US3028809A - Multiple detonator operation - Google Patents
Multiple detonator operation Download PDFInfo
- Publication number
- US3028809A US3028809A US837302A US83730259A US3028809A US 3028809 A US3028809 A US 3028809A US 837302 A US837302 A US 837302A US 83730259 A US83730259 A US 83730259A US 3028809 A US3028809 A US 3028809A
- Authority
- US
- United States
- Prior art keywords
- detonator
- detonators
- series
- coils
- electrical
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
Definitions
- Another object of the invention is a novel circuit means whereby positive functioning of electrically actuated detonators in proximity fuses or other detonator functioned devices is insured.
- Another object of the invention is means whereby a multiplicity of detonators may be caused to fire or the remainder of detonators in the circuit may be fired irrespective of faulty detonators or connections thereto.
- FIGURE 2 shows a modification of the circuit of the invention.
- FIGURE 3 shows another modification of the invention.
- number 1 indicates an electrical feed line of a proximity fuse or any electrical detonator exciter means, not shown, connected to the center tap 3 of a choke 2.
- One end terminal 4 of the choke is connected to a lead of detonator 6 and the opposite end terminal 5 to a lead of detonator 7.
- the remaining leads 6a and 7a of the detonators are joined in a common return line 8 of the exciter means.
- detonator 6 If, for example, detonator 6 is open circuited, all the current will flow through detonator 7. It, on the other hand, detonator 6 is short circuited, the current will pass in approximately equal amounts through the short circuited detonator 6 and the operating detonator 7 because of the negligibl resistance of the detonators and thus cause detonator 7 to function.
- the electrical detonator firing circuit is substantially the same as that shown in FIGURE 1 with the exception that the Series connected capacitors 9 and 10 have been substituted for the center tapped choke 2.
- the feed 1 line is connected to the series connector 11 in order to provide an equal amount of energy for the detonators.
- FIGURE 3 Another system for insuring detonation of explosive missiles or the like is shown in FIGURE 3 wherein the detonators 12, 13 and 14 are connected across spaced coils 15, 16 and 17, respectively. Positioned in inductive relationship to coils 15 and 16 is a coil or link coupling 18 which is in series with a similar coil or link 19 positioned in inductive relationship between coils 16 and 17. The terminals of the series connected coils comprising link coupling means are connected across the feed line 1 and return line 8. In operation, a pulse of current is caused to flow in the link coupling means which in turn induces a current in each of the detonator shunted coils to function the detonators. It is apparent that irrespective of the fact that some detonators or circuits thereof may fail to function, detonation of the explosive missile in which the invention is incorporated may be obtained if but one detonator and circuit remain in operative condition.
- a detonator firing circuit comprising electrical energy supply means including a feed line and a return line, a link coupling means having a plurality of spaced inductive links connected in series, said lin'k coupling means connected to said supply means for receiving electrical impulses therefrom, and a plurality of series circuits each consisting of a coil and a detonator, all of said detonators being responsive to the same condition, each of said coils being closely coupled to one of said spaced inductive links so that the functioning of each of said detonators is independent of the response by the rest of said detonators.
Description
April 10, 1962 M. APSTEIN 3,028,809
MULTIPLE DETONATOR OPERATION Original Filed March 13, 1952 8 FIG. 1 7o 7 8 FIG. 2
3/19 INVENTOR 8 mama/5 APSTV/V 4 2,23 0 4.910% BY ya 21% y/fi mq United States Patent Ofiice 3,028,809 Patented Apr. 10, 1962 3,028,809 MULTIPLE DETONATOR OPERATION Maurice Apstein, Bethesda, Md., assignor to the United States of America as represented by the Secretary of the Army Original application Mar. 13, 1952, Ser. No. 276,433, now Patent No. 2,921,522, dated Jan. 19, 1960. Divided and this application Aug. 31, 1959, Ser. No. 837,302 1 Claim. (Cl. 10270.2) (Granted under Title 35, US. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes without the payment to me of any royalty thereon.
In order to insure that proximity and/or electrical types of fuses employed in artillery projectiles, guided missiles and the like shall function despite a defective detonator, it is desirable that. two or more detonators be used and so arranged that both may fire or that either will fire if the other is short circuited or open circuited. To this end, the novel circuitry of the invention hereinafter described has been devised.
Multiple detonator firing is accomplished by introducing a plurality of coupled isolating impedance elements in series with each of th detonators. This prevents one detonator from short-circuiting the others. As will become apparent, either inductance or capacitance may be used as the isolating impedance, although inductance is to be preferred.
Another object of the invention is a novel circuit means whereby positive functioning of electrically actuated detonators in proximity fuses or other detonator functioned devices is insured.
Another object of the invention is means whereby a multiplicity of detonators may be caused to fire or the remainder of detonators in the circuit may be fired irrespective of faulty detonators or connections thereto.
The specific nature of the invention as well as other objects and advantages thereof will clearly appear from the following description and accompanying drawings in which:
FIGURE 1 shows an embodiment of the invention whereby two detonators are functioned through an inductive means.
FIGURE 2 shows a modification of the circuit of the invention.
FIGURE 3 shows another modification of the invention.
Referring more particularly to the drawings wherein like reference characters designate the same parts throughout the drawings, number 1 indicates an electrical feed line of a proximity fuse or any electrical detonator exciter means, not shown, connected to the center tap 3 of a choke 2. One end terminal 4 of the choke is connected to a lead of detonator 6 and the opposite end terminal 5 to a lead of detonator 7. The remaining leads 6a and 7a of the detonators are joined in a common return line 8 of the exciter means. When a pulse of current is applied to the inductive means 2 through feed line 1, it will divide equally about the center tap 3 and will proportionately flow through detonators 6 and 7 to the return line 8. If, for example, detonator 6 is open circuited, all the current will flow through detonator 7. It, on the other hand, detonator 6 is short circuited, the current will pass in approximately equal amounts through the short circuited detonator 6 and the operating detonator 7 because of the negligibl resistance of the detonators and thus cause detonator 7 to function.
In the modification shown in FIGURE 2, the electrical detonator firing circuit is substantially the same as that shown in FIGURE 1 with the exception that the Series connected capacitors 9 and 10 have been substituted for the center tapped choke 2. In this modification the feed 1 line is connected to the series connector 11 in order to provide an equal amount of energy for the detonators.
Another system for insuring detonation of explosive missiles or the like is shown in FIGURE 3 wherein the detonators 12, 13 and 14 are connected across spaced coils 15, 16 and 17, respectively. Positioned in inductive relationship to coils 15 and 16 is a coil or link coupling 18 which is in series with a similar coil or link 19 positioned in inductive relationship between coils 16 and 17. The terminals of the series connected coils comprising link coupling means are connected across the feed line 1 and return line 8. In operation, a pulse of current is caused to flow in the link coupling means which in turn induces a current in each of the detonator shunted coils to function the detonators. It is apparent that irrespective of the fact that some detonators or circuits thereof may fail to function, detonation of the explosive missile in which the invention is incorporated may be obtained if but one detonator and circuit remain in operative condition.
It will be apparent that the embodiments shown are only exemplary and that various modifications can be made in construction and arrangement within the scope of the invention as defined in the appended claims.
This application is a divisional application of Multiple Detonator Operation, Serial No. 276,433, filed March 13, 1952, now Patent No. 2,921,522.
I claim as my invention:
A detonator firing circuit comprising electrical energy supply means including a feed line and a return line, a link coupling means having a plurality of spaced inductive links connected in series, said lin'k coupling means connected to said supply means for receiving electrical impulses therefrom, and a plurality of series circuits each consisting of a coil and a detonator, all of said detonators being responsive to the same condition, each of said coils being closely coupled to one of said spaced inductive links so that the functioning of each of said detonators is independent of the response by the rest of said detonators.
References Cited in the file of this patent UNITED STATES PATENTS 1,794,421 Ruhlemann Mar. 3, 1931 2,514,359 Allison July 11, 1950 2,748,704 Dinsmoor June 5, 1956 2,789,506 Filbert et al Apr. 23, 1957
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US837302A US3028809A (en) | 1952-03-13 | 1959-08-31 | Multiple detonator operation |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US276433A US2921522A (en) | 1952-03-13 | 1952-03-13 | Multiple detonator operation |
US837302A US3028809A (en) | 1952-03-13 | 1959-08-31 | Multiple detonator operation |
Publications (1)
Publication Number | Publication Date |
---|---|
US3028809A true US3028809A (en) | 1962-04-10 |
Family
ID=26957969
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US837302A Expired - Lifetime US3028809A (en) | 1952-03-13 | 1959-08-31 | Multiple detonator operation |
Country Status (1)
Country | Link |
---|---|
US (1) | US3028809A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4220871A (en) * | 1977-09-08 | 1980-09-02 | Nippondenso Co., Ltd. | Electric control circuit for safety apparatus in automotive vehicles |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1794421A (en) * | 1929-06-13 | 1931-03-03 | Rheinische Metallw & Maschf | Electric percussion fuse for shells, etc. |
US2514359A (en) * | 1945-12-28 | 1950-07-11 | Malcolm G Allison | Proximity fuse |
US2748704A (en) * | 1951-11-29 | 1956-06-05 | Theodore E Dinsmoor | Arming device for torpedo exploders |
US2789506A (en) * | 1949-12-07 | 1957-04-23 | Jr Howard C Filbert | Water discriminating fuze |
-
1959
- 1959-08-31 US US837302A patent/US3028809A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1794421A (en) * | 1929-06-13 | 1931-03-03 | Rheinische Metallw & Maschf | Electric percussion fuse for shells, etc. |
US2514359A (en) * | 1945-12-28 | 1950-07-11 | Malcolm G Allison | Proximity fuse |
US2789506A (en) * | 1949-12-07 | 1957-04-23 | Jr Howard C Filbert | Water discriminating fuze |
US2748704A (en) * | 1951-11-29 | 1956-06-05 | Theodore E Dinsmoor | Arming device for torpedo exploders |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4220871A (en) * | 1977-09-08 | 1980-09-02 | Nippondenso Co., Ltd. | Electric control circuit for safety apparatus in automotive vehicles |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1841983A (en) | Electric igniter with condenser as storing device for the ignition current | |
US3225695A (en) | Pyrotechnic bridge detonating circuit with zener diode circuit controlling switching of scr | |
US2696191A (en) | Electrically operated primer | |
US4378738A (en) | Electromagnetic and electrostatic insensitive blasting caps, squibs and detonators | |
US4136617A (en) | Electronic delay detonator | |
US4314507A (en) | Sequential initiation of explosives | |
EP0013835B1 (en) | Selectively actuable control circuit for a fusehead igniter assembly and detonators containing said circuit | |
US4967665A (en) | RF and DC desensitized electroexplosive device | |
US3343493A (en) | Arming and firing circuit | |
KR950033411A (en) | Continuous blasting system | |
US2921522A (en) | Multiple detonator operation | |
US3028809A (en) | Multiple detonator operation | |
EP2122295B1 (en) | Detonator ignition protection circuit | |
US4960033A (en) | Gun firing relay circuit | |
US2485887A (en) | Projectile | |
DE2434700A1 (en) | ENERGY GENERATING DEVICE FOR ONE SHOT, GRENADE OD. DGL | |
US3363566A (en) | Piezoelectric power supply | |
US4649821A (en) | Electrical circuit continuity test apparatus for firing unit | |
US3343491A (en) | Protective circuit for electrofiring devices | |
US3759183A (en) | Multiple option electric detonator | |
US3269315A (en) | Explosive primer | |
US2509910A (en) | Time-delay circuit | |
US3218470A (en) | Direct coupled logic circuit | |
US4882993A (en) | Electronic back-up safety mechanism for hand-emplaced land mines | |
US3734021A (en) | Solid state fuze select circuit |