US3420174A - Pulse sensitive electro-explosive device - Google Patents

Pulse sensitive electro-explosive device Download PDF

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US3420174A
US3420174A US671885A US3420174DA US3420174A US 3420174 A US3420174 A US 3420174A US 671885 A US671885 A US 671885A US 3420174D A US3420174D A US 3420174DA US 3420174 A US3420174 A US 3420174A
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bridge
explosive
heat sink
electro
explosive device
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Richard R Potter
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/10Initiators therefor
    • F42B3/18Safety initiators resistant to premature firing by static electricity or stray currents

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  • the cartridges are exposed to electro-magnetic fields wherein currents are induced in the lead-in pin.
  • the cartridges are exposed to electromagnetic radiation. Cartridges which are ordinarily safe may become dangerous in such environments. Currents sent accidentally through the bridge wire may be sufficient to heat the primer to its critical temperature, causing it and the cartridge to explode.
  • the heat sink button used in the prior art was limited to use with a Patented Jan. 7, 1969 bridge wire.
  • the instant disclosure utilizes a thin film bridge deposited on the surface of an electrically non-conducting heat sink and therefore a heat sink button could not be used successfully with a thin film bridge since it would allow the primary explosive charge to contact the bridge only over the lead wires and would thus prevent exploitation of the advantageous of the thin film bridge.
  • the pulse sensitive electro-explosive device of the present invention, consists of four essential elements: 1) the primary explosive charge which is initiated by application of heat; (2) the electric heating element in the form of a thin film of electrically conducting material having surface thermal contact with the explosive charge; (3) the heat sink made of electrically insulating material having high thermal conductivity and large thermal capacity arranged so as to have good thermal contact with all parts of the heating element; and (4) the electrical leads which conduct electric current to the heating element and which are made of an electrically conductive material of sufficient cross-section so as not to be a significant source of heat to. the system from electrical energy dissipation.
  • the bridge film In thin film bridge initiators electrical energy dissipation takes place either as heating at the interface between the substrate and the explosive or, more probably, as a small explosion of the bridge film itself caused by vaporization of .the film along the line across the current path.
  • the bridge film In practice, the bridge film is shaped with a narrow or thin section where initiation is desired.
  • the total result of the thin film bridge device is electrical energy conversion to heat in a controllable location, efiicient transfer of the thermal energy into the priming explosive and substantial independence of thermal, electrical and geometrical parameters.
  • Another object of the present invention is to provide an improved pulse sensitive electro-explosive device which combines greater resistance to accidental actuation with unchanged or shorter delay of time of intentional firing.
  • a further object of the present invention is the provision of a pulse sensitive electro-explosive device that requires about one-fourth the firing energy of conventional electro-explosive devices but tolerates five to six times as much spurious input current.
  • Still another object of the present invention is to provide a pulse sensitive electro-explosive device giving a hundredfold or more improvement in the protection ratio compared to a conventional wire bridge electro-explosive device.
  • Yet another object of the present invention is the provision of a thin film bridge pulse sensitive electro-explosive device that has the advantages of ruggedness, ease of fabrication and safet from accidental initiation.
  • FIG. 1 is a conceptual view of the essential elements of a pulse sensitive electro-explosive device
  • FIG. 2 is a view in elevation and in section of an electro-explosive device embodying the principle of the present invention
  • FIG. 3 is the top view of a section taken along line 33 of FIG. 2;
  • FIGS. 4, 5 and 6 are alternative configurations taken along the line 33 in FIG. 2;
  • FIG. 7 is a schematic diagram of an external firing circuit for the pulse sensitive electro-explosive device.
  • FIG. 1 shows the conceptual arrangement of the four essential elements: the priming explosive charge 4, which is initiated by the application of heat; the electric heating element 3, in the form of a gold thin film bridge deposited on the surface of heat sink and having surface thermal contact with the explosive charge; the heat sink 1, made of electrically insulating material, such as sintered beryllium oxide, having high thermal conductivity and large thermal capacity; and arranged so as to have good thermal contact with all parts of the heating element 3; electrical leads 2 and 2', which conduct electric current to the thin film bridge and which are made of an electrically conductive material of sufficient cross-section so as not to be a significant source of heat to the system from electrical energy dissipation.
  • the priming explosive charge 4 which is initiated by the application of heat
  • the electric heating element 3 in the form of a gold thin film bridge deposited on the surface of heat sink and having surface thermal contact with the explosive charge
  • the heat sink 1 made of electrically insulating material, such as sintered beryllium oxide, having high thermal conductivity and large thermal capacity; and
  • the bridge By utilizing a gold thin film for the bridge, the bridge is compatible with the explosive and is ductile enough and thick enough to ensure reliable continuity. Further, it allows the film to be a sufficient thickness to offer an adequate electrical load to the source of electrical initiating energy without destroying the initial protective ratio of electrical to thermal conductivity.
  • FIG. 2 shows a conventional electro-explosive configuration modified to incorporate the PSED features of FIG. 1.
  • the leads 2-2 are molded or cemented into the heat sink 1.
  • the heat sink is made of a strong stable material such as beryllium oxide ceramic so as to have a surface on which to support the bridge film.
  • a bridge film 3, composed of gold is deposited on the polished surface of the heat sink.
  • a metal or plastic charge holder 5 is attached to heat sink 1 and a priming charge 4 is pressed against the surface of bridge 3 to ensure good thermal contact and proper density of charge.
  • a working explosive 6 is pressed into place above the priming charge 4 to give the device the desired ignition or detonation characteristics. Any conventional explosive could be used so long as the primer chosen is sufiicient for ignition.
  • a cover disc 7 is installed over the charge holder 5 and the working explosive 6. Finally, the assembly is permanently sealed by crimping a metal cup 8 over the base of heat sink 1.
  • FIG. 3 is a view taken along 33 of FIG. 2 showing the leads 2 and 2', thin film bridge 3, heat sink 1 and metal cup 8. The ends of the two leads 2 and 2 are made fiush with the surface of heat sink 1 so that the thin film bridge 3 may be deposited on the heat sink surface and may also make good electrical contact with the leads 2-2.
  • FIG. 4 shows an alternative configuration for the bridge shown 4 in FIG. 3.
  • Thin film bridge 13 is identical to thin film bridge 3 except that the shape has been contoured to be narrow at the center. In so doing, there is a greater concentration of electrical energy at this point which aids in igniting priming charge 4.
  • Bridge 23 consists of three regions. A thin film 24 is deposited on the heat sink. An additional layer of film 25 and 26 is then placed over leads 2 and 2'. This provides a better and more reliable contact between the bridge and leads as well as having more efiicient power dissipation at the center.
  • FIG. 6 shows an alternative embodiment where two independent firing circuits are incorporated in a single PSED by having two identical bridges 33 and 33' and four leads 2. and 2 and 32 and 32; Bridges 33 and 33 combine the features shown in FIGS. 4 and 5 wherein the bridge is narrow at the center as well as being thin at the center due to an additional deposit of gold film being placed on the lead wire surface. This configuration yields a higher reliability since the charge can then be detonated from two sources.
  • the PS-ED In use the PS-ED must be connected to an external firing circuit as shown schematically in FIG. 7.
  • firing switch 71 When firing switch 71 is closed current from source 72 flows through the leads 2 and 2' and therefore through the film bridge of FIG. 2.
  • Electrical power dissipation in the film bridge causes heat to flow into the heat sink from the bridge.
  • the temperature of the bridge depends on the rate of heat flow, being less than the ignition temperature for moderate values of input power. If source 72 and the firing circuit supply electrical power to the bridge at a high enough rate, the bridge temperature will rise above the ignition temperature of the primary explosive, and an explosion will eventually result.
  • the most desirable effect would be for the bridge film to fail along a line across the current fiow because of a regenerative local rise in temperature, resistivity and dissipation. The resulting spark explosion would suddenly deliver more energy to the explosive and the priming charge would be immediately initiated.
  • the pulse sensitive electro explosive device fabricated in accordance with the disclosed process are the following 1) the pulse sensitive electro-explosive device with a film bridge on a beryllium oxide heat sink required only one-ninth as much firing energy as a conventional wire-bridge electro-explosive device but tolerated. from one and one-quarter to two times as much spurious current without firing as the wirebridge device.
  • the film bridge on a beryllium oxide heat sink improved the protection ratio more than tenfold compared to a conventional bridge wire electro-explosive device; and the pulse-sensitive electro-explosive device with a gold film bridge on a beryllium oxide heat sink required about one-fourth the firing energy of a conventional electro-explosive device but tolerated five to six times as much spurious input current, i.e., 25 to 36 times as much input power.
  • the pulse sensitive electro-explosive device gave a hundredfold or more improvement in the protection ratio compared to a wire bridge electric-explosive device.
  • a pulse sensitive electro-explosive device comprising a cup-shaped housing
  • an explosive capsule disposed within said cup-shaped housing consisting of a beryllium oxide heat sink;
  • a first gold thin film bridge deposited on one surface of said heat sink and connecting said lead wires wherein said deposited thin film bridge is of non-uniform thickness being thicker at the junctions with said lead wires;

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Description

Jan. 7, 1969 R. R. POTTER 3,420,174
PULSE SENSITIVE ELECTRO-EXPLOSIVE DEVICE Filed Sept. 29. 1967 R ELECTRICAL EXPLOSIVE DEVICE I FIG: 7
INVENTOR RICHA/PD R. POTTER BY gs/M ATTORNEY United States Patent Office 3,420,174 PULSE SENSITIVE ELECTRO- EXPLOSIVE DEVICE Richard R. Potter, Dahlgren, Va., assignor to the United States of America as represented by the Secretary of the Navy Filed Sept. 29, 1967, Ser. No. 671,885
US. Cl. 102-28 Int. Cl. F42]: 37/00 4 Claims ABSTRACT OF THE DISCLOSURE BACKGROUND OF THE INVENTION Field of the invention The present invention relates. to improvements in electro-explosive cartridges, and more particularly, to improved electro-explosive cartridges of the exploding bridgewire type that are better protected from accidental firing.
Description of the prior art In the field of pulse sensitive electro-explosive devices it has been the general practice to employ a high resistance wire, known as a bridge wire, welded to the interior ends of lead-in pins which are directly in contact with the explosive primer. When the firing current passes through the bridge wire, the current heats the bridge wire. The heat from the bridge wire is used to raise the temperature of the explosive primer. When the primer has been heated to its activation temperature, it explodes and fires the cartridge. While such a device has served its purpose, it has not proved entirely satisfactory under all conditions of service for the reason that considerable difliculty has been experienced where the cartridges are used in environments where they are subject to conditions that accidentally send current through the bridge wire. Sometimes the cartridges are exposed to electro-magnetic fields wherein currents are induced in the lead-in pin. Sometimes the cartridges are exposed to electromagnetic radiation. Cartridges which are ordinarily safe may become dangerous in such environments. Currents sent accidentally through the bridge wire may be sufficient to heat the primer to its critical temperature, causing it and the cartridge to explode.
It has been the objective of the prior art to achieve lower initiation sensitivity to spurious currents over substantial exposure times, while maintaining the same, or preferably, a reduced requirement for input electrical energy for prompt intended initiation of the explosive component. The devices of the prior art were therefore required to deliver a large part of the firing energy as heat to the priming explosive charge while directing almost all of the spurious power to a heat sink. The prior art utilized a heat sink button clamped over a conventional wire bridge to increase the electrical input required to initiate the explosive for both desired and spurious modes. This has proved unsatisfactory since it was not an improvement in the protection ratio, i.e., maximum safe sustained power divided by minimum required firing energy, but merely a general reduction in sensitivity. Further, the heat sink button used in the prior art was limited to use with a Patented Jan. 7, 1969 bridge wire. The instant disclosure utilizes a thin film bridge deposited on the surface of an electrically non-conducting heat sink and therefore a heat sink button could not be used successfully with a thin film bridge since it would allow the primary explosive charge to contact the bridge only over the lead wires and would thus prevent exploitation of the advantageous of the thin film bridge.
Another undesirable characteristic of the heat sink button utilized by the prior art was that it conducted heat toward the priming charge rather than away from it. A
third disadvantage to the heat sink button utilized in the prior art was that it was more difiicult to load the priming explosion charge through the small hole in the button. Further, due to the relatively thick cross-section of the wire bridge, the wire bridge initiators required that the heat flow radially outward through the wire, through the wire explosive interface, and finally into some depth of explosive. Ignition characteristics were constrained by the interdependence between thermal, electrical and geometrical parameters. In addition, the primary charge could not be readily pressed against the wire to insure good thermal contact.
SUMMARY OF THE INVENTION The pulse sensitive electro-explosive device (PSED), of the present invention, consists of four essential elements: 1) the primary explosive charge which is initiated by application of heat; (2) the electric heating element in the form of a thin film of electrically conducting material having surface thermal contact with the explosive charge; (3) the heat sink made of electrically insulating material having high thermal conductivity and large thermal capacity arranged so as to have good thermal contact with all parts of the heating element; and (4) the electrical leads which conduct electric current to the heating element and which are made of an electrically conductive material of sufficient cross-section so as not to be a significant source of heat to. the system from electrical energy dissipation. In thin film bridge initiators electrical energy dissipation takes place either as heating at the interface between the substrate and the explosive or, more probably, as a small explosion of the bridge film itself caused by vaporization of .the film along the line across the current path. In practice, the bridge film is shaped with a narrow or thin section where initiation is desired. The total result of the thin film bridge device is electrical energy conversion to heat in a controllable location, efiicient transfer of the thermal energy into the priming explosive and substantial independence of thermal, electrical and geometrical parameters. By utilizing a gold thin film bridge deposited on if heat sink of beryllium oxide, the disadvantages of the prior art can be overcome.
It is therefore an object of the present invention to provide a pulse sensitive electro-explosive device which has greater resistance to accidental actuation.
Another object of the present invention is to provide an improved pulse sensitive electro-explosive device which combines greater resistance to accidental actuation with unchanged or shorter delay of time of intentional firing.
A further object of the present invention is the provision of a pulse sensitive electro-explosive device that requires about one-fourth the firing energy of conventional electro-explosive devices but tolerates five to six times as much spurious input current.
Still another object of the present invention is to provide a pulse sensitive electro-explosive device giving a hundredfold or more improvement in the protection ratio compared to a conventional wire bridge electro-explosive device.
Yet another object of the present invention is the provision of a thin film bridge pulse sensitive electro-explosive device that has the advantages of ruggedness, ease of fabrication and safet from accidental initiation.
Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a conceptual view of the essential elements of a pulse sensitive electro-explosive device;
FIG. 2 is a view in elevation and in section of an electro-explosive device embodying the principle of the present invention;
FIG. 3 is the top view of a section taken along line 33 of FIG. 2;
FIGS. 4, 5 and 6 are alternative configurations taken along the line 33 in FIG. 2; and
FIG. 7 is a schematic diagram of an external firing circuit for the pulse sensitive electro-explosive device.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings wherein like reference characters designate like or corresponding parts throughout the several views, FIG. 1 shows the conceptual arrangement of the four essential elements: the priming explosive charge 4, which is initiated by the application of heat; the electric heating element 3, in the form of a gold thin film bridge deposited on the surface of heat sink and having surface thermal contact with the explosive charge; the heat sink 1, made of electrically insulating material, such as sintered beryllium oxide, having high thermal conductivity and large thermal capacity; and arranged so as to have good thermal contact with all parts of the heating element 3; electrical leads 2 and 2', which conduct electric current to the thin film bridge and which are made of an electrically conductive material of sufficient cross-section so as not to be a significant source of heat to the system from electrical energy dissipation. By utilizing a gold thin film for the bridge, the bridge is compatible with the explosive and is ductile enough and thick enough to ensure reliable continuity. Further, it allows the film to be a sufficient thickness to offer an adequate electrical load to the source of electrical initiating energy without destroying the initial protective ratio of electrical to thermal conductivity.
FIG. 2 shows a conventional electro-explosive configuration modified to incorporate the PSED features of FIG. 1. The leads 2-2 are molded or cemented into the heat sink 1. The heat sink is made of a strong stable material such as beryllium oxide ceramic so as to have a surface on which to support the bridge film. A bridge film 3, composed of gold is deposited on the polished surface of the heat sink. A metal or plastic charge holder 5 is attached to heat sink 1 and a priming charge 4 is pressed against the surface of bridge 3 to ensure good thermal contact and proper density of charge. A working explosive 6 is pressed into place above the priming charge 4 to give the device the desired ignition or detonation characteristics. Any conventional explosive could be used so long as the primer chosen is sufiicient for ignition. A cover disc 7 is installed over the charge holder 5 and the working explosive 6. Finally, the assembly is permanently sealed by crimping a metal cup 8 over the base of heat sink 1.
FIG. 3 is a view taken along 33 of FIG. 2 showing the leads 2 and 2', thin film bridge 3, heat sink 1 and metal cup 8. The ends of the two leads 2 and 2 are made fiush with the surface of heat sink 1 so that the thin film bridge 3 may be deposited on the heat sink surface and may also make good electrical contact with the leads 2-2.
For better firing efficiency it is advantageous to concentrate the firing energy in a limited central area. FIG. 4 shows an alternative configuration for the bridge shown 4 in FIG. 3. Thin film bridge 13 is identical to thin film bridge 3 except that the shape has been contoured to be narrow at the center. In so doing, there is a greater concentration of electrical energy at this point which aids in igniting priming charge 4.
The same effect can be accomplished by depositing extra film over the leads. This is depicted in FIG. 5. Bridge 23 consists of three regions. A thin film 24 is deposited on the heat sink. An additional layer of film 25 and 26 is then placed over leads 2 and 2'. This provides a better and more reliable contact between the bridge and leads as well as having more efiicient power dissipation at the center.
FIG. 6 shows an alternative embodiment where two independent firing circuits are incorporated in a single PSED by having two identical bridges 33 and 33' and four leads 2. and 2 and 32 and 32; Bridges 33 and 33 combine the features shown in FIGS. 4 and 5 wherein the bridge is narrow at the center as well as being thin at the center due to an additional deposit of gold film being placed on the lead wire surface. This configuration yields a higher reliability since the charge can then be detonated from two sources.
In use the PS-ED must be connected to an external firing circuit as shown schematically in FIG. 7. When firing switch 71 is closed current from source 72 flows through the leads 2 and 2' and therefore through the film bridge of FIG. 2.. Electrical power dissipation in the film bridge causes heat to flow into the heat sink from the bridge. The temperature of the bridge depends on the rate of heat flow, being less than the ignition temperature for moderate values of input power. If source 72 and the firing circuit supply electrical power to the bridge at a high enough rate, the bridge temperature will rise above the ignition temperature of the primary explosive, and an explosion will eventually result. The most desirable effect would be for the bridge film to fail along a line across the current fiow because of a regenerative local rise in temperature, resistivity and dissipation. The resulting spark explosion would suddenly deliver more energy to the explosive and the priming charge would be immediately initiated.
Several factors affect the efficiency of operation. For intentional firing of the device, heat flow into the heat sink is a loss. This loss increases with time and is dependent on thermal contact between film bridge and its heat sink substrate. If the external firing circuit delivers electrical energy to the film bridge as a very short pulse of high power, the resultant burnout and spark explosion of the film bridge will produce three beneficial effects: (1) heat will be concentrated in a small region, (2) the film explosion will carry a significant part of the heat energy away from the surface of the heat sink, and (3) the film explosion will carry heat energy into the explosive effecting an improvement over the quiescent thermal contact between film bridge and explosive. By constructing the film bridge with a narrow and/or thin region, the efficiency of ignition can be further optimized as a trade-off with reliability.
Among the advantages of the pulse sensitive electro explosive device fabricated in accordance with the disclosed process are the following 1) the pulse sensitive electro-explosive device with a film bridge on a beryllium oxide heat sink required only one-ninth as much firing energy as a conventional wire-bridge electro-explosive device but tolerated. from one and one-quarter to two times as much spurious current without firing as the wirebridge device. Therefore, use of the film bridge on a beryllium oxide heat sink improved the protection ratio more than tenfold compared to a conventional bridge wire electro-explosive device; and the pulse-sensitive electro-explosive device with a gold film bridge on a beryllium oxide heat sink required about one-fourth the firing energy of a conventional electro-explosive device but tolerated five to six times as much spurious input current, i.e., 25 to 36 times as much input power. Thus,
the pulse sensitive electro-explosive device gave a hundredfold or more improvement in the protection ratio compared to a wire bridge electric-explosive device.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. A pulse sensitive electro-explosive device comprising a cup-shaped housing;
an explosive capsule disposed within said cup-shaped housing consisting of a beryllium oxide heat sink;
two lead wires passing through said heat sink;
a first gold thin film bridge deposited on one surface of said heat sink and connecting said lead wires wherein said deposited thin film bridge is of non-uniform thickness being thicker at the junctions with said lead wires;
a heat sensitive explosive prime charge adjacent to said bridge and heat sink surface;
a working explosive adjacent to said prime charge;
a charge holder circularly enclosing said prime charge, said Working charge and said bridge being adjacent to said heat sink; and
a cover disc placed atop said charge holder and said working explosive.
2. A pulse sensitive electro-explosive device as in claim 1 wherein said deposited thin film bridge is narrower at its center than at said lead wire junctions and is of non uniform thickness being thicker at the junctions with said lead wire.
3. A pulse sensitive electro-explosive device as in claim 1 wherein an additional deposited thin film bridge is connected to two additional wires and placed adjacent to said first thin film bridge to form two alternative detonating circuits.
4. A pulse sensitive electro-explosive device as in claim 3 wherein said first and said additional deposited thin film bridges are narrower at their center than at said lead wire junctions and are of non-uniform thickness being thicker at the junctions with said lead wires.
References Cited UNITED STATES PATENTS 3,158,098 11/1964 Reithel 102--28 3,198,678 8/1965 Zeman et al. 10228 3,227,083 1/1966 Moses et al. 102-28 3,306,202 2/1967 Menichelli et al. 10228 FOREIGN PATENTS 581,316 4/1957 Canada.
SAMUEL FEINBERG, Primary Examiner.
VERLIN R. PENDEGRASS, Assistant Examiner.
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US3763782A (en) * 1970-04-24 1973-10-09 Dynamit Nobel Ag Metal layer initiator
US3987733A (en) * 1975-02-10 1976-10-26 The Ensign-Bickford Company Millisecond delay surface connector
US3987732A (en) * 1975-02-10 1976-10-26 The Ensign-Bickford Company Non-electric double delay borehole downline unit for blasting operations
US4208967A (en) * 1978-05-15 1980-06-24 The United States Of America As Represented By The Secretary Of The Army Squib design
US4307663A (en) * 1979-11-20 1981-12-29 Ici Americas Inc. Static discharge disc
US4316412A (en) * 1979-06-05 1982-02-23 The United States Of America As Represented By The United States Department Of Energy Low voltage nonprimary explosive detonator
US4422381A (en) * 1979-11-20 1983-12-27 Ici Americas Inc. Igniter with static discharge element and ferrite sleeve
DE3415625A1 (en) * 1984-04-26 1985-10-31 Dynamit Nobel Ag, 5210 Troisdorf Electrical detonating element having a desired spark gap
US4592281A (en) * 1982-07-29 1986-06-03 Special Devices, Inc. Arming and firing device
US4729315A (en) * 1986-12-17 1988-03-08 Quantic Industries, Inc. Thin film bridge initiator and method therefor
EP0314898A1 (en) 1987-09-14 1989-05-10 Nippon Koki Co., Ltd. Igniter for electric ignition systems
US5468016A (en) * 1993-05-10 1995-11-21 Nippon Koki Co., Ltd. Gas generating agent pack of air bag inflation gas generator
US5596163A (en) * 1993-08-25 1997-01-21 Ems-Patvag Ag Gas generator igniting capsule
US5847309A (en) * 1995-08-24 1998-12-08 Auburn University Radio frequency and electrostatic discharge insensitive electro-explosive devices having non-linear resistances
US5932832A (en) * 1996-04-15 1999-08-03 Autoliv Asp, Inc. High pressure resistant initiator with integral metal oxide varistor for electro-static discharge protection
US6105503A (en) * 1998-03-16 2000-08-22 Auburn University Electro-explosive device with shaped primary charge
US6196584B1 (en) 1998-12-01 2001-03-06 Trw Inc. Initiator for air bag inflator
US6516724B2 (en) * 2000-11-27 2003-02-11 Trw Airbag Systems Gmbh & Co. Kg Gas generator
US6772692B2 (en) 2000-05-24 2004-08-10 Lifesparc, Inc. Electro-explosive device with laminate bridge
FR2866106A1 (en) * 2004-02-11 2005-08-12 Ncs Pyrotechnie & Tech Electro-pyrotechnic initiator, e.g. for motor vehicle airbag, has heat dissipator insulated electrically from resistive heating element
US20060208474A1 (en) * 2003-12-24 2006-09-21 Nippon Kayaku Kabushiki Kaisha Gas producer
US20110107934A1 (en) * 2009-11-11 2011-05-12 Rustick Joseph M Electronic component deactivation device
US20150260496A1 (en) * 2010-06-18 2015-09-17 Battelle Memorial Institute Non-energetics based detonator
US11041442B2 (en) * 2017-12-06 2021-06-22 Williams International Co., L.L.C. Self-eroding single-use gas-turbine-engine igniter

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US3158098A (en) * 1963-08-09 1964-11-24 Robert J Reithel Low voltage detonator system
US3198678A (en) * 1960-10-03 1965-08-03 Thiokol Chemical Corp Pyrotechnic compositions
US3227083A (en) * 1964-01-30 1966-01-04 Holex Inc Electroexplosive cartridge with heat sink button
US3306202A (en) * 1964-12-02 1967-02-28 Vincent J Menichelli Electric initiator

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Publication number Priority date Publication date Assignee Title
CA581316A (en) * 1959-08-11 Canadian Industries Limited Blasting caps with printed circuit bridge
US3198678A (en) * 1960-10-03 1965-08-03 Thiokol Chemical Corp Pyrotechnic compositions
US3158098A (en) * 1963-08-09 1964-11-24 Robert J Reithel Low voltage detonator system
US3227083A (en) * 1964-01-30 1966-01-04 Holex Inc Electroexplosive cartridge with heat sink button
US3306202A (en) * 1964-12-02 1967-02-28 Vincent J Menichelli Electric initiator

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3763782A (en) * 1970-04-24 1973-10-09 Dynamit Nobel Ag Metal layer initiator
US3987733A (en) * 1975-02-10 1976-10-26 The Ensign-Bickford Company Millisecond delay surface connector
US3987732A (en) * 1975-02-10 1976-10-26 The Ensign-Bickford Company Non-electric double delay borehole downline unit for blasting operations
US4208967A (en) * 1978-05-15 1980-06-24 The United States Of America As Represented By The Secretary Of The Army Squib design
US4316412A (en) * 1979-06-05 1982-02-23 The United States Of America As Represented By The United States Department Of Energy Low voltage nonprimary explosive detonator
US4422381A (en) * 1979-11-20 1983-12-27 Ici Americas Inc. Igniter with static discharge element and ferrite sleeve
US4307663A (en) * 1979-11-20 1981-12-29 Ici Americas Inc. Static discharge disc
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