CN213932211U - Attached ammunition firing speed adjusting device - Google Patents

Attached ammunition firing speed adjusting device Download PDF

Info

Publication number
CN213932211U
CN213932211U CN202023070516.3U CN202023070516U CN213932211U CN 213932211 U CN213932211 U CN 213932211U CN 202023070516 U CN202023070516 U CN 202023070516U CN 213932211 U CN213932211 U CN 213932211U
Authority
CN
China
Prior art keywords
control device
emission
projectile
electronic ignition
propellant
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.)
Active
Application number
CN202023070516.3U
Other languages
Chinese (zh)
Inventor
董金龙
刘洋
郭若飞
谭勇军
刘杰
唐碧文
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hunan Ordnance Science And Technology Research Institute Co ltd
Original Assignee
Hunan Xiangke Science And Technology Research Institute Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hunan Xiangke Science And Technology Research Institute Co ltd filed Critical Hunan Xiangke Science And Technology Research Institute Co ltd
Priority to CN202023070516.3U priority Critical patent/CN213932211U/en
Application granted granted Critical
Publication of CN213932211U publication Critical patent/CN213932211U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The utility model discloses an attached ammunition launching speed adjusting device, which comprises a laser range finder, a powder charge pellet, a control device, a receiver and a gun barrel, wherein the laser range finder measures the distance of targets with different distances and displays the measured distance on a combat panel in real time for a user to check, and transmits the target distance information to the control device; the charge projectile is used for meeting the requirements of different emission energies; the control device is used for controlling the emission energy; the electronic ignition heads correspond to the propellant powder on the porous cartridge case one by one; because the weight of the propellant charge contained in each propellant hole is determined, the corresponding projectile outlet speed is obtained by resolving according to a micro-electronic chip arranged in the control device, and the purpose of regulating the projectile outlet speed by controlling energy is realized. The utility model discloses attach controlling means in the casket, combine powder charge shot, control the transmitting energy through the mode of control propellant powder, adjust shot exit velocity, can realize invariable kinetic energy to the target of different distances and strike.

Description

Attached ammunition firing speed adjusting device
Technical Field
The utility model belongs to the technical field of firearms, especially, relate to an attach formula ammunition firing rate adjusting device.
Background
A non-lethal weapon is a new concept of weapon that causes a temporary or permanent loss of normal function of a target without causing death of personnel. The method mainly comprises the following steps of kinetic energy percussion incapacity, electric shock incapacity and acousto-optic interference. Constant kinetic energy striking belongs to kinetic energy striking incapability, and the striking kinetic energy of targets with different distances is accurately controlled mainly by controlling the initial speed of a bullet to achieve the aim of non-lethal striking.
At present, the constant kinetic energy striking is mainly realized in a pneumatic emission mode, a barrel is additionally provided with an air leakage hole mode, an electromagnetic emission mode and the like, the pneumatic emission mode needs to adjust the gas pressure, the time consumption is long, and the operation is inconvenient. The mode of additionally arranging the air leakage hole is difficult to effectively control because the speed of the shot in the chamber is increased very fast when the firearm is launched. The electromagnetic emission method is difficult to be miniaturized and lightened due to technical condition limitations.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve the defect that exists among the above-mentioned prior art and not enough, provide one kind with controlling means attaches the cartridge case in, combine purpose-made powder charge shot of adjustable propellant powder, control the energy of launching through the mode of control propellant powder, and then adjust projectile exit velocity, can be to the target of different distances, realize the attached ammunition firing rate adjusting device that attaches that invariable kinetic energy strikes.
The technical scheme of the utility model: an attached ammunition launching speed adjusting device comprises a laser range finder, a powder-filled bullet, a control device, a case and a gun barrel,
the laser range finder measures the distance of targets with different distances, displays the measured distance on a combat panel in real time for a user to check, and transmits the target distance information to the control device;
the charge projectile is used for meeting the requirements of different emission energies and comprises a porous projectile shell, emission charges and a projectile head, wherein a plurality of emission holes for filling the emission charges with specific weights are formed in the porous projectile shell, all the emission holes are not communicated with each other, and the emission charges with different weights are ignited by igniting the emission holes with different numbers, so that the switching of different emission doses is realized, and different emission energies are obtained; the warhead is used for realizing the non-lethal striking function;
the control device is used for controlling the emission energy and comprises an electronic ignition head, a microelectronic chip and a shell, aiming at different target distances measured by a laser range finder, the internal and external ballistic trajectories are calculated through the built-in microelectronic chip, the number of the emission holes required to be ignited is calculated, and the electronic ignition head is fixed;
the electronic ignition heads correspond to the emission holes in the porous cartridge case one by one; as the weight of the propellant charge contained in each propellant hole is determined, the propellant energy is also determined, and meanwhile, the inner ballistic law is known, and the corresponding projectile outlet speed is obtained through calculation according to the built-in microelectronic chip of the control device, so that the aim of regulating the projectile outlet speed through controlling the energy is fulfilled.
The utility model discloses attach controlling means in the machine casket, combine the powder charge shot of adapted, control the transmitting energy through the mode of control propellant powder, and then adjust shot exit velocity, can realize invariable kinetic energy to the target of different distances and strike.
Preferably, the control device is installed in the casing, the barrel is rotatably installed on the casing, the explosive-filled projectile is loaded in the barrel on the side corresponding to the control device, and the laser range finder is installed outside the barrel on the side corresponding to the explosive-filled projectile.
The structure makes the structure compact and the assembly firm.
Preferably, the housing and the casing are connected by a screw thread.
The structure facilitates the installation of the control device and ensures the firm installation of the control device.
Preferably, the emission holes of the porous cartridge case are arranged in a honeycomb shape, and the electronic ignition heads on the control device are also arranged in a honeycomb shape.
Preferably, the emission holes of the porous cartridge case are arranged in a ring shape, a fan shape or a rectangular shape, and the electronic ignition heads on the control device are arranged in a ring shape, a fan shape or a rectangular shape.
The operation process of the attached ammunition firing speed regulating device comprises the following steps:
1) firstly, loading explosive loading pellets 2 from the tail part of a gun tube 5, then, rotating the gun tube 5 to align the receiver 4, and enabling each single emission hole on the porous shell 21 to correspond to the honeycomb type electronic ignition head 31 on the control device 3 one by one, so that the loading is finished;
2) measuring by the laser range finder 1 to obtain a target distance, and transmitting target distance information to the control device 3;
3) according to the target distance information, the internal microelectronic chip 32 of the control device 3 calculates the internal and external trajectories to obtain the number of the emitting holes to be ignited, and the ignition setting is carried out;
4) after the honeycomb electronic ignition head 31 is installed, the part to be ignited on the honeycomb electronic ignition head is in a closed circuit state, and the part not needing to be ignited is in an open circuit state;
5) after the operator performs the launching action, the microelectronic chip 32 sends an ignition instruction, and the honeycomb electronic ignition head 31 ignites the propellant powder in the corresponding launching hole to complete the launching action;
6) under the push of gunpowder gas obtained by burning the specific propellant powder, the bullet 23 is taken out of the chamber to complete non-lethal killing striking;
7) after the shooting is finished, the barrel is rotated to expose the porous cartridge case 21, and the cartridge case is withdrawn for recovery; at this time, the whole round of working process is completed, and the next specially-made explosive-filled projectile 2 can be loaded for continuous shooting.
The utility model discloses attach controlling means in the machine casket, combine the powder charge shot of adapted, control the transmitting energy through the mode of control propellant powder, and then adjust shot exit velocity, can realize invariable kinetic energy to the target of different distances and strike.
Drawings
Fig. 1 is a schematic cut-away view of embodiment 1 of the present invention;
FIG. 2 is a schematic structural view of a loading bullet of example 1 of the present invention with the bullet removed;
fig. 3 is a schematic structural diagram of a control device in embodiment 1 of the present invention;
FIG. 4 is a schematic sectional view of a loading pellet in example 2 of the present invention;
FIG. 5 is a schematic sectional view of a loading pellet in example 3 of the present invention;
FIG. 6 is a schematic sectional view of a loading pellet in example 4 of the present invention;
in the figure, 1, a laser range finder, 2 charge pills, 21, a porous bullet shell, 22, a propellant charge, 23, a bullet, 3, a control device, 31, an electronic ignition head, 32, a microelectronic chip, 33, a shell, 4, a case and 5, a gun barrel are shown.
Detailed Description
The present invention will be described in further detail with reference to the following drawings and examples, but the present invention is not limited thereto.
Example 1
As shown in fig. 1-3, an attached ammunition firing rate regulating device comprises a laser rangefinder 1, a tailored charge pellet 2, a control device 3, a receiver 4 and a barrel 5.
The main function of the laser distance measuring instrument 1 is to measure the distance of targets with different distances and display the measured distance on a battle panel for a user to check, and transmit the target distance information to the control device 3.
The charge projectile 2 comprises a porous shell 21, a propellant charge 22 and a bullet 23, see figure. The main function of the multi-hole bullet shell is to meet the requirements of different emission energies, and the multi-hole bullet shell 21 is mainly characterized in that multiple honeycomb-shaped circular emission holes are formed in the bullet shell, the emission holes are not communicated with each other, and the emission charge 22 is arranged in the multi-hole bullet shell. The switching of different emission doses can be realized by igniting different numbers of emission holes so as to obtain different emission energies. The bullet 23 mainly realizes a non-lethal striking function.
The main function of the control device 3 is to control the emitted energy, including the cellular electronic ignition head 31, the microelectronic chip 32 and the housing 33. Through the connection of the threads on the shell 33 and the machine, aiming at different target distances measured by the laser range finder 1, the internal and external trajectories are calculated through the built-in microelectronic chip 32, the number of the emission holes required to be ignited is calculated, and the honeycomb type electronic ignition head 31 is fixed. The honeycomb electronic ignition heads 31 correspond to the electronic ignition heads on the porous cartridge case 21 one by one, and the ignition action of a specific emission hole can be realized. As the weight of the propellant charge contained in each propellant hole is determined and calculated according to the microelectronic chip 32 arranged in the control device 3, the corresponding projectile outlet speed can be obtained, and the aim of adjusting the projectile outlet speed by controlling energy is fulfilled.
The receiver 4 and the barrel 5 are the usual components of a firearm, the control device 3 being mounted inside the receiver 4. The barrel 5 can rotate integrally, the part which is contacted with the case 4 is exposed, so that the bullet loading is convenient, the control device 3 is arranged in the case 4, the bullet loading part 2 is arranged in the barrel 5 and corresponds to the control device 3, and the laser range finder 1 is arranged outside the barrel 5 and corresponds to the bullet loading part 2.
The working process of the emission speed adjusting device is as follows: the loading is completed by first loading the specially-made loaded projectiles 2 from the rear of the barrel 5, then rotating the barrel 5 into alignment with the magazine 4, and the individual electrical fires on the porous cartridge shell 21 in one-to-one correspondence with the cellular electrical firing heads 31 on the control device 3. The target distance is measured by the laser range finder 1, and the target distance information is transmitted to the control device 3. According to the target distance information, the internal microelectronic chip 32 of the control device 3 calculates the internal and external trajectories to obtain the number of the emitting holes to be ignited, the ignition is fixed, and after the fixing is finished, the part to be ignited on the honeycomb electronic ignition head 31 is in a closed circuit state, and the part not required to be ignited is in an open circuit state. After the operator performs the launching action, the microelectronic chip 32 sends an ignition instruction, and the honeycomb electronic ignition head 31 ignites the propellant powder in the corresponding launching hole to complete the launching action. Under the push of gunpowder gas obtained by burning the specific propellant powder, the bullet 23 is taken out of the chamber to complete non-lethal killing striking. After the firing is completed, the barrel is rotated to expose the porous cartridge case 21 and the cartridge case is withdrawn for recovery. At this time, the whole round of working process is completed, and the next specially-made explosive-filled projectile 2 can be loaded for continuous shooting.
Example 2
As shown in fig. 4, the emission holes of the porous cartridge case 21 are arranged in a ring shape, and the electronic ignition heads on the control device 3 are arranged in a ring shape.
Example 3
As shown in fig. 5, the firing holes of the perforated cartridge case 21 are arranged in a fan shape, and the electronic ignition heads on the control device 3 are arranged in a fan shape.
Example 4
As shown in fig. 6, the emission holes of the porous cartridge case 21 are arranged in a rectangular shape, and the electronic ignition heads on the control device 3 are arranged in a rectangular shape.
The utility model discloses a shot exit velocity is controlled to the weight that the regulation was lighted the transmission powder charge, realizes that the route is for lighting a plurality of solitary transmission powder charges through the electronic control mode. The preferred embodiment of the present invention is the honeycomb-shaped propellant charge and electronic ignition head shown in embodiment 1, which can be designed into other forms as required, such as annular hole group (embodiment 2), fan-shaped hole group (embodiment 3), and rectangular hole group (embodiment 4), and the like, and the present invention is in accordance with the core concept and should be applied to the realization of the path.

Claims (5)

1. An attached ammunition firing rate adjustment device, characterized in that: which comprises a laser range finder, a powder-filled bullet, a control device, a case and a gun barrel,
the laser range finder measures the distance of targets with different distances, displays the measured distance on a combat panel in real time for a user to check, and transmits the target distance information to the control device;
the charge projectile is used for meeting the requirements of different emission energies and comprises a porous projectile shell, emission charges and a projectile head, wherein a plurality of emission holes for filling the emission charges are formed in the porous projectile shell, all the emission holes are not communicated with each other, and different emission doses are switched by igniting different numbers of emission holes so as to obtain different emission energies; the warhead is used for realizing the non-lethal striking function;
the control device is used for controlling the emission energy and comprises an electronic ignition head, a microelectronic chip and a shell, aiming at different target distances measured by a laser range finder, the internal and external ballistic trajectories are calculated through the built-in microelectronic chip, the number of the emission holes required to be ignited is calculated, and the electronic ignition head is fixed;
the electronic ignition heads correspond to the emission holes in the porous cartridge case one by one; the weight of the propellant charge contained in each propellant hole is determined, and the corresponding projectile outlet speed is obtained through calculation according to a micro-electronic chip arranged in the control device, so that the aim of regulating the projectile outlet speed through controlling energy is fulfilled.
2. An attached ammunition firing rate regulating device according to claim 1, wherein: the control device is installed in the machine case, the gun barrel is rotatably installed on the machine case, the explosive-filled projectile is installed in the gun barrel and corresponds to the control device, and the laser range finder is installed outside the gun barrel and corresponds to the explosive-filled projectile.
3. An attached ammunition firing rate regulating device according to claim 1, wherein: the shell is connected with the casing through threads.
4. An attached ammunition firing rate regulating device according to claim 1, wherein: the emission holes of the porous cartridge case are arranged in a honeycomb shape, and the electronic ignition heads on the control device are also arranged in a honeycomb shape.
5. An attached ammunition firing rate regulating device according to claim 1, wherein: the emission holes of the porous cartridge case are annularly arranged, fanned or rectangularly arranged, and the electronic ignition heads on the control device are annularly arranged, fanned or rectangularly arranged.
CN202023070516.3U 2020-12-18 2020-12-18 Attached ammunition firing speed adjusting device Active CN213932211U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023070516.3U CN213932211U (en) 2020-12-18 2020-12-18 Attached ammunition firing speed adjusting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023070516.3U CN213932211U (en) 2020-12-18 2020-12-18 Attached ammunition firing speed adjusting device

Publications (1)

Publication Number Publication Date
CN213932211U true CN213932211U (en) 2021-08-10

Family

ID=77153537

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202023070516.3U Active CN213932211U (en) 2020-12-18 2020-12-18 Attached ammunition firing speed adjusting device

Country Status (1)

Country Link
CN (1) CN213932211U (en)

Similar Documents

Publication Publication Date Title
RU2549599C1 (en) Cartridge case-free gun
KR100915857B1 (en) Dual-barrel air-burst weapon
KR920004613B1 (en) Small-arm and ammunition
US9879963B2 (en) Systems to measure yaw, spin and muzzle velocity of projectiles, improve fire control fidelity, and reduce shot-to-shot dispersion in both conventional and airbursting programmable projectiles
US20210048273A1 (en) Training attachment
CN112524995A (en) Attached ammunition firing speed adjusting device and working method thereof
RU2744227C1 (en) Grenade launcher ammunition against unmanned aerial vehicles
CN213932211U (en) Attached ammunition firing speed adjusting device
RU2326334C1 (en) Practice round
US20120085259A1 (en) Cartridge for light-weighted projectiles
RU2308656C2 (en) Automatic grenade launcher and a set of grenades to it
RU145386U1 (en) SELF-DEFENSE WEAPONS AND CASE-FREE CARTRIDGE FOR HIM
KR100498085B1 (en) Electronic imitation gun magazine for substituting a blank shot and controlling method thereof
CN202013148U (en) 120mm antitank rocket training missile
CN215337971U (en) Universal gun launching device
WO2019226075A1 (en) Pneumatic training attachment
RU201838U1 (en) Caseless chuck
RU203103U1 (en) Throwing device structurally similar to a firearm product
CN212082151U (en) Multi-functional transmission trainer based on modular design
CN2200811Y (en) Internal bore and its imitation shell of 82 mm recoiless gun
KR200332601Y1 (en) Electronic imitation gun magazine for substituting a blank shot
RU172020U1 (en) ELECTRIC BULLET FOR APPLICATION IN A FIRE OR PNEUMATIC WEAPON
RU2373485C2 (en) Method of high-accuracy firing from automatic gun and set of shells to this end
CN2656930Y (en) 78 type platform force less cannon inner bore cannon and its analogue cannon ball
RU2231730C1 (en) Multifunctional pneumatic gun

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20230210

Address after: Room 919, 9th Floor, No. 9, Lixiang East Road, Changsha Economic and Technological Development Zone, Changsha, Hunan Province, 410000

Patentee after: Hunan Ordnance Science and Technology Research Institute Co.,Ltd.

Address before: 410200 1206, Jingu building, 319 Jinxing Middle Road, Yuelu District, Changsha City, Hunan Province

Patentee before: Hunan Xiangke science and Technology Research Institute Co.,Ltd.