GB2265209A - Explosive cutting arrangements - Google Patents
Explosive cutting arrangements Download PDFInfo
- Publication number
- GB2265209A GB2265209A GB9205850A GB9205850A GB2265209A GB 2265209 A GB2265209 A GB 2265209A GB 9205850 A GB9205850 A GB 9205850A GB 9205850 A GB9205850 A GB 9205850A GB 2265209 A GB2265209 A GB 2265209A
- Authority
- GB
- United Kingdom
- Prior art keywords
- arrangement
- initiators
- explosive
- charge
- initiator
- 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.)
- Withdrawn
Links
- 239000002360 explosive Substances 0.000 title claims description 59
- 239000003999 initiator Substances 0.000 claims description 63
- 230000005540 biological transmission Effects 0.000 claims description 14
- 239000003990 capacitor Substances 0.000 claims description 14
- 238000005474 detonation Methods 0.000 claims description 13
- 230000000977 initiatory effect Effects 0.000 claims description 12
- 239000008188 pellet Substances 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 9
- 230000035939 shock Effects 0.000 claims description 6
- 239000011888 foil Substances 0.000 claims description 4
- 101100074836 Caenorhabditis elegans lin-22 gene Proteins 0.000 claims 1
- 230000001419 dependent effect Effects 0.000 claims 1
- 238000004880 explosion Methods 0.000 description 5
- 238000005553 drilling Methods 0.000 description 4
- 238000010304 firing Methods 0.000 description 3
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical group [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 2
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000001976 improved effect Effects 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 2
- 101100343342 Caenorhabditis elegans lin-11 gene Proteins 0.000 description 1
- 101100074828 Caenorhabditis elegans lin-12 gene Proteins 0.000 description 1
- 101100074829 Caenorhabditis elegans lin-13 gene Proteins 0.000 description 1
- 101100364669 Caenorhabditis elegans lin-18 gene Proteins 0.000 description 1
- 101100181929 Caenorhabditis elegans lin-3 gene Proteins 0.000 description 1
- 101100021281 Caenorhabditis elegans lin-8 gene Proteins 0.000 description 1
- 101100456282 Caenorhabditis elegans mcm-4 gene Proteins 0.000 description 1
- 108010088874 Cullin 1 Proteins 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 101150072601 lin-14 gene Proteins 0.000 description 1
- 108091053735 lin-4 stem-loop Proteins 0.000 description 1
- 108091032363 lin-4-1 stem-loop Proteins 0.000 description 1
- 108091028008 lin-4-2 stem-loop Proteins 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
- F42D1/04—Arrangements for ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D3/00—Particular applications of blasting techniques
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Geophysics And Detection Of Objects (AREA)
- Excavating Of Shafts Or Tunnels (AREA)
Description
9 z 2265209 1 Explosive Arrangements This invention relates to explosive
arrangements and more particularly to arrangements which are concerned with producing substantially simultaneous detonations of an explosive charge from two or more spaced apart initiation points such that detonation fronts travelling through the explosive material meet and produce an outward force.
In drilling operations, for example, in the oil industry, a drill is often used which consists of a hollow cylindrical shaft carrying a drill head or other tool. The shaft has a thick wall which must be robust enough to withstand the considerable strains placed upon it during operation.
Sometimes the drill head becomes jammed or obstructed in the bore hole. If it is not possible to remove the drill in order to steer around the obstruction, it is necessary to release the end of the drill from its shaft. This may be achieved using a explosive collar cutting assembly which is lowered down within the inside of the drill. The assembly has a thin cylindrical casing within which is packed an explosive material, typically HMX (High Melting Point Explosive). When the assembly is at the P/8815/LIN 1 1 2 depth where it is believed the drill has become stuck, the explosive charge is detonated at both ends substantially simultaneously, producing detonation fronts within the explosive material which travel.axially in opposite directions. Where the fronts meet, a radial outward force is produced which is sufficient to cut through the assembly casing and the wall of the drill shaft.
Figure 1 is a schematic longitudinal sectional view of a conventional collar cutting assembly as presently used.
The assembly comprises an outer casing 1 within which is located a hollow tube 2 which extends centrally along the whole length of the casing 1. The left hand end, as shown, is uppermost when the assembly is lowered into the drill shaft and includes a compartment 3 in which part of the detonation arrangement is housed. The remainder of the length of the casing is occupied by an explosive charge 4, typically of HMX, having a central aperture 6 through which the tube 2 passes. The length of the charge employed is chosen to control the magnitude of the explosive force created according to the requirements of a given situation. The charge 4 is bounded at each end by end plates 7 and 8 which are clamped into position on the tube 2.
1 P/8815/LIN 3 The detonation arrangement for initiating the explosive charge 4 employs detonating cord. This consists of a plastic walled tube filled,with explosive material. The detonating cord is initiated at one end and the explosion travels along it to deliver a mechanical shock to a main charge and hence detonate it. In the assembly shown in Figure 1, two detonating cords are used. One detonating cord 9 is folded within the compartment 3 and is used to detonate the charge 4 at its upper end. The other detonating cord 11 is located within the hollow tube 2 and extends to the lower end of the charge 4. The tube 2 must be cut to a suitable length depending on the length of charge chosen.
An initiator 14 is positioned at the upper end of the assembly, the ends 12 and 13 of the detonating cords 9 and 11 respectively being located adjacent to it. Typically, the initiator 14 is of the exploding bridge wire type in which an electrical pulse is passed through it to cause a wire to break. The resulting fragments impact on the ends 12 and 13 of the detonating cords to initiate them. A cable 15 forms a transmission line for the triggering electrical signal to the initiator 14.
1 P/8815/LIN 4 The end 16 of the detonating cord 9 remote from the initiator 14 is clamped in position and abuts a booster pellet 17 placed adjacent the explosive charge 4. The detonating cord 11 located within the tube 2 is looped around the end of the tube and back on itself outside the tube 2 to a holder 18 where its end 19 is clamped against a booster pellet 20 placed adjacent the lower end of explosive charge 4.
To detonate the explosive charge, an electrical signal is transmitted along the cable 15 to the initiator 14 causing the explosive contained within the detonating cords 9 and 11 to ignite. "The explosion fronts travel along the detonating cords 9 and 11 to the booster pellets 19 and 20 to initiate the main explosive charge 4 at two points. Providing the timing of the initiations at the upper and lower ends of the charge 4 is sufficiently close, the detonation fronts meet and produce an outward force which cuts through the drill shaft wall.
The detonating fronts travel through the detonating cords 9 and 11 at a speed of approximately 5000 metres per second. Therefore, the lengths of the detonating cords 9 and 11 are critical in order for initiation to occur substantially simultaneously at each end of the charge 4.
P/8815/LIN The detonating cords 9 and 11 must be the same length to within tight tolerances to ensure that the detonating fronts meet in the explosive charge 4.
If the detonating cord 11 is longer than the other one, then the charge 4 will be initiated from the uppermost end first, and this may result in a downwards explosion which will not free the drill head. Alternatively, if the central detonating cord 11 is shorter than the folded detonating cord 9, the explosion of the main charge is initiated from the lowermost end first, and this can cause an explosive shock wave to travel upwardly through the drill, with the possibility of sensitive monitoring instruments on the surface being damaged..
Another difficulty encountered when using the assembly is in ensuring that the connections between the detonating cords and the initiator, and with the booster pellets, are sufficiently secure.
For safety reasons it is essential that radio silence be maintained during deployment the drill cutting assembly as any electrical interference may be sufficient to unintentionally trigger the initiator.
P/8815/LIN 6 The present invention arose from an attempt to produce an improved explosive arrangement suitable for use in drilling operations but it is envisaged that it may also be advantageously used in other fields.
According to the invention there is provided an explosive arrangement comprising: substantially elongate explosive charge means having a longitudinal axis; and initiator means comprising at least two initiators disposed substantially adjacent to the charge means and spaced apart from one another in a longitudinal direction, the initiators being electrically initated to detonate explosive material, the initiator means being arranged such that, when the initiators are initiated, detonation fronts are produced in the charge means sufficiently simultaneously so as to meet and thereby produce a force in a direction substantially transverse to the longitudinal axis.
By employing the invention, the detonating cord used in previous arrangements may be dispensed with as there is no need for an intermediary explosive between the initiator and the main explosive charge. The explosive path between the initiator and the main charge is very short in comparison with the length required in conventional P/8815/LIN 7 arrangements using detonating cords to deliver a detonating force to the main charge. Thus the timing of the initiator firing is no longer governed by the velocity of detonation for the explosive of detonating cord but by the length of the time taken for an electrical signal to travel along electrical transmission lines to the initiators. The velocity of an electrical pulse along a transmission line is very much greater than that of an explosion travelling along a detonating cord. Therefore the tight tolerances previously imposed need not-be observed with an arrangement in accordance with the invention. As it is not necessary to precisely measure the length of the electrical transmission line or lines involved in delivering the initiating pulse to the charge means, an operator may set up an assembly much more easily than is the case with a conventional assembly and hence the time for which drilling operations, for example, must be suspended is greatly reduced, giving significant cost benefits.
Another significant benefit which arises from using the invention is that as the explosive used in the detonating cord, which typically is PETN (Pentaerythritoltetranitrate), need no longer be used, the assembly as a whole has improved temperature stability, enabling it to be used at depths of, say, 8 kilometres into the earth P/8815/LIN 8 where temperatures may be in the region of 2000 Celsius. The explosive charge means may typically include material such as HMX which is stable at these temperatures.
Another advantage which arises from eliminating the need to use detonating cord is that connections made between various components of the arrangement in accordance with the invention may be more secure, this sometimes being difficult to achieve with detonating cord. Also, it is not necessary to include a compartment for housing the folded detonating cord for connection to the upper end of the charge means and there is no concern about adjacent folded sections of detonating cord interfering with one another and causing a problem in the timing of the simultaneous detonations.
Although the invention may be particularly advantageously employed in explosive cutting arrangements it is believed to have uses in other fields also, for example, it may be used in seismic applications.
In some applications it may be necessary to have more than two detonation points. For example, it may be wished to create transverse forces at two spaced apart locations, in which case an initiator can be positioned at 1 9 each end of the elongate charge means with a third initiator centrally located.
P/8815/LIN In a particularly advantageous embodiment of the invention, the initiators are of the exploding foil initiator type (EFI). An EFI initiator is fired by discharging a capacitor, or some other source of high current pulse, through it, causing a foil to vaporise and to produce a high velocity plastic disc or flyer which is directed onto an explosive to initiate detonation. The pulse may require a peak current amplitude in the range 4 to 1OkA with a rise time in the range 20 to 100 nanoseconds. As these conditions are unlikely to be accidentally produced within the environment in which an arrangement in accordance with the invention is to be operated, such an arrangement is inherently safe. This has particular advantages in the drilling industry. At present, radio silence must be maintained whilst an explosive cutter is deployed and all activities giving rise to potentially interfering electrical signals must be shut down. By employing the invention, normal activities may be maintained where these do not directly interfere with the deployment of the explosive device and radio communication can be continuous, enabling personnel to be updated as to the progress of the operation to free a drill head.
P/8815/LIN In one preferred embodiment of the invention, the initiators are electrically connected in series so that the same electrical pulse travelling along a transmission line fires two initiators one after the other. Over a typical length of travel of one metre, there is a delay of the order of 3 to 10 nanoseconds between initiation of the first and second initiators. Where the initiators are arranged electrically in series, only one electrically conductive track is required, simplifying the arrangement. However, for some requirements, it may be preferable to have the initiators in parallel or independently fired.
Preferably, at least one of the initiators is connected to stripline along which an electrical firing signal is transmitted. Stripline is particularly convenient because of its low inherent inductance enabling the fast current rise times necessary for use with EFIts to be achieved. It is also easily handled and good connections to it may be readily made.
In one embodiment of the invention, at least one of the initiators is arranged to be directly in contact with explosive of the charge means. However, in some circumstances, it may be desirable to include an intervening booster pellet to amplify the mechanical shock P/8815/LIN 11 produced by the initiator to initiate the secondary explosive of the explosive charge means. In either case, one or both of the initiators may include a plate member, a piece which of breaks off upon triggering and is expelled with the vaporised foil, in the case of an EFI,to transmit the mechanical shock directly to the secondary explosive of the charge means or via a booster pellet.
Preferably, the electrical signal to one or both of the initiators is transmitted by a spark gap device, which conveniently is of the over voltage type. In such an arrangement, it may be preferred that one terminal of the spark gap device be directly adjacent, and in physical contact with, an electrical transmission line for transmitting the signal to the initiator or initiators. The other terminal of the spark gap device may be in contact with a terminal of a capacitor from which an initiating pulse is derived when the spark gap exceeds its breakdown voltage.
Preferably, the arrangement includes a housing in which the explosive charge means and the initiators are contained. Also, a capacitor may be included within the housing so as to ensure that the distance along which an electrical pulse is transmitted is minimized, hence P/8815/LIN 12 reducing inductive losses. The capacitor may be charged by a line from the surface providing a high voltage supply. However, it may be preferable to include a transformer within the housing for the capacitor supply to permit use with a low voltage.
In a particularly advantageous embodiment of the invention, an end plate is included adjacent one end of the explosive charge means, the end plate being movable in a longitudinal direction. This allows the amount of explosive material of the charge means to be varied as desired. It is also preferable that a second movable plate be included, being located on the side of the end plate other than that adjacent the charge means. one of the initiators may be mounted on the end plate and connected by an electrical transmission line to pulse supply means, the electrical transmission line being taken around the second plate or through an aperture therein. Such an arrangement enables different lengths of explosive charge to be used without needing to cut the transmission line to a particular length. The explosive charge is loaded into the assembly and the movable end plate placed adjacent it. The second end plate is then moved in the opposite direction to take up any slack in the transmission line.
P/8815/LIN 13 Some ways in which the invention may be performed are now described by way of example with reference to the accompanying drawings in which:
Figure 2 schematically illustrates part of an explosive arrangement in accordance with the invention; Figures 3a and 3b are explanatory diagrams relating to the operation of the arrangement of Figure 2; Figure 4 is a schematic external view of an assembly including the arrangement of Figure 2; and Figure 5 schematically illustrates another arrangement in accordance with the invention.
With reference to Figure 2, a collar cutting assembly for deployment in bore holes to cut through drills includes a cylindrical outer casing 21, only part of which is shown, within which is housed a main explosive charge 22 of HMX. The charge 22 is in the form of apertured discs 23 located on a central shaft 24. The assembly typically has a diameter of about 5cm and a length of lm.
The left hand end of the assembly, as shown, which is P/8815/LIN 14 the uppermost end when in use, contains a cylindrical low inductance capacitor 25 having an earthed terminal 26 and an HT terminal 27 to which charging currdnt is applied via a lead 28. The HT terminal 27 is in direct physical contact with a terminal 29 of an adjacent spark gap 30 of the over-voltage type.
The main charge 22 is bounded by two end plates 31 and 32 which are clamped to the shaft 24 and secure the charge 22 in place. An EFI initiator 33 and 34 is mounted on each end plate 31 and 32 respectively so that it is directly adjacent to an end surface of the charge 22. The two EFI's 33 and 34 are electrically connected in series by low inductance stripline 35. The stripline 35 extends from the spark gap device 30 via an aperture 36 in end plate 31 and to the first EFI 33 to which it is connected. The stripline 35 is positioned along the length of the charge 22 over its outer surface, with the high voltage side of the stripline being on the inside. An electrically insulating film covers the inner surface of the stripline 35. The stripline 35 passes through an aperture 37 in another plate 38 and is connected to the second EFI 34, being fixed to the end plate 32. The insulating film ensures that the adjacent parts of the stripline 35 do not form a short circuit.
P/8815/LIN is When it is wished to deploy the assembly, the amount of charge required is estimated and an appropriate number of discs 23 placed in position to form the charge 22. The assembly is lowered into the central cavity of the drill shaft to the desired depth. The capacitor 25 is then charged via HT lead 28. The spark gap device 30 typically has a breakdown voltage of 3 to 4.5kV and when this exceeded, the capacitor discharges through the spark gap 30 to produce a pulse which is transmitted along the stripline 35, causing the initiators 33 and 34 to be triggered in turn. The value of the capacitor is chosen so as to be able to produce a current pulse with a peak amplitude of about 6kA and a pulse rise time of approximately 30 nanoseconds. Typically, there is a 3 and 10 nanoseconds delay between the firing of the initiators 33 and 34. The initiators 33 and 34 thus are fired sufficiently simultaneously that detonation fronts are generated at each end of the charge 22 and meet to produce a radially outward force which shears through the surrounding drill wall.
The end plate 32 and further plate 38 on the right hand side of the assembly, as shown, are movable. When setting up the assembly, the discs 23 are placed in position and the two plates 32 and 38 moved towards them, P/8815/LIN 16 the plate 32 being arranged to securely abut charge 22 and the plate 38 being positioned to allow sufficient slack in the stripline 35 to place the end plate 32 in the required position, as illustrated in Figute 3a. The end plate 32 is clamped in position and'then the second plate 38 is moved away from it, as shown by the arrow in Figure 3b. This enables different size explosive charges to be used without needing to alter the length of the striPline 35 or disturb the attachment of the EFIls 33 and 34 to it.
Figure 4 schematically illustrates a collar cutting assembly showing the location of the arrangement illustrated in Figure 2. The assembly includes centralising parts 39 and 40 to guide the assembly as it is dropped into position.
Another embodiment of the invention is schematically illustrated in Figure 5 and is similar to that shown in Figure 2. In this embodiment of the invention, a transformer 41 is included for providing an HT supply to the capacitor and is connected to a low voltage supply via lead 42. Also, each of the EFI's 43 and 44 is located adjacent a booster pellet 45 and 46 with a thin aluminium plate 47 and 48 between them. This enables the initiating mechanical shock produced by the EFI to be amplified prior P/8815/LIN 17 to it being applied to the main explosive charge.
It should be noted that the dimensions of the arrangements shown in Figure 2 afid 5 are not to scale. For example, the gaps between the charge and the end plates are exaggerated to enable the initiators and initiators/booster pellets to be more clearly shown.
In the arrangements shown in Figure 2 and 5 the transmission line to the lower EFI is arranged around the outer edge of the end plate. However, the end plate could be apertured and the stripline located through the aperture.
The EFIs and striplines are shown as being mounted on the surfaces of the end plates but they need not be fixed in position. In another embodiment, not shown, recesses are provided in each end plate 2 and the associated EFI (or booster pellet where one is used) is located in them to give a flush surface in contact with the explosive charge.
The initiators are shown adjacent the end faces of the elongate charge. However, they could be located on the outer, cylindrical surface but this arrangement is likely to be less efficient in generating the required P/8815/LIN 18 transverse force.
P/8815/LIN 19
Claims (20)
1. An explosive arrangement comprising: substantially elongate explosive charge means having a longitudinal axis; and initiator means comprising at least two initiators disposed substantially adjacent the charge means and spaced apart from one another in a longitudinal direction, the initiators being electrically initiated to detonate explosive material, the initiator means being arranged such that, when the initiators are initiated, detonation fronts are produced in the charge means sufficiently simultaneously so as to meet and thereby produce a force in a direction transverse to the longitudinal axis.
2. An arrangement as claimed in claim 1 wherein the initiators are of the exploding foil initiator type.
3. An arrangement as claimed in claim 1 or 2 wherein the initiators are arranged electrically in series.
4. An arrangement as claimed in claim 1, 2 or 3 wherein at least one of the initiators is connected to stripline along which an electrical initiating signal is P/8815/LIN transmitted.
5. An arrangement as claimed in any preceding claim wherein at least one of the initiators is arranged to be directly in contact with explosive of the charge means.
6. An arrangement as claimed in claim 1, 2, 3 or 4 wherein at least one of the initiators initiates explosive of the charge means via a booster pellet.
7. An arrangement as claimed in any preceding claim wherein at least one of the initiators includes a plate member which, upon initiation, transmits mechanical shock produced by the initiator to explosive material.
8. An arrangement as claimed in any preceding claim wherein an electrical initiating signal to one or both initiators is transmitted via a spark gap device.
9. An arrangement as claimed in claim 8 wherein one terminal of the spark gap device is directly adjacent transmission line means for transmitting the signal to the initiator or initiators.
10. An arrangement as claimed in claim 8 or 9 wherein P/8815/LIN 1 21 one terminal of the spark gap device is in direct contact with a terminal of a capacitor from which the electrical initiating signal is derived.
11. An arrangement as claimed in any preceding claim and including low inductance cylindrical capacitor means.
12. An arrangement as claimed in any preceding claim and including a housing in which the explosive charge means and initiators are contained.
13. An arrangement as claimed in claim 12 when dependent on claim 11 wherein the capacitor means is included within the housing.
14. An arrangement as claimed in claim 13 and including transformer means within the housing to provide a high voltage supply for the capacitor.
15. An arrangement as claimed in any preceding claim wherein the initiators are arranged adjacent to transverse end faces of the explosive charge means.
16. An arrangement as claimed in any preceding claim and including an end plate adjacent one end of the explosive P/8815/LIN 22 charge means, the end plate being movable in a longitudinal direction.
17. An arrangement as claimed.in claim 16 and including a second movable plate located on the side of the end plate other than that adjacent to the charge means, one of the initiators being mounted on the end plate and being connected by an electrical transmission line to signal supply means, the transmission line being located through an aperture in the second plate.
18. An arrangement as claimed in any preceding claim and including signal supply means for producing an electrical pulse to initiate the initiator or initiators having a peak current amplitude in the range 4 to 1OkA with a pulse rise time in the range 20 to 100 nanoseconds.
19. Anarrangement as claimed in any preceding claim and adapted for deployment in drill holes.
20. An explosive arrangement substantially as illustrated in and described with reference to Figure 2, 3, 4 or 5 of the accompanying drawings.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9205850A GB2265209A (en) | 1992-03-18 | 1992-03-18 | Explosive cutting arrangements |
| EP93301045A EP0561499A1 (en) | 1992-03-18 | 1993-02-12 | Explosive arrangements |
| CA002090158A CA2090158A1 (en) | 1992-03-18 | 1993-02-23 | Explosive arrangements |
| NO93930921A NO930921L (en) | 1992-03-18 | 1993-03-15 | EXPLOSIVE-ARRANGEMENT |
| AU35299/93A AU3529993A (en) | 1992-03-18 | 1993-03-17 | Explosive arrangements |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9205850A GB2265209A (en) | 1992-03-18 | 1992-03-18 | Explosive cutting arrangements |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB9205850D0 GB9205850D0 (en) | 1992-04-29 |
| GB2265209A true GB2265209A (en) | 1993-09-22 |
Family
ID=10712348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9205850A Withdrawn GB2265209A (en) | 1992-03-18 | 1992-03-18 | Explosive cutting arrangements |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0561499A1 (en) |
| AU (1) | AU3529993A (en) |
| CA (1) | CA2090158A1 (en) |
| GB (1) | GB2265209A (en) |
| NO (1) | NO930921L (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2288005A (en) * | 1994-03-29 | 1995-10-04 | Schlumberger Ltd | Firing well perforating guns |
| US6148263A (en) * | 1998-10-27 | 2000-11-14 | Schlumberger Technology Corporation | Activation of well tools |
| US6283227B1 (en) | 1998-10-27 | 2001-09-04 | Schlumberger Technology Corporation | Downhole activation system that assigns and retrieves identifiers |
| US6385031B1 (en) | 1998-09-24 | 2002-05-07 | Schlumberger Technology Corporation | Switches for use in tools |
| US6752083B1 (en) | 1998-09-24 | 2004-06-22 | Schlumberger Technology Corporation | Detonators for use with explosive devices |
| US6938689B2 (en) | 1998-10-27 | 2005-09-06 | Schumberger Technology Corp. | Communicating with a tool |
| US7347278B2 (en) | 1998-10-27 | 2008-03-25 | Schlumberger Technology Corporation | Secure activation of a downhole device |
| US9464508B2 (en) | 1998-10-27 | 2016-10-11 | Schlumberger Technology Corporation | Interactive and/or secure activation of a tool |
| US9568288B2 (en) | 2014-02-05 | 2017-02-14 | Battelle Memorial Institute | Surface mount exploding foil initiator |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8091477B2 (en) | 2001-11-27 | 2012-01-10 | Schlumberger Technology Corporation | Integrated detonators for use with explosive devices |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4091870A (en) * | 1976-10-26 | 1978-05-30 | Physics International Company | Method for generating horizontal fractures in a wellbore |
| GB2055663A (en) * | 1979-06-25 | 1981-03-11 | Jet Research Center | Method and apparatus for severing conduits |
| GB1604688A (en) * | 1977-06-29 | 1981-12-16 | Jet Research Center | Method and apparatus for severing tubing |
| GB2158207A (en) * | 1984-04-26 | 1985-11-06 | Vetco Ltd C E | Explosive cutting device |
| GB2179124A (en) * | 1985-06-29 | 1987-02-25 | Deepwater Oil Services | Explosive cutting device |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3955505A (en) * | 1950-05-31 | 1976-05-11 | The United States Of America As Represented By The United States Energy Research And Development Administration | Detonating apparatus |
| US2737115A (en) * | 1952-09-25 | 1956-03-06 | Addison G Bissell | Method and apparatus for explosively fracturing tubular members |
| US3076408A (en) * | 1958-06-11 | 1963-02-05 | Borg Warner | Controlled fracturing of solids by explosives |
| GB1138654A (en) * | 1966-02-07 | 1969-01-01 | Ici Ltd | Explosive charges for seismic prospecting |
| US3726215A (en) * | 1971-07-16 | 1973-04-10 | Us Navy | Explosive destruct device |
| US4008117A (en) * | 1973-05-21 | 1977-02-15 | Bell Telephone Laboratories, Incorporated | Apparatus for bonding and plating with exploding foil |
| DE3165351D1 (en) * | 1980-05-09 | 1984-09-13 | Emi Ltd | Arrangements for igniting a pyrotechnic charge |
| US4493260A (en) * | 1983-11-08 | 1985-01-15 | The United States Of America As Represented By The Secretary Of The Navy | Annular shaped charge for breaching masonary walls |
| DE3544747A1 (en) * | 1985-12-18 | 1987-06-19 | Diehl Gmbh & Co | COMBAT HEAD WITH ROTATIONALLY SYMMETRIC CHARGE |
| US4944225A (en) * | 1988-03-31 | 1990-07-31 | Halliburton Logging Services Inc. | Method and apparatus for firing exploding foil initiators over long firing lines |
-
1992
- 1992-03-18 GB GB9205850A patent/GB2265209A/en not_active Withdrawn
-
1993
- 1993-02-12 EP EP93301045A patent/EP0561499A1/en not_active Withdrawn
- 1993-02-23 CA CA002090158A patent/CA2090158A1/en not_active Abandoned
- 1993-03-15 NO NO93930921A patent/NO930921L/en unknown
- 1993-03-17 AU AU35299/93A patent/AU3529993A/en not_active Abandoned
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4091870A (en) * | 1976-10-26 | 1978-05-30 | Physics International Company | Method for generating horizontal fractures in a wellbore |
| GB1604688A (en) * | 1977-06-29 | 1981-12-16 | Jet Research Center | Method and apparatus for severing tubing |
| GB2055663A (en) * | 1979-06-25 | 1981-03-11 | Jet Research Center | Method and apparatus for severing conduits |
| GB2158207A (en) * | 1984-04-26 | 1985-11-06 | Vetco Ltd C E | Explosive cutting device |
| GB2179124A (en) * | 1985-06-29 | 1987-02-25 | Deepwater Oil Services | Explosive cutting device |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5505134A (en) * | 1993-09-01 | 1996-04-09 | Schlumberger Technical Corporation | Perforating gun having a plurality of charges including a corresponding plurality of exploding foil or exploding bridgewire initiator apparatus responsive to a pulse of current for simultaneously detonating the plurality of charges |
| GB2288005B (en) * | 1994-03-29 | 1998-07-29 | Schlumberger Ltd | A perforating gun having a plurality of charges |
| GB2288005A (en) * | 1994-03-29 | 1995-10-04 | Schlumberger Ltd | Firing well perforating guns |
| US6386108B1 (en) | 1998-09-24 | 2002-05-14 | Schlumberger Technology Corp | Initiation of explosive devices |
| US6752083B1 (en) | 1998-09-24 | 2004-06-22 | Schlumberger Technology Corporation | Detonators for use with explosive devices |
| US6385031B1 (en) | 1998-09-24 | 2002-05-07 | Schlumberger Technology Corporation | Switches for use in tools |
| US6148263A (en) * | 1998-10-27 | 2000-11-14 | Schlumberger Technology Corporation | Activation of well tools |
| US6604584B2 (en) | 1998-10-27 | 2003-08-12 | Schlumberger Technology Corporation | Downhole activation system |
| US6283227B1 (en) | 1998-10-27 | 2001-09-04 | Schlumberger Technology Corporation | Downhole activation system that assigns and retrieves identifiers |
| US6938689B2 (en) | 1998-10-27 | 2005-09-06 | Schumberger Technology Corp. | Communicating with a tool |
| US7347278B2 (en) | 1998-10-27 | 2008-03-25 | Schlumberger Technology Corporation | Secure activation of a downhole device |
| US9464508B2 (en) | 1998-10-27 | 2016-10-11 | Schlumberger Technology Corporation | Interactive and/or secure activation of a tool |
| US9568288B2 (en) | 2014-02-05 | 2017-02-14 | Battelle Memorial Institute | Surface mount exploding foil initiator |
Also Published As
| Publication number | Publication date |
|---|---|
| GB9205850D0 (en) | 1992-04-29 |
| EP0561499A1 (en) | 1993-09-22 |
| NO930921D0 (en) | 1993-03-15 |
| AU3529993A (en) | 1993-09-23 |
| CA2090158A1 (en) | 1993-09-19 |
| NO930921L (en) | 1993-09-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |