Venting system for a shaped charge in the event of deflagration

Abstract

A shape charge venting apparatus and method for venting gases generated during deflagration. The venting apparatus and method including vent grooves inside the shape charge providing a pathway for deflagration gases to escape the shape charge. The venting apparatus and method also may include using a retainer ring in addition to the vent groove in order to hold the components of the shape charge in place. The venting of the gases during deflagration facilitates pressure relief within the shape charge and increases safety from accidental detonation during a fire.

Claims

1. A shape charge assembly comprising: a case with at least one cylindrical opening and an inner cavity defined by an inner wall having a cylindrical portion and a concave portion; a liner having a liner apex and a liner skirt located proximate to the inner wall; at least one longitudinal inner facing vent groove in the cylindrical portion only, of the inner wall; an explosive material in contact with the inner wall and in contact with the at least one vent groove; wherein the liner skirt is adjacent to the inner wall, and the explosive material is adjacent to the inner wall and the liner; and wherein the at least one vent groove vents gases along the inner wall, around the liner skirt, and towards the cylindrical opening.

2. The assembly according to claim 1, wherein the liner skirt has an interference fit with the inner wall.

3. The assembly according to claim 1, wherein the at least one vent groove is adapted to vent gases across the inner wall.

4. The assembly according to claim 3, wherein the at least one vent groove is a plurality of vent grooves.

5. The assembly according to claim 1, wherein the at least one vent groove is adapted to prevent a high energy release during the deflagration of the explosive material.

6. The assembly according to claim 1, further comprising a retainer ring that prevents the liner from moving in relation to the case.

7. The assembly according to claim 6, wherein the retainer ring has an interference fit with the inner wall.

8. The assembly according to claim 7, wherein the at least one vent groove is a plurality of vent grooves adapted to prevent a high energy release during the deflagration of the explosive material.

9. The assembly according to claim 1, wherein the at least one vent groove is located in the inner wall such that the vent groove is adjacent to the liner skirt.

10. The assembly according to claim 9, wherein the at least one vent groove is a plurality of vent grooves.

11. A shape charge case comprising: at least one conical cross sectioned portion with a first opening and a second opening; at least one cylindrical cross sectioned portion having a third opening, a fourth opening, and an inner wall; and at least one longitudinal inner facing vent groove along a portion of the inner wall of the cylindrical cross sectioned portion only, wherein the vent groove vents gases within the shape charge case; and wherein the conical cross sectioned portion is adjacent to the cylindrical cross sectioned portion whereby the second opening and the third opening are adjacent and whereby the fourth opening is larger than the first opening.

12. The apparatus according to claim 11, wherein the at least one vent groove is adapted to vent gases around a liner skirt positioned adjacent to the vent groove.

13. The apparatus according to claim 12, wherein the at least one vent groove comprises a plurality of vent grooves which are spaced equally around the center axis of the cylindrical portion.

14. The apparatus according to claim 11, wherein the at least one vent groove is adapted to vent pressure across the inner wall.

15. The apparatus according to claim 11, wherein the case is further adapted to accept a retainer ring.

16. The apparatus according to claim 11, wherein the case is further adapted to contain a liner and an explosive material.

17. The apparatus according to claim 11, wherein the at least one vent groove is forged into the inner wall.

18. A shape charge assembly comprising: a case with at least one opening, at least one inner diameter, and at least one longitudinal inner facing vent groove in a cylindrical cross-sectioned portion only of an inner wall of the case; an explosive material; a retainer ring with an outer diameter larger than the at least one inner diameter of the case; a liner with a liner skirt having an outer diameter larger than the at least one inner diameter of the case; wherein the movement of the liner and explosive material is restricted by the retainer ring's interference fit with the case; and wherein the liner skirt is adjacent to and in contact with the vent groove where at least a portion of the liner skirt does not contact inner wall, and the explosive material is adjacent to the inner wall and the liner.

19. The assembly according to claim 18, wherein the retainer ring is placed adjacent to the liner skirt.

20. The assembly according to claim 19, wherein the retainer ring is adapted to allow venting around the liner skirt.

21. The assembly according to claim 20, wherein the retainer ring contains at least one vent hole.

22. The assembly according to claim 21, wherein the retainer ring's material composition is substantially similar to the liner's material composition.

23. The assembly according to claim 18, wherein the at least one vent groove is adapted to vent gases around the liner skirt.

24. The assembly according to claim 23, wherein the at least one vent groove is a plurality of vent grooves.

25. A shape charge case comprising: at least one conical cross sectioned portion with an apex having a first opening; at least one cylindrical cross sectioned portion having an inner surface and a second opening larger than the first opening; and at least one longitudinal inner facing vent groove cut along a portion of the inner surface of the cylindrical cross sectioned portion only; and wherein the at least one conical cross section is located coaxial with and adjacent to the at least one cylindrical cross section portion, wherein the two portions are integral and form a shaped charge case with an apex end first opening and a second opening, opposite of the apex end first opening.

26. The apparatus according to claim 25, wherein the at least one vent groove is a plurality of vent grooves.

27. The apparatus according to claim 26, wherein the plurality of vent grooves is adapted to vent gas along the inner surface.

28. The apparatus according to claim 27, wherein the plurality of vent grooves is further adapted to prevent pressure buildup in the case.

29. The apparatus according to claim 28, wherein the plurality of vent grooves are formed in a forging process.

30. The apparatus according to claim 25, wherein the at least one vent groove is the length of the cylindrical cross sectioned portion.

31. The apparatus according to claim 25, wherein the case is further adapted to contain a liner having a liner skirt.

32. The apparatus according to claim 31, wherein the liner is position such that the liner skirt is adjacent to the inner surface.

33. The apparatus according to claim 32, wherein the at least one vent groove is positioned adjacent to the liner skirt.

34. The apparatus according to claim 33, wherein the at least one vent groove is adapted to vent gas around the liner skirt.

35. The apparatus according to claim 34, wherein the at least one vent groove is a plurality of vent grooves.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) For a thorough understating of the present invention, reference is made to the following detailed description of the preferred embodiments, taken in conjunction with the accompanying drawings in which reference numbers designate like or similar elements throughout the several figures of the drawing. Briefly:

(2) FIG. 1 is an axial cross-section of an example shape charge assembly with vent grooves.

(3) FIG. 2a is a top view of an example shape charge case with a vent groove.

(4) FIG. 2b is an axial cross-section of an example shape charge case with a vent groove.

(5) FIG. 3 is an axial cross-section of an example shape charge with a vent groove and a ring groove containing a retainer ring.

DETAILED DESCRIPTION OF THE DRAWINGS

(6) In the following description, certain terms have been used for brevity, clarity, and examples. No unnecessary limitations are to be implied therefrom and such terms are used for descriptive purposes only and are intended to be broadly construed. The different systems and method steps described herein may be used alone or in combination with other systems and method steps. It is to be expected that various equivalents, alternatives, and modifications are possible within the scope of the appended claims.

(7) FIG. 1 illustrates an example of a shaped charge 9 for well pipe and formation perforation. A shape charge 9 generally comprises at least a case 10, a liner 16, and an explosive material 12 placed in between the case 10 and the liner 16. The case 10 serves as a containment vessel designed to hold the detonation force of the detonating explosive material 12 long enough for a perforating jet to form from the liner 16. The perforating jet is capable of penetrating metal and/or rock. The case 10 has an inner wall 33 and an outer wall 34. The case has a relatively large open front end 36 and a smaller open primer end 35. Common materials used for the case 10 include steel, zinc, aluminum, ceramics and glass.

(8) Explosive material 12 is contained inside the outer case 10 and integrally fills the space between the inside surface of the outer case and the external surface of a concave liner 16. The explosive charge may be detonated by a variety of methods that are well known in the art. The explosive material 12 may be one or a combination of compositions known in the art by trade designations such as HMX, HNS, PETN, PATB and HTX.

(9) The liner 16 of a typical shaped charge is internally open. When the explosive charge 12 is detonated, the force of the detonation collapses the liner 16 into the internal space 41 and causes it to be ejected from the case 10 as a very high velocity plasma jet. The high velocity plasma jet then exits the case via the front end 36.

(10) The liner 16 of the present invention is preferably formed from a mixture of powdered metals such as copper and lead. Other powdered metals may be included or substituted such as brass, bismuth, tin, zinc, silver, antimony, cobalt, nickel, tungsten, uranium or other malleable, ductile metals in proportions and formulations known to a person of ordinary skill in the art. It is also known to include certain plastics or polymers in the liner mixture.

(11) Although the liner 16 is preferably formed from a mixture of powdered metals, those of ordinary skill will understand that the invention objectives may be served by a solid material form of metal alloy that is stamped, forged, machined, molded, layered or otherwise formed.

(12) The case 10 has one or more vent grooves 21 that are drilled into the inner wall 33 of the case 10. The vent grooves 21 allow for gases to escape from inside the case to the outside of the case when the explosive material is in place. The vent hole can be a singular hole or a plurality of holes. The vent groove 21 can be cylindrical in shape, rectangular in shape, or some other shape that is well known in the art. The vent groove 21 may be manufactured by a variety of methods that are well known in the art and suitable for the materials used to make the case, including but not limited to stamping, forging, and machining.

(13) FIG. 2a illustrates an example shape charge case 10 viewed from the top. The vent grooves 21 are spaced about the center axis. There is an inner wall 33 and an outer wall 34. The vent grooves 21 in this example are machined into the inner wall 33, however the vent grooves 21 may be formed by a variety of manufacturing methods including machining, stamping, forging, electrical discharge machining, or other methods known in the art.

(14) FIG. 2b illustrates an example shape charge case 10 viewed as a cutaway from the side. The vent grooves 21 are machined into the inner wall 33. The vent grooves 21 are long enough such that a sufficient channel is created along the inner wall 33 in order to relieve pressure building up inside the shape charge due to heat and/or deflagration of the explosive material 12.

(15) FIG. 3 illustrates an assembly with all of the components for a shape charge, including the explosive material 12 and the liner 16. FIG. 3 also shows a retainer ring 23 in place that restricts the movement of the explosive material and liner in relation to the case 10. The case has a ring groove 24 that is capable of accepting one or more rings 23 of various geometries. In at least one embodiment the retainer ring 23 has an interference fit with the ring groove 24.

(16) In another embodiment, there is no retainer ring and instead the liner 16 is held in place by an interference fit between the liner 16 and the inner wall 33 of the case 10. In this configuration, the liner has an outer diameter that is slightly larger than the inner diameter of the case 10. The explosive material 12 is put into place and then the liner 16 is pressed in using methods well known in the art. The interference fit allows for the liner 16 to be frictionally engaged with the case 10.

(17) In another embodiment there is no retainer ring and instead the liner 16 is held in place by an adhesive applied to the top of the liner skirt 43. The adhesive is commonly used in the art.

(18) In another embodiment, the liner 16 is engaged to the case 10 by an interference fit between the liner 16 and the inner wall 33 of the case 10. In addition, there is a retainer ring 23 placed above the liner 16 to further hold the liner 16 and explosive material 12 in place. The retainer ring 23 is sized such that the outer diameter is larger than the inner diameter of the inner wall 33.

(19) In another embodiment the liner 16 is held in place by a retainer ring 23 placed in the ring groove 24. The retainer ring 23 is sized such that the ring fits tightly within the ring groove 24 and prevents the liner 16 from moving axially in relation to the case 10.

(20) In another embodiment, the liner 16 is held in place by a retainer ring 23 placed in the ring groove 24 whereby the retainer ring 23 is sized to have an interference fit within the ring groove 24, thereby preventing the liner 16 from moving axially in relation to the case 10.

(21) In another embodiment the retainer ring 23 can be a snap ring design as commonly used by a person of ordinary skill in the art. A person of ordinary skill in the art will understand that a snap ring has a gap that allows it to be compressed or expanded in order to install as required.

(22) In another embodiment, the retainer ring 23 can be a wave shaped ring. The wave shaped ring uses a wave design such that when it is installed in place in the ring groove 24, there will exist gaps between the wave retainer ring 23 and the ring groove 24, allowing for gases to exit the case 10 with minimal pressure buildup when exposed to heat and/or deflagration. The retainer ring 23 is installed in ring groove 24 with the explosive material 12 and liner 16 in place.

(23) In another embodiment, the retainer ring 23 can contain one or more vent holes. These vent holes allow for the gases to exit the case 10 with minimal pressure buildup when exposed to heat and/or deflagration. The retainer ring 23 is installed in ring groove 24 with the explosive material 12 and liner 16 in place.

(24) The material of the retainer ring 23 may include one or more of the material steel, zinc, aluminum, plastic, or a polymer. It is preferable that the material of the retainer ring 23 is the same or substantially similar to the material of the liner 16.

(25) Although the invention has been described in terms of particular embodiments which are set forth in detail, it should be understood that this is by illustration only and that the invention is not necessarily limited thereto. Alternative embodiments and operating techniques will become apparent to those of ordinary skill in the art in view of the present disclosure. Accordingly, modifications of the invention are contemplated which may be made without departing from the spirit of the claimed invention. In particular, use of the terms vent groove, ring, liner, ring groove, explosive material, deflagration, and vent herein and within the claims to follow is defined expansively to encompass equivalent terms that are well known in the art.