CN114963885A - Hot-press-connection sealing sleeve type composite non-lethal kinetic energy bullet - Google Patents
Hot-press-connection sealing sleeve type composite non-lethal kinetic energy bullet Download PDFInfo
- Publication number
- CN114963885A CN114963885A CN202210695197.XA CN202210695197A CN114963885A CN 114963885 A CN114963885 A CN 114963885A CN 202210695197 A CN202210695197 A CN 202210695197A CN 114963885 A CN114963885 A CN 114963885A
- Authority
- CN
- China
- Prior art keywords
- warhead
- cavity
- bullet
- assembly
- cylinder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 231100001160 nonlethal Toxicity 0.000 title claims abstract description 19
- 239000002131 composite material Substances 0.000 title claims abstract description 15
- 238000007789 sealing Methods 0.000 title claims abstract description 12
- 239000000843 powder Substances 0.000 claims abstract description 46
- 239000006260 foam Substances 0.000 claims abstract description 42
- 238000007731 hot pressing Methods 0.000 claims abstract description 24
- 239000007921 spray Substances 0.000 claims abstract description 22
- 230000004936 stimulating effect Effects 0.000 claims abstract description 12
- 238000004043 dyeing Methods 0.000 claims abstract description 8
- 230000000149 penetrating effect Effects 0.000 claims abstract description 4
- 239000003380 propellant Substances 0.000 claims description 13
- 230000005540 biological transmission Effects 0.000 claims description 9
- 239000010410 layer Substances 0.000 claims description 8
- 230000006835 compression Effects 0.000 claims description 7
- 238000007906 compression Methods 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 7
- 239000007850 fluorescent dye Substances 0.000 claims description 6
- 239000002356 single layer Substances 0.000 claims description 6
- 239000003721 gunpowder Substances 0.000 claims description 5
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 239000006261 foam material Substances 0.000 claims description 4
- 230000005484 gravity Effects 0.000 claims description 4
- 229920000915 polyvinyl chloride Polymers 0.000 claims description 4
- 239000004800 polyvinyl chloride Substances 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 229910001369 Brass Inorganic materials 0.000 claims description 3
- 239000004831 Hot glue Substances 0.000 claims description 3
- 239000004677 Nylon Substances 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 239000010951 brass Substances 0.000 claims description 3
- 238000001746 injection moulding Methods 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 238000005192 partition Methods 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 3
- 229920000642 polymer Polymers 0.000 claims description 3
- 230000001413 cellular effect Effects 0.000 claims description 2
- 150000001875 compounds Chemical class 0.000 claims description 2
- 230000006378 damage Effects 0.000 abstract description 9
- 208000027418 Wounds and injury Diseases 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 230000000694 effects Effects 0.000 abstract description 2
- 230000000638 stimulation Effects 0.000 abstract description 2
- 238000003860 storage Methods 0.000 abstract description 2
- 238000002360 preparation method Methods 0.000 description 5
- 239000007789 gas Substances 0.000 description 3
- 238000009987 spinning Methods 0.000 description 3
- 239000002737 fuel gas Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 238000002679 ablation Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000011499 joint compound Substances 0.000 description 1
- 230000001665 lethal effect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/74—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
- F42B12/80—Coatings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/02—Bullets
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Abstract
The invention discloses a hot-press-connection sealing sleeve type composite non-lethal kinetic energy bomb which comprises a front warhead assembly, a bomb body assembly, a rear warhead assembly and a launching assembly which are all in an axisymmetric structure, wherein the central axes of the front warhead assembly, the bomb body assembly, the rear warhead assembly and the launching assembly are mutually superposed and are connected in series from front to back, hot-pressing sealing sleeves are adopted between an elastic foam head of the front warhead assembly and a front warhead cylinder as well as between the front warhead cylinder and a bomb body front arch in the bomb body assembly to be firmly connected in a hot-pressing curling mode, compared with a penetrating bonding mode, the connection is more reliable, the storage time limit is longer, the hot-pressing sealing sleeves and a load body are rapidly broken during impact, the front warhead assembly is deformed under pressure, OC stimulating powder and fluorescent dyeing powder in the front warhead assembly are respectively ejected from upper and lower layers of spray pipes at high speed, impact energy can be effectively dissipated, excessive injury is reduced, and multiple non-acting effects of kinetic energy, stimulation dissipation and dyeing marks are achieved; the bullet body subassembly is the stereoplasm structure, but only the bullet takes part to expose, can effectively avoid the direct injury incident of stereoplasm bullet body, and the safety in utilization is higher.
Description
Technical Field
The invention relates to the technical field of non-lethal ammunition, in particular to a hot-press-fit sealing sleeve type composite non-lethal kinetic energy bomb.
Background
The non-lethal kinetic energy bullet develops from rubber bullets, wooden stick bullets, rubber bullets and cloth bag bullets to the attenuated energy kinetic energy bullet, the structure is continuously changed, the styles are continuously increased, the safety is continuously improved, and the purpose of continuous optimization and upgrading is to effectively uniform the target on the premise of ensuring the safety. The novel energy attenuation type kinetic energy bullet is characterized in that a composite type non-lethal kinetic energy bullet is used as a main body, a composite soft bullet and a hard bullet are used as components, the bullet is shot by a thread chamber riot gun, high-precision point striking is realized by spinning of a bullet, impact energy is dissipated by the self deformation of the bullet and a shear damage or buckling deformation mechanism designed in the bullet, the deformation and damage are large during short-distance high-speed impact, the energy consumption is high, and the probability of excessive injury can be reduced; however, gyro-stabilized projectiles have the possibility of air rolling when being disturbed by unstable factors, so that the situation that hard projectiles directly hit a live target is inevitably generated, and serious damage is caused, and therefore, a class of non-lethal kinetic energy projectiles need to be developed, which not only has the advantages of high precision and relatively controllable energy of the traditional composite non-lethal kinetic energy projectiles, but also does not cause the potential risk that the hard projectiles directly damage the target.
In addition, the composite non-lethal kinetic energy projectile is generally combined with various types of components, and due to different materials, the effect is often poor when the traditional bonding means is adopted between different components, so that a new technical means is required to be adopted to realize the reliable connection between different components of the projectile.
Disclosure of Invention
The invention aims to provide a thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb so as to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a hot pressing joint compound non-fatal kinetic energy bullet of cutting ferrule formula, includes preceding warhead subassembly, projectile body subassembly, back warhead subassembly and transmission subassembly, its characterized in that:
the front warhead assembly comprises an elastic foam head, a front warhead cylinder, a load body, OC stimulating powder, fluorescent dye powder, a hot-pressing sleeve and a front warhead lower cavity, the elastic foam head is of a hemispherical structure, an elastic foam head inner cavity is formed in the lower end of the elastic foam head and comprises an upper cylinder cavity and a lower cylinder cavity, the outer diameter of the upper cylinder cavity of the elastic foam head inner cavity is larger than that of the lower cylinder cavity, the front warhead cylinder is connected to the lower side of the elastic foam head in an embedded mode and is of a cylindrical structure, the front warhead cylinder comprises a load cavity, spray pipes and an embedded head, the load cavity is used for bearing the load body, the spray pipes penetrating through the side wall of the front warhead cylinder are formed in the outer side of the side wall of the load cavity and are arranged in an upper layer and a lower layer, the number of the spray pipes in a single layer is 6, and the spray pipes in a single layer are distributed in a circumferential array mode along the central axis of the front warhead cylinder, the upper part of the front warhead cylinder is provided with an embedding head in a protruding way, the embedding head comprises an upper cylinder and a lower cylinder, the outer diameter of the upper cylinder of the embedding head is larger than that of the lower cylinder, the embedding head is clamped into the inner cavity of the elastic foam head, the load body is a thin-wall cylinder, the load body comprises an upper load body cavity, a lower load body cavity and a middle load body clapboard, the upper cavity and the lower cavity of the load body are both cylindrical cavities, the middle clapboard of the load body is used for separating the upper cavity and the lower cavity of the load body, the upper cavity of the load body is filled with OC stimulating powder, the lower cavity of the load body is filled with fluorescent dyeing powder, the outer walls of the elastic foam head and the front warhead cylinder are tightly wrapped with hot-pressing envelopes, the hot-pressing envelope is designed into a thin-wall structure with a rear cylinder, a front sphere and an opening at the top, and a front warhead lower cavity is formed on a central axis at the lower part of the front warhead cylinder;
the middle lower part of the front warhead assembly is embedded with a projectile body assembly which comprises a main projectile body, a projectile band, a projectile body front arch, a projectile body clamping column and a projectile body inner cavity, the main projectile body comprises a main projectile body cylinder and a main projectile body cone, the cylinder which is arranged on the outer edge of the upper end part of the main projectile body in an extending mode is a projectile band, the upper end surface of the elastic belt abuts against the lower end surface of the front warhead cylinder, the middle part of the upper end surface of the elastic belt extends upwards to be provided with an elastic body front arch with a concave side wall, the bullet front arch is embedded into the front bullet lower cavity, the outer wall of the bullet front arch is consistent with the shape of the cavity wall of the bullet lower cavity and is tightly abutted against the cavity wall, the lower part of the main projectile body cylinder is extended with 4 projectile body clamping columns in a cylindrical shape, the 4 projectile body clamping columns are distributed in a circumferential array along the central axis of the projectile body assembly, the main projectile body and the projectile body front arch are provided with mutually communicated cavities in the central axes, namely projectile body inner cavities;
the rear warhead assembly is embedded in the lower part of the warhead assembly and comprises an upper rear warhead, a lower rear warhead, a rear warhead concave ring, a rear warhead bearing cavity and a rear warhead cylindrical cavity, wherein the upper rear warhead and the lower rear warhead are both cylindrical, an annular groove with a semicircular section is formed in the outer edge of the contact surface of the upper rear warhead and the lower rear warhead, namely the rear warhead concave ring, a rear warhead bearing cavity is formed in the central axis of the upper rear warhead, the rear warhead bearing cavity comprises a rear warhead conical cavity and a rear warhead cylindrical cavity, the rear warhead conical cavity bears a main warhead cone, the rear warhead cylindrical cavity bears the main warhead, the upper end face of the upper rear warhead cylinder abuts against the lower end face, the lower rear warhead is provided with a cylindrical rear warhead cylindrical cavity, the number of the rear warhead cylindrical cavities is 4, and the rear warhead cylindrical cavities are distributed in a circumferential array along the central axis of the rear warhead assembly, a projectile body clamping column is embedded into the rear warhead column cavity;
the lower side of the rear warhead assembly is mechanically spliced with a launching assembly, the launching assembly comprises a warhead body, a warhead holder, a powder charge and a low-pressure chamber, the warhead body comprises a warhead shell, a warhead convex ring, a warhead shell bottom edge, a fire bottom hole, a high-pressure chamber and a fire transfer hole, the upper end surface of the warhead shell abuts against the outer edge of the lower side of the rear warhead on the upper part, the convex ring which is integrally arranged on the inner side of the upper end part of the warhead shell and has a semicircular section is the warhead convex ring, the outer diameter of the warhead shell is equal to the outer diameter of the rear warhead on the upper part, the warhead convex ring is extruded into the rear warhead concave ring, the side wall of the rear warhead on the lower part abuts against the inner side wall of the warhead shell, the bottom edge of the warhead shell is convexly arranged at the bottom of the bottom, a cylindrical fire bottom hole is arranged at the axis of the bottom surface of the warhead shell, a cylindrical high-pressure chamber is integrally arranged at the axis of the upper end surface of the high-pressure chamber, the fire transfer hole is sealed by a brass diaphragm, the cartridge case is characterized in that the inner side wall of the cartridge case is abutted against a cartridge support, the cartridge support comprises a cartridge support push disc and a cartridge support cylinder, the lower end part of a lower rear warhead is located on the upper end face of the cartridge support push disc, the lower end face of the cartridge support cylinder is abutted against the bottom of the cartridge case, the outer side wall of the cartridge support cylinder and the inner side wall of the cartridge case are sealed by hot melt adhesive, the cartridge case is internally filled with powder charges, the powder charges comprise primer and propellant powder, the primer is columnar mechanical impact type primer, the primer is riveted inside a primer hole, the propellant powder is bulk smokeless powder, the propellant powder is filled inside a high-pressure chamber, and a cavity formed by the inner side of the cartridge support and the outer side of the high-pressure chamber is a low-pressure chamber.
Preferably, preceding warhead subassembly, bullet body subassembly, back warhead subassembly and emission subassembly are the axisymmetric structure, the axis coincidence of preceding warhead subassembly, bullet body subassembly, back warhead subassembly and emission subassembly, series connection around preceding warhead subassembly, bullet body subassembly, back warhead subassembly and the emission subassembly.
Preferably, the elasticity foam head is by cellular obturator foam processing preparation, preceding warhead cylinder is by foamed aluminum processing preparation, load cavity wall is by fragile material processing preparation, the hot pressing big-envelope is the polyvinyl chloride pipe, main body, elastic ribbon, the preceding arch of body and the whole injection moulding of body card post by nylon materials, back warhead subassembly is by hard polymer foam processing preparation, the tip is covering high temperature resistant coating under the lower part back warhead, the bullet holds in the palm by light high temperature resistant plastics processing preparation, the shell of bullet is by high strength aluminum alloy material integral type machine-shaping.
Preferably, the elastic foam head, the front warhead cylinder and the front arch of the projectile body are firmly connected through hot crimping of the hot-pressing sleeve.
Preferably, after the wall of the loading body cavity is crushed under pressure, the OC stimulating powder is sprayed out along the upper spraying pipe, and the fluorescent dyeing powder is sprayed out along the lower spraying pipe.
Preferably, the shape of the projectile body cavity is of an axisymmetric structure, and the size of the projectile body cavity is set to ensure that the center of gravity and the center of thrust of a projectile formed by the front projectile body assembly, the projectile body assembly and the rear projectile body assembly coincide.
Preferably, high-temperature and high-pressure gunpowder gas generated by propellant powder combustion acts on the bullet holder, so that the bullet holder can be flushed out of the bullet shell body to push the front bullet assembly, the bullet assembly and the rear bullet assembly to advance, the bullet belt and the gun barrel rifling are matched to enable the front bullet assembly, the bullet assembly and the rear bullet assembly to synchronously spin, and after the bullet holder flies out of the gun barrel, the bullet holder is quickly separated from the rear bullet assembly due to the fact that the bullet holder is light in weight and is acted by air flow resistance force.
Compared with the prior art, the invention has the following advantages:
1. according to the hard bullet body assembly designed by the invention, only the bullet belt part is exposed, and most of structures are embedded into the front bullet head assembly and the rear bullet head assembly, so that the condition that the hard bullet body directly damages a target can be effectively avoided, and the safety performance is greatly improved;
2. the invention adopts the mode of thermally curling the elastic foam head, the front warhead cylinder and the front arch of the projectile body by the hot-pressing sleeve to realize the reliable connection of the projectile assembly, and compared with the traditional bonding means, the connection is firmer and the storage life is relatively longer;
3. when the elastic foam head is impacted, the elastic foam head is compressed, the hot-pressing envelope made of the polyvinyl chloride tube is firstly broken, the envelope is extruded by the front arch of the projectile body, the wall of the load cavity is broken, and the OC stimulating powder and the fluorescent dyeing powder are respectively sprayed out from the upper layer spray pipe and the lower layer spray pipe at high speed, so that the impact energy can be effectively dissipated, the excessive damage is reduced, and the multiple non-lethal effects of kinetic energy, stimulation dissipation and dyeing marking are achieved;
4. according to the invention, the elastic foam head, the front bullet head cylinder and the bullet front arch are firmly connected by hot curling through the hot pressing sleeve, and meanwhile, the bullet assembly and the rear bullet head assembly are clamped through 4 bullet body clamping cylinders, so that when the bullet spinning gun is spun in a gun barrel, synchronous spinning can be realized among all the assemblies, and the striking precision is favorably improved;
5. the shape of the cavity of the projectile body is in an axisymmetric structure, and the coincidence of the center of gravity and the center of thrust of the projectile is ensured by scientifically setting the size of the cavity of the projectile body, so that the flight stability of the projectile can be further improved;
6. the light high-temperature-resistant bullet holder designed by the invention can effectively isolate the ablation of high-temperature and high-pressure gunpowder fuel gas on the rear bullet head assembly, can support the restraint of the convex ring of the bullet shell by being pushed by certain fuel gas pressure, and is convenient for forming the pulling elasticity with better consistency; in addition, the lower part of the rear warhead assembly is covered with a high-temperature resistant coating, so that the rear warhead assembly can be further prevented from being ablated by high-temperature and high-pressure gunpowder gas;
7. the invention adopts a high-low pressure launching system, the launching powder adopts bulk smokeless powder, the outlet speed with better consistency can be obtained, simultaneously, the smoke amount at the muzzle is less, the normal tactical actions of users can not be interfered, and the invention does not generate excessive powder residue in the gun barrel, thereby not influencing the precision of repeated shooting and projectile and further ensuring that the invention has higher battlefield applicability.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a schematic structural view of the present invention;
FIG. 3 is a perspective view of 3/4 showing the resilient foam head 1-1 and the front warhead cartridge 1-2 of the present invention;
FIG. 4 is a perspective view 3/4 of the loading mass 1-3 of the present invention;
fig. 5 is a perspective view of the projectile assembly 2 of the present invention;
fig. 6 is a perspective view of the rear warhead assembly 3 of the present invention;
fig. 7 is a schematic structural view of the radiation module 4 of the present invention;
fig. 8 is a perspective view of the emitter assembly 4 of the present invention;
fig. 9 is a top view of the emitter assembly 4 of the present invention;
fig. 10 is a bottom view of the emitter assembly 4 of the present invention.
In the figure: 1. 1-1 part of front bullet head component, 1-1 part of elastic foam head, 1-1-1 part of elastic foam head inner cavity, 1-2 parts of front bullet head cylinder, 1-2-1 part of load cavity, 1-2-2 parts of spray pipe, 1-2-3 parts of embedding head, 1-3 parts of load body, 1-3-1 parts of load body upper cavity, 1-3-2 parts of load body lower cavity, 1-3-3 parts of load body middle partition board, 1-4 parts of OC stimulating powder, 1-5 parts of fluorescent dye powder, 1-6 parts of hot-pressing envelope, 1-7 parts of front bullet head lower cavity, 2 parts of bullet body component, 2-1 part of cone body, 2-1 part of main bullet body, 2-1-1 part of main bullet body cylinder, 2-1-2 parts of main bullet body, 2-2 parts of bullet belt, 2-3 parts of bullet belt, 2-4 parts of projectile body front arch, 2-5 parts of projectile body clamping column, 2-5 parts of projectile body inner cavity, 3 parts of rear projectile head assembly, 3-1 parts of upper rear projectile head, 3-2 parts of lower rear projectile head, 3-3 parts of rear projectile head concave ring, 3-4 parts of rear projectile head receiving cavity, 3-4-1 parts of rear projectile head conical cavity, 3-4-2 parts of rear projectile head cylindrical cavity, 3-5 parts of rear projectile head cylindrical cavity, 4 parts of launching assembly, 4-1 parts of projectile body, 4-1-1 parts of projectile shell, 4-1-2 parts of projectile shell convex ring, 4-1-3 parts of projectile shell bottom edge, 4-1-4 parts of bottom fire hole, 4-1-5 parts of high-pressure chamber, 4-1-6 parts of fire transfer hole, 4-2 parts of projectile holder, 4-2-1 parts of projectile holder push disk, 4-2-2 parts of projectile holder push disk, 4-3 parts of bullet support cylinder, 4-3-1 parts of explosive charge, 4-3-2 parts of primer, 4-4 parts of propellant powder and a low-pressure chamber.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-10, the present invention provides a technical solution: a hot-press-connection sealing-sleeve type compound non-lethal kinetic energy bullet comprises a front bullet head assembly 1, a bullet body assembly 2, a rear bullet head assembly 3 and a launching assembly 4.
With reference to fig. 2, 3 and 4, the front warhead assembly 1 includes an elastic foam head 1-1, a front warhead cylinder 1-2, a load body 1-3, OC stimulating powder 1-4, fluorescent dye powder 1-5, a hot-pressing envelope 1-6 and a front warhead lower cavity 1-7, the elastic foam head 1-1 is in a hemispherical structure, an elastic foam head inner cavity 1-1 is formed at the lower end of the elastic foam head 1-1, the elastic foam head inner cavity 1-1 includes an upper cylinder cavity and a lower cylinder cavity, the outer diameter of the upper cylinder cavity of the elastic foam head inner cavity 1-1-1 is larger than that of the lower cylinder cavity, the front warhead cylinder 1-2 is embedded and connected to the lower side of the elastic foam head 1-1, and the front warhead cylinder 1-2 is in a cylindrical structure, the front warhead cylinder 1-2 comprises a load cavity 1-2-1, spray pipes 1-2-2 and an embedding head 1-2-3, the load cavity 1-2-1 is used for bearing a load body 1-3, the spray pipes 1-2-2 penetrating through the side wall of the front warhead cylinder 1-2 are arranged on the outer side of the side wall of the load cavity 1-2-1, the spray pipes 1-2-2 are distributed in an upper layer and a lower layer, the number of the single-layer spray pipes 1-2-2 is 6, the 6 single-layer spray pipes 1-2-2 are distributed in a circumferential array along the central axis of the front warhead cylinder 1-2, the embedding head 1-2-3 is arranged on the upper portion of the front warhead cylinder 1-2 in a protruding mode, and the embedding head 1-2-3 comprises an upper cylinder and a lower cylinder, the outer diameter of the upper cylinder of the embedding head 1-2-3 is larger than that of the lower cylinder, the embedding head 1-2-3 is clamped into the inner cavity 1-1-1 of the elastic foam head, the load body 1-3 is a thin-walled cylinder, the load body 1-3 comprises a load body upper cavity 1-3-1, a load body lower cavity 1-3-2 and a load body middle clapboard 1-3-3, the load body upper cavity 1-3-1 and the load body lower cavity 1-3-2 are both cylinder cavities, the load body middle clapboard 1-3-3 is used for separating the load body upper cavity 1-3-1 and the load body lower cavity 1-3-2, the load body upper cavity 1-3-1 is filled with OC stimulating powder 1-4, the load body lower cavity 1-3-2 is filled with fluorescent dye powder 1-5, the outer walls of the elastic foam head 1-1 and the front warhead cylinder 1-2 are tightly wrapped with a hot-pressing sleeve 1-6, the hot-pressing sleeve 1-6 is in a thin-wall structural design with a rear cylinder, a front ball body and an opening at the top, and a front warhead lower cavity 1-7 is formed in the central axis of the lower part of the front warhead cylinder 1-2;
with reference to fig. 2 and 5, a bullet assembly 2 is embedded in the middle lower portion of the front bullet assembly 1, the bullet assembly 2 includes a main bullet 2-1, a bullet belt 2-2, a bullet front arch 2-3, a bullet clamping column 2-4 and a bullet inner cavity 2-5, the main bullet 2-1 includes a main bullet cylinder 2-1-1 and a main bullet cone 2-1-2, a cylinder extending from the upper end of the main bullet 2-1 is the bullet belt 2-2, the upper end of the bullet belt 2-2 abuts against the lower end of the front bullet cylinder 1-2, a bullet front arch 2-3 with a concave side wall is upwardly extended from the middle of the upper end of the bullet belt 2-2, the bullet front arch 2-3 is embedded into the front bullet lower cavity 1-7, the outer wall of the bullet front arch 2-3 is in accordance with and tightly abutted against the cavity wall of the bullet lower cavity 1-7, the lower part of the main projectile body cylinder 2-1-1 is provided with cylindrical projectile body clamping columns 2-4 in an extending mode, the number of the projectile body clamping columns 2-4 is 4, the 4 projectile body clamping columns 2-4 are distributed in a circumferential array mode along the central axis of the projectile body assembly 2, and cavities formed in the main projectile body 2-1 and the central axis inside the projectile body front arch 2-3 and communicated with each other are projectile body inner cavities 2-5;
referring to fig. 2 and 6, the lower part of the bullet assembly 2 is embedded with a rear bullet assembly 3, the rear bullet assembly 3 comprises an upper rear bullet 3-1, a lower rear bullet 3-2, a rear bullet concave ring 3-3, a rear bullet receiving cavity 3-4 and a rear bullet cylindrical cavity 3-5, the upper rear bullet 3-1 and the lower rear bullet 3-2 are both cylindrical, an annular groove with a semicircular section is formed on the outer edge of the contact surface of the upper rear bullet 3-1 and the lower rear bullet 3-2, and is the rear bullet concave ring 3-3, a rear bullet receiving cavity 3-4 is formed on the axial line of the upper rear bullet 3-1, the rear bullet receiving cavity 3-4 comprises a rear bullet conical cavity 3-4-1 and a rear bullet cylindrical cavity 3-4-2, the rear bullet conical cavity 3-4-1 receives a main bullet 2-1-2 cone, the rear warhead cylindrical cavity 3-4-2 is used for receiving a main warhead cylinder 2-1-1, the upper end face of the upper rear warhead 3-1 abuts against the lower end face of the elastic belt 2-2, the lower rear warhead 3-2 is provided with a cylindrical rear warhead cylindrical cavity 3-5, the number of the rear warhead cylindrical cavities 3-5 is 4, 4 rear warhead cylindrical cavities 3-5 are distributed in a circumferential array along the central axis of the rear warhead assembly 3, and a warhead clamping column 2-4 is embedded in each rear warhead cylindrical cavity 3-5;
with reference to fig. 2 and 7-10, a launching assembly 4 is mechanically inserted at the lower side of the rear warhead assembly 3, the launching assembly 4 comprises a cartridge case 4-1, a cartridge holder 4-2, a charge 4-3 and a low pressure chamber 4-4, the cartridge case 4-1 comprises a cartridge case 4-1-1, a cartridge case convex ring 4-1-2, a cartridge case bottom edge 4-1-3, a fire bottom hole 4-1-4, a high pressure chamber 4-1-5 and a fire transfer hole 4-1-6, the upper end face of the cartridge case 4-1-1 is abutted against the outer edge of the lower side of the upper rear warhead 3-1, the convex ring with a semicircular section is integrally arranged at the inner side of the upper end of the cartridge case 4-1-1 and is the cartridge case convex ring 4-1-2, the outer diameter of the cartridge case 4-1-1 is equal to the outer diameter of the upper rear warhead 3-1, the bullet shell convex ring 4-1-2 is extruded into the rear bullet concave ring 3-3, the side wall of the lower rear bullet 3-2 abuts against the inner side wall of the bullet shell 4-1-1, the bottom of the bullet shell 4-1-1 is provided with a bullet shell bottom edge 4-1-3 in a protruding mode, the axis of the bottom end face of the bullet shell 4-1-1 is provided with a cylindrical bottom fire hole 4-1-4, a cylindrical high-pressure chamber 4-1-5 is integrally arranged on the axis of the center of the bullet shell 4-1-1 and the upper side of the bottom fire hole 4-1-4, the axis of the upper end face of the high-pressure chamber 4-1-5 is provided with a cylindrical fire transfer hole 4-1-6, the fire transfer hole 4-1-6 is sealed by a brass diaphragm, and the inner side wall of the bullet shell 4-1-1 abuts against the bullet holder 4-2, the bullet holder 4-2 comprises a bullet holder push tray 4-2-1 and a bullet holder cylinder 4-2-2, the lower end part of the lower rear bullet head 3-2 is located on the upper end surface of the bullet holder push tray 4-2-1, the lower end surface of the bullet holder cylinder 4-2-2 abuts against the bottom of a bullet shell 4-1-1, the outer side wall of the bullet holder cylinder 4-2-2 and the inner side wall of the bullet shell 4-1-1 are sealed by hot melt adhesive, a charge 4-3 is filled in the bullet shell 4-1, the charge 4-3 comprises a primer 4-3-1 and a propellant powder 4-3-2, the primer 4-3-1 is a columnar mechanical impact primer, the primer 4-3-1 is riveted inside a primer hole 4-1-4, the propellant powder 4-3-2 is bulk smokeless powder, the propellant powder 4-3-2 is filled in the high-pressure chamber 4-1-5, and a cavity formed by the inner side of the bullet holder 4-2 and the outer side of the high-pressure chamber 4-1-5 is the low-pressure chamber 4-4.
Combine fig. 1 and fig. 2, preceding warhead subassembly 1, projectile body subassembly 2, back warhead subassembly 3 and transmission subassembly 4 are the axisymmetric structure, the axis coincidence of preceding warhead subassembly 1, projectile body subassembly 2, back warhead subassembly 3 and transmission subassembly 4, preceding warhead subassembly 1, projectile body subassembly 2, back warhead subassembly 3 and transmission subassembly 4 front and back series connection.
In this embodiment, the elastic foam head 1-1 is made of a honeycomb closed-cell foam material, the front bullet cylinder 1-2 is made of foamed aluminum, the cavity wall of the load body 1-3 is made of a fragile material, the hot-pressing sleeve 1-6 is a polyvinyl chloride pipe, the main bullet 2-1, the bullet belt 2-2, the bullet front arch 2-3 and the bullet clamping column 2-4 are integrally formed by injection molding of a nylon material, the rear bullet assembly 3 is made of a hard polymer foam material, a high-temperature-resistant coating is covered on the lower end of the lower rear bullet 3-2, the bullet holder 4-2 is made of a light high-temperature-resistant plastic, and the bullet shell 4-1 is integrally formed by a high-strength aluminum alloy material.
In the embodiment, the elastic foam head 1-1, the front bullet column 1-2 and the bullet front arch 2-3 are firmly connected through hot curling of the hot-pressing sleeve 1-6.
In this embodiment, after the cavity wall of the load body 1-3 is crushed by pressure, the OC stimulating powder 1-4 is sprayed out along the upper spray pipe 1-2-2, and the fluorescent dyeing powder 1-5 is sprayed out along the lower spray pipe 1-2-2.
In this embodiment, the shape of the projectile cavity 2-5 is an axisymmetric structure, and the size of the projectile cavity 2-5 is set to ensure that the center of gravity and the center of thrust of the projectile formed by the front projectile assembly 1, the projectile assembly 2 and the rear projectile assembly 3 coincide.
In this embodiment, high-temperature and high-pressure gunpowder gas generated by burning the propellant powder 4-3-2 acts on the cartridge holder 4-2, so that the cartridge holder 4-2 can rush out of the cartridge case 4-1 to push the front bullet assembly 1, the bullet assembly 2 and the rear bullet assembly 3 to advance, the cooperation of the cartridge belt 2-2 and the gun barrel line enables the front bullet assembly 1, the bullet assembly 2 and the rear bullet assembly 3 to synchronously spin, and after the cartridge holder 4-2 flies out of the gun barrel, the cartridge holder is quickly separated from the rear bullet assembly 3 due to light mass and air flow resistance.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a compound non-fatal kinetic energy bullet of hot pressing seal cover formula, includes preceding warhead subassembly (1), projectile body subassembly (2), back warhead subassembly (3) and transmission subassembly (4), its characterized in that:
the front warhead assembly (1) comprises an elastic foam head (1-1), a front warhead cylinder (1-2), a load body (1-3), OC stimulating powder (1-4), fluorescent dye powder (1-5), a hot-pressing sleeve (1-6) and a front warhead lower cavity (1-7), the elastic foam head (1-1) is of a hemispherical structure, an elastic foam head inner cavity (1-1-1) is formed in the lower end part of the elastic foam head (1-1), the elastic foam head inner cavity (1-1-1) comprises an upper column cavity and a lower column cavity, the outer diameter of the upper column cavity of the elastic foam head inner cavity (1-1-1) is larger than that of the lower column cavity, the lower side of the elastic foam head (1-1) is connected with the front warhead cylinder (1-2) in an embedded mode, the front warhead cylinder (1-2) is of a cylindrical structure, the front warhead cylinder (1-2) comprises a load cavity (1-2-1), spray pipes (1-2-2) and embedding heads (1-2-3), the load cavity (1-2-1) is used for bearing the load body (1-3), the spray pipes (1-2-2) penetrating through the side wall of the front warhead cylinder (1-2) are arranged on the outer side of the side wall of the load cavity (1-2-1), the spray pipes (1-2-2) are distributed in an upper layer and a lower layer, the number of the single-layer spray pipes (1-2-2) is 6, the 6 single-layer spray pipes (1-2-2) are distributed in a circumferential array mode along the central axis of the front warhead cylinder (1-2), and the embedding heads (1-2-3) are arranged on the upper portion of the front warhead cylinder (1-2) in a protruding mode ) The embedding head (1-2-3) comprises an upper cylinder and a lower cylinder, the outer diameter of the upper cylinder of the embedding head (1-2-3) is larger than that of the lower cylinder, the embedding head (1-2-3) is clamped into an inner cavity (1-1-1) of the elastic foam head, the load body (1-3) is a thin-walled cylinder, the load body (1-3) comprises an upper load body cavity (1-3-1), a lower load body cavity (1-3-2) and a middle load body partition plate (1-3-3), the upper load body cavity (1-3-1) and the lower load body cavity (1-3-2) are cylindrical cavities, and the middle load body partition plate (1-3-3) is used for separating the upper load body cavity (1-3-1) and the lower load body cavity (1-3-2), the loading body upper cavity (1-3-1) is filled with OC stimulating powder (1-4), the loading body lower cavity (1-3-2) is filled with fluorescent dye powder (1-5), the outer walls of the elastic foam head (1-1) and the front warhead cylinder (1-2) are tightly wrapped with a hot-pressing sleeve (1-6), the hot-pressing sleeve (1-6) is designed into a thin-wall structure with a rear cylinder, a front sphere and an open top, and a front warhead lower cavity (1-7) is formed in the central axis of the lower part of the front warhead cylinder (1-2);
the middle lower part of the front warhead assembly (1) is embedded with a projectile body assembly (2), the projectile body assembly (2) comprises a main projectile body (2-1), a projectile band (2-2), a projectile body front arch (2-3), a projectile body clamping column (2-4) and a projectile body inner cavity (2-5), the main projectile body (2-1) comprises a main projectile body cylinder (2-1-1) and a main projectile body cone (2-1-2), a cylinder extending from the outer edge of the upper end of the main projectile body (2-1) is the projectile band (2-2), the upper end of the projectile band (2-2) abuts against the lower end face of the front projectile body cylinder (1-2), the middle part of the upper end face of the projectile band (2-2) extends upwards to be provided with a projectile body front arch (2-3) with a side wall concave inwards, and the projectile body front arch (2-3) is embedded into the front warhead lower cavity (1-7), the outer wall of the projectile body front arch (2-3) is consistent with the shape of the cavity wall of the projectile head lower cavity (1-7) and tightly abutted against the cavity wall, 4 projectile body clamping columns (2-4) in a cylindrical shape are arranged on the lower portion of the main projectile body cylinder (2-1-1) in an extending mode, the 4 projectile body clamping columns (2-4) are distributed in a circumferential array mode along the central axis of the projectile body assembly (2), and the mutually communicated cavities formed in the main projectile body (2-1) and the inner central axis of the projectile body front arch (2-3) are projectile body inner cavities (2-5);
the rear warhead assembly (3) is embedded in the lower portion of the warhead assembly (2), the rear warhead assembly (3) comprises an upper rear warhead (3-1), a lower rear warhead (3-2), a rear warhead concave ring (3-3), a rear warhead bearing cavity (3-4) and a rear warhead cylindrical cavity (3-5), the upper rear warhead (3-1) and the lower rear warhead (3-2) are cylindrical, annular grooves with semicircular sections are formed in the outer edges of contact surfaces of the upper rear warhead (3-1) and the lower rear warhead (3-2) and are the rear warhead concave ring (3-3), the rear warhead bearing cavity (3-4) is formed in the axis of the upper rear warhead (3-1), and the rear warhead bearing cavity (3-4) comprises a rear warhead conical cavity (3-4-1) and a rear warhead cylindrical cavity (3-4-2), the rear warhead conical cavity (3-4-1) is used for bearing a main warhead cone body (2-1-2), the rear warhead cylindrical cavity (3-4-2) is used for bearing a main warhead cylinder (2-1-1), the upper end face of the upper rear warhead (3-1) is abutted against the lower end face of the belt (2-2), the lower rear warhead (3-2) is provided with a cylindrical rear warhead cylindrical cavity (3-5), the number of the rear warhead cylindrical cavities (3-5) is 4, the 4 rear warhead cylindrical cavities (3-5) are distributed in a circumferential array along the central axis of the rear warhead assembly (3), and a warhead clamping column (2-4) is embedded in the rear warhead cylindrical cavity (3-5);
the lower side of the rear warhead assembly (3) is mechanically spliced with a launching assembly (4), the launching assembly (4) comprises a warhead shell (4-1), a warhead (4-2), a charge (4-3) and a low-pressure chamber (4-4), the warhead shell (4-1) comprises a warhead shell (4-1-1), a warhead shell convex ring (4-1-2), a warhead shell bottom edge (4-1-3), a bottom fire hole (4-1-4), a high-pressure chamber (4-1-5) and a fire transfer hole (4-1-6), the upper end face of the warhead shell (4-1-1) abuts against the outer edge of the lower side of the upper rear warhead (3-1), the warhead shell (4-1-1) is integrally provided with the convex ring with a semicircular cross section, namely the warhead shell convex ring (4-1-2), the outer diameter of the cartridge case (4-1-1) is equal to that of the upper rear bullet (3-1), the rear bullet concave ring (3-3) is extruded into the cartridge case convex ring (4-1-2), the side wall of the lower rear bullet (3-2) abuts against the inner side wall of the cartridge case (4-1-1), the bottom of the cartridge case (4-1-1) is provided with a cartridge case bottom edge (4-1-3) in a protruding manner, the axis of the bottom end face of the cartridge case (4-1-1) is provided with a cylindrical bottom fire hole (4-1-4), the axis of the cartridge case (4-1-1) and the upper side of the bottom fire hole (4-1-4) are integrally provided with a cylindrical high-pressure chamber (4-1-5), and the axis of the upper end face of the high-pressure chamber (4-1-5) is provided with a cylindrical fire transmission hole (4-1-6), the fire transfer hole (4-1-6) is sealed by a brass diaphragm, the inner side wall of the cartridge case (4-1-1) is abutted against a cartridge holder (4-2), the cartridge holder (4-2) comprises a cartridge holder push tray (4-2-1) and a cartridge holder cylinder (4-2-2), the lower end part of the lower rear cartridge (3-2) is located on the upper end surface of the cartridge holder push tray (4-2-1), the lower end surface of the cartridge holder cylinder (4-2-2) is abutted against the bottom of the cartridge case (4-1-1), the outer side wall of the cartridge holder cylinder (4-2-2) and the inner side wall of the cartridge case (4-1-1) are sealed by hot melt adhesive, a charge (4-3) is filled in the cartridge case (4-1), and the charge (4-3) comprises a bottom fire (4-3-1) and a propellant powder (4-3-2) The primer (4-3-1) is a columnar mechanical impact type primer, the primer (4-3-1) is riveted inside a primer hole (4-1-4), the propellant powder (4-3-2) is bulk smokeless powder, the propellant powder (4-3-2) is filled inside a high-pressure chamber (4-1-5), and a cavity formed by the inner side of the bullet holder (4-2) and the outer side of the high-pressure chamber (4-1-5) is a low-pressure chamber (4-4).
2. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: preceding warhead subassembly (1), bullet body subassembly (2), back warhead subassembly (3) and transmission subassembly (4) are the axisymmetric structure, the axis coincidence of preceding warhead subassembly (1), bullet body subassembly (2), back warhead subassembly (3) and transmission subassembly (4), series connection around preceding warhead subassembly (1), bullet body subassembly (2), back warhead subassembly (3) and transmission subassembly (4).
3. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: the elastic foam head (1-1) is made of cellular closed-cell foam material, the front warhead cylinder (1-2) is made of foamed aluminum, the cavity wall of the load body (1-3) is made of fragile materials, the hot-pressing envelope (1-6) is a polyvinyl chloride pipe, the main projectile body (2-1), the projectile belt (2-2), the projectile body front arch (2-3) and the projectile body clamping column (2-4) are integrally formed by injection molding of nylon materials, the rear warhead component (3) is made of hard polymer foam material, the lower end part of the lower rear warhead (3-2) is covered with a high temperature resistant coating, the bullet holder (4-2) is made of light high-temperature-resistant plastic, and the bullet shell (4-1) is integrally formed by high-strength aluminum alloy materials.
4. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: the elastic foam head (1-1), the front warhead cylinder (1-2) and the front bullet arch (2-3) are firmly connected through hot curling of the hot-pressing envelope (1-6).
5. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: after the cavity wall of the load body (1-3) is crushed by pressure, the OC stimulating powder (1-4) is sprayed out along the upper spray pipe (1-2-2), and the fluorescent dyeing powder (1-5) is sprayed out along the lower spray pipe (1-2-2).
6. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: the shape of the projectile body cavity (2-5) is of an axisymmetric structure, and the size of the projectile body cavity (2-5) is set to ensure that the gravity center and the thrust center of a projectile formed by the front projectile body component (1), the projectile body component (2) and the rear projectile body component (3) coincide.
7. The thermal compression joint sealing sleeve type composite non-lethal kinetic energy bomb according to claim 1, characterized in that: high-temperature and high-pressure gunpowder gas generated by burning the propellant powder (4-3-2) acts on the bullet holder (4-2), so that the bullet holder (4-2) can rush out of the bullet shell (4-1), the front bullet assembly (1), the bullet assembly (2) and the rear bullet assembly (3) are pushed to advance, the bullet belt (2-2) is matched with the rifling of the gun barrel, so that the front bullet assembly (1), the bullet assembly (2) and the rear bullet assembly (3) can rotate synchronously, and after the bullet holder (4-2) flies out of the gun barrel, the bullet holder is quickly separated from the rear bullet assembly (3) due to the fact that the bullet is light in weight and is acted by air flow resistance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210695197.XA CN114963885B (en) | 2022-06-20 | 2022-06-20 | Thermal compression sleeve type composite non-fatal kinetic energy bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210695197.XA CN114963885B (en) | 2022-06-20 | 2022-06-20 | Thermal compression sleeve type composite non-fatal kinetic energy bomb |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114963885A true CN114963885A (en) | 2022-08-30 |
| CN114963885B CN114963885B (en) | 2023-11-24 |
Family
ID=82971228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210695197.XA Active CN114963885B (en) | 2022-06-20 | 2022-06-20 | Thermal compression sleeve type composite non-fatal kinetic energy bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114963885B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009150237A1 (en) * | 2008-06-13 | 2009-12-17 | Nobel Sport | Non-lethal munition |
| CN201575760U (en) * | 2009-09-23 | 2010-09-08 | 齐齐哈尔雄鹰猎弹有限公司 | Bullet with soft warhead |
| CN103688130A (en) * | 2011-03-30 | 2014-03-26 | 诺贝尔运动器材公司 | Less lethal weapon projectile |
| CN204788076U (en) * | 2015-07-07 | 2015-11-18 | 刘子杰 | Shotgun is with only first bullet |
| CN205482625U (en) * | 2016-01-19 | 2016-08-17 | 郭三学 | Simple target rubber bullet |
| CN205482627U (en) * | 2016-01-19 | 2016-08-17 | 郭三学 | Penetration type tear -gas shells |
| CN211651397U (en) * | 2019-12-25 | 2020-10-09 | 中国人民武装警察部队工程大学 | Double-wall cloth bag bullet with self-formed tail wing |
| CN113154956A (en) * | 2021-02-22 | 2021-07-23 | 中国人民武装警察部队工程大学 | Non-pyrotechnic explosion-catalysis type composite kinetic energy bomb |
| CN113865441A (en) * | 2021-10-09 | 2021-12-31 | 中国人民武装警察部队工程大学 | Twice-impact composite anti-riot kinetic energy bomb |
-
2022
- 2022-06-20 CN CN202210695197.XA patent/CN114963885B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009150237A1 (en) * | 2008-06-13 | 2009-12-17 | Nobel Sport | Non-lethal munition |
| CN201575760U (en) * | 2009-09-23 | 2010-09-08 | 齐齐哈尔雄鹰猎弹有限公司 | Bullet with soft warhead |
| CN103688130A (en) * | 2011-03-30 | 2014-03-26 | 诺贝尔运动器材公司 | Less lethal weapon projectile |
| CN204788076U (en) * | 2015-07-07 | 2015-11-18 | 刘子杰 | Shotgun is with only first bullet |
| CN205482625U (en) * | 2016-01-19 | 2016-08-17 | 郭三学 | Simple target rubber bullet |
| CN205482627U (en) * | 2016-01-19 | 2016-08-17 | 郭三学 | Penetration type tear -gas shells |
| CN211651397U (en) * | 2019-12-25 | 2020-10-09 | 中国人民武装警察部队工程大学 | Double-wall cloth bag bullet with self-formed tail wing |
| CN113154956A (en) * | 2021-02-22 | 2021-07-23 | 中国人民武装警察部队工程大学 | Non-pyrotechnic explosion-catalysis type composite kinetic energy bomb |
| CN113865441A (en) * | 2021-10-09 | 2021-12-31 | 中国人民武装警察部队工程大学 | Twice-impact composite anti-riot kinetic energy bomb |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114963885B (en) | 2023-11-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN115127404B (en) | Impact blasting type composite kinetic energy bullet with rear buried tail wing | |
| CN112361893B (en) | Empennage stable type composite anti-riot kinetic energy bomb | |
| CN113154956B (en) | Non-pyrotechnic explosion-catalysis type composite kinetic energy bomb | |
| CN112945024B (en) | Composite kinetic energy bullet with coupled spinning stability and resistance stability | |
| CN113865441B (en) | Twice-impact composite anti-riot kinetic energy bomb | |
| CN112815786A (en) | Composite kinetic energy bullet with point-face dual hitting capability | |
| CN111765816B (en) | Composite anti-riot kinetic energy bullet matched with smoothbore weapon | |
| CN113587736B (en) | Composite type anti-riot kinetic energy bullet with delay boosting function | |
| CN112344809B (en) | Fin-stabilized energy attenuation type anti-riot kinetic energy bomb | |
| CN113720212A (en) | Projectile body telescopic tail wing stable multi-effect composite kinetic energy projectile | |
| CN115127405B (en) | Explosion deceleration type composite kinetic energy bomb with built-in distance detection fuze | |
| CN113899253B (en) | Composite anti-riot kinetic energy bullet of leading honeycomb warhead of super-caliber | |
| CN114963885A (en) | Hot-press-connection sealing sleeve type composite non-lethal kinetic energy bullet | |
| CN115014133B (en) | Composite non-lethal kinetic energy bomb with embedded projectile body | |
| CN115031589B (en) | Composite non-lethal kinetic energy bullet with multistage buckling structure | |
| CN114923374B (en) | Composite non-lethal kinetic energy bullet with progressive deceleration characteristic | |
| CN115574665B (en) | Composite spherical cloth bag bullet for knocking and spraying | |
| CN115507709B (en) | Impact crushing type non-lethal kinetic energy projectile with built-in multi-cloth-bag projectile | |
| CN114858009B (en) | Non-lethal kinetic energy projectile with better aerodynamic characteristics and without hard projectile body | |
| CN115540697B (en) | Composite dragging stable cloth bag bullet for bursting and opening bin | |
| CN115597440B (en) | Bullet cabin bearing type multi-effect integrated non-lethal ammunition | |
| CN115540698B (en) | Impact buffering type non-lethal kinetic energy bullet with extended inner core | |
| CN113587738B (en) | Impact sliding type multi-effect integrated composite anti-riot kinetic energy bomb | |
| CN113587742B (en) | Composite anti-riot kinetic energy bullet with multiple impact destruction mechanism | |
| CN113587735B (en) | Multi-effect kinetic energy bullet with large effective shooting distance |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |