EP2951137A1 - Pulver zur beschleunigung von geschossen für mörsersysteme - Google Patents
Pulver zur beschleunigung von geschossen für mörsersystemeInfo
- Publication number
- EP2951137A1 EP2951137A1 EP13704344.4A EP13704344A EP2951137A1 EP 2951137 A1 EP2951137 A1 EP 2951137A1 EP 13704344 A EP13704344 A EP 13704344A EP 2951137 A1 EP2951137 A1 EP 2951137A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- powder
- inert
- additive
- weight
- present
- 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.)
- Granted
Links
- 239000000843 powder Substances 0.000 title claims abstract description 113
- 239000004570 mortar (masonry) Substances 0.000 title claims abstract description 31
- 239000000654 additive Substances 0.000 claims abstract description 40
- 230000000996 additive effect Effects 0.000 claims abstract description 33
- 239000000020 Nitrocellulose Substances 0.000 claims abstract description 18
- 150000001875 compounds Chemical class 0.000 claims abstract description 18
- 229920001220 nitrocellulos Polymers 0.000 claims abstract description 18
- BSPUVYFGURDFHE-UHFFFAOYSA-N Nitramine Natural products CC1C(O)CCC2CCCNC12 BSPUVYFGURDFHE-UHFFFAOYSA-N 0.000 claims abstract description 13
- POCJOGNVFHPZNS-UHFFFAOYSA-N isonitramine Natural products OC1CCCCC11CNCCC1 POCJOGNVFHPZNS-UHFFFAOYSA-N 0.000 claims abstract description 13
- 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 abstract description 12
- 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 abstract description 12
- 239000000028 HMX Substances 0.000 claims abstract description 5
- 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 abstract description 5
- DSSYKIVIOFKYAU-XCBNKYQSSA-N (R)-camphor Chemical compound C1C[C@@]2(C)C(=O)C[C@@H]1C2(C)C DSSYKIVIOFKYAU-XCBNKYQSSA-N 0.000 claims description 22
- 241000723346 Cinnamomum camphora Species 0.000 claims description 22
- 229960000846 camphor Drugs 0.000 claims description 22
- 229930008380 camphor Natural products 0.000 claims description 22
- 238000000034 method Methods 0.000 claims description 14
- 239000002904 solvent Substances 0.000 claims description 12
- 230000008569 process Effects 0.000 claims description 7
- 238000001035 drying Methods 0.000 claims description 5
- 229910002651 NO3 Inorganic materials 0.000 claims description 4
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 claims description 3
- 239000008187 granular material Substances 0.000 claims description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 1
- 239000004480 active ingredient Substances 0.000 claims 1
- KZTZJUQNSSLNAG-UHFFFAOYSA-N aminoethyl nitrate Chemical compound NCCO[N+]([O-])=O KZTZJUQNSSLNAG-UHFFFAOYSA-N 0.000 claims 1
- 229960001557 itramin tosilate Drugs 0.000 claims 1
- 239000002245 particle Substances 0.000 abstract description 5
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 abstract description 4
- 239000003380 propellant Substances 0.000 abstract description 3
- 239000004323 potassium nitrate Substances 0.000 abstract description 2
- 235000010333 potassium nitrate Nutrition 0.000 abstract description 2
- OTYBMLCTZGSZBG-UHFFFAOYSA-L potassium sulfate Chemical compound [K+].[K+].[O-]S([O-])(=O)=O OTYBMLCTZGSZBG-UHFFFAOYSA-L 0.000 abstract 1
- 229910052939 potassium sulfate Inorganic materials 0.000 abstract 1
- 239000001120 potassium sulphate Substances 0.000 abstract 1
- 235000011151 potassium sulphates Nutrition 0.000 abstract 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 24
- FJWGYAHXMCUOOM-QHOUIDNNSA-N [(2s,3r,4s,5r,6r)-2-[(2r,3r,4s,5r,6s)-4,5-dinitrooxy-2-(nitrooxymethyl)-6-[(2r,3r,4s,5r,6s)-4,5,6-trinitrooxy-2-(nitrooxymethyl)oxan-3-yl]oxyoxan-3-yl]oxy-3,5-dinitrooxy-6-(nitrooxymethyl)oxan-4-yl] nitrate Chemical compound O([C@@H]1O[C@@H]([C@H]([C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O)O[C@H]1[C@@H]([C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@@H](CO[N+]([O-])=O)O1)O[N+]([O-])=O)CO[N+](=O)[O-])[C@@H]1[C@@H](CO[N+]([O-])=O)O[C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O FJWGYAHXMCUOOM-QHOUIDNNSA-N 0.000 description 15
- 229940079938 nitrocellulose Drugs 0.000 description 15
- 239000007789 gas Substances 0.000 description 14
- 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 10
- -1 nitramine compound Chemical class 0.000 description 10
- 239000000126 substance Substances 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 6
- 239000013078 crystal Substances 0.000 description 6
- 230000037452 priming Effects 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 5
- 238000007605 air drying Methods 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 230000020169 heat generation Effects 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- 238000004381 surface treatment Methods 0.000 description 5
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 4
- 239000000006 Nitroglycerin Substances 0.000 description 4
- 238000004200 deflagration Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 229960003711 glyceryl trinitrate Drugs 0.000 description 4
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 3
- UIIMBOGNXHQVGW-UHFFFAOYSA-M Sodium bicarbonate Chemical compound [Na+].OC([O-])=O UIIMBOGNXHQVGW-UHFFFAOYSA-M 0.000 description 3
- 238000007707 calorimetry Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000001514 detection method Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- 238000004898 kneading Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- GWEHVDNNLFDJLR-UHFFFAOYSA-N 1,3-diphenylurea Chemical compound C=1C=CC=CC=1NC(=O)NC1=CC=CC=C1 GWEHVDNNLFDJLR-UHFFFAOYSA-N 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 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 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- WNLRTRBMVRJNCN-UHFFFAOYSA-N adipic acid Chemical compound OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910000019 calcium carbonate Inorganic materials 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 2
- 238000005755 formation reaction Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 229920006395 saturated elastomer Polymers 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
- IDCPFAYURAQKDZ-UHFFFAOYSA-N 1-nitroguanidine Chemical compound NC(=N)N[N+]([O-])=O IDCPFAYURAQKDZ-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
- 241000239290 Araneae Species 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
- 241000251730 Chondrichthyes Species 0.000 description 1
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 1
- 206010010071 Coma Diseases 0.000 description 1
- 241000233866 Fungi Species 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- IOVCWXUNBOPUCH-UHFFFAOYSA-M Nitrite anion Chemical compound [O-]N=O IOVCWXUNBOPUCH-UHFFFAOYSA-M 0.000 description 1
- 235000011941 Tilia x europaea Nutrition 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 239000001361 adipic acid Substances 0.000 description 1
- 235000011037 adipic acid Nutrition 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
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 239000001913 cellulose Substances 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
- 238000011161 development 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
- 238000001125 extrusion Methods 0.000 description 1
- 239000003063 flame retardant 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
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000011835 investigation Methods 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
- 239000000395 magnesium oxide Substances 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
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 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
- 230000035515 penetration Effects 0.000 description 1
- 125000005498 phthalate group Chemical class 0.000 description 1
- 150000003022 phthalic acids Chemical class 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000035939 shock 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
- 239000003381 stabilizer Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
-
- 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 primer for accelerating mortar mortar systems, which is based on nitrocellulose and contains a crystalline nitrite-based energy carrier in 1-3% by weight and an inorganic misfire damper, the powder being in the form of granules and the grains optionally have on their surface an inert p-type additive. Furthermore, the invention relates to a method for the production of such a powder. State of the art
- Nitrochemie had recognized the signs of the times and started the development of a new generation of nitroglycerin-free high-performance powders, which showed no change in ballistic and chemical stability, even during prolonged use in hot climates. H. their use and storage in hot climates posed absolutely no security risk.
- This new generation of powders was initially developed specifically for high-performance applications in mid-barrel guns, such as low-caliber APFSDS T or full-bore Airburst ammunition.
- Such weapon systems are typically equipped with relatively long gun barrels, with relatively high peak gas pressures of typically 3 ⁇ -5000 bar occurring during firing.
- the object of the invention is to provide a Puiver belonging to the technical field mentioned above as a drive powder or ignition powder for accelerating projectiles for Mörsersysterne, which has excellent chemical and ballistic stability and can thereby implement high power output.
- the solution of the problem is defined by the Merkmaie of claim 1.
- a powder is provided as a driving spinner or primer for accelerating projectiles for mortar systems based on nitrocellulose.
- the powder contains a nitrate-based crystalline energy source in 1-30 wt.% And an inorganic misfire damper in 0.1-10 wt.%.
- the powder is lying. In the form of grains in front.
- the grains may have on their surface an inert plasticizing additive. This additive is not more than 1 wt .-%, d, h. in a range of 0-1 wt%, above.
- the grains preferably have on their surface an inert plasticizing additive in 0.01-1% by weight. It is surprising that by using relatively small amounts of an inert plasticizing additive on the surface of the powder, the dependence of the pressure with increasing temperatures can be reduced. In fact, it is known from the drive powder for middle-caliber applications that it is possible to make the dripping process flatter with larger amounts of an inert plasticizing additive. With less than 2 wt .-% are hardly effects to achieve. It has been shown, however, that this relationship does not apply to the driving force for mortar applications. In the case of the drives according to the invention for mortar systems, a relatively flat amount of an inert plasticizing additive achieves a flat pressure gradient.
- the pressure curve is gradually steeper, and with an addition of significantly more than 1 wt .-%, the pressure increases significantly with increasing temperature.
- the increase in the muzzle velocity with increasing temperature is also relatively low, so that the drive as a whole is characterized by a largely neutral temperature characteristic.
- no inert plasticizing additive is necessary.
- the powder according to the invention has a high degree of energy conversion at a low pressure ratio, which leads to a high internal ballistic performance.
- mortar systems are generally understood systems that have a relatively short tube and are fired at relatively steep angles.
- the most important are the heavy mortars in the caliber 60 - 120 mm.
- Particularly in the focus of the invention are the mortars and the corresponding drives for systems of Kaiiber 60 mm, 81 mm and 120 mm.
- the powders according to the invention can also be used as ignition powders for mortar applications.
- An ignition powder is accommodated in the shank of a mortar shell and is required to reinforce the momentum of the pyrotechnic initiation and to transfer it to the drive powder in the surrounding ⁇ Horse Shoes).
- the composition of a priming powder is identical to the composition of a driving powder. However, they can differ in the dimension and in the comgeometry,
- Both the drive powder and the ignition powder are extrudable bulk powders which can be prepared in the solution-center process and contain nitrocellulose as the main component.
- Nitrocellulose has been the most important raw material for the production of monobasic and tri-aspirated cellulosic fungi for over one hundred years. It is obtained by nitration of cellulose (Baumwoii linters, pulp), is available in large quantities at low cost and is available with a wide range of different types chemical-physical properties offered. Nitrocellulose varies z. B, in terms of nitrogen content, molecular weight or viscosity and can be processed due to these differences from the various homogeneous types of propellant charge powder. The energy content of nitrocellulose is adjusted via the nitrogen content. In monobasic 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 source and an inorganic muzzle-fire damper.
- the crystalline energy carrier increases the energy content of the powder and is used in a concentration in the range of 1 to 30% by weight. With these proportions in a base of nitrocellulose, it is achieved that the average distances between the individual crystals of the crystalline energy carrier are sufficiently large so that the individual crystals do not predominantly touch each other. This ensures that, when external mechanical stimuli are applied, the Scbock impulse can not be passed on from one explosive crystal to the adjacent crystals. Thus, a primarily acting shock pulse is not multiplied and transmitted over the entire amount of powder. In contrast, at higher Gewiehisan turnover of crystalline energy carrier, the individual crystals are statistically too close to each other, whereby the vulnerability of the powder increases sharply.
- the inorganic muzzle fire damper is used in a concentration in the range of 0.1 to 10 wt .-%.
- the addition of an inorganic flashback suppresses the reaction of unburned gases such as hydrogen or carbon monoxide in the area of the gun muzzle, so that they ignite or only to a lesser extent.
- the muzzle flash is reduced, which on the one hand reduces the Biend Angel of the fire for the shooter and also makes it difficult to locate the shooter.
- the crystalline energy carrier based on nitramine is preferably at least one compound from the group comprising hexogen (RDX) and octogen (HX).
- RDX is used as a crystalline energy source. It is cheaper and safer to manufacture compared to HMX. H X is more expensive than RDX, but offers no special advantages. Other nitramine compounds (such as z., 8. NIGU, etc.) have relatively little power compared to RDX. To stabilize known agents such. B, Akardit II can be used
- the crystalline nitramine compound particularly preferably has a defined average particle size. So z. B. RDX preferably used with a mean particle size of 4 - 8 microns, especially 6 microns.
- the homogeneous particle size of the crystalline energy carrier makes it possible to produce powders which have relatively constant chemical and ballistic properties.
- nitrate esters are crazy! Compared to nitramine compounds less chemically stable.
- hexanitro isovurtzitane (CL-20, CAS ⁇ # 14 13-74-7), nitroguanidine (NIGU, NQ, CAS # 70-25-7, N- WSetyinitramine (tetryl, N-methyl-N3-a-tetranitrobenzenamine, CAS # 479-45-8) and nitrotriazoione (NTO, CAS # 932-64-9) and triaminotrinitrobenzene (TATB, CAS # 3058-38-6).
- NIGU nitroguanidine
- NTO nitrotriazoione
- TATB triaminotrinitrobenzene
- the proportion of the crystalline energy carrier is particularly preferably 5-25% by weight.
- the crystalline energy carriers in proportions of 10 - have 20 wt .-%.
- the individual crystals of the energy carrier are spaced apart such that the Vulnerability of the powder at a very low level.
- the use of an inert plasticizing additive may somewhat mitigate the vulnerability of the powder at relatively high weight fractions of the crystalline amine compound. It is thus readily possible to use high levels of the crystalline nitramine compound.
- DX In addition to its property as a crystalline energy source DX also has certain stabilizing properties, which are already from about 1 wt.%% To bear and increase with increasing proportion only slightly.
- the inorganic mündungs85dämpfer is preferably at least one compound from the group of Alkalisaize such.
- B. alium nitrate and aiiumsuifat In addition to the reduction of muzzle fire, these compounds can also accelerate the burning and thereby reduce the formation of residues, which further increases the degree of energy conversion.
- the inorganic misfire fire retardant is present in a proportion of 0.1-5% by weight.
- the inert plasticizing additive which may be on the surface of the powder grain, is in particular at least one compound from the group comprising camphor, Diaikylphthaiate [preferably Dh ⁇ C8-C12) phthalates or hydrogenated derivatives thereof) and Dialkyldiphenyiharnscher (preferred Dimethyidiphenyiurea, known by the common name Centralit Ii).
- the inert piastifying additive can also be applied as a combination of several single compounds.
- the most preferred compound which is optionally applied to the surface of the powder grain is camphor.
- the surface of the Puiverkorns 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 plasticized with an inert Treated additive.
- the inert plasticizing additive penetrates into the near-surface areas of the Puiverkorns and remains there, ie it is localized and not distributed in the grain matrix, the inert plasticizing additive has a penetration depth of a few 100 micrometers, z. ß. at most 4 microns, preferably 100-300 microns. This means that at least 95% by weight of the inert plasticizing additive up to this depth is contained.
- the applied graphite preferably remains on the surface of the Puiverkorns.
- the surface treatment, d, h, by the application of ethanol and graphite, and optionally the inert plasticizing additive on the surface of the extruded Puiverkorns the properties of Puiverkorns are positively influenced.
- a temperature-neutral behavior and bulk density ie, how much powder can be accommodated in a given container volume
- the pressure level ie the ratio of peak gas pressure to muzzle velocity
- the grain matrix contains no more inert compounds than necessary, and thereby can have the largest possible amount of energetic compounds.
- the inert plasticizing additive at the surface of the grain is not more than 0.1 wt%, d, h, 0-0.1 wt%, more preferably 0.01-0.1 wt%. ⁇ % before.
- the change in the muzzle velocity and also the pressure increase during the transition to high temperatures is relatively small.
- significantly larger amounts of the inert plasticizing additive the possibility of achieving a temperature-neutral behavior decreases.
- the grains for the drive have a circular cylindrical geometry with longitudinal channels in the axial direction.
- the number of channels is arbitrary, often has a grain a channel, 7 or 1 9 channels on.
- a propellant charge powder also called hole powder, is consequently pourable or free-flowing, and can thus be bottled industrially in pods.
- the length of the circular cylinder is z, B. in the range of 0.3 - 10 mm and the diameter in the range of ⁇ .3 - 10 mm.
- the invention is designed as a multi-hole powder, then a geometry with a small pitch circle and thus a greater outer wall thickness is preferred.
- six longitudinal channels in a 7-hole pump with a total average of approximately 3.6 mm have a pitch circle with a diameter of approximately 2.1 mm.
- the individual longitudinal channels of a ⁇ ntriebspulvers on a hole diameter of 0.1 - 0.5 mm are typically smaller than in the application for the drive. In addition, they often have a circular cylindrical geometry with a central L Lucasskanai. You have z. B an outer diameter of 1 .3-1, 7 mm, a length of 1 .5-2.0 mm, an average wall thickness of G.ö8.8 mm and a hole diameter of about ⁇ .1 ⁇ mm.
- the material for the powders may be in the form of strips or extruded directly into a particular form suitable for guns. In this form it is particularly suitable for large-scale ammunition.
- the thickness is at z. B. 1-2 mm, the width at z. B. 10 mm or more and the length at z. B "1 Gö - 150 mm.)
- shape bodies ie high-altitude forms for an ammunition, in which the hüise fehit or is replaced by the hinfer of the ignition arranged "shaped body”,
- the grain matrix may optionally contain other additives known per se.
- additives known per se.
- sodium bicarbonate C ⁇ S ⁇ #: 144-55-8
- calcium carbonate CAS #: 471-34-1
- agnesia CA $ - #: 1 309-48-4
- acardite CAS
- Centraiit I CAS * 90-93-7
- Centraiit II CAS #: 6 1 1-92-7
- 2-niirodiphenyiamine CAS #: 836-30- 6
- diphenylamine CAS #: 1 22-39-4.
- Additives such as lime, anganoxide, magnesia (CAS #: 1 303-48-4), fumediamine dioxide (CAS #: 1313-27-5), magnesium silicate (GAS #: 14807-96-6), calcium carbonate (CAS - *: 471-34-1), titanium dioxide (CAS #: 1 3463-67-7), olframtrioxid (CAS #: 1314-35-8) are used to protect the pipe, compounds such as phthalic acid esters, Ciironen yarnreester or adipic acid are übiiohe plasticizer .
- the green grain aiso the still untreated powder per se, in the matrix, other known additives, eg. As to improve the ⁇ nzünd s and modulating the ⁇ bbrandverhaitens included.
- a process for producing a powder according to the invention is characterized in that a solvent-based powder dough based on nitroceilulose and a crystalline energy carrier based on nitramine is produced in 1-30% by weight and an inorganic muzzle-fire damper. Subsequently, a Grunkorn is produced by extruding a powder from the solvent-containing powder dough. From this green grain, the solvent is removed and the green grain is optionally surface treated with an inert plasticizing additive. Finally, the optionally finished green grain is dried.
- a powder according to the invention whose binder consists predominantly of nitro-cellulose, and which additionally contains a crystalline energy carrier based on nitramine and an inorganic muzzle-fire damper, can be produced on existing production equipment.
- the solid formulation components may, for. B, be mixed with a solvent mixture.
- the resulting solvent-moist kneading dough can be used in a kneader kneaded and then extruded in a press to the desired geometry, the extruded strands can be pre-dried and cut to the desired grain length.
- the grain can then optionally be surface-treated with an inert plasticizing additive and / or subjected to finishing.
- the green grain is surface-treated with ethanol and graphite, i. H. graphitized.
- the graphitization can be carried out as a single process step.
- the solvent is removed from the green com via a wet air process.
- the green coma obtained by extrusion contains an inorganic misfire damper in the ornmatrix.
- the greenscom for removing the solvent from the grain matrix should not be subjected to a bathing process, otherwise the water-soluble inorganic muzzle fire damper would be washed out of the grain matrix.
- the solvent used in the manufacturing process is therefore removed by the wet air method.
- the agent-rich green grain is flowed through at high flow rates of several hundred m 3 per hour for 10 to 60 hours with an air stream at temperatures between 20 and 70 ° C., which is saturated with water vapor.
- the proportion of the solvent is reduced to ⁇ 1% while the water-soluble misfire damper is not removed from the grain matrix, but remains there.
- finishing takes place after drying of the surface-treated grain. This is understood to mean, in particular, the careful drying and sieving of the surface-treated grain. From the following detailed description and the totality of the claims, further advantageous embodiments and Merkmaiskombinationen of the invention.
- various additives are added to the powder dough based on nitrocellulose, i. H. the additives are distributed in the matrix.
- the total amount of these additives except the crystalline nitramine compound is 0-10% by weight to nitrocellulose, preferably 2-7% by weight.
- the total amount of the crystalline nitramine compound, which is typically RDX, is 0-30 % By weight of the amount of nitrocellulose, preferably at 0-20% by weight.
- the crystalline nitramine compound may need to be pretreated to improve the attachment to the matrix before it is added to the powder dough.
- the green grain After kneading the powdered dough with solvents, the green grain is extruded through a die. Subsequently, the water and the solvent are removed, preferably by means of wet air drying, the green grain is subjected to a surface treatment in which z. B, optionally an inert plasticizing additive and preferably other additives such as, for example, graphite are applied in the presence of ethanol (impregnation + coating).
- an inert plasticizing additive and preferably other additives such as, for example, graphite are applied in the presence of ethanol (impregnation + coating).
- Bess sd 1 - ⁇ sitriabs uiver 1 (FSV! 4651/21)
- FSV! 4651/21 For the production of 520 kg of a 7-hole Puiver, 20% by weight RDX, 1.2% by weight Akardit II and 3.2% by weight potassium nitrate and Nitrocellulose with a Stickstoffgehait of 13.20 wt .-% (supplement to 100 wt -%) with the addition of diethyl ether and ethanol for 70 min processed to a K ⁇ lungsrnitteifeuchten kneading dough, Ansehliessen the powder dough is pressed through a die with 7-hole geometry and 5.2 mm strand cross-section (ie extruded).
- the extruded strands are briefly pre-dried in the air, cut to the desired length, and the resulting green grain on a fine mesh sieve gieichmässig interpreted.
- the green grain is then left for 30 hours with a water saturated air flow of 200 m ; t / n and a temperature of 30 ° G and then flows through for 30 hours with an air flow 400 m 3 / h and a temperature of 65 ° C (moist air drying).
- To 60 kg of heated to 60 ° C green grain are then added in a heated to 55 ° C Poiiertrommei copper 0.05 wt -% graphite and 1, 2 liters of ethanol added, then leaving it for 1 hour unier constantly turning act.
- the powder is spread on sheets and dried at 60 ° C for 24 hours.
- the resulting Arsprayspuiver 1 with the designation FM 4651/2 1 has the following physical properties: 3.63 mm Outer Diameter, 3.6 mm length, 0.76 mm average wall thickness and 0.20 mm hole diameter, 4251 j / gificatinhait and 1048 g / i bulk density.
- Chemical stability: deflagration temperature - 172 ° C, heat flow aero- metry according to ST ⁇ NAG 4582 44 j / g resp. 30.4 ⁇ (rement according to standard STANAG 4582: maximum heat generation ⁇ 1 14 ⁇ .
- a powder dough according to Example 1 is pressed through a die having a 7-hole geometry and a 4.8 mm strand cross-section (ie exiruded).
- the extruded strands are briefly pre-dried in air, cut to the desired length, and the resulting green grain is subjected to wet air drying (as described in Ex. 1).
- 60 kg of the green grain are preheated to 60 ° C and transferred to a heated to 55 ° C Poiiertrommei copper.
- the green grain is mixed with 0.05% graphite and a solution of 1 wt .-% camphor in 1 .2 kg Ethanoi and constantly rotated for 1 hour.
- the powder is spread on 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, 41.sup.22 j / g heat content and 1002 g / l bulk density.
- Chemical stability: deflagration temperature 172 ° C, heat flow cascade according to STANAG 4582 » 47 j / g resp. 30.9 ⁇ (rement according to standard ST ⁇ NAG 4582: maximum heat generation ⁇ 1 14 ⁇ ⁇ ).
- a powder dough according to Example 1 is extruded through a die with 7 ⁇ Loehgeometrie and 5, 1 mrn strand cross-section.
- the extruded strands are briefly pre-dried in air, cut to the desired length, and subjected to the Grünkom a Moisture-moisture drying (as described in Example 1), then 120 kg of the green grain are preheated to 60 ° C and in one to 55 ° C heated Poiiertromrnel transferred from copper.
- the green grain is mixed with 0.05% graphite and a solution of 0, 1 wt .-% camphor in 2.4 kg of ethanol and constantly rotated for 1 hour. Finally, the powder is spread on sheets and dried at 60 ° C for 24 hours.
- the resulting drive powder 3 with the designation FM 4714 has the following physical properties: 3.58 mm outside diameter, 3.59 mm length, 0.75 mm average wall thickness and 0.20 mm hole diameter, 4269 j / g heat content and 1026 g / l bulk density, Chemical stability: deflagration temperature V / 2 "C. Heat flow calorimetry according to STANAG 4582 » 50 j / g or 32.6 ⁇ W (rement according to standard STA NAG 4582: maximum heat generation ⁇ 1 14 ⁇ ⁇ ),
- a powder dough according to Example 1 is pressed through a die with 1-hole geometry and 2.1 mm strand cross-section (d, h, extruded).
- the extruded strands are briefly pre-dried in air to the desired length and subjected to the resulting green grain of a wet air drying (as described in Ex. 1).
- 20 kg of the green grain are preheated to 60 ° G and in a heated to 55 ° C Poiiertrommel transferred from copper.
- 0.3% by weight of graphite and 0.3 kg of ethanol are added to the green grain, after which they are allowed to act for one hour while being rotated continuously.
- the resulting priming powder 1 with the designation FM 4483/21 has the following physical properties: 1.47 mm outside diameter, 1.75 mm length, 0.69 mm average wall thickness and 0, 0 mm hole diameter, 4393 J / g heat content and 1001 g / i bulk density, Chemical stability: low temperature * 172 ° C.
- a powder dough according to Example 1 is pressed through a die with 1-hole geometry and 2. 1 mm Sirang cross section (ie extruded).
- the exuded strands are briefly pre-dried in air, cut to the desired length, and subjected to wet-air drying the green grain (as described in Ex. 1).
- 20 kg of the green grain are preheated to 60 ° C and transferred to a polished at 55 ° C Poliertrommei copper.
- the green grain is mixed with 0.3% by weight of graphite, 0.5% by weight of camphor and 0, 1 5 kg of ethanol, then allowed to act under constant rotation for 1 hour.
- the powder is spread on sheets and dried at 60 ° C for 24 hours.
- the resulting priming powder 2 with the designation FM 4483/22 has the following physical properties: 1.47 mm outer diameter, 1.75 mm length, 0.69 mm average wall thickness and 0.10 mm hole diameter, 4343 j / g heat content and 995 g / i bulk density , Chemical stability: Deflagration temperature » 1 72 C G. Flux flow calorimetry according to STANAG 4582 - 52 j / g resp. 32.4 ⁇ [Requirement according to standard STANAG 4582: maximum heat generation ⁇ 1 14 ⁇ ⁇ ).
- the bullet mass of the used inert mortar shell was 14.0 kg.
- the speed measurement was carried out by Doppler radar, the detection of the peak gas pressure was piezoeiektronisoh in the region of the mouth.
- the experiment was carried out with charge 4, ie using four standard VI234 increments.
- the nitrocelluideal powders according to the invention are suitable as propulsion powders or priming powders which contain a crystalline energy carrier based on nitramine and an inorganic misfire steamer and have small amounts of an inert piastifying additive on the surface for accelerating projectiles for mortar systems show a temperature-independent behavior and thus can 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)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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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 |
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PCT/CH2013/000017 WO2014117280A1 (de) | 2013-01-29 | 2013-01-29 | Pulver zur beschleunigung von geschossen für mörsersysteme |
Publications (2)
Publication Number | Publication Date |
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EP2951137A1 true EP2951137A1 (de) | 2015-12-09 |
EP2951137B1 EP2951137B1 (de) | 2021-03-03 |
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EP13704344.4A Active EP2951137B1 (de) | 2013-01-29 | 2013-01-29 | Pulver zur beschleunigung von geschossen für mörsersysteme |
Country Status (8)
Country | Link |
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US (1) | US20150321969A1 (de) |
EP (1) | EP2951137B1 (de) |
JP (1) | JP6165269B2 (de) |
KR (1) | KR101944300B1 (de) |
CA (1) | CA2899260C (de) |
ES (1) | ES2872299T3 (de) |
PL (1) | PL2951137T3 (de) |
WO (1) | WO2014117280A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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CA2990862C (en) | 2015-07-03 | 2022-05-31 | Nitrochemie Wimmis Ag | Propelling charge system for artillery shells |
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 |
US20090208647A1 (en) * | 2000-06-15 | 2009-08-20 | Nitrochemie Wimmis Ag | Method for producing a funtional, high-energy material |
DE50009362D1 (de) * | 2000-06-15 | 2005-03-03 | Nitrochemie Wimmis Ag Wimmis | Verfahren zur Herstellung eines funktionalen hochenergetischen Materials |
PL1857429T3 (pl) * | 2006-05-19 | 2013-08-30 | Nitrochemie Wimmis Ag | Układ napędowy do przyspieszania pocisków |
BR112014005789B1 (pt) * | 2011-09-15 | 2020-06-23 | Nitrochemie Wimmis Ag | Sistema propelente multiperfurado isento de nitroglicerina, seu uso e método para produzir propelentes multiperfurados |
-
2013
- 2013-01-29 ES ES13704344T patent/ES2872299T3/es active Active
- 2013-01-29 EP EP13704344.4A patent/EP2951137B1/de active Active
- 2013-01-29 PL PL13704344T patent/PL2951137T3/pl unknown
- 2013-01-29 WO PCT/CH2013/000017 patent/WO2014117280A1/de active Application Filing
- 2013-01-29 KR KR1020157020466A patent/KR101944300B1/ko active IP Right Grant
- 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/en active Active
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See references of WO2014117280A1 * |
Also Published As
Publication number | Publication date |
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ES2872299T3 (es) | 2021-11-02 |
KR20150122129A (ko) | 2015-10-30 |
US20150321969A1 (en) | 2015-11-12 |
KR101944300B1 (ko) | 2019-04-17 |
CA2899260C (en) | 2020-01-14 |
EP2951137B1 (de) | 2021-03-03 |
JP2016511210A (ja) | 2016-04-14 |
PL2951137T3 (pl) | 2021-08-30 |
JP6165269B2 (ja) | 2017-07-19 |
WO2014117280A1 (de) | 2014-08-07 |
CA2899260A1 (en) | 2014-08-07 |
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