WO1998039615A1 - High impedance semiconductor bridge detonator - Google Patents
High impedance semiconductor bridge detonator Download PDFInfo
- Publication number
- WO1998039615A1 WO1998039615A1 PCT/US1998/004025 US9804025W WO9839615A1 WO 1998039615 A1 WO1998039615 A1 WO 1998039615A1 US 9804025 W US9804025 W US 9804025W WO 9839615 A1 WO9839615 A1 WO 9839615A1
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- WO
- WIPO (PCT)
- Prior art keywords
- scb
- detonator
- initiator
- bridge
- charge
- Prior art date
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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
- F42B3/10—Initiators therefor
-
- 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
- F42B3/10—Initiators therefor
- F42B3/12—Bridge initiators
- F42B3/13—Bridge initiators with semiconductive bridge
Definitions
- the present invention relates to semiconductor bridge detonators. More particularly, the invention relates to such a detonator having a high impedance, thin-film bridge with certain electrical characteristics for special applications.
- Detonators are used to initiate various types of explosive charges, for example, to initiate boosters for downhole explosive charges in blasting operations.
- a conventional detonator comprises an elongated shell having one closed end and one open end. An explosive output charge is disposed in the closed end of the shell. An initia- tion signal transmission line is passed through the open end of the shell and is opera- tively connected to the output charge, so that the initiation signal can be transferred from the signal transmission line to the output charge to fire the detonator.
- Some detonators comprise electric initiator elements such as a hot wire, an exploding bridgewire or a semiconductor bridge (SCB) that initiate the output charge. The ini- tiator elements extend between electrical contacts to which lead wires provide an electrical firing signal.
- SCB igniter elements which are described as comprising an electrical semiconductor material disposed on a non-conductive substrate.
- the semiconductor material may be, e.g., a layer of n-type silicon that has been doped with phosphorus. As indicated in this Patent, other semiconductor materials and dopants can be used with similar effect.
- the resistivity of the doped material varies with the dopant level, as is well- understood in the art.
- the semiconductor material is disposed on the non- conductive substrate by a chemical vapor deposition process by which the thickness of the material can be precisely controlled.
- the surface of the non-conductive substrate is usually masked during the deposition process so that the layer of semiconductor material is rendered in an hourglass shape, i.e., it forms two relatively large pads joined together by a small bridge. Two pads of conductive material are then disposed upon the large pads of the semiconductor material and are separated by the bridge of semiconductor material between them.
- the resistivity of the semiconductor material and the dimensions of the semiconductor bridge between the conductive pads determines the effective resistance that the semiconductor bridge provides between the conductive pads.
- the Patent teaches a preference for SCBs of low resistance, e.g., no larger than 10 ohms, for safety reasons, i.e., in case the SCB is used with an electrostatic sensitive ignition charge, (see column 7, lines 44-50) and for a reduction in resistivity with an increase in SCB size (see column 7, lines 53-55).
- the firing data provided pertain to high amperage (e.g., 10 amps and higher), short duration electrical initiation signals of less than 100 microseconds duration (see column 5, line 62 through column 6, line 3).
- the comparative data of Table 2 are difficult to interpret because SCB1 and SCB2 differ not only in resistance but also in thickness (2 microns vs. 4 microns).
- U.S. Patent 5,179,248 to Hartman et al, dated January 12, 1993, relates to a zener diode for protection of SCBs.
- the zener diode which is connected across the lands of the SCB, helps to avoid premature energization of the explosive due to electrostatic discharge or other voltages greater than the firing voltage.
- the Patent specifies a bridge resistance no greater than 1 ohm, as a larger resistance would detrimentally affect the heating of the explosive (see, e.g., column 5, lines 60-66).
- API American Petroleum Institute
- the discrete resistors are typically positioned in the detonator shell between the closure bushing for the open end of the detonator and an internal rubber plug, and the resistors and internal rubber plug account for a significant portion of the overall length of the detonator.
- the present invention relates to a semiconductor bridge initiator element comprising an electrically non-conductive carrier substrate.
- a semiconductor material is disposed on the substrate.
- Two conductive lands are carried on the substrate in contact with the semiconductor material with a bridge of semiconductor material, i.e., a semiconductor bridge (SCB), extending between them.
- the SCB has a resistance of at least about 50 ohms.
- the SCB may have a volume in the range of from about 13,160 to 600,000 cubic micrometers (" ⁇ m 3 "), e.g., about 76,000 ⁇ m 3 . Further, the SCB may have a length to width ratio in the range of about 1 :2 to 1:4.
- the invention also provides an initiator module comprising an electrically non-conductive base, a pair of connector terminals mounted in the base, and a semiconductor bridge initiator element, as described above, mounted on the base wherein each connector terminal is electrically connected to a conductive pad on the semiconductor bridge initiator element.
- the invention also provides a detonator comprising a housing, an output charge in the housing and an initiator assembly for initiating the output charge.
- the initiator assembly comprises the initiator module described above.
- the detonator may comprise an ignition charge in the housing.
- the ignition mixture comprises a static-insensitive composition.
- Figure 1 is a schematic cross-sectional view of a prior art hot wire detonator including a pair of internal resistors
- Figure 2 is a schematic cross-sectional view of a detonator in accordance with a particular embodiment of the present invention
- Figure 3 is an enlarged perspective view of the initiator assembly of the detonator of Figure 2;
- Figure 4A is an enlarged elevational view of the semiconductor bridge (SCB) initiator element in the initiator assembly of Figure 3; and
- Figure 4B is a view of the SCB initiator element of Figure 4A taken along line 4B-4B.
- Detonator 110 comprises a metal detonator shell or housing 112 which is generally cylindrical in configuration and which has a closed end 112a and an open end 112b. At closed end 112a housing 112 contains a base charge 14 that comprises a secondary explosive material.
- a secondary explosive material for oil and gas applications, explosive materials that are useful at high temperatures, such as RDX or HNS (hexanitrostilbene), are preferred over others such as, e.g., PETN (pentaerythritol tetranitrate).
- an intermediate charge 16 Tamped into housing 112 adjacent to base charge 14, and thus in signal transfer relation thereto, is an intermediate charge 16 that typically comprises a primary explosive material such as lead azide. Together, base charge 14 and intermediate charge 16 comprise the output charge of the detonator. The output charge generates the explosive detonation output that bursts housing 112 and provides the output signal of the detonator.
- Adjacent intermediate charge 16 is an ignition charge 18 that preferably comprises a static insensitive material, such as a mixture of boron and ferric oxide. A typical mixture of this type, comprising about 15 percent boron by weight, is disclosed in U.S. Patent 4,484,960, issued to Rucker on November 27, 1984. As is well-known in the art, other reactive mixtures, e.g., TiE. !
- Em- bedded within ignition charge 18 is an initiator element comprising a hot wire 20.
- Hot wire 20 extends between a pair of hot wire leads 22a, 22b.
- Ignition charge 18 is secured in place by an internal plug or bushing 24, through which hot wire leads 22a and 22b pass.
- Closure bushing 28 is secured within the open end 112b of housing 112 by a crimp 30, which also serves to seal the interior of housing 112 against bushing 28, thus helping to protect against the entry of environmental contaminants such as water and oil into the interior of housing 112.
- in- put leads 26a, 26b are joined to hot wire leads 22a, 22b through resistors 32a, 32b.
- resistors 32a and 32b each provide twenty-five ohms of resistance, thus satisfying one of the American Petroleum Institute's recommended safety criteria.
- input leads 26a, 26b carry an electrical initiation signal to hot wire 20 through resistors 32a, 32b and hot wire leads 22a, 22b.
- the current of the initiation signal generates sufficient heat in hot wire 20 to initiate the boron/ferric oxide ignition charge 18, thus initiating the detonator.
- the duration of the initiation signal which in the oil and gas industry is applied as a ramped applied voltage, is generally not less than 100 milliseconds, and may be as long as 3 seconds and, as discussed below, the current level of the initiation signal is small.
- Applicant attempted to substitute the conventional hot wire 20 with a semiconductor bridge (SCB) initiator module that comprises an SCB initiator element.
- SCB semiconductor bridge
- an SCB initiator element comprising a conventional 1- ohm SCB measuring 17 x 36 x 2 microns (which has been used successfully to initiate ignition charges comprising, e.g., BNCP) was unable to reliably initiate a boron/ferric oxide ignition charge when provided with the 800 milliamp current that is dictated by industry standards as an all-fire current for oil and gas applications.
- the Applicant found that approximately 50 percent more current was required (i.e., about 1200 mil- liamp) for such an SCB to initiate the boron/ferric oxide ignition charge, for an initiation power of 1.44 watts.
- the current necessary to provide 1.44 watts could be reduced by increasing the resistance of the semiconductor bridge.
- the conventional 1-ohm, 17 x 36 x 2 micron SCB could be doped to provide 50-ohm resistance, but then the 1.44 watt threshold initiation power would be met by a current of only about 170 milliamp, which is less than the 200 milliamp no-fire safety requirement.
- the present invention arises from the general knowledge that among SCBs with the same thickness and electrical resistance, larger SCBs required more current to initiate the boron/ferric oxide ignition charge than did smaller SCBs. In other words, the power required to initiate the ignition charge varies with the size of the SCB.
- the Applicant's experimentation revealed a specific relationship between size limitations of SCBs and initiation threshold currents not previously known or suggested in the art.
- the "length" dimension indicated in TABLE I is measured between the conductive lands on the SCB element, i.e., from end to end; the width dimension is measured from side to side, i.e., at right angles to the length measurement. If the SCBs were doped to have the resistivity necessary to provide about 50 ohms resistance, they will provide the indicated threshold power with less current, as also shown in TABLE I.
- SCBs in excess of 600,000 cubic microns will require more than 800 milliamps to initiate the boron/ferric oxide ignition charge, a current level that exceeds a useful limit detonator all-fire current.
- the SCBs of the present invention have a thickness of about 2 ⁇ m and a length to width ratio in the range of about 1 :2 to 1 :4.
- An SCB detonator in accordance with the present invention is shown schematically in Figure 2.
- Detonator 10 comprises a housing 12 that has a generally cylindrical configuration with a closed end 12a and an open end 12b and contains the same output charge as a conventional detonator 110 (Figure 1), i.e., a base charge 14 and an intermediate charge 16.
- An optional, preferably static-insensitive ignition charge 18 is loosely disposed in housing 12 adjacent to intermediate charge 16.
- Input leads 26a and 26b extend into the interior of housing 12 and are secured therein by a closure bushing 28 and crimp 30.
- Input leads 26a and 26b carry an electrical initiation signal to an initiator module 34.
- Initiator module 34 comprises a semiconductor bridge initiator element 36, which is shown and described in greater detail in Figures 3 through 4B and the accompanying text.
- the SCB initiator element 36 initiates the ignition charge 18, thus initiating the output charge of the detonator.
- bushing 28 (with leads 26a, 26b therein) and initiator module 34 comprise an initiator assembly 35.
- the igni- tion charge can be omitted, and the SCB can directly initiate the intermediate charge.
- SCB initiator element 36 is a high impedance component which is manufactured to provide a resistance of at least about 50 ohms, i.e., 55 + 5 ohms. Accordingly, detonator 10 satisfies the safety requirement promulgated by the American Petroleum Institute without the need to "resistorize" the initiator element, i.e., add one or more discrete resistors to the detonator circuitry, as was done in the prior art.
- resistors 32a and 32b are not required in detonator 10 ( Figure 2) according to the present invention.
- the internal bushing 24 is no longer required.
- the elimination of resistors 32a and 32b and internal bushing 24 allows detonator 10 to be significantly shorter than the prior art detonator 110 since initiator module 34 occupies significantly less space in a detonator housing than resistors 32a, 32b and internal bushing 24. This yields greater manufacturing efficiency, lower costs and greater flexibility in the design of other devices with which the detonator will be used.
- one aspect of the invention can be described as excluding discrete resistors from the detonator circuitry.
- Bushing 28 has a head portion 28a within which connector studs 38a and 38b are disposed.
- Bushing 28 is preferably formed from an elastic synthetic polymeric material.
- the head portion 28a of bushing 28 is generally cylindrical and it has a diameter that corresponds approximately to the interior diameter of the detonator housing (not shown), e.g., about 0.233 inch (5.9 mm).
- the remainder of bushing 28 is split at seam 40 to facilitate the insertion of the exposed ends of electrical leads 26a and 26b into the open ends of connector studs 38a and 38b.
- Initiator module 34 comprises a generally cylindrical non-conductive pill 44 that may be formed from a polymeric material, e.g., an epoxy resin.
- Connector terminals 46 and 48 extend through pill 44 to top surface 34a and bottom surface 34b. Near bottom surface 34b, connector terminals 46 and 48 form coupling recesses 46a, 48a, which are dimensioned and configured to engage connector studs 38a and 38b on bushing 28.
- the SCB initiator element 36 is adhered to the top surface 34a of pill 44, preferably between connector terminals 46 and 48, in any convenient manner, e.g., by epoxy adhesive.
- Two 5 mil (0.005 inch) aluminum bond wires 52, 54 extend between the exposed ends of connector terminals 46 and 48 and associated conductor pads (not shown) on SCB initiator element 36, and may be sonically welded in place at each end by a process well-known in the art.
- pill 44 is generally cylindrical and has a diameter D that corresponds to the internal diameter of the detonator housing (not shown).
- connector studs 38a, 38b and coupling recesses 46a, 48a are configured so that once studs 38a and 38b are inserted into recesses 46a, 48a, they will be securely retained therein, e.g., by a locking mechanism such as a leaf spring detent on studs 38a, 38b and corresponding grooves in coupling recesses 46a, 48a.
- initiator module 34 and bushing 28 (including leads 26a, 26b) will be joined together to constitute initiator assembly 35 and to provide electrical continuity between leads 26a, 26b and bond wires 52, 54.
- Initiator assembly 35 allows an initiation signal to be conveyed from an external device to the interior of the detonator and, in particular, to the ignition charge.
- SCB initiator element 36 is seen to com- prise a non-electrically conducting substrate 56 that may comprise a silicon base 56a with a layer of silicon dioxide 56b.
- substrate 56a may comprise a silicon base 56a with a layer of silicon dioxide 56b.
- silicon is preferred because of its favorable thermal properties.
- layer 56b On silicon dioxide layer 56b is a 2- micron thick layer of semiconductor material 58 which may comprise a phosphorus- doped polysilicon semiconductor layer in an hourglass configuration having two spaced apart pads 58a, 58b ( Figure 4B) joined by a thin-film bridge 60.
- Bridge 60 has a width 60a, a length 60b and a thickness equal to the thickness of layer 58.
- a typical thickness for semiconductor layer 58 is two microns.
- the level of doping in layer 58 which determines the resistivity of the semiconductor material, is coordinated with the planned length 60b ( Figure 4B) and width 60a and thickness of the semiconductor bridge 60 that will extend between the metallized lands to provide the desired resistance between them.
- Electrically conductive metallized lands 62a and 62b (seen partially broken away in Figure 4B for purposes of illustration) respectively cover pads 58a, 58b of the semiconductor layer.
- Electrically conductive bond wires 52, 54 ( Figure 3) are connected to metallized lands 62a and 62b, respectively.
- the electrical resistance between bond wires 52, 54 is substantially equal to the electrical resistance provided by bridge 60 between lands 62a and 62b.
- the resistance provided by bridge 60 is the resistance attributed to the SCB initiator element.
- SCB initiator element 36 may be manufactured by well-known procedures involving photolithographic masking, chemical vapor deposition, etc., to precisely con- trol the thickness, configuration and doping concentration of each layer of material, yielding highly consistent performance for large numbers of SCBs.
- the Applicant found that for the SCB measuring 100 x 380 x 2 microns, about 0.34 amp of current, or 5.6 watts of power, was re- quired for this SCB element to reliably initiate the ignition charge.
- This current requirement is consistent with the industry standard requirement for a 200 milliamp no- fire current.
- it is consistent with the industry requirement for an all-fire current level of at or below 800 milliamp.
- an all-fire current of 670 milliamp and a no-fire cur- rent of 430 milliamp was found.
- bridge 60 of the 50-ohm SCB element must have a volume (given a uniform 2 micron thickness) of at least about 13,160 ⁇ m 3 , and preferably has a volume of from 48,600 to 300,000 ⁇ m 3 or, more preferably, about 76,000 ⁇ m , to initiate the ignition charge while meeting the desired no-fire current criterion.
- semiconductor layer 58 may be manufactured so that bridge 60 provides a DC resistance of 55 ⁇ 5 ohms.
- base charge 14 and intermediate charge 16 are pressed into the empty housing 12.
- the ignition charge 18 is loosely disposed within housing 12 on top of intermediate charge 16, but is not compacted therein.
- input leads 26a and 26b are secured in bushing 28 and initiator module 34, which is manufactured as described above, is secured onto bushing 28 by inserting connector studs 38a and 38b into coupling recesses 46a, 48a, to form the initiator assembly.
- the initiator assembly is inserted into the housing to a depth at which SCB initiator element 36 contacts ignition charge 18 with a minimum of compressive force. Typically, a maximum pressure of approximately 1,000 psi is applied to the initiator assembly.
- crimp 30 is formed in housing 12 to retain bushing 28 in place.
- bridge 60 ( Figure 4B) vaporizes, initiating ignition charge 18, which in turn initiates detonator 10.
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Abstract
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Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA002279924A CA2279924A1 (en) | 1997-03-07 | 1998-03-02 | High impedance semiconductor bridge detonator |
EP98911447A EP0965030A4 (en) | 1997-03-07 | 1998-03-02 | High impedance semiconductor bridge detonator |
RU99121327/02A RU2161292C1 (en) | 1997-03-07 | 1998-03-02 | Initiating element with semiconductor bridge, initiator unit and detonator |
BR9808207-8A BR9808207A (en) | 1997-03-07 | 1998-03-02 | High impedance semiconductor bridge detonator |
NO994920A NO994920D0 (en) | 1997-03-07 | 1999-10-08 | High Impedance Semiconductor Bridge Detonator |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/812,662 | 1997-03-07 | ||
US08/812,662 US5831203A (en) | 1997-03-07 | 1997-03-07 | High impedance semiconductor bridge detonator |
Publications (1)
Publication Number | Publication Date |
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WO1998039615A1 true WO1998039615A1 (en) | 1998-09-11 |
Family
ID=25210270
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1998/004025 WO1998039615A1 (en) | 1997-03-07 | 1998-03-02 | High impedance semiconductor bridge detonator |
Country Status (8)
Country | Link |
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US (1) | US5831203A (en) |
EP (1) | EP0965030A4 (en) |
AR (1) | AR011934A1 (en) |
BR (1) | BR9808207A (en) |
CA (1) | CA2279924A1 (en) |
NO (1) | NO994920D0 (en) |
RU (1) | RU2161292C1 (en) |
WO (1) | WO1998039615A1 (en) |
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- 1997-03-07 US US08/812,662 patent/US5831203A/en not_active Expired - Fee Related
-
1998
- 1998-03-02 EP EP98911447A patent/EP0965030A4/en not_active Withdrawn
- 1998-03-02 RU RU99121327/02A patent/RU2161292C1/en not_active IP Right Cessation
- 1998-03-02 CA CA002279924A patent/CA2279924A1/en not_active Abandoned
- 1998-03-02 BR BR9808207-8A patent/BR9808207A/en unknown
- 1998-03-02 WO PCT/US1998/004025 patent/WO1998039615A1/en not_active Application Discontinuation
- 1998-03-06 AR ARP980101004A patent/AR011934A1/en unknown
-
1999
- 1999-10-08 NO NO994920A patent/NO994920D0/en not_active Application Discontinuation
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1030159A1 (en) * | 1999-02-18 | 2000-08-23 | Livbag SNC | Electro-pyrotechnical igniter with augmented ignition safety |
FR2790078A1 (en) | 1999-02-18 | 2000-08-25 | Livbag Snc | ELECTROPYROTECHNIC IGNITER WITH ENHANCED IGNITION SAFETY |
US6289813B1 (en) | 1999-02-18 | 2001-09-18 | Livbag Snc | Electropyrotechnic igniter with enhanced ignition reliability |
US8069789B2 (en) | 2004-03-18 | 2011-12-06 | Orica Explosives Technology Pty Ltd | Connector for electronic detonators |
EP1933108A1 (en) * | 2005-09-07 | 2008-06-18 | Nippon Kayaku Kabushiki Kaisha | Semiconductor bridge, igniter, and gas generator |
EP1933108A4 (en) * | 2005-09-07 | 2011-11-23 | Nippon Kayaku Kk | Semiconductor bridge, igniter, and gas generator |
US8250978B2 (en) | 2005-09-07 | 2012-08-28 | Nippon Kayaku Kabushiki Kaisha | Semiconductor bridge, igniter, and gas generator |
Also Published As
Publication number | Publication date |
---|---|
RU2161292C1 (en) | 2000-12-27 |
EP0965030A1 (en) | 1999-12-22 |
NO994920L (en) | 1999-10-08 |
AR011934A1 (en) | 2000-09-13 |
EP0965030A4 (en) | 2000-11-15 |
CA2279924A1 (en) | 1998-09-11 |
BR9808207A (en) | 2002-12-24 |
NO994920D0 (en) | 1999-10-08 |
RU99121327A (en) | 2005-01-20 |
US5831203A (en) | 1998-11-03 |
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