57 results about "Artillery shell" patented technology

The present invention relates to a range extension device, particularly to a reversible range extension device, especially reversible base bleed device.There is provided a reversible range extension device, capable in use, of being reversibly engaged to a body of an artillery shell, said range extension device comprising at least one energetic material, and an igniter, wherein the range extension device comprises a first end with an aperture, and second closed end, wherein the range extension device, in use, is selectively arranged to be in an active orientation or inert orientation, wherein in the active orientation the range extension device is arranged such that the aperture faces rearwardly away from the shell to allow the range extension device to function, and in the inert orientation the range extension device is arranged such that the aperture faces inwardly towards the shell.

The utility model relates to the field of shell production, in particular to an automatic assembling device for a shell body butt-joint frame, which comprises a placing table, a press-fitting table arranged on the lower side of the placing table, a linear guide rail arranged between the press-fitting table and the placing table, a servo lifting rotating unit arranged in the middle of the placing table, and a supporting and positioning unit arranged on the front side of the servo lifting rotating unit. The elastic body is driven by the servo lifting rotating unit to rotate so that a positioning pin at the tail of the elastic body can preliminarily correspond to a pin hole of the butt joint frame, then the positioning pin at the tail of the elastic body and the butt joint frame are accurately aligned through the alignment clamping jaw, and the whole elastic body is supported through the front V-shaped supporting block and the rear V-shaped supporting block. And under the supporting of the tail supporting unit, the servo press-fitting unit pushes the butt-joint frame to be press-fitted to the tail of the projectile body, then automatic press-fitting treatment of the butt-joint frame of the whole projectile body is completed, and the butt-joint frame mounting speed of the whole projectile body is increased.

The utility model discloses a cartridge case fixing mechanism and launching device, cartridge case fixing mechanism includes: be equipped with the detachable cannonball's launching cylinder, and, be used for fixing the cannonball in the clamping module of launching cylinder, the cartridge case of cannonball is equipped with fixed groove, and clamping module has the fixed end of adaptation to fixed groove, and the fixed end has the first station of inserting into fixed groove and the second station of separating from fixed groove, and correspondingly, clamping module is used for controlling the station of fixed end. The launching device includes the cartridge case fixing mechanism. Replace the existing thread connection through clamping module, do not need repeatedly screwing loose and tightening thread, reduce the cumbersome nature of cannonball loading, dismounting, realized the quick loading of cannonball, the quick dismounting of cartridge case, make the operation simple and convenient to use, effectively shorten the combat readiness time.

The invention discloses automatic filling equipment for square propellant bags of cannonballs and missiles. The automatic filling equipment is sequentially provided with a square propellant bag feeding mechanism, a propellant bag feeding mechanism, a propellant bag sewing mechanism and a finished product discharging mechanism according to the machining process. The lower ends of the medicine bag feeding mechanisms are provided with medicine bag opening mechanisms corresponding to the medicine bag feeding mechanisms. An ammunition feeding mechanism for realizing feeding for the ammunition packaging mechanism is arranged at the feeding position of the ammunition packaging mechanism; a set of medicine bag transferring mechanisms are further arranged, and the medicine bag transferring mechanisms extend to the finished product discharging mechanism from the square medicine bag feeding mechanism. Automatic ammunition filling processing of square ammunition bags can be achieved, and the effects of automatic adjustment of feeding, automatic bag opening filling, automatic sewing and automatic discharging can be achieved; manual participation is not needed in the working process; the processing effect of accurate weighing and discharging can be achieved through the medicine package feeding mechanism; the filling weight precision of the filling work can be effectively ensured; and the overall machining efficiency, machining precision and machining quality are higher.

The present invention relates to a method for improving flight stability, effective range, accuracy, and destructive force by moving the center of gravity of a bullet (shell) forward, and the bullet (shell). To this end, the front part of a counterweight jacket of the bullet (shell) is designed to be thicker or higher in density than the rear part thereof, so that the center of gravity is naturally moved forward. This structural feature stabilizes the trajectory by minimizing the yaw angle during flight, and increases the force of impact transmission to the target. In addition, a material having a low specific gravity is used inside a gunpowder contact part and the rear part to further strengthen the effect of moving the center of gravity to the front part. The present invention can maintain a stable flight trajectory in both ground and underwater environments, and maximizes the performance of a bullet (shell) to increase an effective range, destructive force, and accuracy.

The utility model discloses a tracer device structure which comprises a shell, a central hole and a main charging groove which is communicated with one circumferential side of the central hole and is wound outside the central hole are arranged in the shell, a hole opening at one axial end of the central hole is an ignition opening, and black powder is filled in the ignition opening. Ignition powder pressed on the black powder and transition powder pressed on the ignition powder are arranged in the center hole, and a double-base emission tablet is further arranged in the ignition opening; the rotating direction of the main charging groove is opposite to the rotating direction of the shell during flying, and the main charging groove is filled with main charging powder and transition powder pressed on the main charging powder. After the cannonball is shot out, a stable and reliable tracer effect is achieved, and the main problems that a traditional tracer device is generally unreliable in ignition performance, scattered in the flying process and broken in fire are solved.

The application provides a cannonball tightening device and relates to the field of machining manufacturing equipment, which comprises a rack, a fixing device and a tightening device; the fixing device is arranged on the rack and is used for fixing a cannonball body; the positioning device is arranged on the rack and is used for grabbing and fixing a tail wing; the tightening device comprises a clamping assembly and a driving assembly, both of which are arranged on the rack; the output end of the driving assembly is connected with the clamping assembly; the clamping assembly is used for clamping and fixing the tail wing; and the driving assembly is used for driving the clamping assembly to tighten the tail wing. The application solves the problems of low safety coefficient and low operation efficiency caused by manual participation in traditional mortar machining equipment and has the advantages of high automation degree, high safety coefficient and high machining efficiency.

A mortar training device includes a barrel body including a bore; a shot detector contained in the barrel body and including a shot detection sensor and configured to output an electronic signal indicating a firing of an inert mortar projectile from the barrel body; a battery; a plurality of orientation sensors contained in the barrel body; and one or more processors and memory storing instructions that, when executed by the one or more processors, cause the one or more processors to receive the electronic signal from the shot detection sensor indicating that an inert mortar projectile is fired from the barrel body, and determine an elevation of the barrel body and an azimuth of the barrel body when the inert mortar projectile is fired from the barrel body based on sensor data received from the plurality of orientation sensors.

The application provides a kind of shell structure piece milling trimming processing device, relating to shell processing technical field.It includes machine body, workpiece, lifting assembly, rotary servo motor, radial assembly, angle adjusting assembly, collection assembly, inner support assembly, clamping assembly, milling assembly;The lifting assembly is arranged in the upper part of machine body, for providing vertical lifting function;The rotary servo motor is installed on the lifting part of lifting assembly, for providing controllable rotation function;The radial assembly is arranged on the rotation end of rotary servo motor, for controlling the radial position of milling;The angle adjusting assembly is arranged in the lower part of radial assembly, for controlling the milling angle.Through the setting of angle adjusting assembly, the milling angle can be changed, the trimming operation suitable for the expanding mouth edge of cannon shell is realized, and without replacing the milling tool, the trimming operation of inner circle and outer circle edge can be carried out, and the trimming effect is good.

A field gun, comprising an elevating mass and a wheeled carriage. The elevating mass includes an ordnance for firing a projectile, and a cradle for holding the ordnance at a traverse and an elevation. The ordnance includes a barrel defining a barrel axis and having a muzzle towards a front end of the field gun and a breech assembly at a rear end of the barrel. The wheeled carriage is connected to the cradle and includes at least one wheel, a rechargeable electric storage device, and a regenerative braking system, which includes a brake control configured for applying a braking force to said at least one wheel in response to movement of the wheeled carriage, said movement caused by a recoil force from the firing of the projectile from the barrel.

The application discloses a kind of remote tail control shell aerodynamic characteristic analysis method and device. Among them, the method includes: the physical modeling of the shell body of shell is carried out, and the shell model is obtained;The shell model is divided into unstructured grid and boundary conditions are set;Based on the grid and the set boundary conditions, the shell model is analyzed, and the variation law of the aerodynamic characteristics of the shell model with flight Mach number and angle of attack is obtained.The application solves the technical problem that the control difficulty caused by high rotation speed of high-rotation shell.

The present invention discloses a method and system for automatically feeding 20 mm rounds into the SPAM (Super Pull Apart Machine) for demilitarization. The method involves deploying a robot to transfer 20 mm rounds from the ammunition bin to a bowl feeder. Additionally, the method incorporates a bowl feeder for aligning and releasing ammunition onto the chain conveyor to feed 20 mm rounds to the SPAM at a specified feed rate. Lastly, the method includes a control and management system to coordinate all components within the feed system through communication units, along with user software for operators to monitor and control the feeding process. The present invention enhances the safety of the demilitarization process by minimizing manual handling of hazardous materials, thus reducing the risk of accidents and injuries. Additionally, it reduces operational costs and increases demilitarization efficiency.

The invention relates to a projectile (10), in particular a medium-caliber projectile for mobile and stationary air, naval and tank guns, comprising: - having a body (12), having: - a cavity (16) for receiving a payload, - a front section (18) having an opening leading to the cavity (16) and an annular end face (22) that is coaxial with a longitudinal axis L of the projectile (10) and surrounds the opening, and - a first connecting element (20); - a hood (14), comprising: - a rear section (26) that closes the opening of the body (12) and has an annular contact surface (30) that runs coaxially to the longitudinal axis L, and - a second connecting element (28) which detachably engages the first connecting element (20) in such a way that the body (12) and the hood (14) are pressed against each other; In order to improve the sealing of the cavity (16) in such a floor (10), it is provided that: - the end face (22) has a first, essentially funnel-shaped sealing surface (24) which extends around the longitudinal axis L with a first cone angle α; - the mounting surface (30) has a second, essentially conical sealing surface (32) which extends around the longitudinal axis L with a second cone angle β; - the two cone angles α, β differ by a difference angle δ1 = β - α ≠ 0°; and - the two sealing surfaces (24, 32) lie sealingly against each other via an essentially circular sealing point (34).

The invention discloses a light-gas gun perforated baffle device, and belongs to the technical field of experimental physics and launching devices. The device comprises a supporting and fixing assembly, a baffle with holes and a centering assembly. The supporting and fixing assembly is composed of a baffle fixing support and a baffle support and used for fixing the device in the light-gas gun impact bin. And a through hole is formed in the perforated baffle plate and is used for separating shots and intercepting experimental debris. The centering assembly comprises a centering stick and a centering stick cap and is used for ensuring that the through hole of the baffle is accurately aligned with the axis of the gun barrel. The device can effectively solve the problems that a traditional light-gas shell is difficult in bullet separation, unstable in energy release, potential in safety hazard and the like, has the advantages of being simple in structure, convenient to operate, high in reliability and the like, and can be widely applied to the field of impact loading experiments.

The embodiment of the present application provides a kind of cannonball conveying power assisting device, cannonball conveying power assisting device includes support, conveying mechanism, jacking mechanism and buffer mechanism, conveying mechanism is used to convey cannonball, conveying mechanism is hingedly connected on support, conveying mechanism can selectively rotate relative to support, conveying mechanism includes the first part and the second part connected, first part and second part are located at the two sides of support respectively, jacking mechanism is connected to first part, buffer mechanism is connected to second part, buffer mechanism is used to form buffer to cannonball, first part constitutes the feeding position of cannonball, second part constitutes the discharge position of cannonball, when conveying mechanism is in unfolded state, jacking mechanism drives first part to rise, synchronously drives second part to drop, to convey cannonball to second part located in first part, realize the conveying of cannonball.The technical scheme of the present application can more conveniently realize the conveying of cannonball.

Systems and methods are presented for control of munitions, missiles and projectiles in flight and more particularly with the use of activatable or deployable flow effectors that remain stowed or inactive during launch or firing, and can be actuated after launch or firing on demand. More specifically, systems and methods are presented for control of munitions, missiles, and projectiles by activating and / or deactivating a control actuation system (CAS) based on measurements of an inertial measurement unit (IMU) and sensors integrated into such IMU, the IMU and sensors being at least part of a configurable guidance sensor suite (CGSS).

The invention relates to the related technical field of cartridge case recovery and treatment devices, in particular to an intelligent bullet and cannon cartridge case comprehensive treatment device which comprises a bottom plate, and a cleaning assembly, a rotating assembly, a collision cylinder, a front baffle, a rear baffle, an adjustable discharging assembly and a safe circulating filtering assembly are arranged on the bottom plate. The rotating assembly drives the collision cylinder to rotate, a plurality of partition plates and a plurality of stirring assemblies are evenly arranged in the collision cylinder and used for conducting high-strength collision on a cartridge case in the closed cavity, an inner cavity of the collision cylinder communicates with the safe circulating filtering assembly and is filled with inert gas, and gunpowder stripping, gas circulation and safe dust collection are achieved. The adjustable discharging assembly is matched with the partition plate to control the collided cartridge cases to be discharged into the cleaning pool in order. Through continuous linkage of inert environment collision stripping and automatic wet cleaning, the safety, high efficiency and automation of the cartridge case treatment process are achieved, and the industrial problems that the burning and explosion risk of residual gunpowder is large, the manual pretreatment efficiency is low, and procedure linkage is broken are thoroughly solved.

The utility model discloses a shell structure of a cracker. Comprising a large-diameter cylinder and a small-diameter cylinder, the large-diameter cylinder and the small-diameter cylinder are in transition through a conical section, annular limiting structures are arranged on the inner walls of the upper end and the lower end of the large-diameter cylinder and used for fixing an upper paperboard and a lower paperboard, and longitudinal ribs are arranged on at least one side of the two sides of the annular limiting structure on the lower side. The artillery shell structure disclosed by the utility model can meet the requirement of mechanical production, and is beneficial to improving the production efficiency and the quality of products.

The application relates to a general artillery shell ejection and bore comprehensive detection device, which comprises a basic module and a functional module; the basic module comprises a rotating unit, a braking unit, a battery unit and a power unit; the functional module comprises a fuze rotating ejection unit, an ejection unit and / or a bore peeping unit; the rotating unit is used for splicing with the functional module and is also used for providing rotating power for the functional module; the braking unit is used for providing a braking function; the power unit is used for providing a moving function; the battery unit is used for power supply; the fuze rotating ejection unit is used for separating a fuze from a shell; the ejection unit is used for pushing the shell away from a bore; and the bore peeping unit is used for providing a bore peeping function. The general artillery shell ejection and bore comprehensive detection device can provide walking, braking and rotating functions through the basic module; different functional modules provide different functions; the functional modules are spliced on the main structure to realize the functions of rotating fuze, ejection and bore peeping; and the artillery maintenance and support requirements are met.

Disclosed herein is a shell simulated shooting simulation system for performing a shell simulated shooting similar to a live shell shooting includes an execution module loading and aiming a shell to perform a shell simulated shooting, a display module visually displaying shooting of a shell according to loading and aiming through the execution module, and a server module collecting information to visually display a result of the live shell shooting on the display module based on the information on the loading and aiming of the shell of the execution module.

The present disclosure introduces an apparatus comprising an artillery projectile, the artillery projectile comprising: a body comprising external threads; and a band threaded to the external threads and configured to cooperate with an inner surface of a barrel of an artillery piece to thereby impart rotation to the artillery projectile during launch from the artillery piece.

Provided is a long-range rocket-assisted artillery projectile comprising an internal rocket engine, an expulsion unit and optionally a base bleed unit, wherein the expulsion unit is configured to induce or pressure-induce efficient mid-flight separation of the projectile rear end part from the front end part.

A method for manufacturing artillery projectiles is disclosed, involving forging a steel base and welding it to a separately formed body using Gas Tungsten Arc Welding / Tungsten Inert Gas (GTAW / TIG) welding. This hybrid approach offers performance comparable to that of fully forged projectiles while reducing the need for large forging presses, thereby lowering production costs and enabling decentralized, scalable manufacturing with modular and mobile facilities. By forging only the base, the method simplifies production, enhances quality control, and increases resilience against supply chain disruptions.

The application provides a kind of guided artillery shell dynamics parameter identification method based on double-layer game UKF, this method mainly includes filter model construction and UKF filtering improvement two parts, according to six degrees of freedom trajectory dynamics model and aerodynamic extension equation, filter model is constructed, so as to obtain system state equation, according to the parameter coupling relationship between guided artillery shell dynamics model and inertial device, decoupling is obtained gyro output angular velocity and accelerometer output specific force, so as to construct system observation equation;Based on the innovation of filter model and prior observation data, design a kind of double-layer game improved UKF method, inner game is composed of noise mapping method and Sage-Husa method, for evaluating the dynamic relationship between prediction and actual measurement;Outer game assesses two kinds of adaptive methods by calculating Mahalanobis distance, which reflects the game between the predicted observation covariance and the actual measurement covariance.The application can adapt to unknown noise environment, self-adapting adjustment observation noise covariance, improve guided artillery shell parameter identification precision.

The utility model relates to the technical field of recoil-free cannon, in particular to a structure for fixedly connecting a bullet and a cartridge barrel of a recoil-free cannon, which comprises a bullet body filled with the bullet, a cartridge case is sleeved outside the bullet body, propellant powder is filled in the cartridge case, and an ignition end of the cartridge case is connected with a throat complex; the tail of the projectile body is connected with a turbine; an annular positioning plate is further arranged in the cartridge case, the outer edge of the positioning plate is fixed between the cartridge case and the throat complex, and the inner edge of the positioning plate is fixed between the projectile body and the turbine. Compared with a traditional cartridge case fixing mode, the cartridge case fixing device has the advantages that the bullet body is assisted to be fixed in the cartridge case through the mode that the positioning plate is clamped between the components, the original stability is kept, meanwhile, the breaking difficulty of the positioning plate during bullet launching is lowered, the synchronism of bullet launching and positioning plate breaking is guaranteed, and the flight stability of the bullet is improved.

The invention relates to a rammer (1) for positioning an artillery shell, the rammer (1) comprising a stretcher (2) intended to receive the shell and guide it in translation, the rammer (1) being characterized in that it comprises a pusher (4) which can be driven in a reciprocating movement along the stretcher (2), reciprocating movement which is provided by a pair of closed flexible links (6) arranged on either side of the pusher (4), each link (6) connecting a drive wheel (6b) and a free wheel (6a), the pusher (4) having a bearing surface intended to correspond with a rear face of the shell in order to push it.

The utility model discloses a multifunctional primer dismounting device, which comprises a fastening component, a primer dismounting component and a primer dismounting component, and is characterized in that the fastening component is used for supporting and fixing a to-be-dismounted shell; and the dismounting assembly is detachably fixed at the tail part of the shell and is used for rotationally taking out the primer from the shell after the primer is fixed. The device provided by the utility model is simple in structure, simple in disassembly operation and convenient to carry; according to the device, the shell can be reliably fixed, it is ensured that no relative sliding exists between the dismounting assembly and the shell, mechanical damage to a shell body in the primer dismounting process is reduced, and the safety in the primer dismounting process is improved; the device can be suitable for dismounting cannonball primers with different calibers, and is good in universality.

The utility model discloses a fire insulation device used for a bird repelling bomb launcher, the fire insulation device is arranged on the bird repelling bomb launcher, and the fire insulation device comprises a mounting seat, a fire extinguishing device and a fire extinguishing device, the mounting seat is arranged on the rear side surface of a gun carriage and is positioned on the tail end side of a gun barrel; the gun barrels are connected with the mounting base, the long partition plates are connected with the mounting base, the long partition plates are arranged between every two adjacent gun barrels and distributed on the rear side face of the gun carriage, the upper surfaces of the long partition plates are higher than the tail end faces of the gun barrels, and each gun barrel is partitioned by the long partition plates to form an independent isolation space. The fire insulation device for the bird repelling bomb launcher is used on the bird repelling bomb launcher, is in a radial shape, is formed by connecting a plurality of long partition plates and a mounting seat, and is mainly used for isolating each gun barrel into an independent space. And flames rushed out after the cannonball explodes in the cannon barrel are prevented from flying to other cannon barrels, so that other cannonball leads are ignited, and the effect of accurately controlling firing is achieved.

This invention discloses a dual-axial flame input and output selectable delay tube for instantaneous / short delay, comprising a tube shell, an upper ignition pad, a lower ignition pad, a washer, a first ignition charge, a second ignition charge, a delay charge, and an initiating charge. Ignition holes are located at the center of the top and bottom surfaces of the tube shell. The upper ignition pad, first ignition charge, delay charge, initiating charge, second ignition charge, lower ignition pad, and washer are sequentially filled into the tube shell from top to bottom. The upper ignition pad is located between the first ignition charge and the tube shell, and the washer is located between the lower ignition pad and the tube shell. This invention is used in the setting bolt of the fuse triggering time setting mechanism for medium and large caliber artillery shells. It adopts a dual-axial flame input excitation structure, replacing the original single-direction flame input excitation method of delay tubes. Combined with the setting bolt setting orientation, it achieves selectable modes for both instantaneous and short delay action times. This simplifies the fuse setting mechanism structure, and its small size and simple charge structure facilitate manufacturing and installation.