US20110162547A1 - Ignition mixtures - Google Patents
Ignition mixtures Download PDFInfo
- Publication number
- US20110162547A1 US20110162547A1 US12/963,794 US96379410A US2011162547A1 US 20110162547 A1 US20110162547 A1 US 20110162547A1 US 96379410 A US96379410 A US 96379410A US 2011162547 A1 US2011162547 A1 US 2011162547A1
- Authority
- US
- United States
- Prior art keywords
- agent
- igniter
- mixtures
- metals
- ammonium
- 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
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
- F42B3/113—Initiators therefor activated by optical means, e.g. laser, flashlight
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C7/00—Non-electric detonators; Blasting caps; Primers
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C9/00—Chemical contact igniters; Chemical lighters
Definitions
- the present invention relates to ignition mixtures and manufacture and use thereof.
- Ignition mixtures and primers are used to ignite pyrotechnic mixtures or primers as well as propellant charges.
- the pyrotechnic mixtures or primers can represent the single charge or a booster charge or a gas-generating primer.
- Propellant charges and primers convert into primarily gaseous components which can be used to trigger rapid-acting processes such as acceleration of projectiles, driving in fastening materials, for example with the aid of bolt setters, or inflating air bags or triggering belt tighteners in vehicle safety.
- One variant is represented by the use of liquid primers instead of solid primers. These exploit the reaction of liquid fuel with oxidizers to generate gases.
- Ignition mixtures are generally triggered mechanically so that they must be sensitive to the action of friction and impact. They generally consist of initial or primary explosives such as lead trinitroresorcinate or diazodinitrophenol, reducing agents such as metal powder, or oxidizers such as barium nitrate or zinc peroxide. Sensitizers such as tetrazene or friction agents such as powdered glass, which increase the sensitivity of the initial explosive materials, are also used. For electrically ignitable systems, the rapid-reacting initial explosives are primarily used. However, the high mechanical sensitivity of the components required for perfect function is a disadvantage when handling the raw materials and mixtures. Handling requires special safety measures. Other types of ignition such as ignition by heat or by coupling high-frequency electromagnetic waves do not solve this problem or are suitable only for highly specialized and sharply limited applications.
- the goal of the present invention is to provide new ignition mixtures.
- the problem is solved by ignition mixtures that can be ignited by the laser light.
- the explosives contained in the ignition mixtures according to the invention can be primary or initial explosives, secondary explosives, or mixtures of these explosives.
- the primary or initial explosives that can be used may for example be lead trinitroresorcinate, diazodinitrophenol, tetrazene, or potassium dinitrobenzofuroxanate, or mixtures of these explosives.
- Appropriate secondary explosives are chosen from nitrocellulose, hexanitrostilbene, nitrided aromatic compounds, and/or nitrided aromatic compounds with a polymer structure such as polynitropolyphenylether or plynitropolyphenylenes, from specific heterocycles such as nitrotriazolone, from the derivatives of tetrazoles such as aminotetrazole, ditetrazole, or diaminoguanidine azotetrazole, and from hexagene or octagene. Secondary explosives derived from urea and its derivatives can also be used.
- urea derivatives biuret guanidine, nitroguanidine, guanidine nitrate, aminoguanidine, aminoguanidine nitrate, thiourea, triaminoguanidine nitrate, aminoguanidine hydrogen carbonate, azodicarboxylic acid diamide, tetrazene, semicarbazide nitrate, as well as urethanes, ureides such as barbituric acid, and their derivatives.
- These explosives can be used alone or in a mixture.
- secondary explosives are preferred, and nitrided aromatic compounds with a polymer structure, in particular polynitropolyphenylether and the polynitropolyphenylenes or mixtures of these secondary explosives are particularly preferred.
- the igniters according to the invention also contain oxidizers and reducing agents which are common per se. Binders, processing agents, and pressing agents can also be used.
- Oxidizers that may be used can be the peroxides of alkali metals and alkaline earth metals, zinc peroxide, and the peroxodisulfates of the aforesaid elements and of ammonium, nitrates of alkali metals, and alkaline earth metals, in particular lithium, sodium, potassium, or strontium nitrate, as well as ammonium nitrate, oxohalogen compounds of alkali metals or alkaline earth metals or of ammonium, and particularly preferably potassium perchlorate or ammonium perchlorate.
- Sulfur is also suitable as an oxidizer. These oxidizers can be used alone or in a mixture.
- the reducing agents used according to the invention are metals such as titanium, zirconium, aluminum, magnesium, and cerium in the finely powdered form. Alloys of these metals as well such as titanium/aluminum or cerium/magnesium can be used according to the invention. Other reducing agents are carbon or boron. These reducing agents can be used alone or in a mixture.
- binders Compounds from the group of polyesters or polyurethanes can be used as binders.
- Processing agents and pressing agents can be substances which for example improve flowability such as Aerosil or substances which impede dust formation and improve slip or meterability, such as graphite or boron nitride.
- the ignition mixtures according to the invention can also be dyed or reacted with dye pigments.
- Heat stability can also be improved if necessary by adding stabilizers.
- Substances used to stabilize nitrocellulose can for example be used for this purpose.
- combustion moderates that affect the rate of combustion can be added to the ignition mixtures according to the invention.
- Moderators that participate in the reaction in the form of heterogenous catalysis are metals, metal oxides, and/or metal carbonates and/or metal sulfides.
- the metals that can preferably be used are boron, silicon, copper, iron, titanium, zinc, or molybdenum. Calcium carbonate can also be used. Mixtures of these moderators can also be used.
- Moderators that react in the form of homogenous catalysis are for example sulfur, copper resorcilates, or ferrocene and its derivatives. These moderators are evaporated by the temperatures produced by the reaction and can thus affect the reaction themselves or as secondary products.
- the ignition mixtures according to the invention can also be treated with protective agents or be coated.
- the ignition mixtures according to the invention have multiple potential uses. For example, they are used to ignite pyrotechnic mixtures or primers as well as propellant charges that trigger rapid processes such as acceleration of projectiles, driving in fastening materials, for example with the aid of bolt setters, or inflating air bags or triggering belt tighteners in vehicle safety.
- thermodynamic computer program for the ignition mixtures according to the invention at constant volume and a loading density of 0.1 g/cm 3 . Table 3 shows the most important data in the thermodynamic calculation. The ignition energy necessary for triggering a reaction was determined experimentally.
- the ignition mixtures according to the invention were produced by methods known of themselves.
- the individual components were sifted through a sieve with a small mesh size of 0.2 mm as shown in Table 1 and mixed in a tumble mixer for 30 minutes. 200 mg portions of these mixtures were pressed into pellets with a diameter of 6 mm with a pressing force of 71 N/mm 2 .
- the pellets so produced were ignited with a laser beam (wavelength 1,060 nm) with an energy of approximately 200 mJ and a pulse length of 2.5 ms.
- the ignition behavior is shown in Table 1.
Abstract
A firing mixture which contains explosives, oxidizing and reducing agents is characterized in that it contains one or several explosives which can be fired by laser light. Also disclosed is a process for producing the same and its use.
Description
- This is a continuation application of Seri. No. 12/750,643 filed Mar. 30, 2010, which is a divisional application of application Ser. No. 11/168,462, filed Jun. 29, 2005 (now abandoned), which is a continuation of application of Ser. No. 09/873,422, filed Jun. 5, 2001 (now abandoned), which is a continuation of application Ser. 09/639,071, filed Aug. 16, 2000 (now abandoned), which is a continuation of application Ser. No. 09/171,805, filed Oct. 14, 1999 (now abandoned), the contents of each of which are incorporated herein by reference.
- The present invention relates to ignition mixtures and manufacture and use thereof.
- Ignition mixtures and primers are used to ignite pyrotechnic mixtures or primers as well as propellant charges. The pyrotechnic mixtures or primers can represent the single charge or a booster charge or a gas-generating primer. Propellant charges and primers convert into primarily gaseous components which can be used to trigger rapid-acting processes such as acceleration of projectiles, driving in fastening materials, for example with the aid of bolt setters, or inflating air bags or triggering belt tighteners in vehicle safety. One variant is represented by the use of liquid primers instead of solid primers. These exploit the reaction of liquid fuel with oxidizers to generate gases.
- Ignition mixtures are generally triggered mechanically so that they must be sensitive to the action of friction and impact. They generally consist of initial or primary explosives such as lead trinitroresorcinate or diazodinitrophenol, reducing agents such as metal powder, or oxidizers such as barium nitrate or zinc peroxide. Sensitizers such as tetrazene or friction agents such as powdered glass, which increase the sensitivity of the initial explosive materials, are also used. For electrically ignitable systems, the rapid-reacting initial explosives are primarily used. However, the high mechanical sensitivity of the components required for perfect function is a disadvantage when handling the raw materials and mixtures. Handling requires special safety measures. Other types of ignition such as ignition by heat or by coupling high-frequency electromagnetic waves do not solve this problem or are suitable only for highly specialized and sharply limited applications.
- The goal of the present invention is to provide new ignition mixtures.
- In a first embodiment of the invention, the problem is solved by ignition mixtures that can be ignited by the laser light. The explosives contained in the ignition mixtures according to the invention can be primary or initial explosives, secondary explosives, or mixtures of these explosives. The primary or initial explosives that can be used may for example be lead trinitroresorcinate, diazodinitrophenol, tetrazene, or potassium dinitrobenzofuroxanate, or mixtures of these explosives. Appropriate secondary explosives are chosen from nitrocellulose, hexanitrostilbene, nitrided aromatic compounds, and/or nitrided aromatic compounds with a polymer structure such as polynitropolyphenylether or plynitropolyphenylenes, from specific heterocycles such as nitrotriazolone, from the derivatives of tetrazoles such as aminotetrazole, ditetrazole, or diaminoguanidine azotetrazole, and from hexagene or octagene. Secondary explosives derived from urea and its derivatives can also be used. Examples of these are the urea derivatives biuret, guanidine, nitroguanidine, guanidine nitrate, aminoguanidine, aminoguanidine nitrate, thiourea, triaminoguanidine nitrate, aminoguanidine hydrogen carbonate, azodicarboxylic acid diamide, tetrazene, semicarbazide nitrate, as well as urethanes, ureides such as barbituric acid, and their derivatives. These explosives can be used alone or in a mixture. According to the invention, secondary explosives are preferred, and nitrided aromatic compounds with a polymer structure, in particular polynitropolyphenylether and the polynitropolyphenylenes or mixtures of these secondary explosives are particularly preferred.
- In addition to the explosives, the igniters according to the invention also contain oxidizers and reducing agents which are common per se. Binders, processing agents, and pressing agents can also be used.
- Oxidizers that may be used can be the peroxides of alkali metals and alkaline earth metals, zinc peroxide, and the peroxodisulfates of the aforesaid elements and of ammonium, nitrates of alkali metals, and alkaline earth metals, in particular lithium, sodium, potassium, or strontium nitrate, as well as ammonium nitrate, oxohalogen compounds of alkali metals or alkaline earth metals or of ammonium, and particularly preferably potassium perchlorate or ammonium perchlorate. Sulfur is also suitable as an oxidizer. These oxidizers can be used alone or in a mixture.
- The reducing agents used according to the invention are metals such as titanium, zirconium, aluminum, magnesium, and cerium in the finely powdered form. Alloys of these metals as well such as titanium/aluminum or cerium/magnesium can be used according to the invention. Other reducing agents are carbon or boron. These reducing agents can be used alone or in a mixture.
- Compounds from the group of polyesters or polyurethanes can be used as binders. Compounds with binding properties that contribute to the heat of explosion and/or the oxygen balance, for example nitrocellulose or polynitropolyphenylene, can also be used as binders.
- Processing agents and pressing agents can be substances which for example improve flowability such as Aerosil or substances which impede dust formation and improve slip or meterability, such as graphite or boron nitride.
- For improved absorption of laser light, the ignition mixtures according to the invention can also be dyed or reacted with dye pigments. Heat stability can also be improved if necessary by adding stabilizers. Substances used to stabilize nitrocellulose can for example be used for this purpose.
- In addition, combustion moderates that affect the rate of combustion can be added to the ignition mixtures according to the invention.
- Substances or mixtures thereof able to affect combustion and combustion rate by heterogenous or homogenous catalysis are used as combustion moderates. Moderator that participate in the reaction in the form of heterogenous catalysis are metals, metal oxides, and/or metal carbonates and/or metal sulfides. The metals that can preferably be used are boron, silicon, copper, iron, titanium, zinc, or molybdenum. Calcium carbonate can also be used. Mixtures of these moderators can also be used.
- Moderators that react in the form of homogenous catalysis are for example sulfur, copper resorcilates, or ferrocene and its derivatives. These moderators are evaporated by the temperatures produced by the reaction and can thus affect the reaction themselves or as secondary products.
- For protection against environmental influences, the ignition mixtures according to the invention can also be treated with protective agents or be coated.
- The ignition mixtures according to the invention have multiple potential uses. For example, they are used to ignite pyrotechnic mixtures or primers as well as propellant charges that trigger rapid processes such as acceleration of projectiles, driving in fastening materials, for example with the aid of bolt setters, or inflating air bags or triggering belt tighteners in vehicle safety.
- The safety data on some of the ignition mixtures according to the invention are provided in Table 2. The data were derived by the methods of the Bundesanstalt für Materialprüfung [Federal Institute for Materials Testing]. By comparison to the primary explosive lead nitroresorcinate, sensitivity to friction and impact are significantly improved with the igniting agents according to the invention.
- In estimating important parameters of the ignition mixtures according to the invention such as the energy released by the reaction (heat of explosion), pressure, explosion temperature, and reaction products produced at this temperature, an adiabatic reaction was calculated with a thermodynamic computer program for the ignition mixtures according to the invention at constant volume and a loading density of 0.1 g/cm3. Table 3 shows the most important data in the thermodynamic calculation. The ignition energy necessary for triggering a reaction was determined experimentally.
- The examples below are intended to illustrate the invention without restricting it.
- The ignition mixtures according to the invention were produced by methods known of themselves. The individual components were sifted through a sieve with a small mesh size of 0.2 mm as shown in Table 1 and mixed in a tumble mixer for 30 minutes. 200 mg portions of these mixtures were pressed into pellets with a diameter of 6 mm with a pressing force of 71 N/mm2. The pellets so produced were ignited with a laser beam (wavelength 1,060 nm) with an energy of approximately 200 mJ and a pulse length of 2.5 ms. The ignition behavior is shown in Table 1.
-
TABLE 1 Examples Components 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 KNO3 52.5 52.5 33.3 32.3 33.3 40 40 B 18.8 18.8 2.9 29 10 10 binder 3.7 3.7 NPE 25 45 44.7 44.5 44.1 66.7 64.8 66.7 64.8 25 50 PNP 25 100 66.7 50 25 ZnO2 50 49.8 49.8 49 33.3 32.3 Ti 5 4.9 4.9 4.9 graphite 0.5 1 2 black powder 75 75 ignition behavior +++ + + + + + + ++ + + + +++ +++ + + +++ + = ignition ++ = good ignition +++ = very good ignition Components Used: KNO3 potassium nitrate <200 μm B amorphous boron Ti titanium metal powder <40 μm binder polyurethane NPE polynitropolyphenylether PNP polynitropolyphenylene ZnO2 zinc peroxide, mean grain size 6.5μ, oxygen content 13.5% -
TABLE 2 Condensate Ignition Pressure T Ex. Heat Percentage Energy Specimen (atm) (K) (cal/g) (%/mol) (mJ) NPE 1109 2932 686 0 ≈10 NPE/KNO3 907.4 3073.5 672 7.5 160 66.7/33.3 NPE/ZnO2Ti 1198 4146 978 14.6 ≈200 45/50/5 black powder/ 430 2290 −179 11.6 ≈200 NPE 75/25 AZM O 622 3265 615 52 ≈200 9531/NPE 75/25 NPE/KNO3/B 843 3374 673 29 ≈90 50/40/10 NPE/ZnO2 1341 4044 1016 7 >200 66.7/33.3 NPE/ZnO2/B 1194 3731 991 14 >200 64.8/32.3/2.9 NPE/KNO3/B 1002 3382 752 2 ≈100 64.8/32.3/2.9 NC/KNO3 872 3282 883 11 no 66.7/33.3 ignition lead 683 3639 550 10 ≈5 trinitroresorcinate -
TABLE 3 Impact Detonation Friction Sensitivity Sensitivity Point Explosive (N) (J) (° C.) lead trinitroresorcinate 2 ≦0.025 280 AZM O 2956 ≧360 5 >400 AZM O 9531 ≧360 4 >400 black powder ≧360 5 >400 HITP ≧360 15-50 >400 (aminotetrazole base) NPE ≧360 7.5 >260 NPE/ZnO2/Ti ≧360 15 230 NPE/ZnO2 240 20 235 NPE/KNO3 + 3% B 160 4 decomposition starting at 230 PNP/KNO3 ≧360 10 293 PNP/KNO3/B ≧360 10 293
Claims (14)
1. An igniter agent comprising at least one oxidizing agent, at least one reducing agent and polynitropolyphenyl ether or polynitropolyphenylene or mixtures of polynitropolyphenyl ether and polynitropolyphenylene, wherein the igniter agent can be ignited by laser light.
2. The igniter agent according to claim 1 , further comprising binders, combustion moderators, processing agents and/or compaction aids.
3. The igniter agent according to claim 1 , wherein the at least one oxidizing agent is selected from the group consisting of sulfur, peroxides of alkali or alkaline earth metals, zinc peroxide, peroxodisulfates of the aforementioned substances and of ammonium, nitrates of alkali and alkaline earth metals, oxohalogen compounds of alkali or alkaline earth metals or ammonium, and mixtures of the aforementioned substances.
4. The igniter agent according to claim 1 , wherein the at least one reducing agent is a metal selected from the group consisting of titanium, zirconium, aluminum, magnesium or cerium, a mixture of these metals, an alloy of these metals, carbon, boron, and a mixture of the aforementioned agents.
5. The igniter agent according to claim 1 , wherein the igniter agent is pigmented or coloring pigments are added thereto.
6. The igniter agent according to claim 1 , further comprising a combustion moderator capable, by heterogeneous or homogeneous catalysis, of influencing the combustion and its rate.
7. The igniter agent according to claim 1 , wherein the at least one oxidizing agent is lithium, sodium, potassium, strontium or ammonium nitrate or mixtures thereof.
8. The igniter agent according to claim 1 , wherein the at least one oxidizing agent is potassium perchlorate or ammonium perchlorate or mixtures thereof.
9. The igniter agent according to claim 1 , wherein the igniter agent includes polynitrophenylether, the at least one oxidizing agent is potassium nitrate, the at least one reducing agent is boron, and the igniter agent includes a binder comprising polyurethane.
10. A process for production of the igniter agent according to claim 1 , comprising mixing the individual components and then compacting the mixed components.
11. A method for igniting an ignition mixture, comprising igniting an ignition mixture with laser light, the ignition mixture comprising at least one oxidizing agent, at least one reducing agent and polynitropolyphenyl ether or polynitropolyphenylene or mixtures of polynitropolyphenyl ether and polynitropolyphenylene.
12. The method according to claim 11 , wherein the at least one oxidizing agent is selected from the group consisting of sulfur, peroxides of alkali or alkaline earth metals, zinc peroxide, peroxodisulfates of the aforementioned substances and of ammonium, nitrates of alkali and alkaline earth metals, oxohalogen compounds of alkali or alkaline earth metals or ammonium, and mixtures of the aforementioned substances.
13. The method according to claim 11 , wherein the at least one reducing agent is a metal selected from the group consisting of titanium, zirconium, aluminum, magnesium or cerium, a mixture of these metals, an alloy of these metals, carbon, boron, and a mixture of the aforementioned agents.
14. The method according to claim 11 , wherein the igniter agent includes polynitrophenylether, the at least one oxidizing agent is potassium nitrate, the at least one reducing agent is boron, and the igniter agent includes a binder comprising polyurethane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/963,794 US20110162547A1 (en) | 1996-04-26 | 2010-12-09 | Ignition mixtures |
Applications Claiming Priority (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19616627.6 | 1996-04-26 | ||
DE19616627A DE19616627A1 (en) | 1996-04-26 | 1996-04-26 | Kindling mixtures |
US17180599A | 1999-10-14 | 1999-10-14 | |
US63907100A | 2000-08-16 | 2000-08-16 | |
US09/873,422 US20010054462A1 (en) | 1996-04-26 | 2001-06-05 | Ignition Mixtures |
US11/168,462 US20070017612A1 (en) | 1996-04-26 | 2005-06-29 | Ignition mixtures |
US12/750,643 US20100180787A1 (en) | 1996-04-26 | 2010-03-30 | Ignition mixtures |
US12/963,794 US20110162547A1 (en) | 1996-04-26 | 2010-12-09 | Ignition mixtures |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/750,643 Continuation US20100180787A1 (en) | 1996-04-26 | 2010-03-30 | Ignition mixtures |
Publications (1)
Publication Number | Publication Date |
---|---|
US20110162547A1 true US20110162547A1 (en) | 2011-07-07 |
Family
ID=7792474
Family Applications (4)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/873,422 Abandoned US20010054462A1 (en) | 1996-04-26 | 2001-06-05 | Ignition Mixtures |
US11/168,462 Abandoned US20070017612A1 (en) | 1996-04-26 | 2005-06-29 | Ignition mixtures |
US12/750,643 Abandoned US20100180787A1 (en) | 1996-04-26 | 2010-03-30 | Ignition mixtures |
US12/963,794 Abandoned US20110162547A1 (en) | 1996-04-26 | 2010-12-09 | Ignition mixtures |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/873,422 Abandoned US20010054462A1 (en) | 1996-04-26 | 2001-06-05 | Ignition Mixtures |
US11/168,462 Abandoned US20070017612A1 (en) | 1996-04-26 | 2005-06-29 | Ignition mixtures |
US12/750,643 Abandoned US20100180787A1 (en) | 1996-04-26 | 2010-03-30 | Ignition mixtures |
Country Status (6)
Country | Link |
---|---|
US (4) | US20010054462A1 (en) |
EP (1) | EP0894235B1 (en) |
AT (1) | ATE304156T1 (en) |
DE (2) | DE19616627A1 (en) |
ES (1) | ES2249799T3 (en) |
WO (1) | WO1997041403A1 (en) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19805976C1 (en) * | 1998-02-13 | 1999-04-29 | Nigu Chemie Gmbh | Pre-ignition powder for thermal safety device for car air-bags |
DE19912622A1 (en) * | 1998-03-20 | 1999-09-23 | Dynamit Nobel Ag | Electrically ignited initiating explosive for igniting boosters or propellant charges or for generating compressed gas |
US6165296A (en) * | 1999-02-02 | 2000-12-26 | Autoliv Development As | Gas generant igniter composition and method |
US6132480A (en) * | 1999-04-22 | 2000-10-17 | Autoliv Asp, Inc. | Gas forming igniter composition for a gas generant |
ATA75099A (en) * | 1999-04-28 | 2001-03-15 | Hirtenberger Ag | IGNITION BLOCK |
DE10058705C1 (en) * | 2000-11-25 | 2002-02-28 | Rheinmetall W & M Gmbh | Pourable bursting charge consisting of crystalline explosive embedded in a polymer matrix, containing finely divided metal powder, e.g. vanadium, as solid lubricant to provide low viscosity at high solids content |
WO2003000624A2 (en) * | 2001-05-10 | 2003-01-03 | Dynamit Nobel Gmbh Explosivstoff- Und Systemtechnik | Igniting agents |
AT410315B (en) * | 2001-11-14 | 2003-03-25 | Josef Koehler | Low signature pyrotechnic product, used as electrically-ignitable bullet-hit for special effects or in cable cutter, pelican hook, glass breaker or trunnion gun, contains atoxic metal diazinate, passivator and nitro compounds |
KR100561952B1 (en) * | 2002-09-13 | 2006-03-21 | 주식회사 한화 | Slight-shock blasting composition |
US20040089383A1 (en) * | 2003-02-06 | 2004-05-13 | Mendenhall Ivan V. | Gas generant igniter coating materials and methods |
DE102004001980A1 (en) * | 2003-01-14 | 2004-07-22 | Ruag Ammotec Gmbh | Propellant charge useful in weapons training systems comprises a soft friction material |
ES2370395T3 (en) | 2003-05-21 | 2011-12-15 | Alexza Pharmaceuticals, Inc. | USE OF A SOLID FUEL LAYER, MANUFACTURING PROCEDURE AND CORRESPONDING HEATING UNIT. |
US7402777B2 (en) | 2004-05-20 | 2008-07-22 | Alexza Pharmaceuticals, Inc. | Stable initiator compositions and igniters |
FR2897864B1 (en) * | 2006-02-24 | 2008-04-11 | Cheddite France Sa | PRIMING COMPOSITION AND APPLICATIONS |
US8540828B2 (en) * | 2008-08-19 | 2013-09-24 | Alliant Techsystems Inc. | Nontoxic, noncorrosive phosphorus-based primer compositions and an ordnance element including the same |
US8641842B2 (en) | 2011-08-31 | 2014-02-04 | Alliant Techsystems Inc. | Propellant compositions including stabilized red phosphorus, a method of forming same, and an ordnance element including the same |
US20130333815A1 (en) * | 2012-06-13 | 2013-12-19 | Alliant Techsystems Inc. | Non-lethal payloads and methods of producing same |
CA2743063C (en) | 2008-11-07 | 2018-01-16 | Ruag Ammotec Gmbh | Ignition sets with improved ignition performance |
US8465606B1 (en) * | 2009-01-16 | 2013-06-18 | The United States Of America As Represented By The Secretary Of The Army | Composition of matter for an incendiary device and method of manufacture |
DE102011108146B4 (en) * | 2011-07-20 | 2014-03-20 | Diehl Bgt Defence Gmbh & Co. Kg | Use of a salt of bistetrazolylamine and detonator |
RU2522611C2 (en) * | 2012-10-18 | 2014-07-20 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" | Light sensitive explosive composition |
KR101740620B1 (en) * | 2015-02-27 | 2017-05-26 | 부산대학교 산학협력단 | Nano Energetic Material Composites with Explosion via Optical Ignition and Method for fabricating the same |
EP3523266A4 (en) * | 2016-10-05 | 2020-06-10 | Olin Corporation | Pyrotechnic compositions |
US10460941B2 (en) * | 2016-11-08 | 2019-10-29 | Varian Semiconductor Equipment Associates, Inc. | Plasma doping using a solid dopant source |
RU2637016C1 (en) * | 2017-03-20 | 2017-11-29 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Method for manufacturing heat-resistant light-sensitive explosive compositions and light detonator on their basis |
RU2729490C1 (en) * | 2019-06-14 | 2020-08-07 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Initiating composition and method for production thereof |
Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519505A (en) * | 1967-03-01 | 1970-07-07 | Space Ordnance Systems Inc | Ignition material containing tellurium dioxide,boron and fluoropolymeric binder |
US3618521A (en) * | 1969-07-07 | 1971-11-09 | Us Navy | Propellant gas generator |
US3682727A (en) * | 1968-08-05 | 1972-08-08 | Dynamit Nobel Ag | Igniter charge for propellant compositions and rocket propellant charges |
US3876478A (en) * | 1972-12-18 | 1975-04-08 | Us Navy | Light sensitive explosive mixture |
US4363679A (en) * | 1979-12-22 | 1982-12-14 | Dynamit Nobel Aktiengesellschaft | Use of zinc peroxide as oxidant for explosives and pyrotechnical mixtures |
US4620046A (en) * | 1983-03-21 | 1986-10-28 | Dynamit Nobel Aktiengesellschaft | Nitrated aryl ethers |
US4656029A (en) * | 1984-04-17 | 1987-04-07 | L'oreal | Cosmetic composition containing aloesin as an agent for protection against sunlight and its use for skin and hair protection |
US4861924A (en) * | 1988-08-25 | 1989-08-29 | Jet Research Center, Inc. | 1,3,5-trinitro-2,4,6-tripicrylbenzene |
US4870903A (en) * | 1987-05-20 | 1989-10-03 | Aerospatiale Societe Nationale Industrielle | Photopyrotechnical detonation device and photopyrotechnical chain using this device |
US4892037A (en) * | 1989-01-03 | 1990-01-09 | The United States Of America As Represented By The Secretary Of The Army | Self consumable initiator |
US4956029A (en) * | 1987-03-11 | 1990-09-11 | Dynamit Nobel Aktiengesellschaft | Electrically primable igniter charges for caseless ammunition and propellant cartridges |
US5099761A (en) * | 1991-01-28 | 1992-03-31 | The United States Of America As Represented By The Secretary Of The Army | Laser actuated thru-bulkhead initiator |
US5179247A (en) * | 1991-07-15 | 1993-01-12 | Ensign-Bickford Aerospace Corporation | Optically initiated detonator |
US5212343A (en) * | 1990-08-27 | 1993-05-18 | Martin Marietta Corporation | Water reactive method with delayed explosion |
US5406889A (en) * | 1993-09-03 | 1995-04-18 | Morton International, Inc. | Direct laser ignition of ignition products |
US5472529A (en) * | 1991-06-26 | 1995-12-05 | Asahi Kasei Kogyo Kabushiki Kaisha | Explosive composition and method for producing the same |
US5538569A (en) * | 1994-08-27 | 1996-07-23 | Eley Limited | Primer compositions containing dinitrobenzofuroxan compounds |
US5552257A (en) * | 1994-01-21 | 1996-09-03 | Minnesota Mining And Manufacturing Company | Thermal decomposition of azide-containing materials |
US5625165A (en) * | 1992-02-24 | 1997-04-29 | Wight; Charles A. | Desensitized energetic materials |
US5747723A (en) * | 1996-11-26 | 1998-05-05 | The United States Of America As Represented By The Secretary Of The Army | Modular artillery charge system |
US6080248A (en) * | 1998-02-10 | 2000-06-27 | Snpe | Non-detonatable pyrotechnic materials for microsystems |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2543971C2 (en) * | 1975-10-02 | 1986-05-22 | Dynamit Nobel Ag, 5210 Troisdorf | Ignition system for high temperature resistant propellants |
DE2752166C2 (en) * | 1977-11-23 | 1986-10-23 | Dynamit Nobel Ag, 5210 Troisdorf | Polynitro aromatic polymers |
SE462092B (en) * | 1988-10-17 | 1990-05-07 | Nitro Nobel Ab | INITIATIVE ELEMENT FOR PRIMARY EXTENSION FREE EXPLOSION CAPS |
JP2956913B2 (en) * | 1991-05-15 | 1999-10-04 | 株式会社アドバンテスト | IC test equipment |
DE4302476C2 (en) * | 1993-01-29 | 1995-12-07 | Dynamit Nobel Ag | Ignition-sensitive electrical detonators with a weak detonative output, process for their production and their use |
-
1996
- 1996-04-26 DE DE19616627A patent/DE19616627A1/en not_active Ceased
-
1997
- 1997-04-24 WO PCT/EP1997/002104 patent/WO1997041403A1/en active IP Right Grant
- 1997-04-24 DE DE59712416T patent/DE59712416D1/en not_active Expired - Lifetime
- 1997-04-24 EP EP97921748A patent/EP0894235B1/en not_active Expired - Lifetime
- 1997-04-24 AT AT97921748T patent/ATE304156T1/en active
- 1997-04-24 ES ES97921748T patent/ES2249799T3/en not_active Expired - Lifetime
-
2001
- 2001-06-05 US US09/873,422 patent/US20010054462A1/en not_active Abandoned
-
2005
- 2005-06-29 US US11/168,462 patent/US20070017612A1/en not_active Abandoned
-
2010
- 2010-03-30 US US12/750,643 patent/US20100180787A1/en not_active Abandoned
- 2010-12-09 US US12/963,794 patent/US20110162547A1/en not_active Abandoned
Patent Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519505A (en) * | 1967-03-01 | 1970-07-07 | Space Ordnance Systems Inc | Ignition material containing tellurium dioxide,boron and fluoropolymeric binder |
US3682727A (en) * | 1968-08-05 | 1972-08-08 | Dynamit Nobel Ag | Igniter charge for propellant compositions and rocket propellant charges |
US3618521A (en) * | 1969-07-07 | 1971-11-09 | Us Navy | Propellant gas generator |
US3876478A (en) * | 1972-12-18 | 1975-04-08 | Us Navy | Light sensitive explosive mixture |
US4363679A (en) * | 1979-12-22 | 1982-12-14 | Dynamit Nobel Aktiengesellschaft | Use of zinc peroxide as oxidant for explosives and pyrotechnical mixtures |
US4620046A (en) * | 1983-03-21 | 1986-10-28 | Dynamit Nobel Aktiengesellschaft | Nitrated aryl ethers |
US4656029A (en) * | 1984-04-17 | 1987-04-07 | L'oreal | Cosmetic composition containing aloesin as an agent for protection against sunlight and its use for skin and hair protection |
US4956029A (en) * | 1987-03-11 | 1990-09-11 | Dynamit Nobel Aktiengesellschaft | Electrically primable igniter charges for caseless ammunition and propellant cartridges |
US4870903A (en) * | 1987-05-20 | 1989-10-03 | Aerospatiale Societe Nationale Industrielle | Photopyrotechnical detonation device and photopyrotechnical chain using this device |
US4861924A (en) * | 1988-08-25 | 1989-08-29 | Jet Research Center, Inc. | 1,3,5-trinitro-2,4,6-tripicrylbenzene |
US4892037A (en) * | 1989-01-03 | 1990-01-09 | The United States Of America As Represented By The Secretary Of The Army | Self consumable initiator |
US5212343A (en) * | 1990-08-27 | 1993-05-18 | Martin Marietta Corporation | Water reactive method with delayed explosion |
US5099761A (en) * | 1991-01-28 | 1992-03-31 | The United States Of America As Represented By The Secretary Of The Army | Laser actuated thru-bulkhead initiator |
US5472529A (en) * | 1991-06-26 | 1995-12-05 | Asahi Kasei Kogyo Kabushiki Kaisha | Explosive composition and method for producing the same |
US5179247A (en) * | 1991-07-15 | 1993-01-12 | Ensign-Bickford Aerospace Corporation | Optically initiated detonator |
US5625165A (en) * | 1992-02-24 | 1997-04-29 | Wight; Charles A. | Desensitized energetic materials |
US5406889A (en) * | 1993-09-03 | 1995-04-18 | Morton International, Inc. | Direct laser ignition of ignition products |
US5552257A (en) * | 1994-01-21 | 1996-09-03 | Minnesota Mining And Manufacturing Company | Thermal decomposition of azide-containing materials |
US5538569A (en) * | 1994-08-27 | 1996-07-23 | Eley Limited | Primer compositions containing dinitrobenzofuroxan compounds |
US5747723A (en) * | 1996-11-26 | 1998-05-05 | The United States Of America As Represented By The Secretary Of The Army | Modular artillery charge system |
US6080248A (en) * | 1998-02-10 | 2000-06-27 | Snpe | Non-detonatable pyrotechnic materials for microsystems |
Also Published As
Publication number | Publication date |
---|---|
EP0894235A1 (en) | 1999-02-03 |
DE19616627A1 (en) | 1997-11-06 |
WO1997041403A1 (en) | 1997-11-06 |
EP0894235B1 (en) | 2005-09-07 |
DE59712416D1 (en) | 2005-10-13 |
ES2249799T3 (en) | 2006-04-01 |
US20070017612A1 (en) | 2007-01-25 |
US20100180787A1 (en) | 2010-07-22 |
US20010054462A1 (en) | 2001-12-27 |
ATE304156T1 (en) | 2005-09-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20110162547A1 (en) | Ignition mixtures | |
US6997998B2 (en) | Lead-and barium-free propellant charges | |
US5861571A (en) | Gas-generative composition consisting essentially of ammonium perchlorate plus a chlorine scavenger and an organic fuel | |
US5380380A (en) | Ignition compositions for inflator gas generators | |
EP0737174B1 (en) | Lead-free priming mixture for percussion primer | |
US6749702B1 (en) | Low temperature autoignition composition | |
CA2135977C (en) | Gas generant compositions | |
US5936195A (en) | Gas generating composition with exploded aluminum powder | |
US6221187B1 (en) | Method of safely initiating combustion of a gas generant composition using an autoignition composition | |
US6007647A (en) | Autoignition compositions for inflator gas generators | |
US20010042577A1 (en) | Temperature fuse | |
US20010001970A1 (en) | Lead- and barium-free propellant charges | |
CA2253196C (en) | Firing mixtures | |
CN100455553C (en) | Thermally initiatable ignition mixture | |
US6645326B2 (en) | Low temperature autoignition material | |
EP0944562B1 (en) | Autoignition compositions for inflator gas generators | |
DE19616628A1 (en) | Ignition mixture used for igniting pyrotechnical mixtures | |
RU2157357C1 (en) | Pellet causing no corrosion | |
Eneh | CHEMICAL EXPLOSIVES: WARHEAD ALLY |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |