The invention related to a method for simulating weapon effect against a specific target comprising at least one three dimensional model of a warhead and a three dimensional model of a target where the model of the warhead is adapted so that the weapon effect against the target for each fragment of the warhead is simulated.
F42B 12/02 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché
G06F 9/44 - Dispositions pour exécuter des programmes spécifiques
G06F 30/23 - Optimisation, vérification ou simulation de l’objet conçu utilisant les méthodes des éléments finis [MEF] ou les méthodes à différences finies [MDF]
G06T 17/20 - Description filaire, p.ex. polygonalisation ou tessellation
F42B 12/22 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation
37 - Services de construction; extraction minière; installation et réparation
Produits et services
Commercial lobbying services; Media relations services; Corporate communications services; Ordering services for third parties. Maintenance, servicing and repair of weapon systems; Maintenance, servicing and repair of vehicles.
37 - Services de construction; extraction minière; installation et réparation
Produits et services
Commercial lobbying services; Media relations services; Corporate communications services; Ordering services for third parties. Maintenance, servicing and repair of weapon systems; Maintenance, servicing and repair of vehicles.
5.
MUZZLE BRAKE AND METHOD FOR MANUFACTURING MUZZLE BRAKE
The present invention concerns a method for manufacturing a muzzle brake for a barrel, characterized by the fact that the method includes the following steps: i.) a capsule assembly (60) is designed including a cavity, ii.) the powder is arranged in the cavity in the capsule assembly (60), iii.) the powder is pressed so that the powder and capsule assembly are joined together, iv.) excess material that covers the opening for outgoing gas flows is removed. The invention also concerns a muzzle brake, a firing barrel and a firing device.
B22F 5/10 - Fabrication de pièces ou d'objets à partir de poudres métalliques caractérisée par la forme particulière du produit à réaliser d'articles avec des cavités ou des trous, non prévue dans les sous-groupes précédents
A method is provided for producing a component for a warhead, wherein the method involves the steps: i.) an inner shell is arranged on a tool, ii.) preshaped projectiles are arranged on the inner shell, iii.) powder is arranged to enclose the preshaped projectiles, iv.) the powder is pressed such that the powder, the preshaped projectiles, and the inner shell are joined together, v.) the tool is removed from the component formed from the powder, the preshaped projectiles, and the inner shell. A warhead and a projectile are also provided.
The invention related to a method for simulating weapon effect against a specific target comprising at least one model of a warhead where the model of the warhead is adapted so that the weapon effect of the warhead is simulated as a volume. The invention further relates to a method for simulating weapon effect against a specific target comprising at least one model of a warhead and a computer program product.
The invention relates to a method for simultaneous blasting of projectiles where the following method steps are included; i.) calculating the position of the target, ii.) estimating the target's position, iii.) firing a first projectile at the target, iv.) firing a second projectile at the target, v.) braking the first projectile with a braking device arranged in the projectile, vi.) detonating the projectiles in a coordinated fashion based on an initiation signal. The invention furthermore consists of a fire-control system for directing fire against a target comprising at least one sensor, in order to measure the position of the target as a function of time. The invention furthermore consists of a combat system including a firing device.
A projectile for short firing ranges includes as a cylinder with a nose having a substantially flat surface arranged with a threaded socket allowing for the arrangement of, for example, a fuze a rear section designed with a substantially flat surface, as well as a projectile body arranged with energetic material enclosed by a casing.
F42C 1/12 - Fusées percutantes, c. à d. fusées actionnées uniquement par l'impact des munitions sans percuteur à action retardée après allumage de la fusée
The invention relates to a projectile (100, 100´, 100´´, 100´´´, 100´´´´) arranged with antenna, where the projectile is intended for launch in a launch device with a propellant charge in a barrel, where the projectile (100, 100´, 100´´, 100´´´, 100´´´´) is arranged with an antenna (110, 110´, 110´´) in the rear edge of the projectile (102) where the antenna is arranged behind any of or a combination of; i. a protective cap (120, 120´) which protects the antenna (110, 110´, 110´´) during the ejection phase in the barrel and which is removed when the projectile (100, 100´, 100´´, 100´´´, 100´´´´) has left the barrel, ii. a protection in the form of a molding compound arranged to protect the antenna (110, 110´, 110´´).
F42B 12/36 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation
F42B 15/01 - Dispositions pour le guidage ou le pilotage sur les projectiles autopropulsés ou les missiles
F42B 30/00 - Projectiles non prévus ailleurs, caractérisés par la catégorie ou le type de munitions, p.ex. par le lanceur ou l'arme utilisés
F42B 10/00 - Moyens pour influencer, p.ex. pour améliorer, les propriétés aérodynamiques de projectiles; Dispositions sur les projectiles pour la stabilisation, le pilotage, le freinage de la chute, la réduction ou l'augmentation de la portée
H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
H01Q 19/00 - Combinaisons d'éléments actifs primaires d'antennes avec des dispositifs secondaires, p.ex. avec des dispositifs quasi optiques, pour donner à une antenne une caractéristique directionnelle désirée
14.
LAUNCHING DEVICE AND METHOD FOR ASSEMBLING PROJECTILES IN A LAUNCHING DEVICE
A modular launching device for launching of projectiles with a propellant charge is provided where the projectile is arranged such that a detonator is arranged at a projectile body in the launching device and assembled together with at least one propellant charge in the launching device. A method of assembling projectiles in a launching device by using modules is also provided.
F41A 1/08 - Canons sans recul, c. à d. armes à feu munies d'un système de propulsion qui ne produit pas de recul
F42B 5/16 - Cartouches, c. à d. projectile et douille avec charge propulsive formant un tout caractérisées par la composition ou les dimensions géométriques ou la forme de la charge propulsive ou de la poudre
F42B 30/00 - Projectiles non prévus ailleurs, caractérisés par la catégorie ou le type de munitions, p.ex. par le lanceur ou l'arme utilisés
The invention relates to a barrel (10) for launching device (1), whereas the barrel (10) is arranged with a bore (20) for the launching of projectiles (100) with a propellant charge (110), whereas the barrel (10) is arranged with at least one cavity (12, 14, 16), whereas a substance for storing thermal energy is arranged in said at least one cavity (12, 14, 16). The invention further consists of an ejection device and a method for storing thermal energy in a barrel.
F41A 13/00 - Systèmes de refroidissement ou de réchauffage; Systèmes pour le soufflage des tubes de l'arme; Systèmes de ventilation
F41A 21/20 - Tubes d'arme caractérisés par le matériau
C09K 5/06 - Substances qui subissent un changement d'état physique lors de leur utilisation le changement d'état se faisant par passage de l'état liquide à l'état solide, ou vice versa
A fire control method against aerial targets flying toward a protection object when the position of the protection object is known includes measuring the position of the aerial target, estimating the position of the aerial target, estimating the velocity of the aerial target, predicting the future path of the aerial target from the estimated position of the aerial target and the estimated velocity of the aerial target, and deciding, on the basis of the predicted path, whether the aerial target i.) is incoming and thus a threat against the protection object, ii.) is passing by and thus not a threat to the protection object.
The invention concerns a projectile (100, 200, 200´) for launching from a launching device (1) with a propellant charge (110) in a barrel (10), where the projectile (100, 200, 200´) is arranged with a cross-section (20) in shape of a curve of constant width.
F42B 10/00 - Moyens pour influencer, p.ex. pour améliorer, les propriétés aérodynamiques de projectiles; Dispositions sur les projectiles pour la stabilisation, le pilotage, le freinage de la chute, la réduction ou l'augmentation de la portée
F42B 10/26 - Dispositions pour la stabilisation par rotation
F42B 10/54 - Moyens pour freiner la rotation d'un projectile
F42B 14/00 - Projectiles caractérisés par des dispositions pour les guider à l'intérieur du canon, pour rendre étanche la surface de contact entre le projectile et le canon, pour lubrifier ou nettoyer le canon
F42B 14/06 - Projectiles sous-calibrés munis de sabots; Sabots pour ces projectiles
F41A 21/00 - Tubes d'arme; Accessoires de bouches de canon; Montage des tubes d'arme
F41A 21/16 - Tubes d'arme caractérisés par la forme de leur alésage
In a brake for detachable arrangement on projectiles, the brake is configured with a surface which is situated in the direction of travel of the projectile, where the surface is larger than a surface given by πR2-πr2, where R is the outer radius of the brake and r is the inner radius of the brake. A method for braking projectiles is also provided.
A plasma generator is provided for initiation of propellant charges in a weapons system, for example when launching projectiles from a barrel weapon, by electrical discharge between a rear electrode and a front electrode in a combustion chamber channel enclosed in a combustion chamber body and filled with filling gas, designed to ignite at least one propellant charge. An ammunition unit and a launching device including the plasma generator are also provided.
F41A 19/63 - Mécanismes de mise à feu électriques comportant des moyens pour la transmission sans contact d'énergie électrique, p.ex. par induction, par étincelles
The invention concerns a barrel (10) for a launching device (1) for launching projectiles (100) with a propellant charge (110) where the barrel (10) is arranged with a cross-section (20) in the form of a curve of constant width. The invention further consists of a launching device and a method for firing a rotation-stabilized projectile from a barrel.
B21C 37/15 - Fabrication de tubes de formes particulières; Fabrication de garnitures de tubes
F42B 14/00 - Projectiles caractérisés par des dispositions pour les guider à l'intérieur du canon, pour rendre étanche la surface de contact entre le projectile et le canon, pour lubrifier ou nettoyer le canon
A method is provided to improve the impact point for at least one subsequent projectile fired towards a target, launched after an initial projectile, where the subsequent projectiles can alter their course, based on information on the previous projectiles' time of automatic detonation, to improve the ability to detect a target. A projectile and a fuse are also provided.
The invention concerns a projectile (1) outfitted with a target finder, intended to be fired from a launching device, comprising one or several fins (3) where the fins (3, 3´), upon being extended, cause the projectile (1) to be urged into a controlled oscillating movement. The invention also concerns a fuse.
F42B 10/14 - Dispositions pour la stabilisation utilisant des ailettes qui sont déployées après le lancement, p.ex. après la sortie du tube de l'arme
F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés
F42B 10/00 - Moyens pour influencer, p.ex. pour améliorer, les propriétés aérodynamiques de projectiles; Dispositions sur les projectiles pour la stabilisation, le pilotage, le freinage de la chute, la réduction ou l'augmentation de la portée
F42B 10/64 - Pilotage par le déplacement de surfaces portantes d'ailettes de pilotage
F42C 19/02 - Corps de la fusée; Logement de la fusée
F42B 14/00 - Projectiles caractérisés par des dispositions pour les guider à l'intérieur du canon, pour rendre étanche la surface de contact entre le projectile et le canon, pour lubrifier ou nettoyer le canon
This invention relates to a method for producing a warhead component comprised of an inner shell, characterized in that the method comprises the following steps: i.) a first casing of a thermoplastic is arranged to enclose the inner shell, ii.) pre-formed projectiles are arranged between the first casing of thermoplastic and the inner shell, iii.) the first casing is heat-treated so that the first casing shrinks and fixes the pre-formed projectiles to the inner shell. The invention further relates to a warhead, to a projectile, and to a bomb.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
This invention relates to a method for producing a warhead component comprised of an inner shell, characterized in that the method comprises the following steps: i.) a first casing of a thermoplastic is arranged to enclose the inner shell, ii.) pre-formed projectiles are arranged between the first casing of thermoplastic and the inner shell, iii.) the first casing is heat-treated so that the first casing shrinks and fixes the pre-formed projectiles to the inner shell. The invention further relates to a warhead, to a projectile, and to a bomb.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
The invention concerns a projectile (1) outfitted with a target finder (5), intended to be fired from a launching device, comprising one or several brake flaps (3, 3´) where the brake flaps (3, 3´), after their being extended, cause the projectile (1) to be arranged in a controlled oscillating movement. The invention also concerns a fuse.
F42B 10/00 - Moyens pour influencer, p.ex. pour améliorer, les propriétés aérodynamiques de projectiles; Dispositions sur les projectiles pour la stabilisation, le pilotage, le freinage de la chute, la réduction ou l'augmentation de la portée
F42B 10/14 - Dispositions pour la stabilisation utilisant des ailettes qui sont déployées après le lancement, p.ex. après la sortie du tube de l'arme
F42B 10/64 - Pilotage par le déplacement de surfaces portantes d'ailettes de pilotage
F42C 19/02 - Corps de la fusée; Logement de la fusée
F42B 14/00 - Projectiles caractérisés par des dispositions pour les guider à l'intérieur du canon, pour rendre étanche la surface de contact entre le projectile et le canon, pour lubrifier ou nettoyer le canon
27.
Method, computer program and weapons system for calculating a bursting point of a projectile
A method is provided for calculating the bursting point of at least one projectile fired at a target object, involving measuring the position of the projectile, estimating the position of the projectile, estimating the speed of the projectile, measuring the position of the target object, estimating the position of the target object, estimating the speed of the target object, calculating optimal bursting points for the projectile based on the estimated position of the projectile, the estimated speed of the projectile, the estimated position of the target object and the estimated speed of the target object, and communicating the bursting points for the projectile to the projectile. A computer program, a computer system, and a weapons system are also provided.
The invention relates to a method for regulating the attachment of a parachute to a warhead where the parachute is attached to the warhead by at least one attachment point arranged on a first rotatable circular disc so that the attachment point is moved when the first rotatable circular disc is rotated. and thus affects the position and/or direction of the warhead relative to the parachute. The invention further relates to a warhead, as well as to a projectile provided with the warhead.
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
The invention concerns a canister (1,1'), which is arranged so as to encompass at least one submunition (10), which is to be housed in a projectile (100), where the canister (1, 1') is outfitted with at least one air brake (2) and at least one rotation brake (4). The invention furthermore comprises a projectile and a method.
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
F42B 10/54 - Moyens pour freiner la rotation d'un projectile
F42B 12/58 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles
A procedure for producing a warhead with controlled fragmentation includes manufacturing an inner shell and filling it with an explosive substance. The procedure further includes providing a net around the outer surface of the inner shell as well as depositing a material on and around the net. A warhead is produced by the procedure and includes an inner shell. A material applied to the warhead comprises weak points for guided fragmentation of the deposited material upon detonation of the warhead.
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
A method for producing a warhead with directed blasting action involves the step of making an outer casing and arranging therein a charge with a cavity situated at the front end of the charge. An insert whose shape corresponds to the shape of the cavity is arranged on the surface of the charge. The method furthermore involves the step of depositing a material on the insert in an additive manufacturing process. A warhead manufactured according to the method includes an outer casing, a charge with a cavity situated at the front end of the charge, and an insert. A material is deposited on the insert.
09 - Appareils et instruments scientifiques et électriques
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
(1) Simulation software; Application simulation software; Simulators for simulating the operation of weapons; Science software (1) Computer software consultancy; Configuration of computer software; Computer programming and software design; Computer systems integration services; Research in the field of computer programs and software; Advisory services relating to the use of computer software; Technical consultancy relating to the application and use of computer software
09 - Appareils et instruments scientifiques et électriques
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Simulation software; Application simulation software; Simulators for simulating the operation of weapons; Science software. Computer software consultancy; Configuration of computer software; Computer programming and software design; Computer systems integration services; Research in the field of computer programs and software; Advisory services relating to the use of computer software; Technical consultancy relating to the application and use of computer software.
The invention relates to a projectile for short firing ranges, where the projectile is designed as a cylinder with a nose having a substantially flat surface arranged with a threaded socket allowing for the arrangement of, for example, a fuze a rear section designed with a substantially flat surface, as well as a projectile body arranged with energetic material enclosed by a casing.
The invention relates to a modular launching device (1) for launching of projectiles (100) with a propellant charge (10) where the projectile (100) is arranged such that a detonator (20) is arranged at a projectile body (50) in the launching device (1) and assembled together with at least one propellant charge (10) in the launching device (1). Moreover, the invention relates to a method of assembling projectiles in a launching device by using modules.
F41A 9/00 - Chargement ou alimentation en munitions; Chargeurs; Moyens de guidage pour l'extraction des cartouches
F42B 5/16 - Cartouches, c. à d. projectile et douille avec charge propulsive formant un tout caractérisées par la composition ou les dimensions géométriques ou la forme de la charge propulsive ou de la poudre
F42B 5/18 - Munitions sans douille; Cartouches à douille combustible
F42B 5/38 - Charges propulsives sans projectile, p.ex. gargousses
F42C 19/085 - Amorces pour des munitions sans douille
39.
LAUNCHING DEVICE AND METHOD FOR ASSEMBLING PROJECTILES IN A LAUNCHING DEVICE
The invention relates to a modular launching device (1) for launching of projectiles (100) with a propellant charge (10) where the projectile (100) is arranged such that a detonator (20) is arranged at a projectile body (50) in the launching device (1) and assembled together with at least one propellant charge (10) in the launching device (1). Moreover, the invention relates to a method of assembling projectiles in a launching device by using modules.
F41A 9/00 - Chargement ou alimentation en munitions; Chargeurs; Moyens de guidage pour l'extraction des cartouches
F42B 5/16 - Cartouches, c. à d. projectile et douille avec charge propulsive formant un tout caractérisées par la composition ou les dimensions géométriques ou la forme de la charge propulsive ou de la poudre
F42B 5/18 - Munitions sans douille; Cartouches à douille combustible
F42B 5/38 - Charges propulsives sans projectile, p.ex. gargousses
F42C 19/085 - Amorces pour des munitions sans douille
40.
Method and system for inductive programming of a fuze
An optical module for an independent line of sight is capable of being arranged on a sight unit. The optical module contains at least a first mirror and at least a movably arranged second mirror. A method for converting an existing weapon station into a weapon station with an independent line of sight, a sight unit arranged with an optical module, and a weapon station embodied with a sight unit, wherein an optical module is arranged on the sight unit, are also provided.
The present invention relates to a method for producing a component for a warhead, wherein the method involves the steps: i.) an inner shell is arranged on a tool, ii.) preshaped projectiles are arranged on the inner shell, iii.) powder is arranged to enclose the preshaped projectiles, iv.) the powder is pressed such that the powder, the preshaped projectiles, and the inner shell are joined together, v.) the tool is removed from the component formed from the powder, the preshaped projectiles, and the inner shell. The invention further relates to a warhead and a projectile.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/22 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
The present invention relates to a method for producing a component for a warhead, wherein the method involves the steps: i.) an inner shell is arranged on a tool, ii.) preshaped projectiles are arranged on the inner shell, iii.) powder is arranged to enclose the preshaped projectiles, iv.) the powder is pressed such that the powder, the preshaped projectiles, and the inner shell are joined together, v.) the tool is removed from the component formed from the powder, the preshaped projectiles, and the inner shell. The invention further relates to a warhead and a projectile.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/22 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
The present invention includes a fire control method against aerial targets flying toward a protection object when the position of the protection object is known, the following method steps being included: measure the position of the aerial target, estimate the position of the aerial target, estimate the velocity of the aerial target, predict the future path of the aerial target from the estimated position of the aerial target and the estimated velocity of the aerial target, decide, on the basis of the predicted path, whether the aerial target i.) is incoming and thus a threat against the protection object, ii.) is passing by and thus not a threat to the protection object.
The present invention includes a fire control method against aerial targets flying toward a protection object when the position of the protection object is known, the following method steps being included: measure the position of the aerial target, estimate the position of the aerial target, estimate the velocity of the aerial target, predict the future path of the aerial target from the estimated position of the aerial target and the estimated velocity of the aerial target, decide, on the basis of the predicted path, whether the aerial target i.) is incoming and thus a threat against the protection object, ii.) is passing by and thus not a threat to the protection object.
The invention relates to a plasma generator (1) for initiation of propellant charges in a weapons system, for example when launching projectiles from a barrel weapon, by electrical discharge between a rear electrode (22) and a front electrode (21) in a combustion chamber channel (3) enclosed in a combustion chamber body (30) and filled with filling gas, designed to ignite at least one propellant charge (11). The invention also relates to an ammunition unit and a launching device comprising said plasma generator.
F41A 19/63 - Mécanismes de mise à feu électriques comportant des moyens pour la transmission sans contact d'énergie électrique, p.ex. par induction, par étincelles
The invention relates to a brake (10, 20, 30, 40, 50) for detachable arrangement on projectiles, characterized in that the brake is configured with a surface (X1, X1', X2, X2', X3, X4, X5) which is situated in the direction of travel of the projectile, where the surface (X1, X1', X2, X2', X3, X4, X5) is larger than a surface (X) given by πR2-πr2, where R is the outer radius of the brake (R1, R1', R2, R2', R3, R4, R5) and r is the inner radius (r1, r1', r2, r2', r3, r4, r5) of the brake. The invention furthermore consists of a method for braking projectiles.
A payload container for providing a horizontal dispersion pattern of sub-projectiles suitable for combatting surface targets is in the form of a cylinder and includes at least two sub-projectiles arranged in a core enclosed by a container wall, wherein the sub-projectiles are linearly disposed. In addition, a projectile and use of the same include at least one payload container or a plurality of sequentially arranged payload containers displaced by a displacement angle relative to each other. The displacement angle is predetermined in such way so that the sub-projectiles are vertically lined at the time when the mechanical force from the carrier shell disappears and the sub-projectiles are spread to the left and to the right, providing a horizontal dispersion pattern.
F42B 12/60 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés radialement
F42B 10/26 - Dispositions pour la stabilisation par rotation
The invention is a method to improve the impact point for at least one subsequent projectile fired towards a target, launched after an initial projectile, where the subsequent projectiles can alter their course, based on information on the previous projectiles' time of automatic detonation, to improve the ability to detect a target. The invention also consists of a projectile and a fuse.
The invention is a method to improve the impact point for at least one subsequent projectile fired towards a target, launched after an initial projectile, where the subsequent projectiles can alter their course, based on information on the previous projectiles' time of automatic detonation, to improve the ability to detect a target. The invention also consists of a projectile and a fuse.
The invention comprises a method for calculating the bursting point of at least one projectile fired at a target object, involving the following method steps: measuring the position of the projectile, estimating the position of the projectile, estimating the speed of the projectile, measuring the position of the target object, estimating the position of the target object, estimating the speed of the target object, calculating optimal bursting points for the projectile based on the estimated position of the projectile, the estimated speed of the projectile, the estimated position of the target object and the estimated speed of the target object, and communicating the bursting points for the projectile to the projectile. The invention furthermore comprises a computer program, a computer system, and a weapons system.
The invention comprises a method for calculating the bursting point of at least one projectile fired at a target object, involving the following method steps: measuring the position of the projectile, estimating the position of the projectile, estimating the speed of the projectile, measuring the position of the target object, estimating the position of the target object, estimating the speed of the target object, calculating optimal bursting points for the projectile based on the estimated position of the projectile, the estimated speed of the projectile, the estimated position of the target object and the estimated speed of the target object, and communicating the bursting points for the projectile to the projectile. The invention furthermore comprises a computer program, a computer system, and a weapons system.
An autonomous weapon system for improved guidance of a projectile for homing a target includes a guided projectile including at least one sensor and a carrier projectile and at least one guidance and reconnaissance unit including a transmitter for communication via light. The system uses emitted light for both positioning and communication of target coordinates which provides an accurate and cost effective system for combatting point and surface targets by indirect fire.
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
F42B 12/36 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation
F41G 7/30 - Systèmes de guidage à liaison de commande
F41G 9/00 - Systèmes de commande des missiles ou projectiles, non prévus ailleurs
F42B 12/58 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles
A tail portion for a fin-stabilized projectile includes at least two deployable fins, which are inclined. The fins are arranged in at least two sections, which are arranged adjacent to another in the axial direction.
A holding device and method for decreasing the contact-impact event on sub-projectiles when fired from a barrel, cylinder, carrier shell or the like includes a core and at least two legs that at least partially enclose at least one sub-projectile each. When a projectile is fired from a barrel or the like the sub-projectiles load the legs of the device which are deformed and open up and release the sub-projectiles in a controlled manner without tumbling which leads them to hit and penetrate their target with the short-side. A holding device including sub-projectiles and a projectile including the holding device are also provided.
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
A fuse is provided with a reversible airbrake intended for a projectile, wherein the airbrake is arranged such that errors which occur in the flight path of the projectile can be corrected by performing one or more extensions and retractions of the airbrake. The airbrake includes at least two braking surfaces symmetrically arranged each behind a respective protective device arranged on the casing surface of the fuse, wherein the brake surfaces can be extended and retracted in a rotational direction behind the at least two protective devices via a twist shaft arranged centrally in the fuse.
A warhead includes an outer casing and an inner shell, which delimits a central space for an explosive substance. The inner shell receives a series of preformed elements, which are arranged in contact with the outer side of the inner shell. The inner shell is arranged for a controlled fragmentation upon a detonation of the explosive substance. The preformed elements are arranged with a surface contact against the inner shell.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
A method for producing a warhead with directed blasting action involves the step of making an outer casing and arranging therein a charge with a cavity situated at the front end of the charge. An insert (9) whose shape corresponds to the shape of the cavity is arranged on the surface of the charge. The method furthermore involves the step of depositing a material (10a, 10b) on the insert (9) in an additive manufacturing process. A warhead manufactured according to the method comprises an outer casing, a charge with a cavity situated at the front end of the charge, and an insert (9). A material (10a, 10b) is deposited on the insert (9).
A procedure for producing a warhead (4) with controlled fragmentation comprising the step that an inner shell (1) is manufactured and filled with an explosive substance. The procedure further comprises the steps of providing a net (5) around 5 the outer surface of the inner shell (1) as well as depositing a material (8) on and around the net (5). A warhead is produced by the procedure and comprises an inner shell (1). A material (8) applied to the warhead (4) comprises weak points for guided fragmentation of the 0 deposited material (8) upon detonation of the warhead (4).
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
B33Y 80/00 - Produits obtenus par fabrication additive
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
A procedure for producing a warhead (4) with controlled fragmentation comprising the step that an inner shell (1) is manufactured and filled with an explosive substance. The procedure further comprises the steps of providing a net (5) around 5 the outer surface of the inner shell (1) as well as depositing a material (8) on and around the net (5). A warhead is produced by the procedure and comprises an inner shell (1). A material (8) applied to the warhead (4) comprises weak points for guided fragmentation of the 0 deposited material (8) upon detonation of the warhead (4).
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
B33Y 80/00 - Produits obtenus par fabrication additive
F42B 33/00 - Fabrication de munitions; Démontage de munitions; Appareils à cet effet
A method for producing a warhead with directed blasting action involves the step of making an outer casing and arranging therein a charge with a cavity situated at the front end of the charge. An insert (9) whose shape corresponds to the shape of the cavity is arranged on the surface of the charge. The method furthermore involves the step of depositing a material (10a, 10b) on the insert (9) in an additive manufacturing process. A warhead manufactured according to the method comprises an outer casing, a charge with a cavity situated at the front end of the charge, and an insert (9). A material (10a, 10b) is deposited on the insert (9).
A projectile with selectable angle of attack for increased impact on a target includes an active charge and controllable initiation device for initiation of the active charge, wherein the projectile also includes at least one side-acting impulse motor for tilting the projectile relative to its trajectory from a substantially vertical position, in which the front face of the projectile is directed toward the target, into a more horizontal position, in which the outer surface of the projectile is directed toward the target.
F42B 10/66 - Pilotage par variation de l'intensité ou de la direction de la poussée
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
65.
Attachment arrangement for a gun module on a carrier
An attachment arrangement for a gun module of a carrier, such as a vehicle, a craft, or a structure fixedly mounted on a foundation, including, fixedly mounted on the carrier, a carrier frame. The carrier frame has at least two elongated frame portions, and the attachment arrangement includes an intermediate beam, on which the gun module is arranged. A subframe is arranged on the carrier frame, and a pair of interacting mounting plates are arranged on the subframe and the intermediate beam respectively. A weapons system includes an attachment arrangement and a superstructure module having storage spaces on top of the subframe.
The invention relates to a brake assembly (100) to enable the braking of a projectile on its trajectory, comprising at least two brake flaps (5, 6), wherein the two brake flaps are formed by an upper brake flap (5) and a lower brake flap (6), arranged at different positions in the axial direction of the projectile, such that the full span (L-L), where the full span is the distance (L-L) between the outer edge of the upper brake flap (5) and the outer edge of the lower brake flap (6) when the brake flaps (5, 6) are situated in the fully unfolded condition, is greater than twice the projectile diameter (D-D). Moreover, the invention relates to a detonator with the described brake assembly, a method of controlling the longitudinal dispersion, and a projectile with the described detonator.
Shell (1) for firing from a barrel, said shell (1) comprises a shell body (2) comprising at least two warheads (8) axially arranged one after another in the shell body (2), said warheads (8) comprising explosive charges (12) arranged for shaped charge effect in the direction of travel of the shell (1). The shell is (1) is arranged to provide the smallest possible radial dispersion of fragments when engaging a target to prevent damages to the civilian population and to civilian equipment. Characteristic for the shell (1) is that the shell body (2) also comprises an ejecting device (13) for ejecting the warheads (8) from the shell body (2) in accordance in a determined time sequence in the direction of travel of the shell (1), and an initiating device (14) for initiating the explosive charges (12) of the warheads (8) in accordance with determined time sequence.
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
68.
SHELL WITH MULTIPLE WARHEADS AND A FIRING PROCEDURE THEREFORE
Shell (1) for firing from a barrel, said shell (1) comprises a shell body (2) comprising at least two warheads (8) axially arranged one after another in the shell body (2), said warheads (8) comprising explosive charges (12) arranged for shaped charge effect in the direction of travel of the shell (1). The shell is (1) is arranged to provide the smallest possible radial dispersion of fragments when engaging a target to prevent damages to the civilian population and to civilian equipment. Characteristic for the shell (1) is that the shell body (2) also comprises an ejecting device (13) for ejecting the warheads (8) from the shell body (2) in accordance in a determined time sequence in the direction of travel of the shell (1), and an initiating device (14) for initiating the explosive charges (12) of the warheads (8) in accordance with determined time sequence.
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
69.
PROCEDURE FOR DIRECTIONAL WARHEAD AND WARHEAD THEREFOR
The present invention relates to a procedure and to a warhead (1) for accomplishing an increased effect at or after penetration of a protection, in which warhead (1) a minimum of two explosive charges (3, 4), a forward placed explosive charge (3) and a rear placed explosive charge (4) are arranged after each other in the warhead's (1) direction of effect A where each rear placed explosive charge (4) separates from each forward placed explosive charge (3) by an intermediate spacer (9) and a confinement element (10) for deflection of a rearward shock effect C generated at initiation. Characterizing is that the confinement element (10) is arranged on the forward explosive charge's (3) rear confinement surface and integrates with the explosive charge (3).
The present invention relates to a procedure and to a warhead (1) for accomplishing an increased effect at or after penetration of a protection, in which warhead (1) a minimum of two explosive charges (3, 4), a forward placed explosive charge (3) and a rear placed explosive charge (4) are arranged after each other in the warhead's (1) direction of effect A where each rear placed explosive charge (4) separates from each forward placed explosive charge (3) by an intermediate spacer (9) and a confinement element (10) for deflection of a rearward shock effect C generated at initiation. Characterizing is that the confinement element (10) is arranged on the forward explosive charge's (3) rear confinement surface and integrates with the explosive charge (3).
fill, wherein the method comprises the following steps: —pre formation of the cavities (5) in the warhead shell (4), —arrangement of at least one projectile (7) in each pre formed cavities (5), —filling of filler material or agent (8) in the cavities (5) so that the cavities (5) are filled, —treatment of the filler material or agent (8) so that the filler material or agent (8) forms a connected structure vid high adhesiveness to the projectiles (7) and to the walls of the cavity (5). The invention further relates to a pre fragmented warhead.
F42B 12/22 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
The invention relates to method for pre-fragmentation of a warhead (1) comprising a warhead body (2), an explosive charge (6), and a warhead shell (4) with the density pSheii/ wherein the warhead shell (4) comprises pre-formed cavities (5), where each cavity (5) comprises at least one pre-formed projectile (7) with the density ppr0j and filler material or agent (8) with the density pfm, wherein the method comprises the following steps (in an arbitrary order) : - pre-formation of the cavities (5) in the warhead shell (4), - arrangement of at least one projectile (7) in each pre-formed cavities (5), - filling of filler material or agent (8) in the cavities (5) so that the cavities (5) are filled, - treatment of the filler material or agent (8) so that the filler material or agent (8) forms a connected structure with high adhesiveness to the projectiles (7) and to the walls of the cavity (5). The invention further relates to a pre-fragmented warhead.
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
74.
AUTONOMOUS WEAPON SYSTEM FOR GUIDANCE AND COMBAT ASSESSMENT
The present invention provides an autonomous weapon system (1) for improved guidance of a projectile for homing a target, the system (1) comprises a guided projectile (3) comprising at least one sensor (33) and a carrier projectile (2) and at least one guidance and reconnaissance unit (A) comprising a transmitter (11) for communication via light. The system use emitted light for both positioning and communication of target coordinates which provides an accurate and cost effective system for combatting point and surface targets by indirect fire.
F41G 3/02 - Dispositifs de pointage utilisant une ligne de visée indépendante, p.ex. télépointeur
F41G 7/30 - Systèmes de guidage à liaison de commande
F41G 9/00 - Systèmes de commande des missiles ou projectiles, non prévus ailleurs
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
F42B 12/36 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
75.
Method and arrangement for modifying a separable projectile
A method for modifying a separable projectile between a test embodiment or an effect embodiment includes detaching the front projectile body from the rear projectile body, arranging a payload container in the front projectile body where the payload container comprises measuring equipment or an effect part, and fitting the front projectile body to the rear projectile body by way of a belt. A separable projectile which can be modified between a test embodiment and an effect embodiment is also provided.
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
F42B 30/00 - Projectiles non prévus ailleurs, caractérisés par la catégorie ou le type de munitions, p.ex. par le lanceur ou l'arme utilisés
F42B 12/36 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation
A warhead (1) comprises an outer casing (8) and an inner shell (7), which delimits a central space (5,6) for an explosive substance. The inner shell (7) receives a series of preformed elements (9), which are arranged in contact with the outer side of the inner shell (7). The inner shell (7) is arranged for a controlled fragmentation upon a detonation of the explosive substance. The preformed elements (9) are arranged with a surface contact against the inner shell (7).
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
A warhead (1) comprises an outer casing (8) and an inner shell (7), which delimits a central space (5,6) for an explosive substance. The inner shell (7) receives a series of preformed elements (9), which are arranged in contact with the outer side of the inner shell (7). The inner shell (7) is arranged for a controlled fragmentation upon a detonation of the explosive substance. The preformed elements (9) are arranged with a surface contact against the inner shell (7).
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
F42B 12/24 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
78.
System and method for the reversible transfer of ammunition between a primary magazine and a secondary magazine in an automatic cannon
An ammunition loading system for loading ammunition into a primary magazine in an automatic cannon includes at least one secondary magazine arranged in an ammunition store beneath the primary magazine of the automatic cannon, a hoisting device for transporting the aforementioned at least one secondary magazine from the ammunition store to the primary magazine, a docking and transfer mechanism for the docking of the secondary magazine with the primary magazine and for the transfer of ammunition between the secondary magazine and the primary magazine, as well as a common drive arrangement for synchronous driving of the secondary magazine and the primary magazine during the transfer of ammunition. A method for the aforementioned ammunition loading system is also provided.
F41A 9/76 - Chargeurs munis d'un convoyeur à bande ou à chaîne sans fin
F41A 9/24 - Alimentation en munitions sans bande utilisant un chargeur ou un magasin mobiles comme dispositif d'alimentation
F41A 9/04 - Alimentation en munitions sans bande utilisant des convoyeurs à bande sans fin supportant plusieurs munitions
F41A 9/21 - Plateaux ou augets mobiles de chargement des munitions, p.ex. pour l'alimentation à partir de chargeurs coulissants, p.ex. à mouvement de va-et-vient dans une direction verticale
79.
DEVICE AND METHOD FOR PROVIDING A HORIZONTAL DISPERSION PATTERN
The present invention provides a payload container (10) for providing a horizontal dispersion pattern of sub-projectiles (1, 1´) suitable for combatting surface targets. The container (10) is in the form of a cylinder and comprises at least two sub-projectiles (1) 5 arranged in a core (3) enclosed by a container wall (2), wherein the sub-projectiles (1) are linearly disposed. The invention also provides a projectile (50) and use of the same comprising at least one payload container (10) or a plurality of sequentially arranged payload containers (10). The displacement is predetermined in such way so that the sub-projectiles (1, 1´) are vertically lined at the time 0 when the mechanical force from the carrier shell disappears and the sub-projectiles (1, 1´) are spread to the left and to the right, providing a horizontal dispersion pattern
F42B 12/60 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés radialement
F42B 10/26 - Dispositions pour la stabilisation par rotation
F42B 14/02 - Ceintures de guidage; Ceintures de rotation
The present invention concerns a fuse (3) with a reversible airbrake (1) intended for a projectile (2), wherein the airbrake (1) is arranged such that errors which occur in the flight path of the projectile (2) can be corrected by performing one or more extensions 5 and retractions of the airbrake (1). The airbrake (1) comprises at least two braking surfaces (8) symmetrically arranged each behind a respective protective device (5) arranged on the casing surface (4) of the fuse (3), wherein the brake surfaces (8) can be extended and retracted in a rotational direction behind said at least two protective devices (5) via a twist shaft arranged centrally in the fuse (3).
The present invention concerns a fuse (3) with a reversible airbrake (1) intended for a projectile (2), wherein the airbrake (1) is arranged such that errors which occur in the flight path of the projectile (2) can be corrected by performing one or more extensions 5 and retractions of the airbrake (1). The airbrake (1) comprises at least two braking surfaces (8) symmetrically arranged each behind a respective protective device (5) arranged on the casing surface (4) of the fuse (3), wherein the brake surfaces (8) can be extended and retracted in a rotational direction behind said at least two protective devices (5) via a twist shaft arranged centrally in the fuse (3).
The present invention provides a holding device (5) and method for decreasing the contact-impact event on sub-projectiles (1) when fired from a barrel, cylinder, carrier shell or the like. The holding device (5) comprises a core (3) and at least two legs (2) that at least partially enclose at least one sub-projectile (1) each. When a projectile is fired from a barrel or the like the sub-projectiles load the legs (2) of the device (5) which are deformed and open up and release the sub-projectiles (1) in a controlled manner without tumbling which leads them to hit and penetrate their target with the short-side. The present invention further provides a holding device (5) comprising sub-projectiles (1) and a projectile comprising the holding device (5).
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
F42B 12/58 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles
83.
DEVICE AND METHOD FOR COUNTERACTING CONTACT-IMPACT EVENTS OF ELONGATED SUB-PROJECTILES
The present invention provides a holding device (5) and method for decreasing the contact-impact event on sub-projectiles (1) when fired from a barrel, cylinder, carrier shell or the like. The holding device (5) comprises a core (3) and at least two legs (2) that at least partially enclose at least one sub-projectile (1) each. When a projectile is fired from a barrel or the like the sub-projectiles load the legs (2) of the device (5) which are deformed and open up and release the sub-projectiles (1) in a controlled manner without tumbling which leads them to hit and penetrate their target with the short-side. The present invention further provides a holding device (5) comprising sub-projectiles (1) and a projectile comprising the holding device (5).
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
F42B 12/58 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles
84.
DEVICE AND METHOD FOR OBTAINING A HORIZONTAL DISPERSION PATTERN
The present invention provides a payload container (10) for providing a horizontal dispersion pattern of sub-projectiles (1, 1´) suitable for combatting surface targets. The container (10) is in the form of a cylinder and comprises at least two sub-projectiles (1) 5 arranged in a core (3) enclosed by a container wall (2), wherein the sub-projectiles (1) are linearly disposed. The invention also provides a projectile (50) and use of the same comprising at least one payload container (10) or a plurality of sequentially arranged payload containers (10). The displacement is predetermined in such way so that the sub-projectiles (1, 1´) are vertically lined at the time 0 when the mechanical force from the carrier shell disappears and the sub-projectiles (1, 1´) are spread to the left and to the right, providing a horizontal dispersion pattern
F42B 12/60 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés radialement
F42B 10/26 - Dispositions pour la stabilisation par rotation
F42B 14/02 - Ceintures de guidage; Ceintures de rotation
A tail portion (1) for a fin-stabilized projectile comprises at least two deployable fins (3), which are inclined. The fins (3) are arranged in at least two sections (2), which are arranged adjacent to another in the axial direction. Each section (2) preferably contains at least two fins (3), and the fins (3) which form part of one and the same section (2) are synchronously deployable by means of a linking member (4), to which the fins (3) forming part of the section (2) are coupled.
A tail portion (1) for a fin-stabilized projectile comprises at least two deployable fins (3), which are inclined. The fins (3) are arranged in at least two sections (2), which are arranged adjacent to another in the axial direction. Each section (2) preferably contains at least two fins (3), and the fins (3) which form part of one and the same section (2) are synchronously deployable by means of a linking member (4), to which the fins (3) forming part of the section (2) are coupled.
A parachute device is provided for a divisible shell that includes an active body and a shell base. The parachute device includes two parachutes, a first, main parachute connected to the active body by parachute lines and a second parachute connected to the shell base.
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
F42B 12/42 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation du type éclairant, p.ex. comportant des fusées éclairantes
B64D 17/58 - Ouverture, p.ex. manuelle automatique commandée par un mécanisme à retardement
B64D 17/72 - Déploiement des parachutes par dispositifs explosifs ou de gonflage
88.
METHOD AND SYSTEM FOR INDUCTIVE PROGRAMMING OF A FUZE
The invention relates to method and system for inductively programming fuze (140) comprising at least one target coil arranged in projectile (110) by means of fuze setter (2) comprising at least one setter coil, said method comprising i) conveying at least projectile (110) or a fuze setter (2) by means of actuating means (100, 101) to bring said at least one target coil and said at least one setter coil in an inductive coupling position, ii) programming fuze (140) by transferring predetermined fuzing data from said at least one setter coil to said at least one target coil iii) optionally transferring fuzing data from at least one target coil to said at least one setter coil to confirm correct programming of the fuze has been performed iv) retracting fuze setter (2) or projectile (110) from inductive coupling position when the transfer of fuzing data has been completed.
The invention relates to method and system for inductively programming fuze (140) comprising at least one target coil arranged in projectile (110) by means of fuze setter (2) comprising at least one setter coil, said method comprising i) conveying at least projectile (110) or a fuze setter (2) by means of actuating means (100, 101) to bring said at least one target coil and said at least one setter coil in an inductive coupling position, ii) programming fuze (140) by transferring predetermined fuzing data from said at least one setter coil to said at least one target coil iii) optionally transferring fuzing data from at least one target coil to said at least one setter coil to confirm correct programming of the fuze has been performed iv) retracting fuze setter (2) or projectile (110) from inductive coupling position when the transfer of fuzing data has been completed.
A dividable parachute grenade is provided including a grenade casing, a nose cone, a detonating fuse, a dividing charge, a payload, a parachute device, a grenade bottom, and a supporting device, wherein the supporting device is annular and includes pretensioned sector elements fixed to a fixing ring in the recess on the inner side of the grenade casing, the sector elements are pretensioned with a tension ring arranged around the annular supporting device via recessed grooves in the sector elements, whereof the supporting device is arranged extensibly in the radial direction in a recess on the inner side of the grenade casing behind the payload and supports the payload in the extended position during the acceleration phase of the grenade, and stays in the grenade after the separation of the payload from the grenade.
F42B 10/56 - Dispositions pour réduire la portée, pour la déstabilisation ou pour le freinage; Moyens pour freiner la chute d'un projectile du type à parachute
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
91.
ATTACHMENT ARRANGEMENT FOR A GUN MODULE ON A CARRIER
An attachment arrangement for a gun module (3) of a carrier (2), such as a vehicle, a craft, or a structure fixedly mounted on a foundation, comprising, fixedly mounted on the carrier (2), a carrier frame (9). The carrier frame (9) has at least two elongated frame portions, and the attachment arrangement comprises an intermediate beam (5), on which the gun module (3) is arranged. A subframe (10) is arranged on the carrier frame (9), and a pair of interacting mounting plates (13) are arranged on the subframe (10) and the intermediate beam (5) respectively. A weapons system (1) comprises an attachment arrangement and a superstructure module (4) having storage spaces (8) on top of the subframe (10).
An attachment arrangement for a gun module (3) of a carrier (2), such as a vehicle, a craft, or a structure fixedly mounted on a foundation, comprising, fixedly mounted on the carrier (2), a carrier frame (9). The carrier frame (9) has at least two elongated frame portions, and the attachment arrangement comprises an intermediate beam (5), on which the gun module (3) is arranged. A subframe (10) is arranged on the carrier frame (9), and a pair of interacting mounting plates (13) are arranged on the subframe (10) and the intermediate beam (5) respectively. A weapons system (1) comprises an attachment arrangement and a superstructure module (4) having storage spaces (8) on top of the subframe (10).
The present invention relates to a projectile (100) with selectable angle of attack for increased impact on a target, comprising an active charge (1) and controllable initiation device (2) for initiation of the active charge (1), wherein the projectile (100) also comprises at least one side-acting impulse motor (3) for tilting the projectile (100) relative to its trajectory from a substantially vertical position, in which the front face (N) of the projectile is directed toward the target, into a more horizontal position, in which the outer surface (M) of the projectile (100) is directed toward the target.
F42B 10/66 - Pilotage par variation de l'intensité ou de la direction de la poussée
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 10/06 - Ailettes placées à l'arrière du projectile
F42B 12/10 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type perforant à charge creuse ou profilée
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
The present invention relates to a projectile (100) with selectable angle of attack for increased impact on a target, comprising an active charge (1) and controllable initiation device (2) for initiation of the active charge (1), wherein the projectile (100) also comprises at least one side-acting impulse motor (3) for tilting the projectile (100) relative to its trajectory from a substantially vertical position, in which the front face (N) of the projectile is directed toward the target, into a more horizontal position, in which the outer surface (M) of the projectile (100) is directed toward the target.
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 10/06 - Ailettes placées à l'arrière du projectile
F42B 12/10 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type perforant à charge creuse ou profilée
F42B 12/32 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p.ex. de sphères en acier
The invention relates to a method for modifying a separable projectile (1,20) between a test embodiment or an effect embodiment by: i. detaching the front projectile body from the rear projectile body (3), ii. arranging a payload container (8,21) in the front projectile body where the payload container comprises measuring equipment or an effect part, and iii. fitting the front projectile body (2) to the rear projectile body (3) by way of a belt (4). The invention also relates to a separable projectile (1,20), which can be modified between a test embodiment and an effect embodiment.
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
F42B 30/00 - Projectiles non prévus ailleurs, caractérisés par la catégorie ou le type de munitions, p.ex. par le lanceur ou l'arme utilisés
97.
METHOD AND ARRANGEMENT FOR MODIFYING A SEPARABLE PROJECTILE
The invention relates to a method for modifying a separable projectile (1,20) between a test embodiment or an effect embodiment by: i. detaching the front projectile body from the rear projectile body (3), ii. arranging a payload container (8,21) in the front projectile body where the payload container comprises measuring equipment or an effect part, and iii. fitting the front projectile body (2) to the rear projectile body (3) by way of a belt (4). The invention also relates to a separable projectile (1,20), which can be modified between a test embodiment and an effect embodiment.
F42B 12/62 - Munitions en grappes ou munitions-cargo, c. à d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur
F42B 30/00 - Projectiles non prévus ailleurs, caractérisés par la catégorie ou le type de munitions, p.ex. par le lanceur ou l'arme utilisés
The invention relates to an optical module (1) for an independent line of sight, wherein the optical module is capable of being arranged on a sight unit and wherein the optical module contains at least a first mirror (2) and at least a movably arranged second mirror (5). The invention further relates to a method for converting an existing weapon station into a weapon station with an independent line of sight. The invention further relates to a sight unit arranged with an optical module. The invention further relates to a weapon station embodied with a sight unit, wherein an optical module is arranged on the sight unit.
The invention relates to an optical module (1) for an independent line of sight, wherein the optical module is capable of being arranged on a sight unit and wherein the optical module contains at least a first mirror (2) and at least a movably arranged second mirror (5). The invention further relates to a method for converting an existing weapon station into a weapon station with an independent line of sight. The invention further relates to a sight unit arranged with an optical module. The invention further relates to a weapon station embodied with a sight unit, wherein an optical module is arranged on the sight unit.
37 - Services de construction; extraction minière; installation et réparation
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Optoelectric gyro-stabilising observation/viewing platforms for artillery guns (cannons); Equipment for electromagnetic action (weapons); Firearms, ammunition and projectiles; Explosives; Fireworks. Maintenance, servicing and repair of weapon systems; Maintenance and repair of defence materials. Computer software consultancy; Configuration of computer software; Computer software design; Computer systems integration services; Installation, maintenance, updating and upgrading of computer software; Installation, maintenance and updating of computer software; Research in the field of computer programs and software; Computer software consultancy; Advisory services relating to the use of computer software; Advisory and information services relating to computer software; Advice and development services relating to computer software; Software creation; Technical consultancy relating to the application and use of computer software.
