EP2951137B1 - Poudre pour accélérer des projectiles pour mortiers - Google Patents
Poudre pour accélérer des projectiles pour mortiers Download PDFInfo
- Publication number
- EP2951137B1 EP2951137B1 EP13704344.4A EP13704344A EP2951137B1 EP 2951137 B1 EP2951137 B1 EP 2951137B1 EP 13704344 A EP13704344 A EP 13704344A EP 2951137 B1 EP2951137 B1 EP 2951137B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- powder
- grain
- weight
- crystalline
- green grain
- 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.)
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- 239000000843 powder Substances 0.000 title claims description 147
- 239000004570 mortar (masonry) Substances 0.000 title claims description 30
- 239000000654 additive Substances 0.000 claims description 36
- 230000000996 additive effect Effects 0.000 claims description 27
- DSSYKIVIOFKYAU-XCBNKYQSSA-N (R)-camphor Chemical group C1C[C@@]2(C)C(=O)C[C@@H]1C2(C)C DSSYKIVIOFKYAU-XCBNKYQSSA-N 0.000 claims description 24
- 241000723346 Cinnamomum camphora Species 0.000 claims description 24
- 229960000846 camphor Drugs 0.000 claims description 24
- 229930008380 camphor Natural products 0.000 claims description 24
- 239000000020 Nitrocellulose Substances 0.000 claims description 22
- 229920001220 nitrocellulos Polymers 0.000 claims description 22
- BSPUVYFGURDFHE-UHFFFAOYSA-N Nitramine Natural products CC1C(O)CCC2CCCNC12 BSPUVYFGURDFHE-UHFFFAOYSA-N 0.000 claims description 18
- POCJOGNVFHPZNS-UHFFFAOYSA-N isonitramine Natural products OC1CCCCC11CNCCC1 POCJOGNVFHPZNS-UHFFFAOYSA-N 0.000 claims description 18
- POCJOGNVFHPZNS-ZJUUUORDSA-N (6S,7R)-2-azaspiro[5.5]undecan-7-ol Chemical compound O[C@@H]1CCCC[C@]11CNCCC1 POCJOGNVFHPZNS-ZJUUUORDSA-N 0.000 claims description 16
- 239000002904 solvent Substances 0.000 claims description 15
- 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 claims description 11
- 150000001875 compounds Chemical class 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 8
- 239000000028 HMX Substances 0.000 claims description 6
- UZGLIIJVICEWHF-UHFFFAOYSA-N octogen Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)CN([N+]([O-])=O)C1 UZGLIIJVICEWHF-UHFFFAOYSA-N 0.000 claims description 6
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 5
- 239000004323 potassium nitrate Substances 0.000 claims description 3
- 235000010333 potassium nitrate Nutrition 0.000 claims description 3
- 238000001035 drying Methods 0.000 claims description 2
- 238000001125 extrusion Methods 0.000 claims description 2
- OTYBMLCTZGSZBG-UHFFFAOYSA-L potassium sulfate Chemical compound [K+].[K+].[O-]S([O-])(=O)=O OTYBMLCTZGSZBG-UHFFFAOYSA-L 0.000 claims description 2
- 229910052939 potassium sulfate Inorganic materials 0.000 claims description 2
- 235000011151 potassium sulphates Nutrition 0.000 claims description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 26
- 239000007789 gas Substances 0.000 description 20
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 13
- 229910002804 graphite Inorganic materials 0.000 description 13
- 239000010439 graphite Substances 0.000 description 13
- 239000011159 matrix material Substances 0.000 description 12
- 239000000126 substance Substances 0.000 description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- 230000008859 change Effects 0.000 description 7
- -1 nitramine compound Chemical class 0.000 description 7
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 6
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 6
- 238000007605 air drying Methods 0.000 description 6
- 239000013078 crystal Substances 0.000 description 6
- 229960003711 glyceryl trinitrate Drugs 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 5
- 238000007707 calorimetry Methods 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 238000004200 deflagration Methods 0.000 description 5
- 238000011161 development Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- 238000005498 polishing Methods 0.000 description 5
- 238000004381 surface treatment Methods 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- QJTIRVUEVSKJTK-UHFFFAOYSA-N 5-nitro-1,2-dihydro-1,2,4-triazol-3-one Chemical compound [O-][N+](=O)C1=NC(=O)NN1 QJTIRVUEVSKJTK-UHFFFAOYSA-N 0.000 description 3
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 3
- AGUIVNYEYSCPNI-UHFFFAOYSA-N N-methyl-N-picrylnitramine Chemical group [O-][N+](=O)N(C)C1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O AGUIVNYEYSCPNI-UHFFFAOYSA-N 0.000 description 3
- 239000000006 Nitroglycerin Substances 0.000 description 3
- UIIMBOGNXHQVGW-UHFFFAOYSA-M Sodium bicarbonate Chemical compound [Na+].OC([O-])=O UIIMBOGNXHQVGW-UHFFFAOYSA-M 0.000 description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 3
- 239000002585 base Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- JKQOBWVOAYFWKG-UHFFFAOYSA-N molybdenum trioxide Chemical compound O=[Mo](=O)=O JKQOBWVOAYFWKG-UHFFFAOYSA-N 0.000 description 3
- 239000003380 propellant Substances 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- ZNOKGRXACCSDPY-UHFFFAOYSA-N tungsten trioxide Chemical compound O=[W](=O)=O ZNOKGRXACCSDPY-UHFFFAOYSA-N 0.000 description 3
- ADCBKYIHQQCFHE-UHFFFAOYSA-N 1,3-dimethyl-1,3-diphenylurea Chemical compound C=1C=CC=CC=1N(C)C(=O)N(C)C1=CC=CC=C1 ADCBKYIHQQCFHE-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 229910000019 calcium carbonate Inorganic materials 0.000 description 2
- 239000000969 carrier Substances 0.000 description 2
- 229920002678 cellulose Polymers 0.000 description 2
- 239000001913 cellulose Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- AMWRITDGCCNYAT-UHFFFAOYSA-L hydroxy(oxo)manganese;manganese Chemical compound [Mn].O[Mn]=O.O[Mn]=O AMWRITDGCCNYAT-UHFFFAOYSA-L 0.000 description 2
- 238000004898 kneading Methods 0.000 description 2
- 239000000395 magnesium oxide Substances 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 2
- 239000004014 plasticizer Substances 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- JDFUJAMTCCQARF-UHFFFAOYSA-N tatb Chemical compound NC1=C([N+]([O-])=O)C(N)=C([N+]([O-])=O)C(N)=C1[N+]([O-])=O JDFUJAMTCCQARF-UHFFFAOYSA-N 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- IDCPFAYURAQKDZ-UHFFFAOYSA-N 1-nitroguanidine Chemical compound NC(=N)N[N+]([O-])=O IDCPFAYURAQKDZ-UHFFFAOYSA-N 0.000 description 1
- RUKISNQKOIKZGT-UHFFFAOYSA-N 2-nitrodiphenylamine Chemical compound [O-][N+](=O)C1=CC=CC=C1NC1=CC=CC=C1 RUKISNQKOIKZGT-UHFFFAOYSA-N 0.000 description 1
- IMFYAZJNDOZIFV-UHFFFAOYSA-N 3-methyl-1,1-diphenylurea Chemical compound C=1C=CC=CC=1N(C(=O)NC)C1=CC=CC=C1 IMFYAZJNDOZIFV-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
- 241000273930 Brevoortia tyrannus Species 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910002651 NO3 Inorganic materials 0.000 description 1
- 235000011941 Tilia x europaea Nutrition 0.000 description 1
- 239000004480 active ingredient Substances 0.000 description 1
- 150000001278 adipic acid derivatives Chemical class 0.000 description 1
- 150000001447 alkali salts Chemical class 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005844 autocatalytic reaction Methods 0.000 description 1
- 238000003287 bathing Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- KRKNYBCHXYNGOX-UHFFFAOYSA-N citric acid Chemical class OC(=O)CC(O)(C(O)=O)CC(O)=O KRKNYBCHXYNGOX-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000005087 graphitization Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 230000001535 kindling effect Effects 0.000 description 1
- 239000004571 lime Substances 0.000 description 1
- HCWCAKKEBCNQJP-UHFFFAOYSA-N magnesium orthosilicate Chemical compound [Mg+2].[Mg+2].[O-][Si]([O-])([O-])[O-] HCWCAKKEBCNQJP-UHFFFAOYSA-N 0.000 description 1
- 239000000391 magnesium silicate Substances 0.000 description 1
- 229910052919 magnesium silicate Inorganic materials 0.000 description 1
- 235000019792 magnesium silicate Nutrition 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 238000006396 nitration reaction Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 150000003021 phthalic acid derivatives Chemical class 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000001120 potassium sulphate Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007873 sieving Methods 0.000 description 1
- 229910000030 sodium bicarbonate Inorganic materials 0.000 description 1
- 235000017557 sodium bicarbonate Nutrition 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000011877 solvent mixture Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- LENZDBCJOHFCAS-UHFFFAOYSA-N tris Chemical compound OCC(N)(CO)CO LENZDBCJOHFCAS-UHFFFAOYSA-N 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/04—Compositions characterised by non-explosive or non-thermic constituents for cooling the explosion gases including antifouling and flash suppressing agents
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/18—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/34—Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
- C06B31/02—Compositions containing an inorganic nitrogen-oxygen salt the salt being an alkali metal or an alkaline earth metal nitrate
- C06B31/12—Compositions containing an inorganic nitrogen-oxygen salt the salt being an alkali metal or an alkaline earth metal nitrate with a nitrated organic compound
- C06B31/22—Compositions containing an inorganic nitrogen-oxygen salt the salt being an alkali metal or an alkaline earth metal nitrate with a nitrated organic compound the compound being nitrocellulose
- C06B31/24—Compositions containing an inorganic nitrogen-oxygen salt the salt being an alkali metal or an alkaline earth metal nitrate with a nitrated organic compound the compound being nitrocellulose with other explosive or thermic component
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
Definitions
- the invention relates to a powder as drive powder or igniter powder for accelerating projectiles for mortar systems, which is based on nitrocellulose and contains a crystalline energy carrier based on nitramine in 1-30% by weight and an inorganic flash hider, the powder being in the form of grains , and the grains optionally have an inert plasticizing additive on their surface.
- the invention also relates to a method for producing such a powder.
- the WO 2011/153655 A2 discloses a drive system for projectiles which does not contain nitroglycerine and is suitable for small-caliber and mortar projectiles.
- the composition of the grain consists of nitrocellulose, a nitramine-based energy carrier and one or more inert plasticizers, which preferably have an increased concentration in an area near the surface.
- the EP 1 857 429 A1 (Nitrochemie Wimmis AG) describes a drive for accelerating projectiles, which is based on nitrocellulose.
- the drive comprises nitrocellulose as a base, a crystalline energy carrier based on nitramine in an amount of 1 - 25% by weight and at least two inert plasticizing additives, one of the additives being homogeneously distributed in the matrix of the drive and the second additive in one near the surface has an increased concentration.
- This composition results in a drive with a high degree of energy conversion, the drive preferably being in the form of grains.
- the object of the invention is to create a powder belonging to the technical field mentioned above as a drive powder or ignition powder for accelerating projectiles for mortar systems, which has excellent chemical and ballistic stability and can be implemented with a high output.
- a powder is provided as a drive powder or ignition powder for accelerating projectiles for mortar systems, which powder is based on nitrocellulose.
- the powder contains a crystalline energy carrier based on nitramine in 1-30% by weight and an inorganic flash hider in 0.1-10% by weight.
- the powder is in the form of grains.
- the grains have an inert plasticizing additive on their surface.
- the additive is camphor and is present in a range of 0.01-1% by weight.
- the increase in the muzzle velocity with increasing temperature is also relatively small, so that the drive is characterized overall by largely neutral temperature characteristics
- the powder according to the invention has a high degree of energy conversion with a flat pressure profile, which leads to a high internal ballistic performance.
- Mortar systems are generally understood to mean systems that have a relatively short barrel and are fired at relatively steep angles. There are mortars from caliber 37 mm (light mortars) up to 240 mm (super-heavy mortars). The most important are the heavy mortars in calibers 60 - 120 mm. The invention particularly focuses on the mortars and the corresponding drives for systems of calibers 60 mm, 81 mm and 120 mm.
- the powders according to the invention can also be used as igniter powders for mortar applications.
- a kindling powder is housed in the shaft of a mortar shell and is needed to amplify the impulse of the pyrotechnic initial ignition and to transfer it to the drive powder in the surrounding increments (horse shoes).
- the composition of a lighting powder is identical to the composition of a drive powder. However, they can differ in grain size and grain geometry.
- Both the drive powder and the ignition powder are extrudable bulk powders that can be produced in a solvent process and contain nitrocellulose as the main component.
- nitrocellulose has been the most important raw material for the production of single-, double- and tri-base propellant powders. It is obtained through the nitration of cellulose (cotton linters, cellulose), is available in large quantities at low cost and is available in a wide range of different chemical-physical properties offered.
- Nitrocellulose varies e.g. B. with regard to the nitrogen content, molecular weight or viscosity and, due to these differences, can be processed into the various homogeneous propellant powder types. The energy content of nitrocellulose is adjusted via the nitrogen content. In single-base formulations, nitrocellulose is the sole energy carrier, which means that the energy density of nitrocellulose is relatively high compared to other synthetic binder polymers.
- the present powders are based on nitrocellulose. This preferably has an average nitrogen content of 12.6-13.25%.
- the other key components contained in the grain matrix are a crystalline energy carrier and an inorganic flash hider.
- the crystalline energy carrier increases the energy content of the powder and is used in a concentration in the range from 1 to 30% by weight. With these proportions in a base made of nitrocellulose, it is achieved that the mean distances between the individual crystals of the crystalline energy carrier are sufficiently large so that the individual crystals do not touch each other for the most part. This ensures that when external mechanical stimuli are applied, the shock pulse cannot be passed on from an explosive crystal to the neighboring crystals. In this way, a primarily acting shock pulse is not multiplied and transmitted over the entire amount of powder. On the other hand, with higher weight proportions of crystalline energy carriers, the individual crystals are statistically too close to one another, which greatly increases the vulnerability of the powder.
- the inorganic flash hider is used in a concentration in the range of 0.1-10% by weight.
- an inorganic flash hider By adding an inorganic flash hider, the conversion of unburned gases such as hydrogen or carbon monoxide in the area of the gun muzzle is suppressed so that they do not ignite or only ignite to a very lesser extent.
- the muzzle flash is reduced, which on the one hand reduces the dazzling effect of the fire for the shooter and also makes it more difficult to locate the shooter.
- the crystalline nitramine-based energy carrier is preferably at least one compound from the group comprising hexogen (RDX) and octogen (HMX).
- RDX hexogen
- HMX octogen
- RDX is preferably used as a crystalline energy carrier. Compared to HMX, it is cheaper and safer to manufacture. HMX is more expensive than RDX, but offers no particular advantages. Other nitramine compounds (such as NIGU etc.) have relatively little performance compared to RDX. For stabilization, active ingredients known per se, such as. B. Akardit II can be used
- the crystalline nitramine compound particularly preferably has a defined mean grain size. So z. B. RDX is preferably used with an average grain size of 4-8 micrometers, in particular 6 micrometers.
- the homogeneous particle size of the crystalline energy carrier enables powders to be produced that have relatively constant chemical and ballistic properties.
- nitrate esters are less chemically stable.
- nitramine compounds Hexanitroisowurtzitan (CL-20, CAS # 14913-74-7 ), Nitroguanidine (NIGU, NQ, CAS # 70-25-7 , N-methylnitramine (tetryl, N-methyl-N, 2,4,6-tetranitrobenzolamine, CAS # 479-45-8 ) as well as nitrotriazolone (NTO, CAS # 932-64-9 ) and triaminotrinitrobenzene (TATB, CAS # 3058-38-6 ). All of these energetic connections can be used individually or in combination with one another.
- the proportion of the crystalline energy carrier is particularly preferably 5-25% by weight.
- powders are favored which contain crystalline energy carriers in proportions of 10-20% by weight.
- proportions by weight below 25% by weight, in particular up to 20% by weight, the individual crystals of the energy carrier are spaced from one another in such a way that the The powder's vulnerability is at a very low level.
- the use of an inert plasticizing additive can somewhat reduce the vulnerability of the powder with a relatively high proportion by weight of the crystalline nitramine compound. It is thereby easily possible to use high proportions of the crystalline nitramine compound.
- RDX In addition to its property as a crystalline energy carrier, RDX also has certain stabilizing properties that come into play from approx. 1% by weight and increase only insignificantly with increasing proportion.
- the inorganic flash hider is preferably at least one compound from the group of alkali salts such as. B. Potassium Nitrate and Potassium Sulphate. In addition to reducing the muzzle flash, these compounds can also accelerate the burn and thereby reduce the formation of residues, which further increases the degree of energy conversion.
- the inorganic flash hider is present in a proportion of 0.1-5% by weight.
- the surface of the powder grain is preferably treated with graphite and ethanol.
- the extruded powder grains are preferably subjected to a surface treatment with ethanol and graphite.
- the surface is treated with camphor as an inert plasticizing additive.
- the inert plasticizing additive penetrates into the near-surface zones of the powder grain and remains there, ie it is localized and does not distribute itself in the grain matrix.
- the inert plasticizing additive has a penetration depth of a few 100 micrometers, e.g. B. a maximum of 400 micrometers, preferably 100-300 Micrometer. This means that at least 95% by weight of the inert plasticizing additive is contained up to this depth.
- the applied graphite preferably remains on the surface of the powder grain.
- the surface treatment i.e. the application of ethanol, graphite and the inert plasticizing additive to the surface of the extruded powder grain, has a positive influence on the properties of the powder grain.
- a temperature-neutral behavior and the bulk density i.e. how much powder can be accommodated in a given container volume
- the pressure level i.e. the ratio of peak gas pressure to muzzle velocity
- the grain matrix does not contain more inert compounds than necessary, and can therefore have the greatest possible amount of energetic compounds.
- a surface treatment with a combination of these substances can achieve the greatest possible effect.
- the inert plasticizing additive is preferably present on the surface of the grain in not more than 0.1% by weight, in particular in a range of 0.01-0.1% by weight. It is precisely with these quantities of the inert plasticizing additive that the change in the muzzle velocity and also the increase in pressure on transition to high temperatures are relatively small. With significantly larger amounts of the inert plasticizing additive, the possibility of achieving temperature-neutral behavior decreases.
- the grains for the drive preferably have a circular cylindrical geometry with longitudinal channels in the axial direction.
- the number of channels is arbitrary, often one grain has one channel, 7 or 19 channels.
- Such a propellant charge powder, also called hole powder, is consequently pourable or free-flowing, and can thus be industrially filled into tubes.
- the ratio of length (L) to diameter (D) of the cylindrical grain has a value L / D - 0.25-5.
- the length of the circular cylinder is z. B. in the range of 0.3-10 mm and the diameter in the range of 0.3-10 mm.
- the invention is designed as a multi-hole powder, a geometry with a small pitch circle and thus a greater external wall thickness is preferred.
- the individual longitudinal channels of a drive powder have a hole diameter of 0.1-0.5 mm.
- the grain dimensions are typically smaller than when used for the drive. In addition, they often have a circular cylindrical geometry with a central longitudinal channel. You have z. B has an outside diameter of 1.3-1.7 mm, a length of 1.5-2.0 mm, an average wall thickness of 0.6-0.8 mm and a hole diameter of approx. 0.10 mm.
- the material for the powders can be in the form of strips or extruded directly into a specific shape suitable for guns. In this form it is particularly suitable for large-caliber ammunition.
- This typically includes shapes in which the width is much smaller (e.g. at least 5 times or at least 10 times) than the length and the thickness is in turn much smaller (e.g. at least 5 times or at least 10 times) than the width.
- the thickness is e.g. B. 1-2 mm, the width at z. B. 10 mm or more and the length at z. B. 100 - 150 mm.
- shaped bodies i.e. hollow cylindrical shapes for ammunition, in which the case is missing or has been replaced by the "shaped body” arranged behind the ignition, are also conceivable.
- the grain matrix can optionally contain further additives known per se.
- Sodium hydrogen carbonate CAS #: 144-55-8
- Calcium carbonate CAS #: 471-34-1
- Magnesium oxide CAS #: 1309-48-4
- Akardite II CAS #: 724-18-5
- Centralit I CAS #: 90-93-7
- Centralit II CAS #: 611-92-7
- 2-nitrodiphenylamine CAS #: 836-30-6
- diphenylamine CAS #: 122-39-4
- Additives such as lime, manganese oxide, magnesium oxide ( CAS #: 1303-48-4 ), Molybdenum trioxide ( CAS #: 1313-27-5 ), Magnesium silicate ( CAS #: 14807-96-6 ), Calcium carbonate ( CAS #: 471-34-1 ), Titanium dioxide ( CAS #: 13463-67-7 ), Tungsten trioxide ( CAS #: 1314-35-8 ) serve to protect the pipes.
- Compounds such as phthalic acid esters, citric acid esters or adipic acid esters are common plasticizers.
- the green grain that is to say the powder that is still untreated per se, can contain other known additives in the matrix, e.g. B. to improve the ignition behavior and to modulate the combustion behavior.
- a method for producing a powder according to the invention is characterized in that a solvent-containing powder dough based on nitrocellulose and a crystalline energy carrier based on nitramine in 1-30% by weight and an inorganic flash hider is produced.
- the solvent-based powder dough is then extruded into a green grain.
- the solvent is removed from this green grain and the surface of the green grain is treated with camphor as an inert plasticizing additive. Finally, the surface-treated green grain is dried.
- a powder according to the invention can be produced on existing production plants.
- the solid formulation components can, for example, be mixed with a solvent mixture.
- the resulting solvent-moist kneading dough can be kneaded in a kneader and then extruded to the desired geometry in a press.
- the extruded strands can be pre-dried and cut to the desired grain length.
- the solvent can then be removed from the grain.
- the grain is with the inert surface-treated plasticizing additive and can optionally be subjected to a finishing.
- the green grain is preferably surface-treated with ethanol and graphite, i.e. graphitized.
- the graphitization can be carried out as a single process step. However, it is also possible to apply graphite and ethanol to the green grain together with the inert plasticizing additive.
- the solvent is particularly preferably removed from the green grain using a moist air process.
- the green grain obtained by extrusion contains an inorganic flash hider in the grain matrix.
- the green grain should not be subjected to a bathing process in order to remove the solvent from the grain matrix, since otherwise the water-soluble inorganic flash hider would be washed out of the grain matrix.
- the solvent that was used in the manufacturing process is therefore removed by means of a humid air process.
- the solvent-moist green grain is flowed through for 10-60 hours with a stream of air at temperatures between 20-70 ° C, which is saturated with water vapor, at high flow rates of several hundred m 3 per hour.
- the proportion of solvent is reduced to ⁇ 1%, while the water-soluble flash hider is not removed from the grain matrix, but remains there.
- finishing is carried out. This means in particular the careful drying and sieving of the surface-treated grain.
- various additives are added to the powder dough, which is based on nitrocellulose, ie the additives are evenly distributed in the matrix.
- the total amount of these additives is 0-10% by weight compared to nitrocellulose, preferably 2-7% by weight.
- the total amount of the crystalline nitramine compound, which is typically RDX, is 1-30% by weight of the amount of nitrocellulose.
- the crystalline nitramine compound may have to be subjected to a pretreatment to improve the connection to the matrix before it is added to the powder dough.
- the green grain is extruded through a die.
- the water and the solvent are then removed, preferably by means of moist air drying.
- the green grain is subjected to a surface treatment in which the inert plasticizing additive and preferably other additives such as graphite are applied in the presence of ethanol (impregnation + coating).
- the extruded strands are short pre-dried in air, cut to the desired length, and the green grain thus obtained fine mesh screens designed uniformly the green grain is then for 30 hours with a water-saturated air stream of 200 m 3 / h and a temperature of 30 ° C and then flowed through for 30 hours with an air stream of 400 m 3 / h and a temperature of 65 ° C (moist air drying).
- 0.05% by weight of graphite and 1.2 liters of ethanol are then added to 60 kg of the green grain heated to 60 ° C. in a copper polishing drum heated to 55 ° C., then allowed to act for 1 hour while rotating continuously.
- the powder is spread out on metal sheets and dried at 60 ° C. for 24 hours.
- Example 2 - drive powder 2 (FM 4650/22)
- a powder dough according to Example 1 is pressed (i.e. extruded) through a die with 7-hole geometry and 4.8 mm strand cross-section.
- the extruded strands are briefly pre-dried in the air, cut to the desired length, and the green grain thus obtained is subjected to moist air drying (as described in Example 1).
- 60 kg of the green grain are preheated to 60 ° C. and transferred to a copper polishing drum heated to 55 ° C. 0.05% of graphite and a solution of 1% by weight of camphor in 1.2 kg of ethanol are added to the green grain and it is continuously rotated for 1 hour.
- the powder is spread out on metal sheets and dried at 60 ° C. for 24 hours.
- the resulting drive powder 2 with the designation FM 4650/22 has the following physical properties: 3.42 mm outside diameter, 3.45 mm length, 0.71 mm mean wall thickness and 0.19 mm hole diameter, 4152 J / g heat content and 1002 g / l bulk density. Chemical stability: Deflagration temperature - 172 ° C. Heat flow calorimetry according to STANAG 4582 - 47 J / g resp. 30.9 ⁇ W (rement according to standard STANAG 4582: maximum heat development ⁇ 114 ⁇ W).
- a powder dough according to Example 1 is extruded through a die with 7-hole geometry and 5.1 mm strand cross-section.
- the extruded strands are briefly pre-dried in the air, cut to the desired length, and the green grain thus obtained is subjected to moist air drying (as described in Example 1).
- 120 kg of the green grain are preheated to 60 ° C. and transferred to a copper polishing drum heated to 55 ° C.
- the green grain is mixed with 0.05% graphite and a solution of 0.1% by weight camphor in 2.4 kg of ethanol and rotated continuously for 1 hour.
- the powder is spread out on metal sheets and dried at 60 ° C. for 24 hours.
- Example 4 Ignition powder 1 (FM 4483/21)
- a powder dough according to Example 1 is pressed (ie extruded) through a die with 1-hole geometry and 2.1 mm strand cross-section.
- the extruded strands are briefly pre-dried in the air, cut to the desired length and the resulting green grain is subjected to moist air drying (as described in Example 1).
- 20 kg of the green grain are preheated to 60 ° C and placed in a polishing drum heated to 55 ° C transferred from copper.
- 0.3% by weight of graphite and 0.3 kg of ethanol are added to the green grain, after which it is left to act for 1 hour while rotating continuously.
- the powder is spread out on metal sheets and dried at 60 ° C. for 24 hours.
- Example 5 Ignition powder 2 (FM 4483/22)
- a powder dough according to Example 1 is pressed (i.e. extruded) through a die with 1-hole geometry and 2.1 mm strand cross-section.
- the extruded strands are briefly pre-dried in the air, cut to the desired length, and the green grain thus obtained is subjected to moist air drying (as described in Example 1).
- 20 kg of the green matter are preheated to 60 ° C. and transferred to a copper polishing drum heated to 55 ° C. 0.3% by weight of graphite, 0.5% by weight of camphor and 0.15 kg of ethanol are added to the green grain, and the mixture is then left to act for 1 hour while rotating continuously.
- the powder is spread out on metal sheets and dried at 60 ° C. for 24 hours.
- the presence of 0.5% by weight of camphor in the ignition powder 2 according to the invention reduces the peak gas pressure at 21 ° C., which can be advantageous for certain applications.
- the igniter powder 2 with 0.5% by weight of camphor shows a higher pressure increase than that without camphor.
- the optimal amount of camphor must be carefully weighed so that the system requirements specified by the application can be met as best as possible.
- the M48 ball powder that has been introduced has the highest gas pressure at 21 ° C. The pressure increase from 21 ° C. to 63 ° C. is significantly higher with the introduced M48 ball powder of approx. 2300 psi compared to the two ignition powders 1 and 2 according to the invention.
- nitrocellulose-containing powders according to the invention are suitable as drive powders or igniter powders, which contain a crystalline energy carrier based on nitramine and an inorganic flash hider, and have small amounts of an inert plasticizing additive on the surface, for accelerating projectiles for mortar systems show a temperature-independent behavior and can therefore be used regardless of climatic conditions.
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- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Air Bags (AREA)
- Medicinal Preparation (AREA)
Claims (10)
- Poudre servant de poudre propulsive ou de poudre d'allumage pour l'accélération de projectiles destinés à des mortiers, qui est à base de nitrocellulose et contient une source d'énergie cristalline à base de nitramine en une quantité de 1 à 30 % en poids et un antilueur inorganique, la poudre se présentant sous forme de grains, et les grains présentant sur leur surface un additif plastifiant inerte, l'antilueur inorganique étant présent en une quantité de 0,1 à 10 % en poids, caractérisée en ce que l'additif plastifiant inerte est le camphre et est présent en une quantité de 0,01 à 1 % en poids.
- Poudre selon la revendication 1, caractérisée en ce que, pour ce qui concerne la source d'énergie cristalline à base de nitramine, il s'agit d'au moins un composé du groupe comprenant l'hexogène (RDX) et l'octogène (HMX).
- Poudre selon l'une des revendications 1 ou 2, caractérisée en ce que la source d'énergie cristalline est présente en une quantité de 5 à 25 %.
- Poudre selon l'une des revendications 1 à 3, caractérisée en ce que, pour ce qui concerne l'antilueur inorganique, il s'agit d'au moins un composé du groupe comprenant le nitrate de potassium et le sulfate de potassium.
- Poudre selon l'une des revendications 1 à 4, caractérisée en ce que l'antilueur inorganique est présent en une quantité de 0,1 à 5 % en poids.
- Poudre selon l'une des revendications 1 à 5, caractérisée en ce que l'additif plastifiant inerte est présent en une quantité de 0,01 à 0,1 % en poids.
- Poudre selon l'une des revendications 1 à 6, caractérisée en ce que les grains ont une géométrie cylindrique circulaire et des canaux longitudinaux courant dans la direction axiale.
- Procédé de fabrication d'une poudre servant de poudre propulsive ou de poudre d'allumage selon l'une des revendications 1 à 7, caractérisé en ce quea) on fabrique une pâte de poudre contenant un solvant, à base de nitrocellulose et d'une source d'énergie cristalline à base de nitramine en une quantité de 1 à 30 % en poids et d'un antilueur inorganique,b) par extrusion de la pâte de poudre contenant un solvant, on fabrique un grain vert,c) on élimine le solvant du grain vert,d) on soumet à un traitement de surface le grain vert avec un additif plastifiant inerte, ete) on sèche le grain vert traité en surface.
- Procédé selon la revendication 8, caractérisé en ce que le solvant est éliminé du grain vert par un procédé à l'air humide.
- Procédé selon l'une des revendications 8 à 9, caractérisé en ce qu'on procède à une finition après le séchage du grain vert traité en surface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL13704344T PL2951137T3 (pl) | 2013-01-29 | 2013-01-29 | Proch do przyspieszania pocisków do systemów moździerzowych |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CH2013/000017 WO2014117280A1 (fr) | 2013-01-29 | 2013-01-29 | Poudre pour accélérer des projectiles pour mortiers |
Publications (2)
Publication Number | Publication Date |
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EP2951137A1 EP2951137A1 (fr) | 2015-12-09 |
EP2951137B1 true EP2951137B1 (fr) | 2021-03-03 |
Family
ID=47715764
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EP13704344.4A Active EP2951137B1 (fr) | 2013-01-29 | 2013-01-29 | Poudre pour accélérer des projectiles pour mortiers |
Country Status (8)
Country | Link |
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US (1) | US20150321969A1 (fr) |
EP (1) | EP2951137B1 (fr) |
JP (1) | JP6165269B2 (fr) |
KR (1) | KR101944300B1 (fr) |
CA (1) | CA2899260C (fr) |
ES (1) | ES2872299T3 (fr) |
PL (1) | PL2951137T3 (fr) |
WO (1) | WO2014117280A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017004726A1 (fr) | 2015-07-03 | 2017-01-12 | Nitrochemie Wimmis Ag | Système de charges explosives pour projectiles d'artillerie |
RU2711143C1 (ru) * | 2018-11-27 | 2020-01-15 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | Высокоэнергетический пироксилиновый порох для метательных зарядов танковой артиллерии |
FR3096047B1 (fr) | 2019-05-13 | 2022-06-24 | Eurenco France | Grains de poudre propulsive comprenant des canaux au moins partiellement obtures |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1661278A (en) * | 1928-03-06 | Bernhart troxler | ||
US2147698A (en) * | 1937-07-06 | 1939-02-21 | Hercules Powder Co Ltd | Method in the preparation of progressive-burning smokeless powder, and product thereof |
US2771351A (en) * | 1953-06-09 | 1956-11-20 | Olin Mathieson | Propellant |
US3108916A (en) * | 1959-09-02 | 1963-10-29 | Olin Mathieson | Dustless propellent powder containing coated spherical nitrocellulose |
US3704185A (en) * | 1965-03-01 | 1972-11-28 | Du Pont | Progressive burning smokeless powder coated with an organic ester |
US3798085A (en) * | 1971-09-03 | 1974-03-19 | Hercules Inc | Manufacture of a burning rate deterrent coated propellant |
US4354884A (en) * | 1980-04-28 | 1982-10-19 | Hercules Incorporated | Process for preparing progressive burning propellant granules |
US5218166A (en) * | 1991-09-20 | 1993-06-08 | Mei Corporation | Modified nitrocellulose based propellant composition |
US6740180B1 (en) * | 1997-07-15 | 2004-05-25 | Anthony Joseph Cesaroni | Thermoplastic polymer propellant compositions |
DE19907809C2 (de) * | 1999-02-24 | 2002-10-10 | Nitrochemie Gmbh | Verfahren zur Herstellung von ein-, zwei- oder dreibasigen Triebladungspulvern für Rohrwaffenmunition |
JP2001002488A (ja) * | 1999-06-17 | 2001-01-09 | Daicel Chem Ind Ltd | プリテンショナー用ガス発生剤組成物 |
ES2235813T3 (es) * | 2000-06-15 | 2005-07-16 | Nitrochemie Wimmis Ag | Procedimiento para la fabricacion de un material funcional altamente energetico. |
US20090208647A1 (en) * | 2000-06-15 | 2009-08-20 | Nitrochemie Wimmis Ag | Method for producing a funtional, high-energy material |
PL1857429T3 (pl) * | 2006-05-19 | 2013-08-30 | Nitrochemie Wimmis Ag | Układ napędowy do przyspieszania pocisków |
WO2011153655A2 (fr) * | 2011-09-15 | 2011-12-15 | Nitrochemie Wimmis Ag | Système de propulsion à perforations multiples haute performance, exempt de nitroglycérine |
-
2013
- 2013-01-29 KR KR1020157020466A patent/KR101944300B1/ko active IP Right Grant
- 2013-01-29 WO PCT/CH2013/000017 patent/WO2014117280A1/fr active Application Filing
- 2013-01-29 US US14/760,643 patent/US20150321969A1/en not_active Abandoned
- 2013-01-29 JP JP2015555513A patent/JP6165269B2/ja active Active
- 2013-01-29 CA CA2899260A patent/CA2899260C/fr active Active
- 2013-01-29 ES ES13704344T patent/ES2872299T3/es active Active
- 2013-01-29 EP EP13704344.4A patent/EP2951137B1/fr active Active
- 2013-01-29 PL PL13704344T patent/PL2951137T3/pl unknown
Non-Patent Citations (1)
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None * |
Also Published As
Publication number | Publication date |
---|---|
CA2899260A1 (fr) | 2014-08-07 |
KR101944300B1 (ko) | 2019-04-17 |
CA2899260C (fr) | 2020-01-14 |
KR20150122129A (ko) | 2015-10-30 |
JP2016511210A (ja) | 2016-04-14 |
EP2951137A1 (fr) | 2015-12-09 |
ES2872299T3 (es) | 2021-11-02 |
JP6165269B2 (ja) | 2017-07-19 |
WO2014117280A1 (fr) | 2014-08-07 |
US20150321969A1 (en) | 2015-11-12 |
PL2951137T3 (pl) | 2021-08-30 |
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