US20050241521A1 - Device enabling the ignition of two explosive charges and warhead implementing such an ignition device - Google Patents
Device enabling the ignition of two explosive charges and warhead implementing such an ignition device Download PDFInfo
- Publication number
- US20050241521A1 US20050241521A1 US11/067,898 US6789805A US2005241521A1 US 20050241521 A1 US20050241521 A1 US 20050241521A1 US 6789805 A US6789805 A US 6789805A US 2005241521 A1 US2005241521 A1 US 2005241521A1
- Authority
- US
- United States
- Prior art keywords
- booster
- explosive
- ignition
- warhead
- splinter
- 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.)
- Abandoned
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 61
- 230000005540 biological transmission Effects 0.000 claims abstract description 17
- 238000005474 detonation Methods 0.000 claims abstract description 16
- 206010041662 Splinter Diseases 0.000 claims description 21
- 230000037452 priming Effects 0.000 claims description 14
- 239000000463 material Substances 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 3
- 239000006185 dispersion Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 description 1
- MKWKGRNINWTHMC-UHFFFAOYSA-N 4,5,6-trinitrobenzene-1,2,3-triamine Chemical compound NC1=C(N)C([N+]([O-])=O)=C([N+]([O-])=O)C([N+]([O-])=O)=C1N MKWKGRNINWTHMC-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000644 propagated effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/095—Arrangements of a multiplicity of primers or detonators, dispersed around a warhead, one of the primers or detonators being selected for directional detonation effects
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0838—Primers or igniters for the initiation or the explosive charge in a warhead
- F42C19/0842—Arrangements of a multiplicity of primers or detonators, dispersed within a warhead, for multiple mode selection
Definitions
- the technical scope of the invention is that of devices enabling the ignition of at least two explosive charges using a single detonator.
- This solution is not well adapted to the design of an ignition device for a piece of ammunition, for example for a splinter-generating warhead.
- the aim of the invention is to propose an ignition device that is simple in design, compact and reliable ensuring the ignition of two explosive charges (namely a piece of ammunition) using a single detonator.
- the invention relates to a device enabling the ignition of at least two explosive charges using a single detonator, device characterized in that it comprises at least a first pyrotechnic booster that is ignited by the detonator, a first booster that firstly ignites a first explosive charge by projecting a casing onto it and which is secondly connected to a second explosive charge by at least one detonation wave transmission booster.
- the path of the projected casing will be of a length such that the ignition of both explosive charges will be practically simultaneous.
- the first booster will be cylindrical and surrounded by a casing, also cylindrical, the projection of the casing occurring through an annular cavity arranged in the first explosive charge.
- Warheads are sought to be made, for example, which in order to destroy a reinforced target (for example a missile nose cone) generate a cone of splinters focused in the vicinity of a radial plane of the warhead.
- a reinforced target for example a missile nose cone
- these “focused cone” warheads are obtained by simultaneously igniting the warhead at both ends. Ignition is considered to be simultaneous when the deviation between both ignitions is less than or equal to 2 micro seconds.
- these same warheads must, additionally, be able to generate an omni directional cone of splinters. It is classical to produce such a cone by igniting the warhead at only one of its ends.
- the invention thus also relates to a warhead of simple design, that is compact and reliable, and which, thanks to the ignition device according to the invention can be made to operate under two different modes.
- the invention also relates to a splinter-generating warhead implementing an ignition device such as that described previously, warhead characterized in that it comprises a block of loading explosive able to be ignited at one of its ends or the other by a first and/or second igniting explosive charge, the first igniting charge being able to be ignited by the projection of a casing surrounding the first booster and the second igniting explosive charge being able to be ignited by means of at least one detonation wave transmission booster connecting it to the first booster.
- the loading explosive block may incorporate an axial channel inside which the detonation wave transmission booster will pass.
- the splinter-generating warhead according to the invention may incorporate an insulating sheath placed in the axial channel and surrounding the transmission booster.
- the warhead may comprise a first detonator placed so as to be able to ignite the first booster, such first detonator being activated by a priming fuse.
- the first igniting explosive charge may be directly ignited by a second priming means separate from the first booster.
- the second priming means may comprise at least three detonating primers evenly spaced angularly and arranged opposite a crown of the first explosive charge.
- FIG. 1 is a section view of a warhead according to the invention implementing the ignition device according to the invention
- FIGS. 2 a and 2 b are two views schematizing the operation of the warhead according to the invention respectively in its focused splinter cone and scattered splinter cone modes.
- a warhead 1 comprises a block 2 of loading explosive that is placed into a splinter-generating casing 3 .
- the casing 3 is closed at each end by a cover 4 a , 4 b .
- the explosive block 2 incorporates a cavity 5 a , 5 b at each of its ends that receives an igniting explosive charge 6 a , 6 b.
- the block 2 further incorporates an axial channel 7 that connects the two cavities 5 a and 5 b .
- the first cavity 5 a encloses a tablet of a first igniting explosive charge 6 a .
- This first charge is constituted, for example, by a relatively insensitive explosive such as an explosive associating triaminotrinitrobenzene and a thermoplastic binder, explosive such as that described by patent FR2671549.
- This first charge 6 a incorporates a cylindrical housing 8 inside which a first detonation booster 9 a is placed, this being placed opposite a first detonator 10 a .
- the booster 9 a will be constituted, for example, by an explosive associating cyclonite and wax. This booster is cylindrical and coaxial to the housing 8 .
- the detonator 10 a is connected by a filament to a priming fuse 14 .
- the first booster 9 a is surrounded by a cylindrical casing 11 , for example metallic, which is intended to be projected radially against the internal cylindrical wall of the housing 8 when the first booster 9 a is ignited.
- the space 12 separating the casing 11 and the first charge 6 a may be either empty or filled with an annular layer of compressible synthetic foam.
- the projection of the casing 11 thus ensures the ignition of the first charge 6 a by the first booster 9 a with a delay that depends on the diameter of the housing 8 , on the nature and thickness of the casing 11 as well as on the presence or absence of a compressible material inside the space 12 .
- a washer 21 (for example metallic) is placed between the end of the booster 9 a and the igniting explosive charge 6 a . This washer enables a direct axial ignition of the charge 6 a by the booster 9 a to be avoided.
- the second igniting explosive charge 6 b is of the same composition as the first charge 6 a . It is, moreover, ignited by a second detonation booster 9 b which is itself ignited by the first booster 9 a and by means of a detonation wave transmission booster 13 , placed between the two boosters 9 a and 9 b.
- Transmission boosters are well known to the Expert. They generally comprise a tube 13 a of plastic material enclosing a fine layer of explosive and carrying a booster 13 b , 13 c at each end.
- cords ensure the transmission of the detonation wave between two boosters at a velocity of around 7,000 m/s.
- the cord 13 is separated from the explosive block 2 by an insulating sheath 15 placed in the axial channel 7 and surrounding the transmission booster 13 .
- This sheath is made, for example, of a plastic material. Its purpose is to protect the explosive block 2 against projections from the cord 13 .
- the first igniting explosive charge 6 a may be ignited directly by second priming means separate from the first booster 9 a.
- These second priming means here comprise at least three detonating primers 10 b, evenly spaced angularly, and placed opposite a crown 16 of the first explosive charge 6 a.
- FIG. 2 a shows one mode of operation of the warhead 1 in the “focused splinter cone” mode.
- the priming fuse then controls the ignition of the axial detonator 10 a.
- the first booster 9 a is then ignited and in turn ignites the second explosive charge 6 b by means of the transmission relay 13 and of the second booster 9 b.
- the ignition of the first booster 9 a causes the casing 11 to be projected through the space 12 .
- the projection velocity of the casing 11 is of around 2,000 m/s whereas the detonation velocity via the transmission booster 13 and the second booster 9 b is of around 7,000 m/s.
- the distance that the projected casing 11 must cover is much less than that to be covered by the detonation wave conducted by the axial booster 13 .
- the device Because of the differences in velocity, it is thus possible for the device to be dimensioned such that there is a simultaneous ignition of the two explosive charges 6 a and 6 b.
- Ignition is considered to be simultaneous when the deviation between both ignitions is less than or equal to 2 micro seconds.
- the explosive block 2 Since the two igniting explosive charges 6 a and 6 b are ignited simultaneously, the explosive block 2 is ignited at its two ends and two detonation wave fronts 18 a and 18 b are propagated in the explosive block 2 in directions that converge towards a median plane 19 , leading to a projection of the casing 3 splinters in the direction of this median plane 19 (arrows E schematize the projection velocities for the splinters).
- FIG. 2 b shows the operation of the warhead 1 in its “scattered splinter cone” mode.
- the priming fuse 14 then controls the ignition of the crown of peripheral detonators 10 b.
- detonators then ignite directly the first explosive charge 6 a .
- the first booster 9 a is not ignited.
- a single detonation wave front 18 c progresses, in this case, through the explosive block 2 . This results in a dispersion of the splinters in a relatively homogeneous manner inside a cylindrical volume around the axis 20 of the warhead.
- peripheral detonators 10 b it is thus possible for the peripheral detonators 10 b to be replaced by a priming device that only has one axial detonator 10 a and a mobile screen (not shown) able to move in the housing 8 , placed between the casing 11 and the first explosive charge 6 a.
- the detonator When the detonator is ignited, it controls the ignition of the second explosive charge 6 b by means of the transmission booster 13 and the second booster 9 b.
- the casing 11 cannot be projected onto the first explosive charge 6 a .
- the explosive block 2 is thus ignited at one end only by the second explosive charge 6 b.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Fire Alarms (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
A device enabling the ignition of at least two explosive charges using a single detonator, device wherein it comprises at least a first pyrotechnic booster that is ignited by the detonator, a first booster that firstly ignites a first explosive charge by projecting a casing onto it and which is secondly connected to a second explosive charge by at least one detonation wave transmission booster.
Description
- 1. Field of the Invention
- The technical scope of the invention is that of devices enabling the ignition of at least two explosive charges using a single detonator.
- 2. Description of the Related Art
- It is known, for example in the field of quarry explosives, to ignite several explosive charges using a single detonator. This detonator is connected to the different explosive charges by detonation wave transmission cords.
- With such a solution, if the different charges are required to be detonated simultaneously, it is necessary for cords of identical length to be provided between the detonator and the different explosive charges.
- This solution is not well adapted to the design of an ignition device for a piece of ammunition, for example for a splinter-generating warhead.
- Indeed, it would in this case be necessary for substantial lengths of cord to be housed in the vicinity of the ammunition's explosive charge.
- The aim of the invention is to propose an ignition device that is simple in design, compact and reliable ensuring the ignition of two explosive charges (namely a piece of ammunition) using a single detonator.
- Thus, the invention relates to a device enabling the ignition of at least two explosive charges using a single detonator, device characterized in that it comprises at least a first pyrotechnic booster that is ignited by the detonator, a first booster that firstly ignites a first explosive charge by projecting a casing onto it and which is secondly connected to a second explosive charge by at least one detonation wave transmission booster.
- According to another characteristic, the path of the projected casing will be of a length such that the ignition of both explosive charges will be practically simultaneous.
- Advantageously, the first booster will be cylindrical and surrounded by a casing, also cylindrical, the projection of the casing occurring through an annular cavity arranged in the first explosive charge.
- Furthermore, at present it is necessary for splinter-generating warheads to be designed that have several different modes of operation, programmable according to operational needs.
- Warheads are sought to be made, for example, which in order to destroy a reinforced target (for example a missile nose cone) generate a cone of splinters focused in the vicinity of a radial plane of the warhead. Classically, these “focused cone” warheads are obtained by simultaneously igniting the warhead at both ends. Ignition is considered to be simultaneous when the deviation between both ignitions is less than or equal to 2 micro seconds.
- To be able to destroy targets with little protection (such as command posts or communication boosters) these same warheads must, additionally, be able to generate an omni directional cone of splinters. It is classical to produce such a cone by igniting the warhead at only one of its ends.
- Known solutions implement igniters, placed at each of the end faces of the warhead and controlled by a single electronic priming device.
- These solutions require complicated electrical connections. Furthermore, the reliability of the simultaneity of the ignition depends on several factors: the reliability of the electronic system controlling the simultaneous ignition and the reliability of the two igniters.
- The invention thus also relates to a warhead of simple design, that is compact and reliable, and which, thanks to the ignition device according to the invention can be made to operate under two different modes.
- Thus, the invention also relates to a splinter-generating warhead implementing an ignition device such as that described previously, warhead characterized in that it comprises a block of loading explosive able to be ignited at one of its ends or the other by a first and/or second igniting explosive charge, the first igniting charge being able to be ignited by the projection of a casing surrounding the first booster and the second igniting explosive charge being able to be ignited by means of at least one detonation wave transmission booster connecting it to the first booster.
- The loading explosive block may incorporate an axial channel inside which the detonation wave transmission booster will pass.
- The splinter-generating warhead according to the invention may incorporate an insulating sheath placed in the axial channel and surrounding the transmission booster.
- The warhead may comprise a first detonator placed so as to be able to ignite the first booster, such first detonator being activated by a priming fuse.
- According to one variant, the first igniting explosive charge may be directly ignited by a second priming means separate from the first booster.
- The second priming means may comprise at least three detonating primers evenly spaced angularly and arranged opposite a crown of the first explosive charge.
- The invention will become more apparent from the additional description that follows of a particular embodiment, such description being made with reference to the appended drawings, in which:
-
FIG. 1 is a section view of a warhead according to the invention implementing the ignition device according to the invention, -
FIGS. 2 a and 2 b are two views schematizing the operation of the warhead according to the invention respectively in its focused splinter cone and scattered splinter cone modes. - With reference to
FIG. 1 , awarhead 1 according to the invention comprises ablock 2 of loading explosive that is placed into a splinter-generatingcasing 3. Thecasing 3 is closed at each end by a 4 a, 4 b. Thecover explosive block 2 incorporates a 5 a, 5 b at each of its ends that receives an ignitingcavity 6 a, 6 b.explosive charge - The
block 2 further incorporates anaxial channel 7 that connects the two 5 a and 5 b .cavities - The
first cavity 5 a encloses a tablet of a first ignitingexplosive charge 6 a. This first charge is constituted, for example, by a relatively insensitive explosive such as an explosive associating triaminotrinitrobenzene and a thermoplastic binder, explosive such as that described by patent FR2671549. Thisfirst charge 6 a incorporates acylindrical housing 8 inside which afirst detonation booster 9 a is placed, this being placed opposite afirst detonator 10 a. Thebooster 9 a will be constituted, for example, by an explosive associating cyclonite and wax. This booster is cylindrical and coaxial to thehousing 8. - The
detonator 10 a is connected by a filament to apriming fuse 14. - The
first booster 9 a is surrounded by acylindrical casing 11, for example metallic, which is intended to be projected radially against the internal cylindrical wall of thehousing 8 when thefirst booster 9 a is ignited. Thespace 12 separating thecasing 11 and thefirst charge 6 a may be either empty or filled with an annular layer of compressible synthetic foam. - The projection of the
casing 11 thus ensures the ignition of thefirst charge 6 a by thefirst booster 9 a with a delay that depends on the diameter of thehousing 8, on the nature and thickness of thecasing 11 as well as on the presence or absence of a compressible material inside thespace 12. - Furthermore, a washer 21 (for example metallic) is placed between the end of the
booster 9 a and the ignitingexplosive charge 6 a. This washer enables a direct axial ignition of thecharge 6 a by thebooster 9 a to be avoided. - The second igniting
explosive charge 6 b is of the same composition as thefirst charge 6 a. It is, moreover, ignited by asecond detonation booster 9 b which is itself ignited by thefirst booster 9 a and by means of a detonationwave transmission booster 13, placed between the two 9 a and 9 b.boosters - Transmission boosters are well known to the Expert. They generally comprise a
tube 13 a of plastic material enclosing a fine layer of explosive and carrying a 13 b, 13 c at each end.booster - These cords ensure the transmission of the detonation wave between two boosters at a velocity of around 7,000 m/s.
- The
cord 13 is separated from theexplosive block 2 by aninsulating sheath 15 placed in theaxial channel 7 and surrounding thetransmission booster 13. - This sheath is made, for example, of a plastic material. Its purpose is to protect the
explosive block 2 against projections from thecord 13. - According to another characteristic of the warhead according to the invention, the first igniting
explosive charge 6 a may be ignited directly by second priming means separate from thefirst booster 9 a. - These second priming means here comprise at least three detonating
primers 10 b, evenly spaced angularly, and placed opposite acrown 16 of the firstexplosive charge 6 a. - The three
peripheral detonators 10 b are carried (as indeed is thefirst detonator 10 a) by asupport 17 integral with thecover 4 a. They are connected (as is thedetonator 10 a) to thepriming fuse 14 by filaments. - The operation of the
warhead 1 and of its ignition device will now be described with reference toFIGS. 2 a and 2 b. -
FIG. 2 a shows one mode of operation of thewarhead 1 in the “focused splinter cone” mode. The priming fuse then controls the ignition of theaxial detonator 10 a. - The
first booster 9 a is then ignited and in turn ignites the secondexplosive charge 6 b by means of thetransmission relay 13 and of thesecond booster 9 b. - In parallel, the ignition of the
first booster 9 a causes thecasing 11 to be projected through thespace 12. - This casing impacts against the internal cylindrical surface of the
housing 8. The shock thus causes the ignition of the firstexplosive charge 6 a. - The projection velocity of the
casing 11 is of around 2,000 m/s whereas the detonation velocity via thetransmission booster 13 and thesecond booster 9 b is of around 7,000 m/s. However, the distance that the projectedcasing 11 must cover is much less than that to be covered by the detonation wave conducted by theaxial booster 13. - Because of the differences in velocity, it is thus possible for the device to be dimensioned such that there is a simultaneous ignition of the two
6 a and 6 b.explosive charges - Ignition is considered to be simultaneous when the deviation between both ignitions is less than or equal to 2 micro seconds.
- Somebody skilled in the art will easily dimension such an ignition device by acting namely on the diameter of the
housing 8, on the thickness of the projectedcasing 11, on the mass of thefirst booster 9 a as well as on the presence or absence of a filling material in thespace 12. - Since the two igniting
6 a and 6 b are ignited simultaneously, theexplosive charges explosive block 2 is ignited at its two ends and two 18 a and 18 b are propagated in thedetonation wave fronts explosive block 2 in directions that converge towards amedian plane 19, leading to a projection of thecasing 3 splinters in the direction of this median plane 19 (arrows E schematize the projection velocities for the splinters). -
FIG. 2 b shows the operation of thewarhead 1 in its “scattered splinter cone” mode. The priming fuse 14 then controls the ignition of the crown ofperipheral detonators 10 b. - These detonators then ignite directly the first
explosive charge 6 a. Thefirst booster 9 a is not ignited. A singledetonation wave front 18 c progresses, in this case, through theexplosive block 2. This results in a dispersion of the splinters in a relatively homogeneous manner inside a cylindrical volume around theaxis 20 of the warhead. - Different variants are possible without departing from the scope of the invention.
- It is thus possible for the
peripheral detonators 10 b to be replaced by a priming device that only has oneaxial detonator 10 a and a mobile screen (not shown) able to move in thehousing 8, placed between thecasing 11 and the firstexplosive charge 6 a. - In this case, when the warhead is required to operate in its “focused cone” mode, operation is effected as described previously with reference to
FIG. 2 a. - When the warhead is required to operate in its “scattered cone” mode the screen is positioned (before ignition) in the
housing 8. This may be carried out using a suitable actuator (such as a stepping motor). - When the detonator is ignited, it controls the ignition of the second
explosive charge 6 b by means of thetransmission booster 13 and thesecond booster 9 b. - Because of the presence of the screen, the
casing 11 cannot be projected onto the firstexplosive charge 6 a. Theexplosive block 2 is thus ignited at one end only by the secondexplosive charge 6 b. - This results in a dispersion of the splinters having an orientation that is symmetrical with respect to a
median plane 19 of that shown inFIG. 2 b.
Claims (9)
1. A device enabling the ignition of at least two explosive charges using a single detonator, wherein said device comprises at least a first pyrotechnic booster that is ignited by said detonator, said first booster that firstly ignites a first explosive charge by projecting a casing onto said charge, said first booster being secondly connected to a second explosive charge by at least one detonation wave transmission booster.
2. An ignition device according to claim 1 , wherein the path of said projected casing is of a length such that the ignition of both said explosive charges is practically simultaneous.
3. An ignition device according to claim 1 , wherein said first booster is cylindrical and surrounded by said casing, also cylindrical, the projection of said casing occurring through an annular cavity arranged in said first explosive charge.
4. A splinter-generating warhead implementing an ignition device according to claim 1 , wherein said warhead comprises a block of loading explosive able to be ignited at one of its ends or the other by a first and/or second igniting explosive charge, said first igniting charge being able to be ignited by the projection of a casing surrounding said first booster and said second igniting explosive charge being able to be ignited by means of at least one detonation wave transmission booster connecting it to said first booster.
5. A splinter-generating warhead according to claim 4 , wherein said loading explosive block incorporates an axial channel inside which said detonation wave transmission relay passes.
6. A splinter-generating warhead according to claim 5 , wherein it incorporates an insulating sheath placed in said axial channel and surrounding said transmission booster.
7. A splinter-generating warhead according to claim 4 , wherein it comprises a first detonator placed so as to be able to ignite said first booster, said first detonator being activated by a priming fuse.
8. A splinter-generating warhead according to claim 7 , wherein said first igniting explosive charge may be directly ignited by a second priming means separate from said first booster.
9. A splinter-generating warhead according to claim 8 , wherein said second priming means comprise at least three detonating primers evenly spaced angularly and arranged opposite a crown of the first explosive charge.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR04.02890 | 2004-03-18 | ||
| FR0402890A FR2867848B1 (en) | 2004-03-18 | 2004-03-18 | DEVICE FOR INITIATION OF TWO EXPLOSIVE LOADS AND MILITARY HEAD USING SUCH AN INITIATION DEVICE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050241521A1 true US20050241521A1 (en) | 2005-11-03 |
Family
ID=34834204
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/067,898 Abandoned US20050241521A1 (en) | 2004-03-18 | 2005-03-01 | Device enabling the ignition of two explosive charges and warhead implementing such an ignition device |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20050241521A1 (en) |
| EP (1) | EP1577635B1 (en) |
| AT (1) | ATE469334T1 (en) |
| DE (1) | DE602005021420D1 (en) |
| ES (1) | ES2346663T3 (en) |
| FR (1) | FR2867848B1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2896577A1 (en) * | 2006-01-24 | 2007-07-27 | Giat Ind Sa | STARTING DEVICE FOR MULTI-MODE LOAD |
| WO2021063615A1 (en) * | 2019-10-01 | 2021-04-08 | Rheinmetall Waffe Munition Gmbh | Active element and method for igniting an active element |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006018687A1 (en) * | 2006-04-21 | 2007-11-08 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Switchable charge |
Citations (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US481585A (en) * | 1892-08-30 | Mole-trap | ||
| US3447463A (en) * | 1967-05-01 | 1969-06-03 | Arthur Alfred Lavine | Dual ignition explosive arrangement |
| US3853059A (en) * | 1971-01-11 | 1974-12-10 | Us Navy | Configured blast fragmentation warhead |
| US4026213A (en) * | 1971-06-17 | 1977-05-31 | The United States Of America As Represented By The Secretary Of The Navy | Selectively aimable warhead |
| US4145972A (en) * | 1976-12-17 | 1979-03-27 | The United States Of America As Represented By The Secretary Of The Navy | Dual-mode warhead initiation system |
| US4160412A (en) * | 1977-06-27 | 1979-07-10 | Thomas A. Edgell | Earth fracturing apparatus |
| US4188884A (en) * | 1964-07-27 | 1980-02-19 | The United States Of America As Represented By The Secretary Of The Navy | Water reactive underwater warhead |
| US4282814A (en) * | 1974-12-20 | 1981-08-11 | The United States Of America As Represented By The Secretary Of The Navy | Dual-end warhead initiation system |
| US4291627A (en) * | 1979-11-27 | 1981-09-29 | General Electric Company | Electrical fuze with a plurality of modes of operation |
| US4357873A (en) * | 1979-02-06 | 1982-11-09 | Messerschmitt-Bolkow-Blohm Gmbh | Apparatus for destroying structures such as concrete walls |
| US4662281A (en) * | 1984-09-28 | 1987-05-05 | The Boeing Company | Low velocity disc pattern fragment warhead |
| US4745864A (en) * | 1970-12-21 | 1988-05-24 | Ltv Aerospace & Defense Company | Explosive fragmentation structure |
| US4823701A (en) * | 1984-09-28 | 1989-04-25 | The Boeing Company | Multi-point warhead initiation system |
| US5467824A (en) * | 1994-12-09 | 1995-11-21 | Senior Engineering Company | Apparatus for and a method of severing multiple casing strings using explosives |
| US5698814A (en) * | 1995-03-10 | 1997-12-16 | The United States Of America As Represented By The Secretary Of The Air Force | Hard target penetrator with multi-segmenting casing cutter |
| US20030167956A1 (en) * | 2001-11-28 | 2003-09-11 | Geke Technologie Gmbh | Projectiles possessing high penetration and lateral effect with integrated disintegration arrangement |
| US6622632B1 (en) * | 2002-03-01 | 2003-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Polar ejection angle control for fragmenting warheads |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2560375B1 (en) * | 1983-03-09 | 1986-10-03 | Saint Louis Inst | EXPLOSIVE DEVICE WITH FRAGMENTATION AND FOCUSING OF SHARDS |
| FR2550857B1 (en) * | 1983-08-16 | 1987-01-23 | Matra | EXPLOSIVE MILITARY LOAD |
| US4815385A (en) * | 1987-12-16 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Army | Blast focusing method and apparatus |
-
2004
- 2004-03-18 FR FR0402890A patent/FR2867848B1/en not_active Expired - Fee Related
-
2005
- 2005-02-23 DE DE602005021420T patent/DE602005021420D1/en not_active Expired - Lifetime
- 2005-02-23 ES ES05290406T patent/ES2346663T3/en not_active Expired - Lifetime
- 2005-02-23 AT AT05290406T patent/ATE469334T1/en not_active IP Right Cessation
- 2005-02-23 EP EP05290406A patent/EP1577635B1/en not_active Expired - Lifetime
- 2005-03-01 US US11/067,898 patent/US20050241521A1/en not_active Abandoned
Patent Citations (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US481585A (en) * | 1892-08-30 | Mole-trap | ||
| US4188884A (en) * | 1964-07-27 | 1980-02-19 | The United States Of America As Represented By The Secretary Of The Navy | Water reactive underwater warhead |
| US3447463A (en) * | 1967-05-01 | 1969-06-03 | Arthur Alfred Lavine | Dual ignition explosive arrangement |
| US4745864A (en) * | 1970-12-21 | 1988-05-24 | Ltv Aerospace & Defense Company | Explosive fragmentation structure |
| US3853059A (en) * | 1971-01-11 | 1974-12-10 | Us Navy | Configured blast fragmentation warhead |
| US4026213A (en) * | 1971-06-17 | 1977-05-31 | The United States Of America As Represented By The Secretary Of The Navy | Selectively aimable warhead |
| US4282814A (en) * | 1974-12-20 | 1981-08-11 | The United States Of America As Represented By The Secretary Of The Navy | Dual-end warhead initiation system |
| US4145972A (en) * | 1976-12-17 | 1979-03-27 | The United States Of America As Represented By The Secretary Of The Navy | Dual-mode warhead initiation system |
| US4160412A (en) * | 1977-06-27 | 1979-07-10 | Thomas A. Edgell | Earth fracturing apparatus |
| US4357873A (en) * | 1979-02-06 | 1982-11-09 | Messerschmitt-Bolkow-Blohm Gmbh | Apparatus for destroying structures such as concrete walls |
| US4291627A (en) * | 1979-11-27 | 1981-09-29 | General Electric Company | Electrical fuze with a plurality of modes of operation |
| US4662281A (en) * | 1984-09-28 | 1987-05-05 | The Boeing Company | Low velocity disc pattern fragment warhead |
| US4823701A (en) * | 1984-09-28 | 1989-04-25 | The Boeing Company | Multi-point warhead initiation system |
| US5467824A (en) * | 1994-12-09 | 1995-11-21 | Senior Engineering Company | Apparatus for and a method of severing multiple casing strings using explosives |
| US5698814A (en) * | 1995-03-10 | 1997-12-16 | The United States Of America As Represented By The Secretary Of The Air Force | Hard target penetrator with multi-segmenting casing cutter |
| US20030167956A1 (en) * | 2001-11-28 | 2003-09-11 | Geke Technologie Gmbh | Projectiles possessing high penetration and lateral effect with integrated disintegration arrangement |
| US6622632B1 (en) * | 2002-03-01 | 2003-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Polar ejection angle control for fragmenting warheads |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2896577A1 (en) * | 2006-01-24 | 2007-07-27 | Giat Ind Sa | STARTING DEVICE FOR MULTI-MODE LOAD |
| WO2021063615A1 (en) * | 2019-10-01 | 2021-04-08 | Rheinmetall Waffe Munition Gmbh | Active element and method for igniting an active element |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2867848A1 (en) | 2005-09-23 |
| EP1577635B1 (en) | 2010-05-26 |
| ATE469334T1 (en) | 2010-06-15 |
| FR2867848B1 (en) | 2006-04-28 |
| ES2346663T3 (en) | 2010-10-19 |
| DE602005021420D1 (en) | 2010-07-08 |
| EP1577635A1 (en) | 2005-09-21 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8365671B2 (en) | Adaptable smart warhead charge and method for use | |
| US20120227609A1 (en) | Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods | |
| US20020088363A1 (en) | Linear ignition system | |
| NO339841B1 (en) | Seismic charge pack and system for use in seismic surveys, and seismic survey method | |
| RU2046281C1 (en) | Guided missile | |
| US4145972A (en) | Dual-mode warhead initiation system | |
| US10605576B1 (en) | Dual mode initiator system | |
| JPS6347755Y2 (en) | ||
| US8770110B2 (en) | Selectable yield warhead and method | |
| US8464639B2 (en) | Shaped charge fuse booster system for dial lethality in reduced collateral damage bombs (RCDB) | |
| US5144893A (en) | Safe ordnance initiation system | |
| US4282814A (en) | Dual-end warhead initiation system | |
| EP2933598A2 (en) | Multi-action separator fitted to a munition for separating the fuze and the warhead of the munition | |
| US20050241521A1 (en) | Device enabling the ignition of two explosive charges and warhead implementing such an ignition device | |
| US3547033A (en) | Ignitor for explosive charge with means for preventing inadvertent ignition | |
| US6283032B1 (en) | Projectile with controlled decomposition and integrated charge in the area of the effective mass | |
| US12173996B2 (en) | Munitions and methods for operating same | |
| KR102416247B1 (en) | Double detonation apparatus for warhead | |
| US6615736B2 (en) | Priming device for an explosive charge and shaped charge incorporating such a priming device | |
| US2900906A (en) | Self-destruction device | |
| JPH028697A (en) | Multi-way initiating method and device for explosive | |
| US20250067545A1 (en) | Warheads, munitions and methods for operating same | |
| BG4259U1 (en) | Anti-hail rocket | |
| BG64719B1 (en) | Multifunctional piezoelectric fuse | |
| JPH09329400A (en) | Forward directional warhead |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: GIAT INDUSTRIES, FRANCE Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:VIVES, MICHEL;DUPARC, JEAN-PAUL;REEL/FRAME:016341/0639 Effective date: 20050223 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |