Exploding bridge wire detonation wave shaper

Abstract

A jet cutter apparatus and method for using a single bridge wire or a plurality of bridge wires to uniformly detonate a booster and thereby cause a uniform detonation of the explosives adjacent to the liners, thereby causing a uniform compression of the liners to form a uniform plasma jet that is substantially radially perpendicular to the jet cutter.

Claims

1. A shaped charge tubing cutter comprising: a substantially cylindrical housing; a shaped charge explosive having an explosive and a liner; a detonation wave shaper comprising an explosive pellet and an exploding bridge wire contained within the explosive pellet; and wherein the detonation wave shaper fits in a cavity in the center of the shaped charge explosive.

2. The shaped charge tubing cutter of claim 1 wherein the detonation wave shaper further comprises a substantially cylindrical shell encasing the explosive pellet, wherein the exploding bridge wire is substantially coaxial with the explosive pellet.

3. A detonation wave shaper comprising: an explosive pellet; and a plurality of exploding bridge wire segments within the explosive pellet.

4. The detonation wave shaper of claim 3 wherein the explosive pellet is substantially cylindrical in shape.

5. The detonation wave shaper of claim 3 wherein the exploding bridge wire segments are mounted on a printed circuit board.

6. The detonation wave shaper of claim 5 wherein the explosive pellet is substantially cylindrical in shape.

7. The detonation wave shaper of claim 6 wherein the exploding bridge wire segments are substantially coaxial with the explosive pellet cylinder.

8. The detonation wave shaper of claim 3 wherein the exploding bridge wire segments are arranged substantially end-to-end and extend through most of the length of the explosive pellet cylinder.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] 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. Briefly:

[0014] FIG. 1 is an axial cross-section of an example jet cutter.

[0015] FIG. 2 is an axial cross-section of an example booster.

[0016] FIG. 3 is an axial cross-section of an example booster.

[0017] FIG. 4 is an axial cross-section close up of an example jet cutter.

[0018] FIG. 5 is a depiction of the explosive wave moving perpendicular to bridge wire segments.

[0019] FIG. 6 is a view of the bridge wires mounted onto a printed circuit board inside a booster.

[0020] FIG. 7a is a view of a tubular with a curved cut.

[0021] FIG. 7b is a view of a tubular with a straight cut.

DETAILED DESCRIPTION OF THE DRAWINGS

[0022] In the following description, certain terms have been used for brevity, clarity, and examples. No unnecessary limitations are implied and such terms are used for descriptive purposes only and are intended to be broadly construed. The different apparatus 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.

[0023] FIG. 1 illustrates an example jet cutter 10 containing an upper housing 11 and a lower housing 12. The lower housing 12 contains a first compression device 13, a first backer plate 14, a first explosive material 15, a first liner 16, a second liner 17, a second explosive material 18, a second backer plate 19, and a second compression device 20. The lower housing 12 also contains an explosive booster 21 used to initiate the first explosive material 15 and second explosive material 18. Liners 16 and 17 may be composed of combinations of metals including brass, copper, tungsten, and lead.

[0024] Existing oilfield pipe cutters are initiated with a typical 50 Ohm detonator placed in close proximity to the booster 21. As the detonation wave propagates through the booster 21, it advances along the cutter axis 29 downwards, with the lower housing 12 being considered lower than the upper housing 11. This advance of detonation wave is collinear to the axis 29 and perpendicular to the liner axis 30. The perpendicular motion of the detonation wave causes the detonation of the second explosive material 18 before the first explosive material 15, causing the asymmetric collapse of the first liner 16 and second liner 17. Ideally, both the first explosive material 15 and the second explosive material 18 would explode at exactly the same time. The result of asymmetric detonation is that the pipe is cut in a curved shape 81, see FIG. 7a as opposed to a desired straight perpendicular cut 83 in FIG. 7b.

[0025] A curved cut is undesirable for several reasons. First, the top of the curved cut typically exhibits greater flare or expansion of the pipe near the cut. Second, the shortest and most efficient cut is exactly perpendicular to the pipe. Straightening out the profile of the cut could increase the depth of the cut for thicker pipe.

[0026] An exploding bridge wire wave shaper, as depicted in FIG. 2, can be used to create a perpendicular cutting jet. The booster 21 has a shell 31 and an explosive pellet 32. A bridge wire 33 is placed in the center of explosive pellet 32 and shell 31. The bridge wire 33 is confined by the pressed explosive pellet 32. The bridge wire 33 is terminated at end 34 against the shell 31. A booster shell 31 in this example is composed of a conductive material, such as brass. The other end of the bridge wire 33 is electrically connected to a wire 35 that is further electrically connected to a fireset or power source (not shown) that provides the electrical discharge needed to burst or explode the bridge wire 33. When current is applied from the fireset the bridge wire 33 explodes. This explosion causes the explosive pellet 32 to explode along its entire length. The explosion then moves out radially, allowing for the detonation of the explosive material 15 and 18 at the same time. The simultaneous detonation of explosive material 15 and 18 causes the first liner 16 and second liner 17 to collapse on each other simultaneously as well.

[0027] Another example of the invention is shown in FIG. 3 using a shorter, discontinuous bridge wire sections electrically connected in parallel. In this example there are bridge wire segments 51 and 53, located 180 degrees from each other. The bridge wire segments 51 and 53 are mounted onto a printed circuit board (PCB) 52. The bridge wire segments may be soldered into place on the PCB 52. Furthermore, in this example the segments 51 are offset from the segments 53. However, one skilled in the art will appreciate that more than two sets of bridge wire segments can be used. For instance, there could be four bridge wire segments located radially 90 degrees from one set to the next. Furthermore, in this example there are shown five bridge wire segments 51 and five bridge wire segments 53. However, more or less than five bridge wire segments may be used. In this example, there are two sets of bridge wire segments 51 and 53, but there can be variations on this design including a single set of bridge wire segments or a plurality of more than two sets of bridge wire segments.

[0028] The discontinuous bride wire design of FIG. 3 can be installed into a jet cutter as shown in FIG. 4. The leads 54 and 55 eventually connect to a fireset (not shown) that will use an electrical discharge to explode the bridge wire segments 51 and 53. The fireset will send a signal to the PCB 52 via leads 54 and 55. The signal will explode the bridge wire segments 51 and 53. The explosion will cause the explosive pellet 57 to detonate outwards radially. The explosion will travel radially in a substantially uniform fashion such that the explosive wave contacts the radial edges of explosives 65 and 68 at substantially the same the time. The explosives 65 and 68 will then start detonating from the inside out. As the explosive wave travels through explosives 65 and 68 it will begin subjecting liners 66 and 67 to high intensity heat and pressure at substantially the same time. The liners 66 and 67 will be crushed inwards and converted into a plasma jet that explodes outwards radially along axis 30. The plasma jet will cut through the lower housing 62 and then cut the surrounding tubular 80 as shown in FIG. 8b. The uniformity of detonation of the booster explosive pellet 57, followed by the uniform detonation of the explosives 65 and 68, combine to cause the near simultaneous compression of both liners 66 and 67. The near simultaneous compression of both liners 66 and 67 result in a straight cut in the tubular 82 as shown in FIG. 7B compared with the prior art which causes a curved cut 81 as shown in FIG. 7A.

[0029] When the bridge wire segments 51 burst, as shown in FIG. 5, they will produce shock waves 59 that will travel substantially perpendicular to the PCB 52. The shock waves 59 will travel at the same speed such that with each time interval, t1, t2, and t3, the shock waves stay roughly the same perpendicular distance from their originating bridge wire segment 51.

[0030] Another example of the discontinuous bridge wire design is shown in FIG. 6. The PCB 52 is located within the booster explosive pellet 57. The bridge wire segments 51 are mounted onto the PCB 52 using contact pads 77. When a detonation signal is sent from a fireset the individual bridge wire segments 51 each explode or burst, causing explosive pellet 57 to detonate at a plurality of locations simultaneously. The design allows for the plurality of detonation points to ensure that the explosive waves are no longer biased to one end of the booster or the other.

[0031] 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.