 2017-11-29 | 2021-03-23 | DynaEnergetics Europe GmbH | Closure member and encapsulated slotted shaped charge with closure member |
US11340047B2 (en) | 2017-09-14 | 2022-05-24 | DynaEnergetics Europe GmbH | Shaped charge liner, shaped charge for high temperature wellbore operations and method of perforating a wellbore using same |
US11378363B2 (en) | 2018-06-11 | 2022-07-05 | DynaEnergetics Europe GmbH | Contoured liner for a rectangular slotted shaped charge |
USD981345S1 (en) | 2020-11-12 | 2023-03-21 | DynaEnergetics Europe GmbH | Shaped charge casing |
US11661824B2 (en) | 2018-05-31 | 2023-05-30 | DynaEnergetics Europe GmbH | Autonomous perforating drone |
US12084962B2 (en) | 2020-03-16 | 2024-09-10 | DynaEnergetics Europe GmbH | Tandem seal adapter with integrated tracer material |
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US2984307A (en) * | 1957-09-27 | 1961-05-16 | Schlumberger Well Surv Corp | Cutting apparatus |
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Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3636875A (en) * | 1970-06-29 | 1972-01-25 | Schlumberger Technology Corp | Shaped charge devices for wire carriers |
US3965993A (en) * | 1974-09-20 | 1976-06-29 | Schlumberger Technology Corporation | Well bore perforating apparatus |
US3991836A (en) * | 1974-09-20 | 1976-11-16 | Schlumberger Technology Corporation | Well bore perforating apparatus |
FR2370257A1 (en) * | 1976-10-01 | 1978-06-02 | Brown Andrew | EXCAVATION CHARGE CASE |
US4280407A (en) * | 1979-05-21 | 1981-07-28 | C-I-L Inc. | Explosive package assembly |
US4510870A (en) * | 1981-07-27 | 1985-04-16 | The United States Of America As Represented By The Secretary Of The Army | Charge liner construction and method |
US4784061A (en) * | 1987-10-05 | 1988-11-15 | Halliburton Company | Capsule charge locking device |
US4817531A (en) * | 1987-10-05 | 1989-04-04 | Jet Research Center, Inc. | Capsule charge retaining device |
EP0352947A3 (en) * | 1988-07-14 | 1991-01-16 | Halliburton Company | Apparatus and method for retaining a charge in a well perforator |
EP0352947A2 (en) * | 1988-07-14 | 1990-01-31 | Halliburton Company | Apparatus and method for retaining a charge in a well perforator |
US4881445A (en) * | 1988-09-29 | 1989-11-21 | Goex, Inc. | Shaped charge |
US6098707A (en) * | 1998-04-24 | 2000-08-08 | The Ensign-Bickford Company | Perforation gun for well casing |
WO2001058832A2 (en) * | 2000-02-03 | 2001-08-16 | Schlumberger Technolgy Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
WO2001058832A3 (en) * | 2000-02-03 | 2002-05-30 | Schlumberger Technolgy Corp | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
US6460463B1 (en) * | 2000-02-03 | 2002-10-08 | Schlumberger Technology Corporation | Shaped recesses in explosive carrier housings that provide for improved explosive performance in a well |
GB2375383A (en) * | 2000-02-03 | 2002-11-13 | Schlumberger Technology Corp | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
AU763218B2 (en) * | 2000-02-03 | 2003-07-17 | Schlumberger Technology B.V. | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
GB2375383B (en) * | 2000-02-03 | 2005-01-05 | Schlumberger Technology Corp | Shaped recesses in explosive carrier housings that provide for improved explosive performance background |
US20050235859A1 (en) * | 2004-04-08 | 2005-10-27 | Baker Hughes, Incorporated | Low Debris perforating gun system for oriented perforating |
US7237486B2 (en) * | 2004-04-08 | 2007-07-03 | Baker Hughes Incorporated | Low debris perforating gun system for oriented perforating |
US20080307951A1 (en) * | 2007-06-13 | 2008-12-18 | Baker Hughes Incorporated | Safety vent device |
WO2008157279A1 (en) * | 2007-06-13 | 2008-12-24 | Baker Hughes Incorporated | Safety vent device |
US7806035B2 (en) | 2007-06-13 | 2010-10-05 | Baker Hughes Incorporated | Safety vent device |
US9459080B2 (en) | 2013-03-15 | 2016-10-04 | Hunting Titan, Inc. | Venting system for a jet cutter in the event of deflagration |
EP3114425B1 (en) * | 2014-03-04 | 2019-08-28 | Hunting Titan, Inc. | Venting system for a jet cutter in the event of deflagration |
US20150292306A1 (en) * | 2014-04-15 | 2015-10-15 | Hunting Titan, Inc. | Venting System for a Shaped Charge in the Event of Deflagration |
EP3132229A4 (en) * | 2014-04-15 | 2017-12-06 | Hunting Titan, Inc. | Venting system for a shaped charge in the event of deflagration |
WO2015160378A1 (en) * | 2014-04-15 | 2015-10-22 | Hunting Titan, Inc. | Venting system for a shaped charge in the event of deflagration |
US10648300B2 (en) | 2014-04-15 | 2020-05-12 | Hunting Titan, Inc. | Venting system for a shaped charge in the event of deflagration |
US11340047B2 (en) | 2017-09-14 | 2022-05-24 | DynaEnergetics Europe GmbH | Shaped charge liner, shaped charge for high temperature wellbore operations and method of perforating a wellbore using same |
US10954760B2 (en) * | 2017-11-29 | 2021-03-23 | DynaEnergetics Europe GmbH | Closure member and encapsulated slotted shaped charge with closure member |
US11492877B2 (en) | 2017-11-29 | 2022-11-08 | DynaEnergetics Europe GmbH | Closure member and encapsulated slotted shaped charge with closure member |
US11661824B2 (en) | 2018-05-31 | 2023-05-30 | DynaEnergetics Europe GmbH | Autonomous perforating drone |
US11378363B2 (en) | 2018-06-11 | 2022-07-05 | DynaEnergetics Europe GmbH | Contoured liner for a rectangular slotted shaped charge |
US12084962B2 (en) | 2020-03-16 | 2024-09-10 | DynaEnergetics Europe GmbH | Tandem seal adapter with integrated tracer material |
USD981345S1 (en) | 2020-11-12 | 2023-03-21 | DynaEnergetics Europe GmbH | Shaped charge casing |
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