Cylindrical case for propellant charge powder

The invention refers to a cylindrical sleeve () for receiving propellant powder () with a dimensionally stable jacket wall of combustible, felted fibre material and an insert () of a textile fabric in the jacket wall, and to a method of manufacturing a cylindrical sleeve (). 1645. A cylindrical case () for receiving propellant powder () with a dimensionally stable jacket wall of combustible , felted fibre material and an insert () of a textile fabric in the jacket wall ,characterized in that{'b': '5', 'the insert () is stretchable.'}25. The case according to claim 1 , in which the insert () is of single-layer construction and is expandable both axially and radially.35. The case according to claim 1 , in which the insert () has at least two or three layers claim 1 , of which a first layer is at least axially stretchable and a second layer is at least radially stretchable.45. The case according to claim 1 , in which the insert () consists of knitted fabric.55. The case according to claim 1 , in which the insert () claim 1 , with respect to the thickness of the jacket wall claim 1 , is arranged in the centre of the jacket wall or closer to an inside or an outside of the jacket wall.65. The case according to claim 1 , in which the insert () is arranged on an inside of the jacket wall.756. The case according to claim 1 , in which the insert () is in the form of a hose whose central axis coincides with the central axis of the case ().8. The case according to claim 7 , in which the hose is seamless.96. A method of manufacturing a cylindrical case () according to one of the previous claims claim 7 , comprising:immersing a screen shape in an aqueous pulp containing nitrocellulose and cellulose,applying negative pressure to conform the pulp to the screen shape so that a fleece is formed,pulling a tubular insert onto the screen shape and/or onto the flow formed.10. The method according to claim 9 , whereby the insert is drawn on before applying the negative pressure or as an ...

Insert Made of a Textile Fabric

The disclosure relates to an insert () made of a textile fabric for being received in a jacket wall of a cylindrical case () made of a combustible, felted fibrous material, wherein in particular embodiments the textile fabric includes one, several, or a plurality of yarns which along a longitudinal direction (L) of the insert form a plurality of mesh rows () which each include a plurality of meshes () that extend in a circumferential direction (U) of the insert. 15612. A textile fabric insert () configured for being received in a jacket wall of a cylindrical case () , wherein the case comprises a combustible , felted fibrous material , wherein the textile fabric is a knitwear () comprising a natural fiber yarn and a natural fiber-plastic blended yarn.2. The insert according to claim 1 , wherein the textile fabric includes only one layer.3. The insert according to claim 1 , wherein the natural fiber is cotton.4. The insert according to claim 1 , wherein the natural fiber-plastic blended yarn comprises polyurethane.5. The insert according claim 1 , wherein the natural fiber yarn comprises a proportional yarn content and/or a weight content of 30% to 50% in the textile fabric and/or the natural fiber-plastic blended yarn comprises a proportional yarn content and/or a weight content of 50% to 70% in the textile fabric.6. The insert according to claim 5 , wherein the proportions of natural fiber yarn and natural fiber-plastic blended yarn are 50/50.7. The insert according claim 1 , wherein the natural fiber-plastic blended yarn has a content of natural fiber from 70% to 95% and/or a content of plastic fiber from 5% to 30%.8. The insert according to claim 7 , wherein the proportions of natural fiber to plastic fiber are 89/11.95. The insert according to claim 1 , wherein the textile fabric insert () includes a knitted claim 1 , woven claim 1 , and/or crocheted fabric.105. The insert according to claim 9 , wherein the insert () is formed as a hose.11. The insert according ...

Propellant charge container

The invention relates to a charge container device, said charge container device having a volume suitable to substantially fill a barrel chamber, said charge container device is formed from a substantially rigid and combustible material, wherein said charge container device comprises at least one wall to define a cavity for the retention of at least one cartridge case, said at least one cartridge case comprising an energetic material, wherein said at least one cartridge case is arranged in a stacked formation within said charge container, the charge container device further comprising a base portion and a top portion, wherein the top portion comprises an aperture to allow for expulsion of energy and the base portion comprising an ignition means.

Munition cartridges formed from fibrous slurries - with woven inlay rolled in during felting process

A mfr. of munition mouldings, e.g. cartridge casings or charge containers, consists of rolling fabric inlays into the crude felt during the felting operation. The woven fabric inlays may be rolled through the entire thickness of the crude felt or only into the outer skin or inner skin of the felt. The inlay may be rolled into the entire length or parts of the length. By rolling woven fabric inlays into the felt, additional strength is provided; for example, in the case of a cartridge casing this prevents breaking during rough handling. The method is partic. important where casings contain powdered explosive.

Combustible shell piercing installation of shot for determining leaky places of charge

FIELD: military equipment.SUBSTANCE: invention relates to devices for assembling ammunition, in particular armor-piercing feathered sub-caliber projectiles of a separate loading shot for medium and large caliber cannons. Piercing installation of the combustible shell of the shot to determine the leaky charge places comprises a table, on which there is a cradle for mounting a shot and a piercing device provided with a needle pointed on one side and having a blind hole on the other, communicating with a radial hole located in the bottom of the blind hole. In this case, compressed air is supplied to the blind hole.EFFECT: technical result consists in determining the leakage of the shot sites by piercing the combustion envelope at the location of the excelsior tape.1 cl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 667 992 C1 (51) МПК F42B 5/18 (2006.01) F42B 35/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F42B 5/181 (2018.01); F42B 35/00 (2018.01) (21)(22) Заявка: 2016149899, 03.04.2017 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Акционерное общество "Производственное объединение "Завод имени Серго" (RU) Дата регистрации: 25.09.2018 (56) Список документов, цитированных в отчете о поиске: RU 2320951 C2, 27.03.2008. RU (45) Опубликовано: 25.09.2018 Бюл. № 27 2 6 6 7 9 9 2 R U (54) Установка прокалывания сгорающей оболочки выстрела для определения негерметичных мест заряда (57) Реферат: Изобретение относится к устройствам для и имеющей глухое отверстие с другой, сборки боеприпасов, в частности бронебойных сообщающееся с радиальным отверстием, оперенных подкалиберных снарядо выстрела расположенным в донной части глухого раздельного заряжания для пушек среднего и отверстия. При этом в глухое отверстие большого калибров. Установка прокалывания осуществляется подача сжатого воздуха. сгорающей оболочки выстрела для определения Технический результат заключается в негерметичных ...

Patent JPS4943437B1

PROCESS FOR THE MANUFACTURE OF FUEL OBJECTS BY STAMPING FUEL PAPER DISCS USING A FLEXIBLE PUNCH

CARTRIDGE WITH SOCKET AND ARROW PROJECTILE

Pour assurer que même dans le cas où les projectiles à flèche (3) pénètrent profondément dans la douille (2), on obtienne avec certitude un allumage de la poudre de charge propulsive (10) et une combustion régulière de la charge, l'invention propose de pourvoir la partie arrière (16) du projectile (3) d'un revêtement en masse d'allumage (17) et de rapprocher le détonateur (7) ou le tube d'allumage (9), rempli de la masse d'allumage, à l'arrière, tout contre le projectile à flèche (3), de manière que la flamme d'allumage enflamme directement la masse d'allumage (17) placée sur le projectile à flèche (3). To ensure that even in the event that the arrow projectiles (3) penetrate deeply into the casing (2), ignition of the propellant charge powder (10) and even combustion of the charge is obtained with certainty, the invention proposes to provide the rear part (16) of the projectile (3) with an ignition mass coating (17) and to bring the detonator (7) or the ignition tube (9), filled with the mass of ignition, at the rear, directly against the arrow projectile (3), so that the ignition flame directly ignites the ignition mass (17) placed on the arrow projectile (3).

Large calibre ammunition loaded from the rear

Non-cartridge explosive mixture - contg nitrocellulose and a high energy cpd

COMBUSTIBLE OBJECTS IN THE FORM OF A BORGNE CASE

POCKET SOCKET FOR PROPULSIVE LOAD.

IGNITION TUBE FOR ARTILLERY AMMUNITION

L'invention a pour objet un tube allumeur (1), notamment pour un chargement propulsif (4) d'une munition d'artillerie (2). Le tube allumeur (1) est constitué d'un corps tubulaire (8) recevant une composition d'allumage (14). Il est caractérisé en ce que le corps tubulaire (8) comporte au moins une surface réceptrice orientée de façon à recevoir la pression des gaz de propulsion engendrés lors de la mise à feu du chargement propulsif (4), gaz assurant ainsi l'entraînement du tube allumeur (1).La surface réceptrice de pression est un disque (20) disposé sensiblement radialement au corps tubulaire (8). The invention relates to an igniter tube (1), in particular for a propellant charge (4) of an artillery ammunition (2). The igniter tube (1) consists of a tubular body (8) receiving an ignition composition (14). It is characterized in that the tubular body (8) comprises at least one receiving surface oriented so as to receive the pressure of the propellant gases generated during the firing of the propellant charge (4), gas thus ensuring the entrainment of the igniter tube (1). The pressure receiving surface is a disc (20) disposed substantially radially to the tubular body (8).

PROCESS FOR MANUFACTURING COMBUSTIBLE OBJECTS BY STAMPING COMBUSTIBLE PAPER AND COMBUSTIBLE OBJECTS THUS OBTAINED

PROCEDE DE FABRICATION D'OBJETS COMBUSTIBLES PAR EMBOUTISSAGE DE PAPIER COMBUSTIBLE ET OBJETS COMBUSTIBLES AINSI OBTENUS. L'INVENTION CONCERNE UN PROCEDE DE FABRICATION D'OBJETS COMBUSTIBLES DE REVOLUTION EN FORME DE CUVETTE A CONTOURS EXTERIEURS CIRCULAIRES A PARTIR DE PAPIER COMBUSTIBLE CONTENANT DE LA NITROCELLULOSE PAR EMBOUTISSAGE D'AU MOINS UN DISQUE 11 DE PAPIER COMBUSTIBLE COMPORTANT UNE PARTIE CENTRALE 12 ET UNE PARTIE PERIPHERIQUE CONSTITUEE PAR UNE PLURALITE DE PORTIONS 13 SEPAREES ENTRE ELLES PAR DES FENTES RADIALES 14 DONT LA LONGUEUR "L" EST INFERIEURE AU RAYON "R" DUDIT DISQUE 11 ET DONT LA LARGEUR "E" EST AU MOINS EGALE A LA LARGEUR MINIMALE NECESSAIRE POUR EVITER LE RECOUVREMENT DESDITES PORTIONS 13 LORS DE LA DEFORMATION DU DISQUE 11 PAR EMBOUTISSAGE. L'INVENTION CONCERNE EGALEMENT LES OBJETS COMBUSTIBLES DE REVOLUTION EN FORME DE CUVETTE A CONTOURS EXTERIEURS CIRCULAIRES CONSTITUES PAR AU MOINS UNE FEUILLE DE PAPIER COMBUSTIBLE CONTENANT DE LA NITROCELLULOSE ET NOTAMMENT CEUX OBTENUS PAR LE PROCEDE SELON L'INVENTION. CES OBJETS TROUVENT LEUR APPLICATION ESSENTIELLE COMME PIECES POUR DOUILLES COMBUSTIBLES ET NOTAMMENT COMME FONDS COMBUSTIBLES OU COMME COUVERCLES COMBUSTIBLES. METHOD OF MANUFACTURING COMBUSTIBLE OBJECTS BY STAMPING OF COMBUSTIBLE PAPER AND COMBUSTIBLE OBJECTS THUS OBTAINED. THE INVENTION RELATES TO A PROCESS FOR MANUFACTURING REVOLUTIONARY COMBUSTIBLE OBJECTS IN THE FORM OF A CUP WITH CIRCULAR OUTER CONTOURS FROM COMBUSTIBLE PAPER CONTAINING NITROCELLULOSE BY STAMPING AT LEAST ONE DISC 11 OF PAPER 12 AND BY A COMBUSTIBLE UNIT 12. PERIPHERAL PART CONSTITUTED BY A PLURALITY OF PORTIONS 13 SEPARATED BETWEEN THEM BY RADIAL SLOTS 14 WHOSE LENGTH "L" IS LESS THAN RADIUS "R" OF SAID DISC 11 AND WHOSE WIDTH "E" IS AT LEAST EQUAL TO THE MINIMUM WIDTH NECESSARY FOR AVOID COVERING THE SAID PORTIONS 13 WHEN THE DISC 11 IS DEFORMED BY STAMPING. THE INVENTION ALSO CONCERNS ...

IGNITION DEVICE FOR PROPULSIVE CHARGING

Fuel case for ammunition

L’invention a pour objet une douille (1) combustible pour munition, douille comprenant une enveloppe cylindrique (2) destinée à renfermer une charge propulsive et à recevoir un projectile au niveau d’une extrémité avant (AV). Cette douille comporte au niveau d’une extrémité arrière (AR) un fond (3) réalisé de façon monobloc avec l’enveloppe cylindrique (2) et qui est destiné à se positionner dans un culot. Cette douille est caractérisée en ce que le fond (3) comporte un anneau central (5) combustible qui est relié à une cuvette (4) périphérique par au moins deux bras (6) radiaux combustibles délimitant des ouvertures (7). Figure à publier avec l’abrégé : Fig. 1 The subject of the invention is a fuel casing (1) for ammunition, said casing comprising a cylindrical casing (2) intended to contain a propellant charge and to receive a projectile at a front end (AV). This sleeve comprises at a rear end (AR) a bottom (3) made in one piece with the cylindrical casing (2) and which is intended to be positioned in a base. This casing is characterized in that the bottom (3) comprises a central combustible ring (5) which is connected to a peripheral bowl (4) by at least two combustible radial arms (6) delimiting openings (7). Figure to be published with abstract: Fig. 1

MUNITION WITHOUT SLEEVE AND METHOD FOR MOUNTING SUCH AMMUNITION

MUNITION OF BIG SIZE CHARGED BY THE BACK

L'invention concerne une munition de gros calibre constituée d'un projectile fixé à une jupe combustible (2) fermée par un culot (4), un dôme de liaison (3) étant prévu entre la jupe et le culot.Le dôme de liaison (3) comporte une première paroi latérale coopérant avec la jupe et une seconde paroi latérale prolongeant la première et coopérant avec le culot (4) et ce dôme comprend des moyens (10) assurant sa liaison avec la jupe (2) lorsqu'ils sont rabattus par le culot (4) sur la paroi latérale de la jupe combustible.Application aux munitions chargeables par l'arrière. The invention relates to a large caliber munition consisting of a projectile attached to a combustible skirt (2) closed by a base (4), a connecting dome (3) being provided between the skirt and the base. (3) has a first lateral wall cooperating with the skirt and a second side wall extending the first and cooperating with the base (4) and this dome comprises means (10) ensuring its connection with the skirt (2) when they are folded by the base (4) on the side wall of the combustible skirt.Application to munitions loadable from the rear.

AMMUNITION WITHOUT SOCKET AND METHOD FOR MOUNTING SUCH AMMUNITION

L'invention a pour objet une munition (1) comprenant un projectile (2), un chargement propulsif (3) et un dispositif (5) d'allumage de ce dernier, dispositif qui est solidaire d'un culot d'étanchéité (6).Cette munition est caractérisée en ce que le chargement propulsif (3) comprend au moins un bloc (4) de charge agglomérée qui est recouvert d'une gaine de protection (7), le culot d'étanchéité (6) étant par ailleurs rendu solidaire d'une partie arrière (2b) du projectile (2) par un moyen de liaison (12). The subject of the invention is a munition (1) comprising a projectile (2), a propellant charge (3) and a device (5) for igniting the latter, a device which is integral with a sealing base (6 This ammunition is characterized in that the propellant charge (3) comprises at least one block (4) of agglomerated charge which is covered with a protective sheath (7), the sealing base (6) being moreover made integral with a rear part (2b) of the projectile (2) by a connecting means (12).

Improvements to mortar cartridges

BODIES OF FUEL OR SEMI-FUEL SOCKETS CONSISTING OF A PLURALITY OF FUEL PAPER STRIPS AND THEIR MANUFACTURING METHOD

Aqueous polyurethane dispersion useful as precursor of protective coating against heat aggressions, preferably heat initiation, comprises refractory fillers

Aqueous polyurethane dispersion comprises refractory fillers. Independent claims are included for: (1) a protective coating against heat aggression, preferably heat initiation, resulting from application of the aqueous polyurethane dispersion; (2) a coated combustible object with a protective coating against heat aggression, preferably heat initiation; and (3) a process of treating the combustible object comprising the application of at least a layer of aqueous polyurethane dispersion to its surface.

ENOUGH MUNITION, CONSISTING OF A PROJECTILE PROVIDED WITH STABILIZER LOADING AND A SOCKET CONTAINING THE PROPULSIVE LOAD AND AT LEAST PARTIALLY COMBUSTIBLE

LA MUNITION COMPORTE UN ELEMENT DE SOUTIEN MONTE ENTRE UNE PARTIE ARRIERE DU PROJECTILE QUI PENETRE A L'INTERIEUR DE LA DOUILLE ET LA DOUILLE. L'ELEMENT DE SOUTIEN 40 S'ETEND ENTRE LA PARTIE ARRIERE 10 DU PROJECTILE ET UNE ZONE 24 DE LA DOUILLE QUI EST SITUEE A UNE DISTANCE AXIALE PREDETERMINEE DE LA PARTIE ARRIERE 10 EN DIRECTION DU FOND 22 DU CULOT 20. L'ELEMENT DE SOUTIEN 40 CONSTITUE UNE LIAISON POSITIVE DETERMINANT UNE FORCE DE TRACTION MINIMALE AXIALE PREDETERMINEE ENTRE LA ZONE 24 ET LA PARTIE ARRIERE 10 DU PROJECTILE LORSQUE LA PRESSION MONTE APRES LA MISE A FEU. THE AMMUNITION INCLUDES A SUPPORT ELEMENT MOUNTED BETWEEN A REAR PART OF THE PROJECTILE WHICH PENETS INSIDE THE BUSH AND THE BUSH. THE SUPPORT ELEMENT 40 EXTENDS BETWEEN THE REAR PART 10 OF THE PROJECTILE AND A ZONE 24 OF THE SOCKET WHICH IS LOCATED AT A PREDETERMINED AXIAL DISTANCE FROM THE REAR PART 10 TOWARDS THE BOTTOM 22 OF THE BASE 20. THE SUPPORT ELEMENT 40 CONSTITUTES A POSITIVE CONNECTION DETERMINING A PREDETERMINED MINIMUM AXIAL TRACTION FORCE BETWEEN ZONE 24 AND THE REAR PART 10 OF THE PROJECTILE WHEN THE PRESSURE RISES AFTER FIRE.

Fuel container elements for artillery ammunition, method of manufacture and use of such elements.

La présente invention concerne des éléments de conteneurs combustible (24) pour munitions d'artillerie. Les dits éléments, obtenus par feutrage, compactage et cuisson, présentent une partie plane de révolution (2, 7) une paroi extérieure (5, 10) et un col interne (4, 9) d'un seul tenant. Deux éléments complémentaires permettent ainsi d'obtenir des conteneurs combustibles faciles à charger avec de la poudre en vrac (25) et qui ne présentent pas de problème de positionnement du canal central puisque ce dernier est constitué par les cols internes (4, 9). Un tube combustible complémentaire d'allumage (26) en poudre agglomérée est avantageusement positionné à l'intérieur du canal central ainsi défini. L'invention concerne également un procédé d'obtention de ces éléments par emploi d'un moule de feutrage spécialement adapté. The present invention relates to fuel container elements (24) for artillery ammunition. Said elements, obtained by felting, compacting and firing, have a flat part of revolution (2, 7), an outer wall (5, 10) and an inner neck (4, 9) in one piece. Two complementary elements thus make it possible to obtain combustible containers which are easy to load with loose powder (25) and which do not present any problem with the positioning of the central channel since the latter is formed by the internal necks (4, 9). A complementary fuel ignition tube (26) in agglomerated powder is advantageously positioned inside the central channel thus defined. The invention also relates to a process for obtaining these elements by using a specially adapted felting mold.

CONTAINER THAT CAN RECEIVE A PROPULSIVE LOAD.

Le secteur technique de l'invention est celui des conteneurs pouvant recevoir une charge propulsive. Le conteneur (1-12-13) selon l'invention, qui est destiné à être rendu solidaire d'un autre conteneur au niveau d'une de ses faces frontales (3a-3b), est caractérisé en ce que les moyens de solidarisation comportent d'une part une bague (2) disposée sur un rétreint (5) aménagé au niveau d'une extrémité du conteneur, bague susceptible de coulisser suivant une direction axiale pour venir recouvrir un deuxième rétreint (6) aménagé sur l'autre conteneur, et d'autre part des moyens d'accrochage (4a-4b) disposés sur l'un et/ou l'autre conteneur au niveau des faces frontales (3a-3b) destinées à venir en contact mutuel. Application aux munitions de char en deux fardeaux. The technical sector of the invention is that of containers capable of receiving a propellant charge. The container (1-12-13) according to the invention, which is intended to be secured to another container at the level of one of its end faces (3a-3b), is characterized in that the securing means comprise on the one hand a ring (2) arranged on a neck (5) arranged at one end of the container, ring capable of sliding in an axial direction to come to cover a second neck (6) arranged on the other container , and secondly hooking means (4a-4b) arranged on one and / or the other container at the front faces (3a-3b) intended to come into mutual contact. Application to tank ammunition in two bundles.

POCKET SOCKET FOR PROPULSIVE LOAD.

Culot de douille d'une charge propulsive comportant une plaque (1) qui loge, par concordance de forme, de préférence par un taraudage (5), une douille de détonateur (7) placée au centre, caractérisé en ce que la douille de détonateur (7) présente un évidement d'emboîtement d'extracteur (11) détalonné, symétrique en rotation, s'ouvrant vers la face arrière du culot, lequel évidement correspond à peu près à un évidement d'emboîtement d'extracteur d'un projectile sous-calibré. Case base of a propellant charge comprising a plate (1) which accommodates, by matching shape, preferably by means of an internal thread (5), a centrally placed detonator sleeve (7), characterized in that the detonator sleeve (7) has a recess for extractor engagement (11), rotationally symmetrical, opening towards the rear face of the base, which recess corresponds approximately to an extractor engagement recess of a projectile sub-calibrated.

Artillery ammunition element and ammunition obtained by assembling a plurality of such elements.

Medium or small caliber ammunition for e.g. aircraft, has propellant load with grain covered by sheath which is made of destructible composite material and which has reduced thickness, where sheath extends beyond front side of grain

La munition (1) selon l'invention comprend un projectile (2), un chargement propulsif (3) et un dispositif d'allumage (4) de ce dernier qui est solidaire d'un culot d'étanchéité (5). Elle est caractérisée en ce que le chargement propulsif comprend au moins un bloc (3) de charge agglomérée qui est recouvert d'une gaine de protection (7), gaine se prolongeant au-delà d'une face avant (3a) du bloc par une partie tubulaire (7a) entourant une partie arrière du projectile (2) au niveau d'au moins une gorge (8) de fixation portée par celui-ci.

A method of manufacturing container for propellant charge and container thus obtained.

Le procédé selon l'invention est caractérisé par les étapes suivantes: - on réalise un étui tubulaire (2) en matériau combustible, - on réalise en matière combustible deux couvercles (3) comprenant un fond (4) solidaire d'un rebord cylindrique (5) de diamètre externe égal au diamètre interne de l'étui, un couvercle au moins ayant un rebord de longueur suffisante pour permettre une mise en place du couvercle avec une partie du rebord disposée hors de l'étui de façon à pouvoir recevoir un prolongement tubulaire solidaire d'un autre conteneur ou une bague de liaison, - on positionne les couvercles (3) relativement à l'étui (2) avec des moyens permettant une mise en place d'au moins un couvercle avec indifféremment au moins deux positions axiales différentes soit: le fond hors de l'étui, le fond à l'intérieur de l'étui, ou le fond au niveau des extrémités de l'étui, - on rend les couvercles et l'étui solidaires par un moyen de fixation. Application à la réalisation de charges propulsives pour l'artillerie. The method according to the invention is characterized by the following steps: - a tubular case (2) is produced in combustible material, - in combustible material is produced two lids (3) comprising a base (4) integral with a cylindrical rim ( 5) of external diameter equal to the internal diameter of the case, at least one cover having a rim of sufficient length to allow the cover to be fitted with part of the rim disposed outside the case so as to be able to receive an extension tubular integral with another container or a connecting ring, - the lids (3) are positioned relative to the case (2) with means allowing the installation of at least one lid with either at least two axial positions different either: the bottom outside the case, the bottom inside the case, or the bottom at the ends of the case, - the lids and the case are made integral by a fastening means. Application to the production of propellant charges ...

Patent FR2170013B3

Patent FR2444251B1

PROCEDURE FOR THE MANUFACTURE OF A CARTRIDGE AND CARTRIDGE WITH A PROJECTABLE WITH PROPULSING CAGE MANUFACTURED ACCORDING TO THIS PROCEDURE.

Procedimiento para la fabricación de un cartucho (1) con un proyectil (2) y un casquillo combustible para carga propulsora (3), así como una tapa del casquillo (4) que une el casquillo para carga propulsora (3) con el proyectil (2), en donde el proyectil (2) presenta un anillo de obturación (8) adyacente a la tapa del casquillo (4), que comprende las etapas de - fabricar la tapa del casquillo (4) mediante moldeo por inyección con un plástico elástico, en donde el anillo de obturación está formado por la zona anterior (8) de la tapa del casquillo (4) enfrentada al proyectil (2), - unir la tapa del casquillo (4) con el casquillo para carga propulsora (3) y el proyectil (2), en donde - la tapa del casquillo (4) es provista de una zona de rotura controlada (10) en forma de anillo entre la zona (8) que forma el anillo de obturación y la zona posterior (9) situada a continuación de ella, y - la zona (8) de la tapa del casquillo (4) que sirve como anillo de obturación se monta a presión o se fija por calado sobre el proyectil (2), o se fija mediante una unión adhesiva al proyectil (2). Procedure for manufacturing a cartridge (1) with a projectile (2) and a fuel bushing for propellant loading (3), as well as a bushing cover (4) that joins the bushing for propellant charge (3) with the projectile ( 2), wherein the projectile (2) has a sealing ring (8) adjacent to the cap of the bushing (4), comprising the steps of - fabricating the cap of the bushing (4) by injection molding with an elastic plastic , wherein the sealing ring is formed by the anterior area (8) of the cap of the bushing (4) facing the projectile (2), - joining the cap of the bushing (4) with the bushing for propellant loading (3) and the projectile (2), where - the cap of the bushing (4) is provided with a controlled breaking zone (10) in the form of a ring between the area (8) that forms the sealing ring and the rear area (9) located next to it, and - the area (8) of the cap cover (4) serving as a sealing ...

Gun ammunition with a flammable cartridge case

METHOD FOR MANUFACTURING A BOX CONTAINING A PYROTECHNICAL LOAD

Procédé de fabrication d’un boîtier renfermant un chargement pyrotechnique L’invention concerne un procédé de fabrication d’un boîtier renfermant un chargement pyrotechnique et une installation pour la mise en œuvre de ce procédé. Figure pour l’abrégé : Fig. 5. Method for manufacturing a box containing a pyrotechnic charge The invention relates to a method for manufacturing a box containing a pyrotechnic charge and an installation for implementing this method. Figure for abstract: Fig. 5.

Patent FR2074832A5

Protective varnish for preventing thermal ignition of ammunition without a cartridge case or with a combustible cartridge case

CARBON AMMUNITION, CONSISTING OF A PROJECTILE PROVIDED WITH A STABILIZING EMPENNIAL AND A SOCKET CONTAINING THE PROPULSIVE CHARGE AND AT LEAST PARTIALLY FUEL

MANUFACTURING PROCEDURE FOR COMBUSTIBLE OBJECTS BY COMBUSTION OF FUEL PAPER AND COMBUSTIBLE OBJECTS SO OBTAINED

Energetic protective coating for caseless ammunition

Caseless ammunition comprising propellant components provided with an energetic thermal and moisture-resistant coating are characterized by good environmental protection. The employment of a high temperature resistant explosive as a component of the coating permits the application of relatively thick coatings to obtain the advantage of increased thermal resistance without a consumability accommodation in the ballistic cycle.

Manufacturing process for a container for propulsive charge and the container thus obtained

A container manufacturing process includes forming a tubular case of combustible material; forming two covers of combustible material, each cover including a base integral with a cylindrical edge having an external diameter equal to the internal diameter of the case. Each cover has at least one edge of sufficient length to permit the positioning of the cover with part of the edge located outside of the case to be able to receive a tubular extension integral with another container or another interconnecting ring. Positioning of the covers with respect to the case is achieved using structure allowing selective positioning of at least one cover in at least two different axial positions that include selected positions in which the base is outside of the case, the base is inside the case or the base is at the ends of the case. The covers and the case are connected using attachment structure such as glue.

METHOD FOR MANUFACTURING A BOX CONTAINING A PYROTECHNICAL LOAD

Procédé de fabrication d’un boîtier renfermant un chargement pyrotechnique L’invention concerne un procédé de fabrication d’un boîtier renfermant un chargement pyrotechnique et une installation pour la mise en œuvre de ce procédé. Figure pour l’abrégé : Fig. 5. Method for manufacturing a box containing a pyrotechnic charge The invention relates to a method for manufacturing a box containing a pyrotechnic charge and an installation for implementing this method. Figure for abstract: Fig. 5.

SURFACE PROTECTION FOR COMBUSTIBLE SOCKET AMMUNITION OR SOCKETLESS AMMUNITION

Revêtement superficiel protecteur. Il comporte une dispersion de métal en poudre dans un vernis difficilement inflammable, dans une proportion de 50 à 70 %, le métal en poudre étant, de préférence, en plaquettes de 10 à 100 microns Applications : notamment aux munitions à douille combustible ou sans douille.

Elastomer-containing casings for propellants

The present invention relates to a process for producing an encased propellant which comprises overwrapping at least one charge of propellant with an elastomeric coating composition to produce the desired encased propellant. The elastomeric coating composition contains at least one elastomer selected from the group consisting of polyacrylates and phenalus and does not contain any cellulosic compound. The process is suitably effected by molding, casting, dipping, or otherwise applying the coating composition to the charge of propellant. The process and composition of the present invention is expected to be useful in the production of encased tank ammunition, and the like.

IGNITION CARTRIDGE UNIT, ESPECIALLY FOR GAS APPLIANCES

AMMITITION OF PROTECTIVE SURFACE LAYER WITH COMBUSTIBLE SLEEVE AND METHOD FOR MANUFACTURING SUCH A SLEEVE.

Combustible ammunition form

AMMUNITION WITH FLAMMABLE SHELTER OR SHELF AMMUNITION PROVIDED WITH A SURFACE LAYER CONSISTING OF MULTIPLE PAINT LAYERS, AND PROCEDURE FOR PREPARING THE AMMUNITION

Surface protection coating for ammunition with a combustible case or caseless ammunition

ITEMS AND CARTRIDGES WITH AN IMPROVED NITROCELLULOSE SURFACE

WICKELKÖRPER AS A SLEEVE FOR AMMUNITION

Gun ammunition with a flammable cartridge case

Surface coatings for propellant charges containing elastomer

Cartridge ammunition and method of making the same

A method of making a cartridge ammunition includes the following steps: providing a cartridge case having a longitudinal axis; introducing bulk propellant powder into the cartridge case; and oscillating the cartridge case about its longitudinal axis for compacting the bulk propellant powder therein.

Thermal effects resisting combustible envelope for propellant charge - consists of plastics foam with secondary explosives

Combustible sleeve for protecting sheel propellant charges against thermal effects, consists of a plastic foam with up to 80% of one or more secondary explosives. Enables propellant charges for large calibre weapons which can be fired at low rate without the need for a protective casing, to be used for automatic weapons at high firing rates. the combustible envelope may have a thickness 0.3-2.0 mm and a density 0.4-1.2 g/cm3. The envelope may have ribs of thickness twice that of the material between the ribs. A suitable wall thickness for the injection moulded envelope is 2-15 mm and the envelope may then form a container or cartridge case for the propellant charge.

Protective surface covering having heat and moisture resistant properties for caseless ammunition

A heat and moisture resistant surface covering for propellant is provided. This surface covering is consumed in the chamber of a gun with the propellant charge being protected by the surface covering. The surface covering is prepared from a polyolefin film base material having a heat resistant and combustible composition bonded to the exterior surface of the base material. The surface covering of this invention has particular utility for use with caseless ammunition.

Patent FR2458687B1

METHOD OF MANUFACTURING AN IMMEDIATELY FULLY BURNING CARTRIDGE CASE

Improved combustible ammunition cartridge case

An ammunition cartridge (50) is disclosed comprising a projectile (54) threadably attached to a combustible case body (64) via a threaded combustible case adapter (62). At least one of the adapter (62) ends has a uniform density of polyurethane resin to provide strength and sufficient support for the threads. The conbustible case body (64) may also have a uniform resin density to support threads (70, 72) corresponding to those on the rear end of the adapter (62). The preferable uniform polyurethane density is about .75 grams per cubic centimeter.

Method of producing progressively burning artillery propellant powder and agent adapted thereto

ABSTRACT The invention relates to a general method of producing progressively burning deterrent-coated powder, more particularly propellant powder for weapons having barrels. According to the method a film-forming, preferably polymerizable deterrent substance is fed to the powder loosely or dispersed in a liquid phase which is thereafter driven off. The invention also relates to a method of giving a deterrent coating to granular powder or powder cut up in to short pieces (so-called tubular powder) in a fluidized bed. Finally, the invention relates to a special deterrent substance in the form of a water-dispersable polyurethane built up on an aliphatic isocyanate and a caprolacton polyester.

Combustible casings for rockets - built from polyester fabrics or fibres impregnated and loaded with epoxy resin, oxidants and combu

Casings, esp. suitable for rejectable starting rockets and rockets for high altitude research, are produced from layers of polyethyleneglycol terephthalate fabric or fibres impregnated with a mixt. comprising epoxy resin, oxidants (KClO3, KClO4, or NH4ClO4) and combustion accelerators (such as MnO2, FeCl3 and Fe2O3). The space between the layers is filled with similar, highly combustible materials, and electrically actuated igniters are provided at the butt end of the casing. These casings are ignited reliably and rapidly, and burn much faster than the known materials of this type.

SLEEVE-LESS PRESSURE CHARGE AND METHOD OF MANUFACTURING THE SAME

FUEL CARTRIDGE SOCKET.

IGNITION DEVICE FOR PROPULSIVE CHARGING

L'invention a pour objet un dispositif d'allumage pour un chargement propulsif (4) contenu dans un étui cylindrique (3) d'une munition.Ce dispositif comprend au moins un élément d'allumage énergétique linéaire (8, 8a) et un moyen d'initiation de ce dernier, il est caractérisé en ce que le moyen d'initiation comprend une pièce tubulaire (10), disposée au niveau d'un fond (13, 22) de fermeture de l'étui et délimitant une chambre (11) qui communique avec un composant pyrotechnique d'initiation (18), pièce tubulaire comprenant un trou axial (16) destiné à permettre le passage et l'entrée dans la chambre (11) du ou des éléments d'allumage (8, 8a) disposés sensiblement au niveau de l'axe (21) de l'étui. The invention relates to an ignition device for a propellant charge (4) contained in a cylindrical case (3) of a munition. This device comprises at least one linear energetic ignition element (8, 8a) and a means of initiation of the latter, it is characterized in that the initiation means comprises a tubular part (10), arranged at a bottom (13, 22) for closing the case and delimiting a chamber ( 11) which communicates with an initiation pyrotechnic component (18), tubular part comprising an axial hole (16) intended to allow passage and entry into the chamber (11) of the ignition element (s) (8, 8a) ) arranged substantially at the level of the axis (21) of the case.

Molded part, and method for the production of the molded part

To increase the function and safety of a weapon, it is proposed that the molded part, as connecting site particularly between a projectile and a preferably combustible sleeve containing a driving mechanism, be constructed in such a way that, in a predefined region, said molded part has a felt with an energetic material and/or an inert material.

Protective varnish for preventing thermal ignition of ammunition without a cartridge case or with a combustible cartridge case

Caseless ammunition

A round of ammunition is formed by molding multiple layers of propellant about the sides and rear of a projectile providing an inner layer of conventional propellant enclosed within an outer layer composed of a mixture of a polynitroaromatic material, such as diaminotrinitrobenzene (DATB), as the primary oxidizer, and a phosphorus-containing hydroxy-terminated polyether binder.

Cartridge-less moulded propellant charge

Explosive composition and method.

Certain classes of organic acids, and salts of those acids and in particular ascorbic acid and erythorbic acid and the salts thereof, and mixtures thereof, which have certain antioxidant and food preservative properties, have been found to be capable of being processed together with sources of nitrate, including inorganic nitrates, ammonium nitrates, organic nitrates, and the like, at temperatures below 480<o>F to produce compositions which are capable of being molded into specific shapes or used in a powered form as a gunpowder substitute, an explosive or a propellent when properly ignited.

ENOUGH MUNITION CONSISTING OF A PROJECTILE AND A COMBUSTIBLE OR PARTIALLY COMBUSTIBLE BUSHING RELATED THERETO

MUNITION ENCARTOUCHEE, CONSTITUEE PAR UN PROJECTILE 2 ET PAR UNE DOUILLE COMBUSTIBLE 6. ELLE COMPORTE UNE PREMIERE LIAISON ENTRE LE PROJECTILE 2 ET LA DOUILLE 6 DANS LA REGION DU COL 8 DE LA DOUILLE, ET UNE DEUXIEME LIAISON REALISEE SOUS FORME D'ELEMENT SUPPORT RADIAL AGISSANT SUR UNE PARTIE ARRIERE DU PROJECTILE S'AVANCANT A L'INTERIEUR DU VOLUME INTERIEUR DE LA DOUILLE. L'ELEMENT SUPPORT EST REALISE SOUS FORME DE DISQUE 12 PERFORE S'APPUYANT CONTRE LE PROJECTILE 2 ET CONTRE LA DOUILLE 6. CARTRIDGED AMMUNITION, CONSTITUTED BY A PROJECTILE 2 AND BY A COMBUSTIBLE SOCKET 6. IT PROVIDES A FIRST LINK BETWEEN PROJECTILE 2 AND SOCKET 6 IN THE SOCKET NECK 8 REGION, AND A SECOND LINK IN THE FORM OF A RADIAL SUPPORT ELEMENT ACTING ON A REAR PART OF THE PROJECTILE ADVANCING INSIDE THE INTERIOR VOLUME OF THE BUSH. THE SUPPORT ELEMENT IS MADE IN THE FORM OF A PERFORATED DISC 12 LENGHING AGAINST PROJECTILE 2 AND AGAINST SOCKET 6.

AMMUNITION CARTRIDGE CONSISTING OF A BULLET AND A CASE TOTALLY OR PARTIALLY COMBUSTIBLE WITH THE BULLET

SURFACE FOR AMMUNITION WITH FLAMMABLE SLEEVE OR SLEEVELESS AMMUNITION

Patent DE3927400C2

Wound body for use as an ammunition shell

According to known techniques for winding an ammunition shell the number of thread layers is often reinforced as compared to the remaining part of the shell wall, especially in those zones of the shell where the load is the highest, thereby, however, inevitably increasing the thickness of the shell wall. If the space for the propelling charge in the wound shell is to be enlarged while the outer geometry of the wound shell remains the same, that is with the same space provided in the weapon for the charge, the wall thickness has to be reduced. In order to provide the shell with the same mechanical stability, despite the reduction in wall thickness, as shells whose wall thickness is not reduced, the wound body of the shell ( 50 ) is produced from chemical fibers ( 53 ), preferably from synthetic and inorganic chemical fibers.

CONNECTION DEVICE BETWEEN A MEANS OF IGNITION OF A PROPULSIVE CHARGE AND A COMBUSTIBLE CASE OF AN AMMUNITION, COMBUSTIBLE CASE AND SPRING WASHER ASSOCIATED WITH SUCH A CONNECTION DEVICE.

L’invention a pour objet un dispositif de liaison entre un moyen d’allumage (8) d’une charge propulsive et un étui (2) combustible d’une munition comportant un fond percé d’une ouverture axiale (20) au travers de laquelle se place le moyen d’allumage (8) et d’au moins une ouïe périphérique (21) destinée à permettre le chargement de l’étui avec la charge propulsive. Ce dispositif est caractérisé en ce qu’il comporte un moyen de maintien du moyen d’allumage (8) sur l’étui combustible (2) , moyen qui assure l’immobilisation du moyen d’allumage avant le chargement de l’étui combustible, le moyen de maintien comportant d’une part une bague de butée (12) solidaire du moyen d’allumage (8) et venant en appui contre une surface interne (2a) du fond de l’étui par l’intermédiaire d’une rondelle élastique (17) et d’autre part une bague de maintien (19) solidaire du moyen d’allumage (8) qui coopère avec au moins une surface d’arrêt (22) solidaire du fond de l’étui (2). Figure à publier avec l’abrégé : Fig. 1 The subject of the invention is a connecting device between an ignition means (8) of a propellant charge and a combustible case (2) of an ammunition comprising a bottom pierced with an axial opening (20) through which is placed the ignition means (8) and at least one peripheral opening (21) intended to allow the loading of the case with the propellant charge. This device is characterized in that it comprises means for holding the ignition means (8) on the combustible case (2), means which ensure the immobilization of the ignition means before the loading of the combustible case. , the holding means comprising on the one hand a stop ring (12) integral with the ignition means (8) and bearing against an internal surface (2a) of the bottom of the case by means of a elastic washer (17) and on the other hand a retaining ring (19) secured to the ignition means (8) which cooperates with at least one stop surface (22) secured to the bottom of the case (2). Figure to be published with ...

METHOD FOR PRODUCING COMBUSTIBLE OBJECTS BY DEEP-DRAWING COMBUSTIBLE PAPER DISCS WITH AN ELASTIC PATRICE, AND DEVICE FOR CARRYING OUT THE PROCESS.

PERFECTIONED MUNITION

Mouldable compositions containing polyvinyl nitrate

ABSTRACT OF THE DISCLOSURE A mouldab1e thermoplastic composition comprises (i) polyvinyl nitrate, (ii) nitrocellulose and/or polyvinyl acetate and (iii) 2-nitro-diphenylamine and may be used to form combustible articles such as cartridge cases. Preferably, the composition comprises from 30 to 90% by weight of polyvinyl nitrate based on the total weight of components (i) and (ii). The composition may comprise up to about 30% by weight, based on the weight of components (i) and (ii), of at least one additive selected from cellulose acetate, dinitrotoluene, phthalates, non-volatile esters, heterocyclic ketones, ureas and ABS copolymers. The combustible articles may be formed by compression moulding or injection moulding. Preferably the mouldable composition is formed into granules using the "with solvent" technique for making single base propellants, and the granules are mixed with a porous powder comprising nitro-cellulose prior to being moulded to form the combustible article.

Process for the surface treatment of ammunition casings made of combustible materials and ammunition casings or cartridges produced therefrom

Molded part, and method for the production of the molded part

To increase the function and safety of a weapon, it is proposed that the molded part (1), as connecting site particularly between a projectile and a preferably combustible sleeve containing a driving mechanism, be constructed in such a way that, in a predefined region (2), said molded part (1) has a felt (3) with an energetic material (4) and/or an inert material (5).

PROCESS FOR MANUFACTURING PROPELLANT POWDER AND COMBUSTION INHIBITOR

Combustion inhibitor for gas-producing charges

Granulated Block Propellant Device for Firearms

The present invention relates to a granulated block propellant device for firearms that is comprised of a generally rectangular body that has a flat top surface and a flat bottom surface, in addition to a set and a second set of generally parallel side surfaces. In differing embodiments, the body may be in the form of an axial slab body, a radial disc body, or a concentric-wrapped body. The body is further comprised of at least one perforation that can be arranged in a plurality of configurations. The body may also be comprised of at least one partial cut on a surface of the body that does not have the plurality of configurations. In one embodiment, the device can be placed in the casing of a projectile and used as a propellant. Multiple devices may also be stacked atop one another within a projectile casing.

Patent DE3009342C2

Device for installing fixing ring on the cartridge body shell

FIELD: weapons and ammunition. SUBSTANCE: device for installing a fixing ring on the shell of the projectile contains a bed, a top plate on which the feeder of the fixing rings is mounted with a mechanism for their delivery, a movable table with a lodgement for laying the projectile, a mechanism for removing and lifting the projectile from the cradle to the position of securing the projectile by semi- feeding the fixing ring to the shell of the shell of the projectile. The feeder consists of a tray connected to a take-up sleeve in which a pushing mechanism of the feed mechanism of the fixing ring is placed. The piece delivery mechanism contains a magazine connected to the feeder tray, and between them is located the unitary clipper of the fixing ring from the total flow of rings located in the store, including a rocker having stops and a rocker arm connected by a pull rod with a pick-up and lifting mechanism. EFFECT: ensuring the centering of the projectile in the shell of the burner sleeve. 8 dwg

THERMAL PROTECTION FOR POWDER PROPELLERS, FREE OF ASBESTOS

L'INVENTION CONCERNE LE DOMAINE DES PROTECTIONS THERMIQUES DESTINEES A PROTEGER LES PAROIS INTERNES DES PROPULSEURS A POUDRE LORS DE L'EMISSION DES GAZ CHAUDS PRODUITS PAR LA COMBUSTION DES BLOCS DE PROPERGOL. L'INVENTION SE RAPPORTE A UNE PROTECTION THERMIQUE EXEMPTE D'AMIANTE CONSTITUEE ESSENTIELLEMENT DE 100 PARTIES EN POIDS DE CAOUTCHOUC SYNTHETIQUE, DE 0 A 100 PARTIES EN POIDS D'UN COMPOSE CHIMIQUE A DECOMPOSITION ENDOTHERMIQUE ET DE 50 A 150 PARTIES EN POIDS D'UN MATERIAU DE CHARGE A BASE DE SILICE ET DE FIBRES DE POLYAMIDE AROMATIQUE, LADITE PROTECTION THERMIQUE COMPORTANT AU MOINS 15 PARTIES EN POIDS DE FIBRES DE POLYAMIDE AROMATIQUE. LES PROTECTIONS THERMIQUES REALISEES SELON L'INVENTION PRESENTENT DES PERFORMANCES SIMILAIRES AUX PROTECTIONS THERMIQUES COMPORTANT DE L'AMIANTE. THE INVENTION CONCERNS THE FIELD OF THERMAL PROTECTIONS INTENDED TO PROTECT THE INTERNAL WALLS OF POWDER THRUSHERS DURING THE EMISSION OF HOT GASES PRODUCED BY THE COMBUSTION OF THE PROPERGOL BLOCKS. THE INVENTION RELATES TO A THERMAL PROTECTION FREE OF ASBESTOS CONSTITUTED ESSENTIALLY OF 100 PARTS BY WEIGHT OF SYNTHETIC RUBBER, FROM 0 TO 100 PARTS BY WEIGHT OF AN ENDOTHERMAL COMPOSITION CHEMICAL AND FROM 50 TO 150 PARTS BY WEIGHT OF ONE. FILLING MATERIAL BASED ON SILICA AND AROMATIC POLYAMIDE FIBERS, THE SAID THERMAL PROTECTION CONTAINING AT LEAST 15 PARTS BY WEIGHT OF AROMATIC POLYAMIDE FIBERS. THE THERMAL PROTECTIONS ACHIEVED ACCORDING TO THE INVENTION SHOW SIMILAR PERFORMANCES TO THERMAL PROTECTIONS INCLUDING ASBESTOS.

Method for connecting the sleeve cover arranged on a projectile to the sleeve jacket of a cartridge

Die Erfindung betrifft ein Verfahren zur Verbindung des an einem Geschoss (3) angeordneten Hülsendeckels (6) an dem aus einem verbrennbaren Material bestehenden Hülsenmantel (4) einer Treibladungshülse (2) einer Patrone (1). Um auf einfache Weise den Hülsendeckel (6) und den Hülsenmantel (4) sicher miteinander zu verbinden, schlägt die Erfindung vor, über den/die Verbindungsbereich/e (9) von Hülsendeckel (6) und Hülsenmantel (4) einen Schrumpfschlauch (11) zu positionieren und diesen dann kurzzeitig auf eine Temperatur zu erwärmen, bei welcher er sich fest an die miteinander zu verbindenden Bauteile (4, 6) anlegt, wobei die Zeitdauer der Erwärmung derart gewählt wird, dass eine Entzündung des Hülsenmaterials sicher vermieden wird. The invention relates to a method for connecting the sleeve cover (6) arranged on a projectile (3) to the sleeve jacket (4) of a combustible material of a propellant charge sleeve (2) of a cartridge (1). In order to securely connect the sleeve cover (6) and the sleeve jacket (4) together in a simple manner, the invention proposes that a shrink sleeve (11) is provided via the connecting region (s) (9) of sleeve cover (6) and sleeve jacket (4). to position and then briefly to heat it to a temperature at which it applies firmly to the components to be joined together (4, 6), wherein the duration of the heating is selected such that an ignition of the sleeve material is reliably avoided.

Method for producing a cartridge having a sabot projectile produced according to said method

Die Erfindung betrifft ein Verfahren zur Herstellung einer Patrone (1) sowie einer Patrone, hergestellt nach diesem Verfahren mit einem Geschoss (2) und einer verbrennbaren Treibladungshülse (3) sowie einem die Treibladungshülse (3) mit dem Geschoss (2) verbindenden Hülsendeckel (4), wobei das Geschoss (2) einen dem Hülsendeckel (4) benachbarten Dichtungsring (8) aufweist. Um eine kostengünstige Montage einer derartigen Patrone (1) zu erreichen, schlägt die Erfindung vor, den Hülsendeckel (4) als Spritzgussteil aus einem elastischen Kunststoff herzustellen, wobei der dem Geschoss (2) zugewandte vorderseitige Bereich (8) des Hülsendeckels (4) den Dichtungsring bildet.

COMBUSTIBLE OBJECTS, AND IN PARTICULAR COMBUSTIBLE SOCKETS, RESISTANT TO HEAT

L'invention se rapporte au domaine des objets combustibles utilisés en armement et notamment à celui des douilles combustibles. Les objets combustibles selon l'invention sont recouverts par une couche mince de vernis à liant organique contenant des microbilles creuses, ledit vernis étant à base d'un liant choisi dans le groupe constitué par les caoutchoucs chlorés, le chlorure de polyvinylidène, les liants cellulosiques, les liants glycérophtaliques, les résines polyuréthanes, les résines polyépoxy. Le vernis contient entre 5 et 20 % en poids, par rapport au polymère dissous, et préférentiellement environ 10 % de microbilles creuses. Les objets combustibles selon l'invention présentent un retard à l'autoinflammation s'ils sont mis au contact d'une paroi chaude sans altération de leurs propriétés thermodynamiques. The invention relates to the field of combustible objects used in weaponry and in particular to that of combustible casings. The combustible objects according to the invention are covered with a thin layer of varnish with an organic binder containing hollow microspheres, said varnish being based on a binder chosen from the group consisting of chlorinated rubbers, polyvinylidene chloride, cellulose binders. , glycerophthalic binders, polyurethane resins, polyepoxy resins. The varnish contains between 5 and 20% by weight, relative to the dissolved polymer, and preferably about 10% of hollow microbeads. The combustible objects according to the invention exhibit a self-ignition retardation if they are brought into contact with a hot wall without altering their thermodynamic properties.

Advanced muzzle loader ammunition

A fixed round of ammunition for a muzzle loader firearm. The round has a bullet within a sabot that is engaged to a consumable cartridge case. The case is filled with propellant that is precisely calibrated to provide optimal ballistic properties with the particular bullet it is engaged to. The consumable cartridge case can be more tailored to respectively increase or decrease the burn rate of the consumable cartridge case. The consumable cartridge case can be constructed out of nitrocellulose or other energetic materials. A wide range of propellant formulas can be used that are safe because the burn rate is precisely calibrated for the bullet used. The propellant can contain pyrotechnic material and/or other ingredients to reduce the burn rate of a smokeless propellant and can contain a stabilizer to increase the shelf life of the ammunition round.

Ignition device for a propellant charge

Method of manufacturing combustible cylindrical body for nonnresidually combustible cartridge case and similar priming tube

Verfahren zur herstellung einer patrone mit einem treibkäfiggeschoss hergestellt nach diesem verfahren

焼尽性容器

Method for manufacturing a housing enclosing a pyrotechnic load

A method for manufacturing a housing enclosing a pyrotechnic charge and an installation for implementing this method includes inserting a pyrotechnic charge into a charging volume laterally delimited by a rigid cylindrical charging wall and into a lower part by a first element of the housing to be obtained; positioning a second element of the housing to be obtained of cylindrical shape above the inserted pyrotechnic charge and in the extension of the cylindrical charging wall. The second element has a lateral cylindrical wall of the same shape and diameter as the cylindrical charging wall and is able to cooperate with the first element, and jointly translating the second element and the cylindrical charging wall relative to the first element such as to make the second element cooperate with the first element and form the housing enclosing the pyrotechnic charge.

Method for manufacturing a housing enclosing a pyrotechnic load

A method for manufacturing a housing enclosing a pyrotechnic charge and an installation for implementing this method includes inserting a pyrotechnic charge into a charging volume laterally delimited by a rigid cylindrical charging wall and into a lower part by a first element of the housing to be obtained; positioning a second element of the housing to be obtained of cylindrical shape above the inserted pyrotechnic charge and in the extension of the cylindrical charging wall. The second element has a lateral cylindrical wall of the same shape and diameter as the cylindrical charging wall and is able to cooperate with the first element, and jointly translating the second element and the cylindrical charging wall relative to the first element such as to make the second element cooperate with the first element and form the housing enclosing the pyrotechnic charge.

焼尽薬莢用または焼尽火管用の燃焼性筒体の製造方法

Propellant charge container

Propellant charge container

The invention relates to a charge container device, said charge container device having a volume suitable to substantially fill a barrel chamber, said charge container device is formed from a substantially rigid and combustible material, wherein said charge container device comprises at least one wall to define a cavity for the retention of at least one cartridge case, said at least one cartridge case comprising an energetic material, wherein said at least one cartridge case is arranged in a stacked formation within said charge container, the charge container device further comprising a base portion and a top portion, wherein the top portion comprises an aperture to allow for expulsion of energy and the base portion comprising an ignition means.

Propellant charge container

Protezione superficiale per munizioni con bossolo combustibile o per munizioni prive di bossolo.