EP0808813B1 - Continuous process for the solventless production of pyrotechnical products having a thermosetting binder - Google Patents
Continuous process for the solventless production of pyrotechnical products having a thermosetting binder Download PDFInfo
- Publication number
- EP0808813B1 EP0808813B1 EP97401051A EP97401051A EP0808813B1 EP 0808813 B1 EP0808813 B1 EP 0808813B1 EP 97401051 A EP97401051 A EP 97401051A EP 97401051 A EP97401051 A EP 97401051A EP 0808813 B1 EP0808813 B1 EP 0808813B1
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- EP
- European Patent Office
- Prior art keywords
- process according
- binder
- products
- styrene
- solid
- Prior art date
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- Expired - Lifetime
Links
- 239000011230 binding agent Substances 0.000 title claims description 54
- 238000004519 manufacturing process Methods 0.000 title claims description 16
- 238000010924 continuous production Methods 0.000 title claims description 11
- 229920001187 thermosetting polymer Polymers 0.000 title description 10
- 239000000203 mixture Substances 0.000 claims description 38
- 238000000034 method Methods 0.000 claims description 34
- 239000000047 product Substances 0.000 claims description 32
- 239000007787 solid Substances 0.000 claims description 27
- 230000008719 thickening Effects 0.000 claims description 26
- 239000000945 filler Substances 0.000 claims description 25
- 239000002131 composite material Substances 0.000 claims description 23
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 claims description 20
- 238000004132 cross linking Methods 0.000 claims description 17
- 239000013067 intermediate product Substances 0.000 claims description 16
- 238000005096 rolling process Methods 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 14
- 239000007788 liquid Substances 0.000 claims description 13
- 230000001590 oxidative effect Effects 0.000 claims description 11
- 229920001169 thermoplastic Polymers 0.000 claims description 10
- 238000005520 cutting process Methods 0.000 claims description 7
- 238000002156 mixing Methods 0.000 claims description 7
- 239000000470 constituent Substances 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 239000008187 granular material Substances 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 5
- 239000004721 Polyphenylene oxide Substances 0.000 claims description 4
- 239000006229 carbon black Substances 0.000 claims description 4
- 229920001577 copolymer Polymers 0.000 claims description 4
- 239000002245 particle Substances 0.000 claims description 4
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 3
- 229920002614 Polyether block amide Polymers 0.000 claims description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 3
- MTAZNLWOLGHBHU-UHFFFAOYSA-N butadiene-styrene rubber Chemical compound C=CC=C.C=CC1=CC=CC=C1 MTAZNLWOLGHBHU-UHFFFAOYSA-N 0.000 claims description 3
- 229920006147 copolyamide elastomer Polymers 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 3
- 229920000636 poly(norbornene) polymer Polymers 0.000 claims description 3
- 239000004814 polyurethane Substances 0.000 claims description 3
- 229920002635 polyurethane Polymers 0.000 claims description 3
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 claims description 2
- 239000005977 Ethylene Substances 0.000 claims description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 239000008119 colloidal silica Substances 0.000 claims description 2
- 150000002430 hydrocarbons Chemical group 0.000 claims description 2
- 125000004433 nitrogen atom Chemical group N* 0.000 claims description 2
- 239000001301 oxygen Substances 0.000 claims description 2
- 229910052760 oxygen Inorganic materials 0.000 claims description 2
- 229920000515 polycarbonate Polymers 0.000 claims description 2
- 239000004417 polycarbonate Substances 0.000 claims description 2
- 229920000570 polyether Polymers 0.000 claims description 2
- 239000011148 porous material Substances 0.000 claims description 2
- 238000010008 shearing Methods 0.000 claims description 2
- 125000000383 tetramethylene group Chemical group [H]C([H])([*:1])C([H])([H])C([H])([H])C([H])([H])[*:2] 0.000 claims description 2
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims description 2
- VSKJLJHPAFKHBX-UHFFFAOYSA-N 2-methylbuta-1,3-diene;styrene Chemical compound CC(=C)C=C.C=CC1=CC=CC=C1.C=CC1=CC=CC=C1 VSKJLJHPAFKHBX-UHFFFAOYSA-N 0.000 claims 1
- 239000004411 aluminium Substances 0.000 claims 1
- 239000011324 bead Substances 0.000 claims 1
- 238000007599 discharging Methods 0.000 claims 1
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 description 9
- 238000001125 extrusion Methods 0.000 description 7
- 239000003380 propellant Substances 0.000 description 7
- 239000002360 explosive Substances 0.000 description 6
- 239000004014 plasticizer Substances 0.000 description 5
- 239000002904 solvent Substances 0.000 description 5
- 239000000654 additive Substances 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000005469 granulation Methods 0.000 description 4
- 230000003179 granulation Effects 0.000 description 4
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 4
- 229920001228 polyisocyanate Polymers 0.000 description 4
- 239000005056 polyisocyanate Substances 0.000 description 4
- 239000004416 thermosoftening plastic Substances 0.000 description 4
- GDDNTTHUKVNJRA-UHFFFAOYSA-N 3-bromo-3,3-difluoroprop-1-ene Chemical compound FC(F)(Br)C=C GDDNTTHUKVNJRA-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- IDCPFAYURAQKDZ-UHFFFAOYSA-N 1-nitroguanidine Chemical compound NC(=N)N[N+]([O-])=O IDCPFAYURAQKDZ-UHFFFAOYSA-N 0.000 description 2
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 description 2
- NDYLCHGXSQOGMS-UHFFFAOYSA-N CL-20 Chemical compound [O-][N+](=O)N1C2N([N+]([O-])=O)C3N([N+](=O)[O-])C2N([N+]([O-])=O)C2N([N+]([O-])=O)C3N([N+]([O-])=O)C21 NDYLCHGXSQOGMS-UHFFFAOYSA-N 0.000 description 2
- 239000000028 HMX Substances 0.000 description 2
- 239000004952 Polyamide Substances 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- SNRUBQQJIBEYMU-UHFFFAOYSA-N dodecane Chemical compound CCCCCCCCCCCC SNRUBQQJIBEYMU-UHFFFAOYSA-N 0.000 description 2
- 235000021183 entrée Nutrition 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 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 description 2
- 229920002647 polyamide Polymers 0.000 description 2
- 229910001487 potassium perchlorate Inorganic materials 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 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 description 1
- 206010001488 Aggression Diseases 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RRHGJUQNOFWUDK-UHFFFAOYSA-N Isoprene Chemical compound CC(=C)C=C RRHGJUQNOFWUDK-UHFFFAOYSA-N 0.000 description 1
- 241000731961 Juncaceae Species 0.000 description 1
- BSPUVYFGURDFHE-UHFFFAOYSA-N Nitramine Natural products CC1C(O)CCC2CCCNC12 BSPUVYFGURDFHE-UHFFFAOYSA-N 0.000 description 1
- 239000005062 Polybutadiene Substances 0.000 description 1
- 230000016571 aggressive behavior Effects 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 238000010923 batch production Methods 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 239000003431 cross linking reagent Substances 0.000 description 1
- HQQADJVZYDDRJT-UHFFFAOYSA-N ethene;prop-1-ene Chemical group C=C.CC=C HQQADJVZYDDRJT-UHFFFAOYSA-N 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 125000003055 glycidyl group Chemical group C(C1CO1)* 0.000 description 1
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- POCJOGNVFHPZNS-UHFFFAOYSA-N isonitramine Natural products OC1CCCCC11CNCCC1 POCJOGNVFHPZNS-UHFFFAOYSA-N 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 239000012764 mineral filler Substances 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 230000000051 modifying effect Effects 0.000 description 1
- 239000012766 organic filler Substances 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- VLTRZXGMWDSKGL-UHFFFAOYSA-M perchlorate Inorganic materials [O-]Cl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-M 0.000 description 1
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical compound OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 description 1
- 150000002978 peroxides Chemical class 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920001281 polyalkylene Polymers 0.000 description 1
- 229920002857 polybutadiene Polymers 0.000 description 1
- 238000006068 polycondensation reaction Methods 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920000193 polymethacrylate Polymers 0.000 description 1
- 229920006264 polyurethane film Polymers 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002562 thickening agent Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
- C06B21/0008—Compounding the ingredient
- C06B21/0025—Compounding the ingredient the ingredient being a polymer bonded explosive or thermic component
-
- 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
- C06B23/001—Fillers, gelling and thickening agents (e.g. fibres), absorbents for nitroglycerine
Definitions
- the present invention relates to the field of composite pyrotechnic products and in particular composite powders for tube weapons, propellants composites for rocket engines and explosives composites for ammunition loading. More precisely the invention relates to a continuous process for solvent-free manufacturing of such pyrotechnic products comprising a thermosetting binder.
- a pulverulent energy charge which can be a mineral charge such as for example ammonium nitrate, ammonium perchlorate or potassium perchlorate or else an organic charge and in particular a nitramine such as for example hexogen, oct
- Binders usable for the manufacture of composite pyrotechnics can be thermoplastic binders or binders thermosetting.
- thermoplastic binders have the advantage of relatively easily lend themselves to implementation continuously due to the fact that they soften by temperature rise. So the patent application French FR-A-2 723 086 describes a manufacturing process continuous and solvent-free of pyrotechnic products composites based on thermoplastic type binders.
- thermoplastic type binders have the disadvantage of leading to products that have a poor temperature resistance due to the very softening of the binder when the temperature.
- the man of profession needs pyrotechnic products presenting good temperature resistance.
- thermosetting binder offer the advantage of presenting good temperature resistance.
- US-A-4,405,534 describes a process for manufacturing composite explosives by cold compression of granules of explosives coated with a polyurethane film made plastic thanks to the presence of plasticizers. This process, apart from the fact that it is discontinuous, has the disadvantage additional to require the presence of a strong plasticizer content which is not always favorable to the energy plan.
- thermosetting binders When the skilled person wants to implement with thermosetting binders a continuous process solvent-free it faces the problem of short "pot life" of these compositions which means that after mixture of the ingredients of the composition, it does have only a very short time to perform the shaping geometry of the product before the crosslinking of the binder does not make any mechanical work of the dough containing the different ingredients.
- thermosetting binder Nevertheless the possibilities of application of these techniques are limited and the skilled person does not have not a general continuous manufacturing process and solvent-free composite pyrotechnic products to thermosetting binder.
- the object of the present invention is precisely to propose such a process as well as an installation industrial allowing the implementation of this process.
- the major originality of the process according to the invention lies in the fact that with the exception of the final phase during which the structure and composition of intermediate products are fixed by crosslinking, the different operations are carried out at a temperature at which the binder is, chemically, almost non-scalable. So the formulation of the product composition is perfectly reproducible insofar as it is fully carried out in start of the process without requiring any adjustment ulterior. The skilled person is not confronted with any condition of "pot life" and intermediate products whose geometric dimensions are imperfect can be recycled in manufacturing.
- the process according to the invention uses a liquid thermosetting binder non-evolving during the process of which the apparent viscosity by use of fillers thickeners.
- said solid thickening filler consists of a porous material whose particle size is between 0.1 and 10 ⁇ m (microns) and whose specific surface is between 60 and 500 m 2 / g .
- this material will also have combustion modifying properties and will be chosen in the group consisting of carbon black, the colloidal silica, alumina, titanium oxide or polynorbornene.
- the weight ratio between said thickening filler and said binder crosslinkable is between 0.05 and 0.25.
- said solid thickening filler is constituted by a thermoplastic polymer with hydrocarbon units which may contain, in addition to carbon and hydrogen atoms, oxygen and nitrogen atoms and whose molecular mass weight average is between 3x10 5 and 3x10 6 .
- thermoplastic polymers usable as solid thickening filler in the framework of the present invention is thus constituted by styrene / butadiene / styrene, styrene / isoprene / styrene copolymers, styrene / ethylene / butylene / styrene and styrene / ethylene / propylene.
- thermoplastic polymers usable as solid thickening fillers in the framework of the present invention is constituted by the polyurethanes with polyether and polycarbonate patterns and by polyether / polyamide block copolymers.
- the weight ratio between said thickening filler and said binder crosslinkable is between 10:90 and 50:50.
- solid oxidizing energy charges we can also incorporate into the premix, consisting by the liquid binder and said thickening fillers, at least one solid reducing energy charge like, for example, aluminum or boron powder.
- the method according to the invention thus makes it possible to obtain continuously, without time constraints linked to "pot life” issues and no use of solvents or energy-unwanted plasticizers, Composite pyrotechnic products with crosslinked binder. These products find their preferred applications as propellant powders in strands or in sticks for ammunition intended for the weapons with tube, like blocks of propellants for rocket and rocket engines, as explosive charges for ammunition explosives or as pyrotechnic charges for gas generators intended for both military applications than civil applications like automotive safety.
- the invention also relates to an installation particularly suitable for the implementation of method according to the invention.
- Figure 1 shows, so schematic, the preferred installation presented above.
- Figure 2 shows, for reasons of clarity, a simplified top view of the rolling mill shear used.
- the invention therefore consists in mixing, at temperature ambient the starting constituents of a composition composite pyrotechnic crosslinkable until obtained a homogeneous composite paste with a viscosity sufficient to be able, always at temperature ambient, be in the form of products intermediaries who already have a stable shape and final dimensions of the finished product that we want to get.
- the form and composition of these intermediate products are then frozen by hot crosslinking so as to obtain the products desired completions.
- thermosetting binder is liquid to room temperature and that its crosslinking cannot start only at a temperature above 40 ° C so as to be certain that as long as we stay at one ambient temperature below 40 ° C, this binder will remain chemically non-evolving.
- binder liquid all of the liquid reactive constituents which, after crosslinking, will give the crosslinked binder solid.
- the crosslinking reaction can be of the type polycondensation reaction, in which case the binders will in particular be of the polyurethane, polyesters or polyamides.
- the crosslinking reaction can be of the type polyaddition reaction with opening of unsaturations ethylenic, in which case the binders will in particular be polyalkylenes, polyacrylates or polymethacrylates. In the latter case, the composition must contain crosslinking catalysts, such as for example peroxides.
- said thickening fillers can be made of porous solid materials of small particle size.
- certain additives usually used as modifiers of combustion like carbon black the process according to the invention in this case offers the advantage of allowing continuously obtaining pyrotechnic compositions already known but which were only accessible by discontinuous processes.
- Said thickening fillers can also be made up of thermoplastic polymers high molecular weight solids so as to get a final product whose binder consists of a alloy of thermoplastic polymers and polymers cross-linked. This type of alloy allows obtaining composite products with characteristics particularly high mechanical properties.
- the premix 2 thus formed may also contain other additives of the final composition. he should have the consistency of a thick fat of so that it can be transported continuously using a positive displacement pump while adhering, without sinking, on the surface of a cylinder rotating with a speed angular of a few tens of revolutions per minute.
- This premix is therefore transported by means of a circulation pump 34, for example a gear, in a reserve 35 provided with a piston cover 36.
- the premix is then taken up by a pump doser 5 with gear to be driven, in a equipment where the operations of mixing with solid energy charges and setting in the form of the composite paste thus obtained in the form of intermediate products that already have the ratings geometries of finished products.
- These two operations can be carried out in a single device like for example a twin screw extruder whose head extrusion will be associated with a cutting device. But, preferentially, these two operations will be carried out by two separate devices, one placed following each other.
- the premix 2 is transported by the pump 5 in a mixer which can be a traditional mixer as a "BUSS" co-kneader but which, preferably and as shown in Figure 1, is a rolling mill shear 6 consisting of two cylindrical rollers 7 and 8 of identical length and having grooves helical. Axes 9 and 10 of these two cylinders are parallel and located in the same horizontal plane being spaced so as to leave a slot 11 between the two rollers. Axes 9 and 10 are supported by support blocks 12 and 13, block 12 being a block engine driving in rotation the two cylinders 7 and 8 which rotate in opposite directions to each other at different speeds.
- Such a shear rolling mill is known to those skilled in the art and described in numerous publications, for example in the patent application FR-A-2 723 086 already cited.
- the pump 5 thus brings the premix 2 to the roller 7 which turns the fastest, the premix forming on this roll a sheet which coats this latest.
- the premix is brought to the end 14 material inlet of the rolling mill 6.
- At least one dosing hopper 16 pours between the material inlet end 14 and the end of material outlet 15 from rolling mill 6, the loads solid energy 17 on the premix sheet coating the roller 7. These solid energy charges are then intimately mixed with premix 2 thanks to the shearing action of the rolling mill 6 so as to form on roll 7 a sheet of composite dough homogeneous which already has sufficient viscosity to ability to maintain stable geometric dimensions.
- Solid energy charges will mainly constituted by the oxidizing charges of the composition which can be mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate, or organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.
- mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate
- organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.
- the different charges may be brought either in mixture by a single hopper, or separately by a succession of hoppers.
- the composite dough sheet thus obtained is recovered in the form of granules 19 by a device for granulation 18 located at the outlet end 15 of the rolling mill 6.
- a device for granulation 18 located at the outlet end 15 of the rolling mill 6.
- the outlet ends of rollers 7 and 8 are not grooved but are smooth.
- the granules 19 are then taken up continuously in an extruder 20, for example a twin extruder screw, fitted with an extrusion head 21 to be profiled in rods 23 driven by a conveyor belt 25.
- an extruder 20 for example a twin extruder screw, fitted with an extrusion head 21 to be profiled in rods 23 driven by a conveyor belt 25.
- a cutting device 22 cuts the rods profiles 23 leaving the extrusion head 21 in 24 intermediate products already with the ratings final of finished products.
- the device cutting 22 has a movement controlled by the speed of progression of the mat 25 on which the rods rest 23.
- the finished products 27 leaving the oven 26 can then be packaged in their packaging 28.
- the method according to the invention thus makes it possible to manufacture in continuous series of products composite pyrotechnics with crosslinked binder, and in particular products of small dimensions, without constraint of "pot life", solvent-free and plasticizer-free undesirable.
- the 7-hole and 19-hole multi-perforated cylindrical powder strands were produced by the continuous process according to the invention from the following three compositions: Composition 1 Composition 2 Composition 3 binder PBHT: 9% PBHT: 10.5% PAG: 13% thickening filler SIS 6% PE-PA: 4.5% PE-PA: 7% oxidizing charge RDX 85% RDX 85% RDX 80% particle size of the oxidizing charge 100 ⁇ m 150 ⁇ m 80 ⁇ m reducing load 0 0 0 0
- Example 4 On 10 meters of propellant extruded continuously for each of the compositions, the dimensional variations obtained after hot cutting and crosslinking are as follows: Example 4 Example 5 Example 6 outer diameter in mm 30.5 ⁇ 0.002 30.0 ⁇ 0.02 29.9 ⁇ 0.02 inside diameter in mm 13.8 ⁇ 0.003 13.9 ⁇ 0.02 14.05 ⁇ 0.02 length in mm 121 ⁇ 0.1 120.5 ⁇ 0.15 120.4 ⁇ 0.1
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- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
- Processes Of Treating Macromolecular Substances (AREA)
- Air Bags (AREA)
Description
La présente invention se rapporte au domaine des produits pyrotechniques composites et notamment des poudres composites pour armes à tube, des propergols composites pour moteurs de fusée et des explosifs composites pour chargements de munitions. Plus précisément l'invention concerne un procédé continu de fabrication sans solvant de tels produits pyrotechniques comportant un liant thermodurcissable.The present invention relates to the field of composite pyrotechnic products and in particular composite powders for tube weapons, propellants composites for rocket engines and explosives composites for ammunition loading. More precisely the invention relates to a continuous process for solvent-free manufacturing of such pyrotechnic products comprising a thermosetting binder.
Les produits pyrotechniques composites constitués par un liant organique et par une charge énergétique pulvérulente qui peut être une charge minérale comme par exemple le nitrate d'ammonium, le perchlorate d'ammonium ou le perchlorate de potassium ou encore une charge organique et notamment une nitramine comme par exemple l'hexogène, l'octogène, la nitroguanidine ou le 2,4,6,8,10,12 hexanitro-2,4,6,8,10,12 hexaazatétracyclo (5.5.O.O 5,9.0 3,11) dodécane encore appelé hexanitrohexaaza-isowurtzitane sont très recherchés par l'homme de métier en raison de leur grande stabilité chimique et de leur faible vulnérabilité aux impacts et aux agressions thermiques.The composite pyrotechnic products constituted by an organic binder and by a pulverulent energy charge which can be a mineral charge such as for example ammonium nitrate, ammonium perchlorate or potassium perchlorate or else an organic charge and in particular a nitramine such as for example hexogen, octogen, nitroguanidine or 2,4,6,8,10,12 hexanitro-2,4,6,8,10,12 hexaazatetracyclo (5.5.OO 5,9. 0 3, 11 ) dodecane also called hexanitrohexaaza-isowurtzitane are highly sought after by those skilled in the art because of their high chemical stability and their low vulnerability to thermal impacts and aggressions.
Par ailleurs, pour des raisons de sécurité et de reproductibilité des fabrications, l'homme de métier préfère les procédés continus aux procédés discontinus.In addition, for security and safety reasons reproducibility of manufacturing, the skilled person prefers continuous processes to discontinuous processes.
Les liants utilisables pour la fabrication de produits pyrotechniques composites peuvent être des liants thermoplastiques ou des liants thermodurcissables.Binders usable for the manufacture of composite pyrotechnics can be thermoplastic binders or binders thermosetting.
Les liants thermoplastiques présentent l'intérêt de se prêter relativement facilement à une mise en oeuvre en continu grâce au fait qu'ils se ramollissent par élévation de la température. Ainsi la demande de brevet français FR-A-2 723 086 décrit un procédé de fabrication en continu et sans solvant de produits pyrotechniques composites à base de liants de type thermoplastique. Néanmoins les liants de type thermoplastique présentent l'inconvénient de conduire à des produits qui ont une mauvaise tenue en température en raison même du ramollissement du liant lorsqu'il y a élévation de la température. Or pour certaines applications, comme par exemple les armes à grande cadence de tir, l'homme de métier a besoin de produits pyrotechniques présentant une bonne tenue en température.Thermoplastic binders have the advantage of relatively easily lend themselves to implementation continuously due to the fact that they soften by temperature rise. So the patent application French FR-A-2 723 086 describes a manufacturing process continuous and solvent-free of pyrotechnic products composites based on thermoplastic type binders. However, thermoplastic type binders have the disadvantage of leading to products that have a poor temperature resistance due to the very softening of the binder when the temperature. However for certain applications, such as example weapons with a high rate of fire, the man of profession needs pyrotechnic products presenting good temperature resistance.
De ce point de vue les produits pyrotechniques à liant thermodurcissable offrent l'avantage de présenter une bonne tenue en température.From this point of view the pyrotechnic products to thermosetting binder offer the advantage of presenting good temperature resistance.
Mais, en raison même du fait que leur liant se durcit de manière irréversible à chaud par réticulation, ces produits présentent l'inconvénient de ne pas bien se prêter aux procédés continus.But, due to the very fact that their binder is irreversibly hardens when cross-linked, these products have the disadvantage of not being well lend to continuous processes.
Ces produits sont donc souvent mis en oeuvre au moyen de procédés discontinus. Ainsi le brevet US-A-4 128 441 décrit un procédé de fabrication discontinue par "coulée" de blocs de propergols. Ce procédé convient bien pour fabriquer des gros chargements pour moteurs de fusée, mais ne convient pas pour fabriquer industriellement en séries de petits objets.These products are therefore often used in using batch processes. So the patent US-A-4 128 441 describes a manufacturing process discontinuous by "pouring" of propellant blocks. This process is well suited for making large rocket engine loads but not suitable to manufacture industrially in series of small objects.
Le brevet US-A- 4,405,534 décrit quant à lui un procédé de fabrication d'explosifs composites par compression à froid de granulés d'explosifs enrobés par un film en polyuréthanne rendu plastique grâce à la présence de plastifiants. Ce procédé, hormis le fait qu'il soit discontinu, présente l'inconvénient supplémentaire de nécessiter la présence d'une forte teneur en plastifiant ce qui n'est pas toujours favorable au plan énergétique.US-A-4,405,534 describes a process for manufacturing composite explosives by cold compression of granules of explosives coated with a polyurethane film made plastic thanks to the presence of plasticizers. This process, apart from the fact that it is discontinuous, has the disadvantage additional to require the presence of a strong plasticizer content which is not always favorable to the energy plan.
Il a été proposé par la demande WO94/05607 un procédé semi-continu de fabrication avec solvant pour de tels produits, mais la nécessité d'avoir recours à un solvant qu'il faut ensuite éliminer limite l'intérêt de ce procédé.It was proposed by application WO94 / 05607 a semi-continuous solvent manufacturing process for such products, but the need to use a solvent which must then be removed limits the interest of this process.
Lorsque l'homme de métier veut mettre en oeuvre avec des liants thermodurcissables un procédé continu sans solvant il est confronté au problème de la courte "vie de pot" de ces compositions qui fait qu'après mélange des ingrédients de la composition, il ne dispose que de très peu de temps pour effectuer la mise en forme géométrique du produit avant que la réticulation du liant ne rende impossible tout travail mécanique de la pâte contenant les différents ingrédients.When the skilled person wants to implement with thermosetting binders a continuous process solvent-free it faces the problem of short "pot life" of these compositions which means that after mixture of the ingredients of the composition, it does have only a very short time to perform the shaping geometry of the product before the crosslinking of the binder does not make any mechanical work of the dough containing the different ingredients.
Il a bien été proposé d'allonger la "vie de pot" en retardant la réticulation finale par exemple par addition fractionnée de l'agent réticulant comme décrit dans le brevet US-A-4,657,607 ou encore en utilisant un double système de liants dont un des systèmes n'est réticulable que par un apport énergétique différent de la chaleur comme décrit dans la demande de brevet EP-A-0 367 445.It has been proposed to extend the "pot life" by delaying final crosslinking for example by fractional addition of the crosslinking agent as described in US-A-4,657,607 or using a double system of binders of which one of the systems is crosslinkable only by a different energy supply than heat as described in the patent application EP-A-0 367 445.
Néanmoins les possibilités d'application de ces techniques sont limitées et l'homme de métier ne dispose pas d'un procédé général de fabrication en continu et sans solvant de produits pyrotechniques composites à liant thermodurcissable. Nevertheless the possibilities of application of these techniques are limited and the skilled person does not have not a general continuous manufacturing process and solvent-free composite pyrotechnic products to thermosetting binder.
L'objet de la présente invention est précisément de proposer un tel procédé ainsi qu'une installation industrielle permettant la mise en oeuvre de ce procédé.The object of the present invention is precisely to propose such a process as well as an installation industrial allowing the implementation of this process.
L'invention concerne donc un procédé continu de
fabrication sans solvant de produits pyrotechniques
composites terminés dont les constituants de départ
comprennent notamment un liant liquide qui est
réticulable à une température supérieure à 40°C et au
moins une charge énergétique oxydante solide, ledit
procédé consistant notamment :
Par rapport aux procédés connus de l'art antérieur, l'originalité majeure du procédé selon l'invention réside dans le fait qu'à l'exception de la phase finale au cours de laquelle la structure et la composition des produits intermédiaires sont figées par réticulation, les différentes opérations sont conduites à une température à laquelle le liant est, au plan chimique, quasiment non évolutif. Ainsi la formulation de la composition des produits est parfaitement reproductible dans la mesure où elle est intégralement effectuée en début de procédé sans nécessiter aucun ajustement ultérieur. L'homme de métier n'est confronté à aucune condition de "vie de pot" et les produits intermédiaires dont les cotes géométriques seraient imparfaites peuvent être recyclés dans la fabrication.Compared to the known methods of the prior art, the major originality of the process according to the invention lies in the fact that with the exception of the final phase during which the structure and composition of intermediate products are fixed by crosslinking, the different operations are carried out at a temperature at which the binder is, chemically, almost non-scalable. So the formulation of the product composition is perfectly reproducible insofar as it is fully carried out in start of the process without requiring any adjustment ulterior. The skilled person is not confronted with any condition of "pot life" and intermediate products whose geometric dimensions are imperfect can be recycled in manufacturing.
Il faut enfin observer que grâce à l'emploi de charges épaississantes solides qui donnent au liant liquide non évolutif une tenue mécanique suffisante, aucun plastifiant n'est nécessaire dans le cadre du présent procédé qui permet ainsi d'obtenir des produits pyrotechniques de très hautes performances.Finally, it should be noted that thanks to the use of solid thickening fillers which give the binder non-evolving liquid sufficient mechanical strength, no plasticizer is required for the present process which thus makes it possible to obtain products very high performance pyrotechnics.
On peut également dire que contrairement aux procédés antérieurs qui utilisent un liant thermodurcissable évolutif en cours de procédé dont on cherche à abaisser la viscosité par l'emploi d'un solvant et/ou d'un plastifiant, le procédé selon l'invention utilise un liant thermodurcissable liquide non évolutif en cours de procédé dont on élève la viscosité apparente par emploi de charges épaississantes.We can also say that unlike previous processes which use a binder thermosetting scalable during the process of which seeks to lower viscosity by using a solvent and / or a plasticizer, the process according to the invention uses a liquid thermosetting binder non-evolving during the process of which the apparent viscosity by use of fillers thickeners.
Selon une première variante préférée de l'invention ladite charge épaississante solide est constituée par un matériau poreux dont la granulométrie est comprise entre 0,1 et 10 µm (microns) et dont la surface spécifique est comprise entre 60 et 500 m2/g.According to a first preferred variant of the invention, said solid thickening filler consists of a porous material whose particle size is between 0.1 and 10 μm (microns) and whose specific surface is between 60 and 500 m 2 / g .
Avantageusement ce matériau possédera également des propriétés modificatrices de combustion et sera choisi dans le groupe constitué par le noir de carbone, la silice colloïdale, l'alumine, l'oxyde de titane ou le polynorbornène.Advantageously, this material will also have combustion modifying properties and will be chosen in the group consisting of carbon black, the colloidal silica, alumina, titanium oxide or polynorbornene.
Selon cette première variante le rapport pondéral entre ladite charge épaississante et ledit liant réticulable est compris entre 0,05 et 0,25.According to this first variant, the weight ratio between said thickening filler and said binder crosslinkable is between 0.05 and 0.25.
Selon une seconde variante préférée de l'invention ladite charge épaississante solide est constituée par un polymère thermoplastique à motifs hydrocarbonés pouvant comporter, en plus des atomes de carbone et d'hydrogène, des atomes d'oxygène et d'azote et dont la masse moléculaire moyenne en poids est comprise entre 3x105 et 3x106.According to a second preferred variant of the invention, said solid thickening filler is constituted by a thermoplastic polymer with hydrocarbon units which may contain, in addition to carbon and hydrogen atoms, oxygen and nitrogen atoms and whose molecular mass weight average is between 3x10 5 and 3x10 6 .
Un premier groupe de polymères thermoplastiques utilisables comme charge épaississante solide dans le cadre de la présente invention est ainsi constitué par les copolymères styrène/butadiène/styrène, styrène/isoprène/styrène, styrène/éthylène/butylène/styrène et styrène/éthylène/propylène.A first group of thermoplastic polymers usable as solid thickening filler in the framework of the present invention is thus constituted by styrene / butadiene / styrene, styrene / isoprene / styrene copolymers, styrene / ethylene / butylene / styrene and styrene / ethylene / propylene.
Un second groupe de polymères thermoplastiques utilisables comme charges épaississantes solides dans le cadre de la présente invention est constitué par les polyuréthannes à motifs polyéthers et polycarbonates et par les copolymères blocs polyéthers/polyamides.A second group of thermoplastic polymers usable as solid thickening fillers in the framework of the present invention is constituted by the polyurethanes with polyether and polycarbonate patterns and by polyether / polyamide block copolymers.
Selon cette seconde variante le rapport pondéral entre ladite charge épaississante et ledit liant réticulable est compris entre 10:90 et 50:50.According to this second variant, the weight ratio between said thickening filler and said binder crosslinkable is between 10:90 and 50:50.
En plus des charges énergétiques oxydantes solides on pourra également incorporer au pré-mélange, constitué par le liant liquide et lesdites charges épaississantes, au moins une charge énergétique réductrice solide comme, par exemple, de l'aluminium ou du bore en poudre.In addition to solid oxidizing energy charges we can also incorporate into the premix, consisting by the liquid binder and said thickening fillers, at least one solid reducing energy charge like, for example, aluminum or boron powder.
Ce n'est que lorsque les opérations de mélange et de mise en forme des produits intermédiaires sont terminées et sont jugées satisfaisantes que l'on fait évoluer le liant en provoquant sa réticulation par chauffage à une température supérieure à 40°C de manière à obtenir des produits terminés réticulés.Only when the mixing and form of intermediate products are completed and are deemed satisfactory that we do evolve the binder by causing it to crosslink by heating at a temperature above 40 ° C so to obtain finished crosslinked products.
Le procédé selon l'invention permet ainsi d'obtenir en continu, sans contrainte de temps liée à des questions de "vie de pot" et sans emploi de solvants ou de plastifiants indésirables au plan énergétique, des produits pyrotechniques composites à liant réticulé. Ces produits trouvent leurs applications préférentielles comme poudres propulsives en brins ou en sticks pour les munitions destinées aux armes à tube, comme blocs de propergols pour les moteurs de roquettes et de fusées, comme chargements explosifs pour les munitions explosives ou encore comme chargements pyrotechniques pour les générateurs de gaz destinés aussi bien aux applications militaires qu'aux applications civiles comme la sécurité automobile. The method according to the invention thus makes it possible to obtain continuously, without time constraints linked to "pot life" issues and no use of solvents or energy-unwanted plasticizers, Composite pyrotechnic products with crosslinked binder. These products find their preferred applications as propellant powders in strands or in sticks for ammunition intended for the weapons with tube, like blocks of propellants for rocket and rocket engines, as explosive charges for ammunition explosives or as pyrotechnic charges for gas generators intended for both military applications than civil applications like automotive safety.
L'invention concerne également une installation convenant particulièrement bien à la mise en oeuvre du procédé selon l'invention.The invention also relates to an installation particularly suitable for the implementation of method according to the invention.
Cette installation est caractérisée en ce qu'elle
comprend dans le sens de progression de la matière :
On donne ci-après une description détaillée de la mise en oeuvre préférée du procédé selon l'invention en se référant à la figure 1 qui représente, de manière schématique, l'installation préférée présentée ci-dessus. La figure 2 représente, pour des raisons de clarté, une vue de dessus simplifiée du laminoir à cisaillement utilisé.A detailed description of the preferred implementation of the method according to the invention in referring to Figure 1 which shows, so schematic, the preferred installation presented above. Figure 2 shows, for reasons of clarity, a simplified top view of the rolling mill shear used.
L'invention consiste donc à mélanger, à température ambiante les constituants de départ d'une composition pyrotechnique composite réticulable jusqu'à obtention d'une pâte composite homogène présentant une viscosité suffisante pour pouvoir, toujours à température ambiante, être mise sous forme de produits intermédiaires présentant déjà, de manière stable, la forme et les dimensions finales du produit terminé que l'on veut obtenir. La forme et la composition de ces produits intermédiaires sont alors figés par réticulation à chaud de manière à obtenir les produits terminés voulus.The invention therefore consists in mixing, at temperature ambient the starting constituents of a composition composite pyrotechnic crosslinkable until obtained a homogeneous composite paste with a viscosity sufficient to be able, always at temperature ambient, be in the form of products intermediaries who already have a stable shape and final dimensions of the finished product that we want to get. The form and composition of these intermediate products are then frozen by hot crosslinking so as to obtain the products desired completions.
Pour ce faire on commence, comme représenté à la figure 1 par fabriquer dans un mélangeur à bras multiples 1 un pré-mélange 2 constitué principalement par le liant 3 thermodurcissable à l'état liquide et par des charges solides épaississantes 4. To do this we start, as shown in figure 1 by manufacturing in an arm mixer multiples 1 a premix 2 consisting mainly by the binder 3 thermosetting in the liquid state and by thickening solid fillers 4.
Il est impératif dans le cadre de la présente invention que le liant thermodurcissable soit liquide à température ambiante et que sa réticulation ne puisse commencer qu'à une température supérieure à 40°C de manière à être certain que, tant que l'on restera à une température ambiante inférieure à 40°C, ce liant demeurera non évolutif au plan chimique.It is imperative in the context of this invention that the thermosetting binder is liquid to room temperature and that its crosslinking cannot start only at a temperature above 40 ° C so as to be certain that as long as we stay at one ambient temperature below 40 ° C, this binder will remain chemically non-evolving.
On entend dans la présente description par "liant liquide" l'ensemble des constituants réactifs liquides qui, après réticulation, donneront le liant réticulé solide.In the present description is meant by "binder liquid "all of the liquid reactive constituents which, after crosslinking, will give the crosslinked binder solid.
La réaction de réticulation peut être du type réaction de polycondensation, auquel cas les liants seront notamment du type polyuréthannes, polyesters ou polyamides.The crosslinking reaction can be of the type polycondensation reaction, in which case the binders will in particular be of the polyurethane, polyesters or polyamides.
La réaction de réticulation peut être du type réaction de polyaddition avec ouverture d'insaturations éthyléniques, auquel cas les liants seront notamment du type polyalkylènes, polyacrylates ou polyméthacrylates. Dans ce dernier cas la composition devra contenir des catalyseurs de réticulation, comme par exemple des peroxydes.The crosslinking reaction can be of the type polyaddition reaction with opening of unsaturations ethylenic, in which case the binders will in particular be polyalkylenes, polyacrylates or polymethacrylates. In the latter case, the composition must contain crosslinking catalysts, such as for example peroxides.
Comme il a déjà été indiqué plus haut dans la description, lesdites charges épaississantes peuvent être constituées par des matériaux solides poreux de faible granulométrie. Dans ce cas on utilisera avantageusement comme charges épaississantes certains additifs employés habituellement comme modificateurs de combustion comme le noir de carbone ; le procédé selon l'invention offre dans ce cas l'avantage de permettre l'obtention en continu de compositions pyrotechniques déjà connues mais qui n'étaient accessibles que par des procédés discontinus. As already indicated above in the description, said thickening fillers can be made of porous solid materials of small particle size. In this case we will use advantageously as thickening fillers certain additives usually used as modifiers of combustion like carbon black; the process according to the invention in this case offers the advantage of allowing continuously obtaining pyrotechnic compositions already known but which were only accessible by discontinuous processes.
Les dites charges épaississantes peuvent également être constituées par des polymères thermoplastiques solides de haute masse moléculaire de manière à obtenir un produit final dont le liant est constitué par un alliage de polymères thermoplastiques et de polymères réticulés. Ce type d'alliages permet l'obtention de produits composites présentant des caractéristiques mécaniques particulièrement élevées.Said thickening fillers can also be made up of thermoplastic polymers high molecular weight solids so as to get a final product whose binder consists of a alloy of thermoplastic polymers and polymers cross-linked. This type of alloy allows obtaining composite products with characteristics particularly high mechanical properties.
Le pré-mélange 2 ainsi constitué pourra également contenir d'autres additifs de la composition finale. Il devra avoir la consistance d'une graisse épaisse de manière à pouvoir être transporté en continu au moyen d'une pompe volumétrique tout en adhérant, sans couler, à la surface d'un cylindre tournant avec une vitesse angulaire de quelques dizaines de tours par minute.The premix 2 thus formed may also contain other additives of the final composition. he should have the consistency of a thick fat of so that it can be transported continuously using a positive displacement pump while adhering, without sinking, on the surface of a cylinder rotating with a speed angular of a few tens of revolutions per minute.
Ce pré-mélange est donc transporté au moyen d'une
pompe de circulation 34, par exemple une pompe à
engrenage, dans une réserve 35 munie d'un couvercle-piston
36. Le pré-mélange est alors repris par une pompe
doseuse 5 à engrenage pour être conduit, dans un
appareillage où seront effectuées les opérations de
mélange avec les charges énergétiques solides et de mise
en forme de la pâte composite ainsi obtenue sous forme
de produits intermédiaires possédant déjà les cotes
géométriques des produits terminés. Ces deux opérations
peuvent être effectuées dans un appareillage unique
comme par exemple une extrudeuse bi-vis dont la tête
d'extrusion sera associée à un dispositif de découpage.
Mais, préférentiellement, ces deux opérations seront
effectuées par deux appareillages distincts placés l'un
à la suite de l'autre. This premix is therefore transported by means of a
Le pré-mélange 2 est transporté par la pompe 5 dans
un mélangeur qui peut être un mélangeur traditionnel
comme un co-malaxeur "BUSS" mais qui, préférentiellement
et comme représenté à la figure 1, est un laminoir à
cisaillement 6 constitué par deux rouleaux cylindriques
7 et 8 de longueur identique et portant des rainures
hélicoïdales. Les axes 9 et 10 de ces deux cylindres
sont parallèles et situés dans un même plan horizontal
en étant espacés de manière à laisser une fente 11 entre
les deux rouleaux. Les axes 9 et 10 sont supportés par
des blocs supports 12 et 13, le bloc 12 étant un bloc
moteur entraínant en rotation les deux cylindres 7 et 8
qui tournent en sens contraire l'un de l'autre à des
vitesses différentes. Un tel laminoir à cisaillement est
connu de l'homme de métier et décrit dans de nombreuses
publications, par exemple dans la demande de brevet
FR-A-2 723 086 déjà citée.The premix 2 is transported by the
La pompe 5 amène ainsi le pré-mélange 2 sur le
rouleau 7 qui tourne le plus vite, le pré-mélange
formant sur ce rouleau une feuille qui enrobe ce
dernier. Le pré-mélange est amené à l'extrémité 14
d'entrée de matière du laminoir 6.The
Au moins une trémie doseuse 16 déverse, entre
l'extrémité d'entrée de matière 14 et l'extrémité de
sortie de matière 15 du laminoir 6, les charges
énergétiques solides 17 sur la feuille de pré-mélange
enrobant le rouleau 7. Ces charges énergétiques solides
sont alors intimement mélangées au pré-mélange 2 grâce à
l'action de cisaillement du laminoir 6 de manière à
former sur le rouleau 7 une feuille de pâte composite
homogène qui présente déjà une viscosité suffisante pour
pouvoir conserver des cotes géométriques stables. At least one
Les charges énergétiques solides seront principalement constituées par les charges oxydantes de la composition qui peuvent être des charges minérales comme par exemple le perchlorate d'ammonium, le perchlorate de potassium ou le nitrate d'ammonium, ou des charges organiques et notamment des nitramines comme l'hexogène, l'octogène, la nitroguanidine ou l'hexanitro-hexaazaisowurtzitane.Solid energy charges will mainly constituted by the oxidizing charges of the composition which can be mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate, or organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.
A côté des charges oxydantes solides, il pourra y avoir des charges énergétiques réductrices solides comme l'aluminium ou le bore et même des additifs solides qui n'auraient pas été incorporés au pré-mélange 2.Besides solid oxidizing charges, there may have solid reducing energy charges like aluminum or boron and even solid additives which would not have been incorporated into premix 2.
Dans ce cas les différentes charges pourront être apportées soit en mélange par une trémie unique, soit séparément par une succession de trémies.In this case the different charges may be brought either in mixture by a single hopper, or separately by a succession of hoppers.
La feuille de pâte composite ainsi obtenue est
récupérée sous forme de granulés 19 par un dispositif de
granulation 18 situé à l'extrémité de sortie 15 du
laminoir 6. Préférentiellement comme représenté sur la
figure 1, les extrémités de sortie des rouleaux 7 et 8
ne sont pas rainurées mais sont lisses.The composite dough sheet thus obtained is
recovered in the form of
Les granulés 19 sont alors repris en continu dans
une extrudeuse 20, par exemple une extrudeuse à deux
vis, munie d'une tête d'extrusion 21 pour être profilés
en joncs 23 entraínés par un tapis roulant 25.The
Un dispositif de découpage 22 découpe les joncs
profilés 23 sortant de la tête d'extrusion 21 en
produits intermédiaires 24 possédant déjà les cotes
définitives des produits terminés. Le dispositif de
découpage 22 a un déplacement asservi à la vitesse de
progression du tapis 25 sur lequel reposent les joncs
23.A cutting
Il est à observer que jusqu'à cette opération de
découpage, aucun chauffage de la composition
pyrotechnique n'a eu lieu, l'extrudeuse 20 pouvant même
être refroidie. Le liant de la composition pyrotechnique
n'a donc pas évolué et les produits intermédiaires 24
peuvent, s'il sont jugés non satisfaisants, être
recyclés dans le circuit de fabrication.It should be noted that until this operation of
cutting, no heating of the composition
pyrotechnic did not take place, the
Ces produits intermédiaires 24, lorsqu'ils sont
jugés satisfaisants, sont alors repris en continu par le
tapis roulant 25 qui assure leur transport et leur
passage dans un four thermique 26 où leur forme
géométrique et leur composition sont définitivement
figées par réticulation de leur liant, à une température
supérieure à 40°C. Avec les compositions usuelles
connues de l'homme de métier la réticulation sera
souvent effectuée à une température voisine de 120°C
pendant environ 5 minutes.These
Les produits terminés 27 sortant du four 26 peuvent
alors être conditionnés dans leur emballage 28.The
Le procédé selon l'invention permet ainsi de fabriquer en séries continues des produits pyrotechniques composites à liant réticulé, et notamment des produits de petites dimensions, sans contrainte de "vie de pot", sans solvant et sans plastifiant indésirable.The method according to the invention thus makes it possible to manufacture in continuous series of products composite pyrotechnics with crosslinked binder, and in particular products of small dimensions, without constraint of "pot life", solvent-free and plasticizer-free undesirable.
Les exemples qui suivent illustrent certaines possibilités de mise en oeuvre de l'invention.The following examples illustrate some possibilities of implementing the invention.
Dans ces exemples, on a utilisé les abréviations suivantes :
- PBHT =
- liant à base de polybutadiène à terminaisons hydroxyles réticulé par un polyisocyanate.
- PAG =
- liant à base de polyazoture de glycidyle à terminaisons hydroxyles réticulé par un polyisocyanate
- S.B.S. =
- copolymère styrène/butadiène/styrènes
- S.I.S. =
- copolymère styrène/isoprène/styrène
- PE-PA =
- copolymère bloc polyéther/polyamide 60/40
- RDX =
- hexogène
- PA =
- perchlorate d'ammonium
- PBHT =
- binder based on polybutadiene with hydroxyl endings crosslinked by a polyisocyanate.
- PAG =
- binder based on glycidyl polyazide with hydroxyl endings crosslinked by a polyisocyanate
- SBS =
- styrene / butadiene / styrene copolymer
- SIS =
- styrene / isoprene / styrene copolymer
- PE-PA =
- polyether / polyamide block copolymer 60/40
- RDX =
- hexogenic
- PA =
- ammonium perchlorate
Tous les pourcentages indiqués dans les exemples sont des pourcentages en masse, les pourcentages indiqués pour le liant incluant les additifs éventuels utilisés.All the percentages given in the examples are percentages by mass, the percentages indicated for the binder including any additives used.
On a fabriqué par le procédé continu selon
l'invention des brins de poudre cylindriques
multiperforés à 7 trous et à 19 trous à partir des trois
compositions suivantes :
Pour une température de matière de 35°C lors de
l'extrusion, les géométries suivantes ont été obtenues :
d = diamètre des trous
d = hole diameter
On a fabriqué par le procédé continu selon
l'invention des blocs de propergols cylindriques à canal
central pour moteurs de petits missiles à partir des
trois compositions suivantes :
Sur 10 mètres de propergol extrudé en continu
pour chacune des compositions, les variations
dimensionnelles obtenues après découpage et réticulation
à chaud sont les suivantes :
On a fabriqué par le procédé continu selon l'invention des bandes d'explosif composite d'épaisseur comprise entre 2 et 5mm à partir de la composition suivante :
- liant PBHT = 11%
- charge épaississante = SIS = 4%
- charge oxydante : RDX (3µm et 90µm) =85%
- PBHT binder = 11%
- thickening load = SIS = 4%
- oxidizing charge: RDX (3 µ m and 90 µ m) = 85%
On a extrudé en continu 10 mètres de bande de largeur
90mm avec des épaisseurs de 2,3 et 5mm. Après
réticulation du liant la variation dimensionnelle des
bandes était de :
On a fabriqué par le procédé continu selon l'invention des blocs de propergols pour générateur pyrotechnique de gaz à partir de la composition suivante :
- liant PBHT : 15,8%
- charge épaississante = SBS : 9,2%
- charge oxydante : PA (90µm, 15µm, 3µm) : 73%
- charge réductrice : Al = 2%
- PBHT binder: 15.8%
- thickening filler = SBS: 9.2%
- oxidizing charge: PA (90 µ m, 15 µ m, 3 µ m): 73%
- reducing load: Al = 2%
Les blocs avaient la forme de cylindres pleins de dimensions :
- diamètre : 30mm + 0,025mm
- longueur : 90mm + 0,10mm
- diameter: 30mm + 0.025mm
- length: 90mm + 0.10mm
Ces blocs ont été tirés au banc d'essai et ont donné les résultats suivants :
- vitesse de combustion à 13 MPa = 25,3mm/s
- exposant de pression = 0,35
- combustion speed at 13 MPa = 25.3mm / s
- pressure exponent = 0.35
Claims (11)
- Continuous process for the solventless manufacture of terminated composite pyrotechnic products of which the starting constituents comprise in particular a liquid binder which can be cross-linked at a temperature above 40°C and at least one solid oxidizing energetic charge, the process consisting in particular of:(i) mixing the starting constituents of the said products so as to obtain a homogeneous composite paste with sufficient viscosity to be able to preserve stable geometric dimensions,(ii) putting the paste thus obtained into the form of intermediate products having the geometric dimensions of the said terminated products.(iii) setting the form and composition of the intermediate products thus obtained by cross-linking the binder,
characterized in that :(iv) the said starting liquid binder is first of all mixed with a solid thickening filler in powdered form so as to obtain a premix with a greasy consistency which is then mixed with the said energetic charges,(v) the mixing and forming operations are carried out at a temperature below 40°C. - Process according to claim 1, characterized in that the said solid thickening filler consists of a porous material of which the particle size lies between 0.1 and 10µm and of which the specific area lies between 60 and 500 m2/g.
- Process according to claim 2 characterized in that the said material is chosen from the group consisting of carbon black, colloidal silica, alumina, titanium oxide and polynorbornene.
- Process according to claim 1, characterized in that the said solid thickening filler consists of a thermoplastic polymer with hydrocarbon units which can carry oxygen and nitrogen atoms of which the mean molecular mass by weight lies between 3×105 and 3×106.
- Process according to claim 4 characterized in that the said thickening filler is chosen from the group consisting of styrene/butadiene/styrene, styrene/isoprene/styrene, styrene/ethylene/butylene/styrene, styrene/ethylene/propylene copolymers.
- Process according to claim 4 characterized in that the said thickening filler is chosen from the group consisting of polyurethanes based on polyethers and polycarbonates and of polyether/polyamide block copolymers.
- Process according to claim 4 characterized in that the weight ratio between the said thickening filler and the said cross-linking binder lies between 10:90 and 50:50.
- Process according to claim 2 characterized in that the weight ratio between the said thickening filler and the said cross-linking binder lies between 0.05 and 0.25.
- Process according to claim 1, characterized in that in addition to the said solid oxidizing energetic charges, at least one solid reducing energetic charge is used.
- Process according to claim 9 characterized in that the said reducing energetic charge consists of powdered aluminium or boron.
- Installation for implementing the process according to any one of claims 1 to 10, characterized in that it comprises, in the direction of the progression of the material :(i) a shearing rolling mill (6) consisting of two grooved cylindrical rollers (7,8) with identical length carrying helical grooves and of which the axes are parallel and situated in the same horizontal plane while being spaced so as to leave a slit (11) between the two rollers which rotate in opposite directions to each other,(ii) a volumetric pump (5) which brings the premix (2) consisting of the liquid binder and the thickening filler to the material inlet end (14) of the rolling mill (6),(iii) at least one metering hopper (16) discharging, between the material inlet end (14) and the material outlet end of the rolling mill (6), solid energetic charges (17) onto the rollers of the latter,(iv) a granulating device (18) for the homogeneous paste thus constituted which is situated on the outlet end (15) of the rolling mill,(v) an extruder (20) in which granules coming from the granulating device are taken up,(vi) a device (22) for cutting the extruded beads (23) leaving the extruder into intermediate products (24),(vii) a conveyer belt (25) which ensures the transport and passage of the intermediate products thus cut into a heating oven (26).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9606397 | 1996-05-23 | ||
| FR9606397A FR2749008B1 (en) | 1996-05-23 | 1996-05-23 | CONTINUOUS PROCESS FOR THE SOLVENT-FREE MANUFACTURE OF THERMOSETTING COMPOSITE PYROTECHNICS |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0808813A1 EP0808813A1 (en) | 1997-11-26 |
| EP0808813B1 true EP0808813B1 (en) | 2001-08-22 |
Family
ID=9492385
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP97401051A Expired - Lifetime EP0808813B1 (en) | 1996-05-23 | 1997-05-12 | Continuous process for the solventless production of pyrotechnical products having a thermosetting binder |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US5831339A (en) |
| EP (1) | EP0808813B1 (en) |
| JP (1) | JP3826226B2 (en) |
| CA (1) | CA2204840C (en) |
| DE (1) | DE69706228T2 (en) |
| FR (1) | FR2749008B1 (en) |
| IL (1) | IL120670A (en) |
| NO (1) | NO307084B1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6315930B1 (en) * | 1999-09-24 | 2001-11-13 | Autoliv Asp, Inc. | Method for making a propellant having a relatively low burn rate exponent and high gas yield for use in a vehicle inflator |
| US6736913B1 (en) * | 2000-10-31 | 2004-05-18 | Alliant Techsystems Inc. | Method for processing explosives containing 2,4,6,8,10,12-hexanitro-2,4,6,8,10,12-hexaazatetracyclo [5.5.0.05,903,11]-dodecan (CL-20) with naphthenic and paraffinic oils |
| GB0205559D0 (en) * | 2002-03-11 | 2002-04-24 | Bae Systems Plc | Improvements in and relating to the filling of explosive ordnance |
| RU2218316C1 (en) * | 2002-03-28 | 2003-12-10 | Федеральный центр двойных технологий "Союз" | Method for production of charge of composite solid propellant |
| JP2006044975A (en) * | 2004-08-03 | 2006-02-16 | Ihi Aerospace Co Ltd | Solid propellant |
| US7854811B1 (en) | 2009-07-11 | 2010-12-21 | Kemzecur, Inc. | Mouldable plastic explosives and inert simulants for mouldable plastic explosives |
| CN109704892A (en) * | 2019-03-03 | 2019-05-03 | 浏阳市浏河机械有限公司 | Pyrotechnic composition mixed tide material prilling |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2995432A (en) * | 1958-08-04 | 1961-08-08 | Phillips Petroleum Co | Solid composite rubber base propellants containing reinforcing agent of resinous aldehyde condensate |
| US4776993A (en) * | 1974-05-14 | 1988-10-11 | The United States Of America As Represented By The Secretary Of The Navy | Extrusion method for obtaining high strength composite propellants |
| US4177227A (en) * | 1975-09-10 | 1979-12-04 | The United States Of America As Represented By The Secretary Of The Air Force | Low shear mixing process for the manufacture of solid propellants |
| US4098627A (en) * | 1976-12-15 | 1978-07-04 | The United States Of America As Represented By The Secretary Of The Navy | Solvolytic degradation of pyrotechnic materials containing crosslinked polymers |
| DE3010052C2 (en) * | 1980-03-15 | 1982-09-09 | Friedrich-Ulf 8899 Rettenbach Deisenroth | Process for the production of plastic-bound explosives |
| US4375522A (en) * | 1980-07-21 | 1983-03-01 | The United States Of America As Represented By The Secretary Of The Navy | Thixotropic restrictor, curable at room temperature, for use on solid propellant grains |
| FR2577919B1 (en) * | 1985-02-27 | 1987-02-20 | Poudres & Explosifs Ste Nale | PROCESS FOR THE MANUFACTURE WITHOUT SOLVENT OF COMPOSITE PYROTECHNIC PRODUCTS WITH THERMOSETTING BINDER AND PRODUCTS THUS OBTAINED, IN PARTICULAR COMPOSITE PROPULSIVE POWDERS |
| US4726919A (en) * | 1985-05-06 | 1988-02-23 | Morton Thiokol, Inc. | Method of preparing a non-feathering nitramine propellant |
| US4650617A (en) * | 1985-06-26 | 1987-03-17 | Morton Thiokol Inc. | Solvent-free preparation of gun propellant formulations |
| US4889571A (en) * | 1986-09-02 | 1989-12-26 | Morton Thiokol, Inc. | High-energy compositions having castable thermoplastic binders |
| DE3635296C2 (en) * | 1986-10-16 | 1995-12-21 | Nitrochemie Gmbh | Process for producing propellant powder |
| GB8730153D0 (en) * | 1987-12-24 | 1988-02-03 | Univ Manchester | Polymer compositions |
| SE465572B (en) * | 1989-06-21 | 1991-09-30 | Nobel Kemi Ab | SET AND DEVICE FOR PREPARING EXPLOSIVE SUBSTANCES |
| EP0417912B1 (en) * | 1989-08-25 | 1994-11-09 | Idemitsu Petrochemical Company Limited | Thermoplastic resin-based molding composition |
| US4994212A (en) * | 1990-05-24 | 1991-02-19 | Trw Vehicle Safety Systems Inc. | Process for manufacturing a gas generating material |
| US5486248A (en) * | 1994-05-31 | 1996-01-23 | Morton International, Inc. | Extrudable gas generant for hybrid air bag inflation system |
| FR2723086B1 (en) * | 1994-07-29 | 1996-09-13 | Poudres & Explosifs Ste Nale | CONTINUOUS PROCESS FOR THE SOLVENT-FREE MANUFACTURE OF COMPOSITE PYROTECHNIC PRODUCTS |
-
1996
- 1996-05-23 FR FR9606397A patent/FR2749008B1/en not_active Expired - Fee Related
-
1997
- 1997-04-15 IL IL12067097A patent/IL120670A/en not_active IP Right Cessation
- 1997-04-23 US US08/839,060 patent/US5831339A/en not_active Expired - Lifetime
- 1997-05-08 CA CA002204840A patent/CA2204840C/en not_active Expired - Fee Related
- 1997-05-12 EP EP97401051A patent/EP0808813B1/en not_active Expired - Lifetime
- 1997-05-12 DE DE69706228T patent/DE69706228T2/en not_active Expired - Lifetime
- 1997-05-21 NO NO19972318A patent/NO307084B1/en not_active IP Right Cessation
- 1997-05-23 JP JP15008897A patent/JP3826226B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| NO972318D0 (en) | 1997-05-21 |
| FR2749008A1 (en) | 1997-11-28 |
| NO307084B1 (en) | 2000-02-07 |
| IL120670A (en) | 2000-07-26 |
| DE69706228T2 (en) | 2002-05-16 |
| IL120670A0 (en) | 1997-08-14 |
| NO972318L (en) | 1997-11-24 |
| EP0808813A1 (en) | 1997-11-26 |
| US5831339A (en) | 1998-11-03 |
| MX9703466A (en) | 1997-11-29 |
| JPH1053484A (en) | 1998-02-24 |
| CA2204840A1 (en) | 1997-11-23 |
| JP3826226B2 (en) | 2006-09-27 |
| FR2749008B1 (en) | 1998-06-26 |
| DE69706228D1 (en) | 2001-09-27 |
| CA2204840C (en) | 2002-01-08 |
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