EP0008265A1 - Process for producing propellant plates partially coated with a combustion inhibitor - Google Patents
Process for producing propellant plates partially coated with a combustion inhibitor Download PDFInfo
- Publication number
- EP0008265A1 EP0008265A1 EP79400528A EP79400528A EP0008265A1 EP 0008265 A1 EP0008265 A1 EP 0008265A1 EP 79400528 A EP79400528 A EP 79400528A EP 79400528 A EP79400528 A EP 79400528A EP 0008265 A1 EP0008265 A1 EP 0008265A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- screen
- composition
- combustion inhibitor
- combustion
- powder
- 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
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 66
- 239000003112 inhibitor Substances 0.000 title claims abstract description 56
- 238000000034 method Methods 0.000 title claims abstract description 27
- 239000003380 propellant Substances 0.000 title claims abstract description 16
- 239000000203 mixture Substances 0.000 claims abstract description 50
- 239000000843 powder Substances 0.000 claims abstract description 33
- 239000000463 material Substances 0.000 claims abstract description 12
- 229920005989 resin Polymers 0.000 claims abstract description 12
- 239000011347 resin Substances 0.000 claims abstract description 12
- 238000004519 manufacturing process Methods 0.000 claims abstract description 7
- 229920000728 polyester Polymers 0.000 claims abstract description 4
- 239000003381 stabilizer Substances 0.000 claims abstract description 3
- 238000007650 screen-printing Methods 0.000 claims description 13
- 229920002857 polybutadiene Polymers 0.000 claims description 4
- 229920002050 silicone resin Polymers 0.000 claims description 4
- 239000004721 Polyphenylene oxide Substances 0.000 claims description 3
- 229920000570 polyether Polymers 0.000 claims description 3
- 238000006116 polymerization reaction Methods 0.000 claims description 3
- 229920005749 polyurethane resin Polymers 0.000 claims description 3
- 239000005062 Polybutadiene Substances 0.000 claims description 2
- IQPQWNKOIGAROB-UHFFFAOYSA-N isocyanate group Chemical group [N-]=C=O IQPQWNKOIGAROB-UHFFFAOYSA-N 0.000 claims description 2
- 238000007790 scraping Methods 0.000 claims description 2
- 239000000976 ink Substances 0.000 abstract description 7
- 239000000470 constituent Substances 0.000 abstract description 2
- 230000002401 inhibitory effect Effects 0.000 abstract 2
- 238000012216 screening Methods 0.000 abstract 2
- 230000008021 deposition Effects 0.000 abstract 1
- 239000011230 binding agent Substances 0.000 description 5
- 239000004744 fabric Substances 0.000 description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 229920001296 polysiloxane Polymers 0.000 description 4
- 238000011068 loading method Methods 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910021538 borax Inorganic materials 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000005764 inhibitory process Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000007639 printing Methods 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 239000004328 sodium tetraborate Substances 0.000 description 2
- 235000010339 sodium tetraborate Nutrition 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- WSLDOOZREJYCGB-UHFFFAOYSA-N 1,2-Dichloroethane Chemical group ClCCCl WSLDOOZREJYCGB-UHFFFAOYSA-N 0.000 description 1
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 239000000020 Nitrocellulose Substances 0.000 description 1
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 1
- 239000000006 Nitroglycerin Substances 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- UKLDJPRMSDWDSL-UHFFFAOYSA-L [dibutyl(dodecanoyloxy)stannyl] dodecanoate Chemical compound CCCCCCCCCCCC(=O)O[Sn](CCCC)(CCCC)OC(=O)CCCCCCCCCCC UKLDJPRMSDWDSL-UHFFFAOYSA-L 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- PZIMIYVOZBTARW-UHFFFAOYSA-N centralite Chemical compound C=1C=CC=CC=1N(CC)C(=O)N(CC)C1=CC=CC=C1 PZIMIYVOZBTARW-UHFFFAOYSA-N 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000003431 cross linking reagent Substances 0.000 description 1
- 239000012975 dibutyltin dilaurate Substances 0.000 description 1
- 239000004205 dimethyl polysiloxane Substances 0.000 description 1
- 235000013870 dimethyl polysiloxane Nutrition 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 229960003711 glyceryl trinitrate Drugs 0.000 description 1
- 239000011256 inorganic filler Substances 0.000 description 1
- 229910003475 inorganic filler Inorganic materials 0.000 description 1
- 239000012764 mineral filler Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229920001220 nitrocellulos Polymers 0.000 description 1
- 229920001084 poly(chloroprene) Polymers 0.000 description 1
- 229920000435 poly(dimethylsiloxane) Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- -1 polysiloxane Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 239000011342 resin composition Substances 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 238000003892 spreading Methods 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
- C06B21/0083—Treatment of solid structures, e.g. for coating or impregnating with a modifier
Definitions
- the present invention relates to a method for manufacturing powder plates, partially coated with combustion inhibitor.
- Propellant blocks are known, the outer surface of which is partially coated with a combustion inhibitor material.
- French patent n ° 2 276 555 filed on June 27, 1974 in the name of the Applicant describes for example propellant blocks whose external surface comprises linear protuberances whose summits are coated with a layer of combustion inhibitor. These protrusions define between them notches which reduce the combustion thickness of these blocks.
- the main purpose of the combustion inhibitor applied to the tops of these protrusions is to reduce the initial combustion surface of the propellant block, so that the overpressure generated at the start of combustion is limited, a goal which is also achieved by implementation of the techniques described in French patent n ° 2 299 519 filed on January 31, 1975 in the name of the plaintiff.
- This combustion inhibitor can be applied by coating with a combustion inhibitor resin composition or by dipping in such a resin.
- combustion inhibitor For such a partial coating of combustion inhibitor to be effective, it is necessary that the latter be broken up into a large number of elements of combustion inhibitors of relatively small dimensions, of the order of magnitude of thickness of these plates. As a result, the application of such elements of combustion inhibitors is very difficult, if not impossible, to be carried out by conventional coating or soaking means.
- the object of the present invention is to provide a method making it possible, in a very easy and very rapid manner, to partially inhibit powder plates having in particular a small thickness relative to their other dimensions, such plates being intended for particular to the pyrotechnic loading of weapons with propulsion tube.
- the serigraphic screens used in the printing field are generally prepared from a fine mesh canvas covered by a mask consisting of a photosensitive resin.
- the openings of this mask are obtained by photoengraving. This technique makes it possible to make very small openings whose edges are remarkably sharp.
- the combustion inhibitor composition has a viscosity greater than 5,000 poises, and preferably between 10,000 and 20,000 poises.
- the inhibitor composition is deposited on the powder plate practically without spreading thereon, thus forming combustion inhibitor elements whose contours are perfectly clear. Therefore, during the mass production of such plates, one obtains for each of them a perfect definition of the combustion surface, and therefore, excellent regularity of the combustion surface of these plates.
- the combustion inhibitor composition is produced from an organic binder which can be polymerized by humidity.
- a binder is advantageously chosen from polyurethane resins with polybutadien or polyether chains and silicone resins.
- binders are compatible with the pyrotechnic compositions used for the plates and, on the other hand, have excellent properties as a combustion inhibitor.
- the powder plate 1 constituting the elementary charge of a pyrotechnic charge, for example for projectiles of tube weapons, has a small thickness relative to its other dimensions.
- a powder plate 1 is thus obtained covered by elements 7 of combustion inhibitor material (see Figures 4 and 5).
- the elements 7 of combustion inhibitor material are constituted by identical rectahgles arranged in parallel rows.
- the screen printing screen 3 is itself prepared in the following manner: There is, on a fine mesh fabric 8 made for example of polyester, polyamide or stainless steel, a layer of photosensitive resin 9 of a type known per se. Openings 4 are then made in this photosensitive resin layer 9 by a photoengraving process. This photoengraving is carried out by applying to the photosensitive resin layer 9 a cover comprising openings identical to the openings 4 to be produced and exposing the assembly to light. The exposed parts are then removed by a chemical process known per se.
- composition 5 of combustion inhibitor material Before applying the composition 5 of combustion inhibitor material to the screen printing screen 3, the latter is stretched a few tenths of a millimeter above the surface 2 of the powder plate 1, as indicated in FIG. 1.
- the composition of the combustion inhibitor material 5 used must be sufficiently fluid to be able to easily pass through the meshes of the fabric 8. This composition must also be sufficiently viscous so that it does not spread over the surface 2 of the plate 1 after having passed through the openings 4 and the fabric 8 of the screen printing screen 3.
- the combustion inhibitor composition 5 must have a viscosity greater than 5000 poises, the best results being obtained when this viscosity is between 10,000 and 20,000 poises approximately.
- the composition of the combustion inhibitor material 5 generally comprises a resin constituted by a base binder added with a curing agent.
- This composition comprises, on the other hand, inorganic fillers to ensure the thermal resistance of the inhibitor and to adjust the viscosity of the composition to the values indicated above.
- This composition is essentially distinguished from the inks usually used in screen printing by the fact that it does not contain any solvent making it possible to adjust and maintain the viscosity of the ink before and during the scraping operation, certain solvents being liable to attack the surface of the powder plate 1.
- certain screen printing inks with solvent may be suitable, for example polyester-based inks, provided that at least one of the inks is added to these inks propellant stabilizers, for example 5% ethyl-centralite for double base propellants.
- the base binder of the combustion inhibitor composition 5 is polymerizable with moisture.
- moisture-polymerizable resins there are in particular resins consisting of molecules whose chains terminate in isocyanate groups.
- resins consisting of molecules whose chains terminate in isocyanate groups.
- polyurethane resins with polybutadien or polyether chains are preferred.
- silicone resins it is also possible to use silicone resins.
- this surface is preferably degreased beforehand, for example by means of dichloroethylene.
- the outline of the combustion inhibitor elements 7 thus deposited on the plate 1 is particularly clear, provided that the thickness of the screen printing screen 3 is less than about 0.2 millimeter.
- the nature of the powder constituting the plate 1 is not critical. However, it is preferable that the latter is a homogeneous powder, such as for example a double-base propellant, constituted by a mixture of nitrocellulose, nitroglycerin and additives, this propellant being able to be covered by a thin layer of primer facilitating adhesion. subsequent to the inhibitor or which may be superficially impregnated with a combustion moderator.
- a homogeneous powder such as for example a double-base propellant, constituted by a mixture of nitrocellulose, nitroglycerin and additives, this propellant being able to be covered by a thin layer of primer facilitating adhesion. subsequent to the inhibitor or which may be superficially impregnated with a combustion moderator.
- the number, shape and dimensions of the combustion inhibitor elements 7 applied to the plates 1 is not critical. These parameters depend, in fact, on the application planned for loading, and in particular on the desired modification for the initial combustion surface of these plates.
- the preferred application of the invention is the partial inhibition of the propellant plates for the propellant charges of tube weapons, such as cannons and rocket launchers.
- the propellant plates 1 have a thickness generally less than 2.5 millimeters, and the largest dimension of the combustion inhibitor elements 7 is of the same order of magnitude as the aforementioned thickness. Furthermore, in such an application, there are a large number of these combustion inhibitor elements 7 on the propellant plates 1, distributed regularly, so as to cover more than 50% of the surface 2 of these plates 1. thus significantly reduces the initial combustion surface of these plates 1.
- the screen printing screen being able to be constituted by a multi-perforated sheet of nickel or stainless steel.
- the method according to the invention is applicable to the partial inhibition of powder plates intended for pyrotechnic charges other than those of tube weapons.
Landscapes
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Organic Chemistry (AREA)
- Inks, Pencil-Leads, Or Crayons (AREA)
- Fats And Perfumes (AREA)
- Air Bags (AREA)
Abstract
Description
La présente invention concerne un procédé de fabrication de plaques de poudre, partiellement revêtues d'inhibiteur de combustion.The present invention relates to a method for manufacturing powder plates, partially coated with combustion inhibitor.
On connait des blocs de propergol dont la surface extérieure est revêtue partiellement par un matériau inhibiteur de combustion. Ainsi, le brevet français n°2 276 555 déposé le 27 juin 1974 au nom de la Demanderesse, décrit par exemple des blocs de propergol dont la surface extérieure comporte des protubérances linéaires dont les sommets sont revêtus par une couche d'inhibiteur de combustion. Ces protubérances définissent entre elles des entailles qui diminuent l'épaisseur de combustion de ces blocs.Propellant blocks are known, the outer surface of which is partially coated with a combustion inhibitor material. Thus, French patent n ° 2 276 555 filed on June 27, 1974 in the name of the Applicant, describes for example propellant blocks whose external surface comprises linear protuberances whose summits are coated with a layer of combustion inhibitor. These protrusions define between them notches which reduce the combustion thickness of these blocks.
L'inhibiteur de combustion appliqué sur les sommets de ces protubérances a principalement pour but de diminuer la surface de combustion initiale du bloc de propergol, de sorte qu'on limite la surpression engendrée au début de la combustion, but qui est également atteint par la mise en oeuvre des techniques décrites dans le brevet français n° 2 299 519 déposé le 31 janvier 1975 au nom de la demanderesse.The main purpose of the combustion inhibitor applied to the tops of these protrusions is to reduce the initial combustion surface of the propellant block, so that the overpressure generated at the start of combustion is limited, a goal which is also achieved by implementation of the techniques described in French patent n ° 2 299 519 filed on January 31, 1975 in the name of the plaintiff.
Cet inhibiteur de combustion peut être appliqué par enduction d'une composition de résine inhibitrice de combustion ou encore par trempage dans une telle résine.This combustion inhibitor can be applied by coating with a combustion inhibitor resin composition or by dipping in such a resin.
On connait également des chargements propulsifs constitués par des plaques de poudre d'épaisseur faible relativement aux autres dimensions, destinées notamment à la propulsion des roquettes, et la Demanderesse a découvert que de telles plaques de poudre pouvaient être utilisées au chargement de munitions pour armes à tubes telles que canon à culasse, obusier, canon sans recul et lance-roquette, à la condition que ces plaques de poudre soient revêtues partiellement d'un inhibiteur de combustion.There are also known propellant charges made up of thin powder plates relative to the other dimen sions, intended in particular for propelling rockets, and the Applicant has discovered that such powder plates could be used for loading ammunition for tube weapons such as breech cannon, howitzer, recoilless cannon and rocket launcher, provided that these powder plates are partially coated with a combustion inhibitor.
Pour qu'un tel revêtement partiel d'inhibiteur de combustion soit efficace, il est nécessaire que ce dernier soit morcelé en un grand nombre d'éléments d'inhibiteurs de combustion de dimensions relativement faibles, de l'ordre de grandeur de l'épaisseur de ces plaques. Il en résulte que l'application de tels éléments d'inhibiteurs de combustion est très difficile, voir impossible, à réaliser par les moyens d'enduction ou de trempage classiques.For such a partial coating of combustion inhibitor to be effective, it is necessary that the latter be broken up into a large number of elements of combustion inhibitors of relatively small dimensions, of the order of magnitude of thickness of these plates. As a result, the application of such elements of combustion inhibitors is very difficult, if not impossible, to be carried out by conventional coating or soaking means.
Le but de la présente invention est de fournir un procédé permettant de réaliser, d'une manière très aisée et très rapide, l'inhibage partiel de plaques de poudre présentant notamment une épaisseur faible relativement à leurs autres dimensions, de telles plaques étant destinées en particulier au chargement pyrotechnique d'armes à tube de propulsion.The object of the present invention is to provide a method making it possible, in a very easy and very rapid manner, to partially inhibit powder plates having in particular a small thickness relative to their other dimensions, such plates being intended for particular to the pyrotechnic loading of weapons with propulsion tube.
Suivant l'invention, ce procédé est caractérisé en ce que :
- - on prépare une composition visqueuse de matériau inhibiteur de com-. bustion ;
- - on applique, sur l'une des faces de la plaque de poudre, un écran sérigraphique comportant une série d'ouvertures régulièrement réparties sur cet écran ;
- - on applique sur cet écran la composition visqueuse d'inhibiteur de combustion, et on racle cette composition sur cet écran, après quoi,
- - on retire l'écran pour permettre la polymérisation de la composition d'inhibiteur de combustion déposée sur la plaque de poudre.
- - A viscous composition of com- inhibitor material is prepared. bustion;
- - We apply, on one side of the powder plate, a screen printing screen comprising a series of openings regularly distributed on this screen;
- - the viscous combustion inhibitor composition is applied to this screen, and this composition is scraped on this screen, after which,
- - The screen is removed to allow the polymerization of the combustion inhibitor composition deposited on the powder plate.
Les écrans sérigraphiques utilisés dans le domaine de l'imprimerie sont préparés, généralement, à partir d'une toile à mailles fines recouverte par un masque constitué par une résine photosensible. Les ouvertures de ce masque sont obtenues par photogravure. Cette technique permet de réaliser des ouvertures de très faibles dimensions dont les bords sont remarquablement nets.The serigraphic screens used in the printing field are generally prepared from a fine mesh canvas covered by a mask consisting of a photosensitive resin. The openings of this mask are obtained by photoengraving. This technique makes it possible to make very small openings whose edges are remarkably sharp.
Il est par conséquent possible, grâce au procédé conforme à l'invention, de revêtir partiellement des plaques de poudre par un grand nombre d'éléments en matériau inhibiteur de combustion répartis régulièrement sur la surface de telles plaques.It is therefore possible, thanks to the process according to the invention, to partially coat plates of powder with a large number of elements of combustion inhibitor material distributed regularly over the surface of such plates.
Par ailleurs, un très grand nombre d'opérations de revêtement peuvent être réalisées à partir de l'écran précité, de sorte que le procédé conforme à l'invention est particulièrement adapté à la fabrication en grande série.Furthermore, a very large number of coating operations can be carried out from the aforementioned screen, so that the method according to the invention is particularly suitable for mass production.
Selon une version préférée de l'invention, la composition d'inhibiteur de combustion présente une viscosité supérieure à 5 000 poises, et de préférence, comprise entre 10 000 et 20 000 poises.According to a preferred version of the invention, the combustion inhibitor composition has a viscosity greater than 5,000 poises, and preferably between 10,000 and 20,000 poises.
Dans de telles conditions de viscosité, la composition d'inhibiteur se dépose sur la plaque de poudre pratiquement sans s'y étaler, en formant ainsi des éléments d'inhibiteur de combustion dont les contours sont parfaitement nets. De ce fait, lors de la fabrication en grande série de telles plaques, on obtient pour chacune d'entre elles une parfaite définition de la surface de combustion, et par suite, une excellente régularité de la surface de la combustion de ces plaques.Under such viscosity conditions, the inhibitor composition is deposited on the powder plate practically without spreading thereon, thus forming combustion inhibitor elements whose contours are perfectly clear. Therefore, during the mass production of such plates, one obtains for each of them a perfect definition of the combustion surface, and therefore, excellent regularity of the combustion surface of these plates.
De préférence également, la composition d'inhibiteur de combustion est réalisée à partir d'un liant organique polymérisable à l'humidité. Un tel liant est choisi avantageusement parmi les résines polyuréthanes à chaînes polybutadiènes ou polyéthers et les résines silicones.Preferably also, the combustion inhibitor composition is produced from an organic binder which can be polymerized by humidity. Such a binder is advantageously chosen from polyurethane resins with polybutadien or polyether chains and silicone resins.
Ces liants sont compatibles avec les compositions pyrotechniques utilisées pour les plaques et, d'autre part, présentent d'excellentes propriétés en tant qu'inhibiteur de combustion.These binders are compatible with the pyrotechnic compositions used for the plates and, on the other hand, have excellent properties as a combustion inhibitor.
D'autres particularités et avantages de l'invention apparaitront encore dans la description.Other features and advantages of the invention will appear in the description.
Aux dessins annexés, donnés à titre d'exemples non limitatifs :
- - La figure 1 est une vue en coupe d'une plaque de poudre au dessus de laquelle est disposé un écran sérigraphique,
- - La figure 2 est une vue en plan de l'écran sérigraphique,
- - La figure 3 est une vue analogue à celle de la figure 1, montrant l'application de la composition d'inhibiteur de combustion,
- - La figure 4 est une vue en coupe d'une plaque de poudre, partiellement revêtue par un inhibiteur de combustion,
- - La figure 5 est une vue de dessus de la plaque de poudre représentée sur la figure 4.
- FIG. 1 is a sectional view of a powder plate above which a screen printing screen is arranged,
- FIG. 2 is a plan view of the screen printing screen,
- FIG. 3 is a view similar to that of FIG. 1, showing the application of the combustion inhibitor composition,
- FIG. 4 is a sectional view of a powder plate, partially coated with a combustion inhibitor,
- - Figure 5 is a top view of the powder plate shown in Figure 4.
En référence à la figure 1, la plaque de poudre 1, constituant la charge élémentaire d'un chargement pyrotechnique par exemple pour projectiles d'armes à tube, présente une épaisseur faible relativement à ses autres dimensions.Referring to FIG. 1, the
Pour revêtir cette plaque 1, partiellement par un matériau inhibiteur de combustion, on procède comme suit :
- - on prépare, tout d'abord, une composition visqueuse de matériau inhibiteur de combustion,
- - on positionne au voisinage de la
face 2 de la plaque depoudre 1, un écran sérigraphique 3 comportant une série d'ouvertures 4 régulièrement réparties sur cet écran (voir figures 1 et 2), - - on applique ensuite, sur cet
écran 3, la composition visqueuse 5 d'inhibiteur de combustion et on racle cette composition sur l'écran 3 au moyen d'une raclette 6 (voir figure 3).
- - firstly, a viscous composition of combustion inhibitor material is prepared,
- a
serigraphic screen 3 is positioned near theface 2 of thepowder plate 1, comprising a series ofopenings 4 regularly distributed on this screen (see FIGS. 1 and 2), - - Then, on this
screen 3, theviscous composition 5 of combustion inhibitor is applied and this composition is scraped on thescreen 3 by means of a squeegee 6 (see FIG. 3).
On obtient ainsi une plaque de poudre 1 recouverte par des éléments 7 de matériau inhibiteur de combustion (voir figures 4 et 5). Dans cet exemple, les éléments 7 de matériau inhibiteur de combustion sont consitutués par des rectahgles identiques disposés en files parallèles.A
L'écran sérigraphique 3 est lui-même préparé de la façon suivante : On dispose, sur une toile 8 à mailles fines réalisée par exemple en polyester, polyamide ou en acier inoxydable, une couche de résine photosensible 9 de type connu en soi. On réalise ensuite dans cette couche de résine photosensible 9 des ouvertures 4 par un procédé de photogravure. Cette photogravure est exécutée en appliquant sur la couche de résine photosensible 9 un cache comportant des ouvertures identiques aux ouvertures 4 à réaliser et en exposant l'ensemble à la lumière. Les parties ainsi exposées sont ensuite éliminées par un procédé chimique connu en soi.The
Avant d'appliquer la composition 5 de matériau inhibiteur de combustion sur l'écran sérigraphique 3, ce dernier est tendu à quelques dizièmes de millimètres au dessus de la surface 2 de la plaque de poudre 1, comme indiqué sur la figure 1.Before applying the
La composition du matériau inhibiteur de combustion 5 utilisée doit être suffisamment fluide pour pouvoir traverser facilement les mailles de la toile 8. Cette composition doit aussi être suffisamment visqueuse pour qu'elle ne s'étale pas sur la surface 2 de la plaque 1 après avoir traversé les ouvertures 4 et la toile 8 de l'écran sérigraphique 3. L'expérience a montré, à cet effet, que la composition d'inhibiteur de combustion 5 devait posséder une viscosité supérieure à 5000 poises, les meilleurs résultats étant obtenus lorsque cette viscosité est comprise entre 10 000 et 20 000 poises environ.The composition of the
La composition du matériau inhibiteur de combustion 5 comprend, généralement, une résine constituée par un liant de base additionné d'un agent de durcissement. Cette composition comprend, d'autre part, des charges inorganiques pour assurer la tenue thermique de l'inhibiteur et pour ajuster la viscosité de la composition aux valeurs indiquées ci-dessus.The composition of the
Cette composition se distingue essentiellement des encres utilisées habituellement en sérigraphie par le fait qu'elle ne renferme pas de solvant permettant d'ajuster et de maintenir la viscosité de l'encre avant et pendant l'opération de raclage, certains solvants étant susceptibles d'attaquer la surface de la plaque de poudre 1. Toutefois, il a été constaté que certaines encres sérigraphiques avec solvant peuvent convenir, par exemple les encres à base de polyester, à la conditions d'ajouter à ces encres au moins l'un- des stabilisants du propergol, par exemple 5% d'éthyl-centralite pour les propergols à double base.This composition is essentially distinguished from the inks usually used in screen printing by the fact that it does not contain any solvent making it possible to adjust and maintain the viscosity of the ink before and during the scraping operation, certain solvents being liable to attack the surface of the
De préférence, le liant de base de la composition d'inhibiteur de combustion 5 est polymérisable à l'humidité.Preferably, the base binder of the
De cette façon, si le mélange des constituants de la composition 5 est réalisé en milieu anhydre, la polymérisation se trouve bloquée pendant toute l'opération d'application de la composition sur les plaques 1 et ce, jusqu'à ce que les plaques de poudre 1 recouvertes par les éléments 7 d'inhibiteur de combustion soient placées dans une atmosphère humide. La composition d'inhibiteur de combustion 5 préparée avant son application sur les plaques 1 peut ainsi être utilisée pendant toute la durée du cycle de fabrication en série d'une grande quantité de plaques de poudre 1 partiellement inhibées.In this way, if the constituents of the
Parmi les résines polymérisables à l'humidité, on trouve notamment les résines constituées de molécules dont les chaines se terminent par des groupements isocyanates. Parmi celles-ci, les résines polyuréthanes à chaines polybutadiènes ou polyéthers sont préférées. On peut cependant également utiliser des résines silicones.Among the moisture-polymerizable resins, there are in particular resins consisting of molecules whose chains terminate in isocyanate groups. Among these, polyurethane resins with polybutadien or polyether chains are preferred. However, it is also possible to use silicone resins.
On donne ci-après deux exemples de compositions d'inhibiteur de combustion 5 pouvant être utilisées :
- Exemple 1 : inhibiteur à base de polyuréthane :
- - polybutadiène hydroxytéléchélique : 100 parties en poids
- - dialcool à chaîne courte : 10 parties en poids
- - diisocyanate : 20 parties en poids (le rapport fonctionnel NCO étant voisin de 2) OH
- - agents de réticulation, anti-oxydant et catalyseur
- - charges minérales contenat par exemple 50 parties d'oxyde de fer et de la silice ultrafine.
- Exemple 2 : inhibiteur à base de silicone nécessitant un primaire d'adhésion :
- - résine silicone de base (diméthyl polysiloxane) : 100 parties en poids
- - catalyseur : dibutyle dilaurate d'étain : 0,5 à 10 parties en poids
- - charges : borax à taux d'humidité constant : 0 à 4 parties en poids, silice : 3 à 6% en poids.
- Example 1: polyurethane inhibitor:
- - hydroxytelechelic polybutadiene: 100 parts by weight
- - short chain dialcohol: 10 parts by weight
- - diisocyanate: 20 parts by weight (the NCO functional ratio being close to 2) OH
- - crosslinking agents, antioxidant and catalyst
- - mineral fillers, for example 50 parts of iron oxide and ultrafine silica.
- Example 2: silicone-based inhibitor requiring an adhesion primer:
- - basic silicone resin (dimethyl polysiloxane): 100 parts by weight
- - catalyst: dibutyl tin dilaurate: 0.5 to 10 parts by weight
- - fillers: borax at constant humidity: 0 to 4 parts by weight, silica: 3 to 6% by weight.
Pour faciliter l'accrochage de la composition d'inhibiteur de combustion 4 sur la face 2 de la plaque de poudre 1, cette surface est, de préférence, dégraissée au préalable, par exemple au moyen de dichlo- réthylène.To facilitate the attachment of the
La raclette 6, utilisée pour permettre à la composition d'inhibiteur de combustion 5 de passer par les ouvertures 4 de l'écran sérigraphique 3, puis par les mailles de la toile 3, ne doit pas adhérer à la composition 5. A cet effet, il est avantageux d'-utiliser une reclette 6 en néoprène,The
On voit, sur la figure 3, que le passage de la raclette 6 permet d'appliquer la toile 8 sur la surface 2 de la plaque 1. Ce contact a pour effet d'imprimer sur la surface 2 de la plaque 1 les éléments 7 d'inhibiteur de combustion, comme indiqué sur les figures 4 et 5.It can be seen in FIG. 3 that the passage of the
Le contour des éléments 7 d'inhibiteur de combustion ainsi déposés sur la plaque 1 est particulièrement net, à condition que l'épaisseur de l'écran sérigraphique 3 soit inférieure à 0,2 millimètre environ.The outline of the
La nature de la poudre constituant la plaque 1 n'est pas critique. Il est préférable cependant que cette dernière soit une poudre homogène, comme par exemple un propergol double-base, constitué par un mélange de nitrocellulose, de nitroglycérine et d'additifs, ce propergol pouvant être recouvert par une fine couche de primaire facilitant l'adhésion ultérieure de l'inhibiteur ou pouvant âtre imprégnée superficiellement par un modérateur de combustion.The nature of the powder constituting the
De la description précitée du procédé conforme à l'invention, il ressort que ce procédé est particulièrement bien adapté à la production en grande série de chargements pyrotechniques en plaques partiellement revêtues d'inhibiteur de combustion.From the above description of the process according to the invention, it appears that this process is particularly well suited to the mass production of pyrotechnic charges in plates partially coated with combustion inhibitor.
Le nombre, la forme et les dimensions des éléments 7 d'inhibiteur de combustion appliqués sur les plaques 1 n'est pas critique. Ces paramètres dépendent, en effet, de l'application prévue pour le chargement, et notamment de la modification désirée pour la surface de combustion initiale de ces plaques.The number, shape and dimensions of the
L'application préférée de l'invention est l'inhibage partiel des plaques de propergol pour les chargements propulsifs d'armes à tube, telles que canons et lance-roquettes.The preferred application of the invention is the partial inhibition of the propellant plates for the propellant charges of tube weapons, such as cannons and rocket launchers.
Dans une telle application, les plaques de propergol 1 présentent une épaisseur généralement inférieure à 2,5 millimètres, et la plus grande dimension des éléments d'inhibiteur de combustion 7 est du même ordre de grandeur que l'épaisseur précitée. Par ailleurs, dans une telle application, on dispose sur les plaques de propergol 1 un grand nombre de ces éléments inhibiteurs de combustion 7, répartis de façon régulière, de manière à recouvrir plus de 50% de la surface 2 de ces plaques 1. On réduit ainsi notablement la surface de combustion initiale de ces plaques 1.In such an application, the
De cette façon, on diminue d'une façon appréciable la pression maximum des gaz de combustion au début du tir, ce qui permet d'alléger considérablement la construction des tubes de canon, lance-roquette et analogue.In this way, the maximum pressure of the combustion gases is appreciably reduced at the start of the firing, which makes it possible to considerably lighten the construction of the barrel tubes, rocket launcher and the like.
Bien entendu, l'invention n'est pas limitée aux exemples que l'on vient de décrire, et on peut apporter à ceux-ci de nombreuses modifications sans sortir du cadre de l'invention, l'écran sérigraphique pouvant être constitué par une feuille multiperforée de nickel ou d'acier inoxydable.Of course, the invention is not limited to the examples which have just been described, and numerous modifications can be made to them without departing from the scope of the invention, the screen printing screen being able to be constituted by a multi-perforated sheet of nickel or stainless steel.
Ainsi, le procédé conforme à l'invention est applicable à l'inhibage partiel de plaques de poudre destinées à des chargements pyrotechniques autres que ceux des armes à tube.Thus, the method according to the invention is applicable to the partial inhibition of powder plates intended for pyrotechnic charges other than those of tube weapons.
Claims (12)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7823878A FR2433498A1 (en) | 1978-08-16 | 1978-08-16 | PROCESS FOR PRODUCING PARTIALLY COATED POWDER PLATES OF COMBUSTION INHIBITOR |
| FR7823878 | 1978-08-16 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0008265A1 true EP0008265A1 (en) | 1980-02-20 |
| EP0008265B1 EP0008265B1 (en) | 1981-09-23 |
Family
ID=9211832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19790400528 Expired EP0008265B1 (en) | 1978-08-16 | 1979-07-24 | Process for producing propellant plates partially coated with a combustion inhibitor |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0008265B1 (en) |
| DE (1) | DE2960893D1 (en) |
| ES (1) | ES483408A1 (en) |
| FR (1) | FR2433498A1 (en) |
| YU (1) | YU195379A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6666140B2 (en) * | 2001-07-13 | 2003-12-23 | Snpe | Ignition device for pyrotechnic microcharges |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2276555A1 (en) * | 1974-06-27 | 1976-01-23 | Poudres & Explosifs Ste Nale | Propellant charge element - for use in e.g. rockets with combustion-inhibiting coating to ensure uniformly increasing combustion gas pressure |
| FR2299519A1 (en) * | 1975-01-31 | 1976-08-27 | Poudres & Explosifs Ste Nale | Charge of projectile propellant with combustion inhibitor - covering propellant surfaces in part and destroyed after time delay |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2299819A1 (en) * | 1975-02-05 | 1976-09-03 | Int Fishing Corp | Digestible protein from proteinaceous materials, e.g. raw fish - by partial hydrolysis with organic acids after comminution (NO280676) |
-
1978
- 1978-08-16 FR FR7823878A patent/FR2433498A1/en active Granted
-
1979
- 1979-07-24 EP EP19790400528 patent/EP0008265B1/en not_active Expired
- 1979-07-24 DE DE7979400528T patent/DE2960893D1/en not_active Expired
- 1979-08-10 YU YU195379A patent/YU195379A/en unknown
- 1979-08-14 ES ES483408A patent/ES483408A1/en not_active Expired
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2276555A1 (en) * | 1974-06-27 | 1976-01-23 | Poudres & Explosifs Ste Nale | Propellant charge element - for use in e.g. rockets with combustion-inhibiting coating to ensure uniformly increasing combustion gas pressure |
| FR2299519A1 (en) * | 1975-01-31 | 1976-08-27 | Poudres & Explosifs Ste Nale | Charge of projectile propellant with combustion inhibitor - covering propellant surfaces in part and destroyed after time delay |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6666140B2 (en) * | 2001-07-13 | 2003-12-23 | Snpe | Ignition device for pyrotechnic microcharges |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0008265B1 (en) | 1981-09-23 |
| FR2433498B1 (en) | 1982-10-29 |
| DE2960893D1 (en) | 1981-12-10 |
| YU195379A (en) | 1982-08-31 |
| ES483408A1 (en) | 1980-04-16 |
| FR2433498A1 (en) | 1980-03-14 |
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