CN218120756U - Vertical bullet dish kinetic energy transmitting system - Google Patents
Vertical bullet dish kinetic energy transmitting system Download PDFInfo
- Publication number
- CN218120756U CN218120756U CN202222314084.9U CN202222314084U CN218120756U CN 218120756 U CN218120756 U CN 218120756U CN 202222314084 U CN202222314084 U CN 202222314084U CN 218120756 U CN218120756 U CN 218120756U
- Authority
- CN
- China
- Prior art keywords
- bullet
- launching
- ammunition
- kinetic energy
- ammunition feed
- 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
Links
Images
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a vertical type bullet disk kinetic energy launching system, which comprises a launching device system, an air supply system and a control system, wherein the launching device system comprises a launching tube, a quick-opening valve, a high-pressure air chamber and a bullet supply mechanism; the two ends of the inner cavity of the ammunition feeding section of the ammunition feeding mechanism are respectively connected with the launching tube and the high-pressure air chamber, and the quick opening valve is arranged between the high-pressure air chamber and the inner cavity of the ammunition feeding section and used for closing the front end outlet of the high-pressure air chamber or quickly opening the front end outlet of the high-pressure air chamber; the gas supply system is connected with the high-pressure gas chamber; the control system is respectively connected with the launching device system and the air supply system and is used for controlling the launching process of the launching device system and the action of the air supply system. The utility model discloses a structural design of ammunition feed mechanism can be accurate ammunition feed rapidly when making the magazine ammunition feed, adopts the ammunition feed structure of the multistage combined type motion of single motor control, realizes the ammunition feed of ammunition feed mechanism, advances the bullet, divides the function of bullet and thorax inner seal, accomplishes the automatic continuous loading of shot, has characteristics such as safe in utilization, convenient operation, reliable operation.
Description
Technical Field
The utility model belongs to the technical field of the shot transmitting system, in particular to vertical bullet dish kinetic energy transmitting system.
Background
The existing projectile launching system mostly adopts gunpowder as the launching kinetic energy of the projectile, but under the requirements of certain special environmental space, compressed gas is required to replace high-pressure gas generated by the combustion of traditional gunpowder to finish the launching of the projectile.
In the existing device for driving the shot to be shot by utilizing compressed gas, because the shot needs to be ensured to be in a relatively closed space in the process of shooting, the structural design of how to realize the shot feeding, the shot separating and the internal sealing of a shot chamber is relatively complex, so that the operation of the shooting device is inconvenient and the working reliability is low.
SUMMERY OF THE UTILITY MODEL
The invention of the utility model aims to: aiming at the problems, the vertical bullet disk kinetic energy launching system is safe to use, convenient to operate and reliable in work.
The utility model discloses a following technical scheme realizes: the utility model provides a vertical bullet dish kinetic energy transmitting system, includes emitter system, air supply system and control system, its characterized in that: the launching device system comprises a launching tube, a quick-opening valve, a high-pressure air chamber and an ammunition feeding mechanism;
the quick-opening valve is arranged between the high-pressure air chamber and the bullet supply section inner cavity and is used for closing a front end outlet of the high-pressure air chamber to isolate gas or quickly opening the front end outlet of the high-pressure air chamber to communicate the high-pressure air chamber with the bullet supply section inner cavity;
the gas supply system is connected with the high-pressure gas chamber and is used for supplying inert gas to the high-pressure gas chamber;
and the control system is respectively connected with the transmitting device system and the gas supply system and is used for controlling the transmitting process of the transmitting device system and the action of the gas supply system.
Vertical bullet dish kinetic energy transmitting system, its ammunition feed mechanism includes the drum magazine and holds a plurality of shots in the drum magazine be provided with out the bullet mouth on the drum magazine be provided with in the drum magazine and be used for dialling out the group bullet tooth of bullet mouth with the shot the drum outside is provided with and dials the drum cage shield of bullet tooth synchronous revolution, the drum cage shield is used for pushing away the shot of dialling bullet tooth and pushes away to the position of launching of bullet section inner chamber, and seals the shot in the bullet section through the drum cage shield.
Vertical bullet dish kinetic energy transmitting system, it a plurality of shots are placed in the fixed motion track that drum magazine internal fixation guide formed, the shot is under the effect of dialling the bullet tooth, along the fixed orbit motion in the drum magazine to play the bullet mouth by seting up on the drum magazine in proper order and dial.
Vertical bullet dish kinetic energy transmitting system, its play bullet mouth of seting up on the drum magazine corresponds with the open end of ammunition feed section drum magazine shield is last to be provided with a plurality ofly and to dial the complex division board that bullet tooth portion corresponds, division board on the drum magazine shield leans on the back to arranging for the corresponding tooth portion of dialling the bullet tooth in the rotation direction, after the bullet was dialled out the bullet mouth through dialling the bullet tooth, again through pushing to the inside position of launching of bullet section of waiting of division board that leans on the back to set up.
Vertical bullet dish kinetic energy transmitting system, its division board on the drum magazine changes to the open end of ammunition feed section to with the butt joint of ammunition feed section sealed, the ammunition feed section inner chamber that makes the loading have the shot forms relative sealed space.
Vertical bullet dish kinetic energy transmitting system, it is in division board both sides on the drum magazine are provided with the boss the open end of ammunition feed section is provided with and corresponds the complex joint groove with division board epirelief platform, when the division board of drum magazine is rotatory to the open end of ammunition feed section, the joint inslot formation of ammunition feed section open end is gone into to boss card on the division board ends and is only detained formula butt joint structure.
Vertical bullet dish kinetic energy transmitting system, it is in be provided with the ammunition feed motor on the barrage, the ammunition feed motor is used for the drive to dial bullet tooth and synchronous rotation of barrage cage be provided with rotary encoder on the power output shaft of ammunition feed motor.
Vertical bullet dish kinetic energy transmitting system, its the launching tube is including launching barrel and chamber barrel, launching barrel one end links to each other with the confession bullet section of confession bullet mechanism, and its other end links to each other with the chamber barrel the launching barrel middle part is provided with at least one and strengthens the section be provided with a plurality of spiral archs and the recess that become certain inclination with the barrel axis on the bore guide part pipe wall of chamber barrel.
The utility model discloses a vertical bullet dish kinetic energy transmitting system, its the control system includes motor rotary transformer control system, pressure control system, sensor control system and communication system;
the motor rotating transformer control system is connected with the ammunition supply motor, and controls the compound ammunition supply mechanism for synchronously rotating the ammunition supply tooth and the drum isolation cover through a single motor control mode;
the pressure control system is respectively connected with the quick-opening valve and the regulating valve;
and the sensor control system is connected with the rotary encoder and is used for detecting the projectile feeding state of the projectile.
Vertical bullet dish kinetic energy transmitting system, its control system still includes ground test system, ground test system is including retrieving room, target plate and the system of testing the speed, it is used for the recovery to the transmission pellet to retrieve the room, the system of testing the speed is used for measuring the muzzle initial velocity of pellet.
The utility model discloses a structural design of ammunition feed mechanism, the ammunition feed that can be rapid accurate when making the magazine ammunition feed adopts the ammunition feed structure of the multistage combined type motion of single motor control, realizes the ammunition feed of ammunition feed mechanism, advances the bullet, divides the bullet and the bore inner seal's function, accomplishes the automatic continuous loading of shot, has characteristics such as safe in utilization, convenient operation, reliable operation.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural diagram of the drum magazine of the present invention.
Fig. 3 is a schematic structural view of the middle poking spring tooth of the present invention.
Fig. 4 is a schematic structural diagram of the drum magazine of the present invention.
Fig. 5 is a schematic structural view of the projectile when the projectile is ejected from the ejection opening by the middle-pulling projectile tooth.
Fig. 6 is a schematic structural view of the projectile feeding section of the present invention when the projectile is sealed by the partition plate.
Fig. 7 is a schematic structural view of the present invention when the middle isolation plate and the ammunition feed section form a locking type butt joint structure.
Fig. 8 is a schematic exploded view of fig. 7.
Fig. 9 is a schematic view of the installation structure of the ammunition supply motor of the present invention.
Fig. 10 is a schematic view of the mounting structure of the rotary encoder of the present invention.
Fig. 11 is a schematic structural view of a launching barrel of the present invention.
Fig. 12 is a schematic structural view of the midriff barrel of the present invention.
Fig. 13 is a control flow chart of the launch program of the present invention.
Fig. 14 is a schematic diagram of the speed measuring system of the present invention.
In the figure: 1 is the drum magazine, 2 is the shot, 3 is the play mouth, 4 is dialling the bullet tooth, 5 is the drum magazine, 6 is the ammunition feed section, 7 is fixed guide, 8 is the division board, 9 is the boss, 10 is the joint groove, 11 is the ammunition feed motor, 12 is rotary encoder, 13 is the launching tube.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by a person skilled in the art without making creative efforts belong to the protection scope of the present invention. It should be noted that, in the case of no conflict, the embodiments and features of the embodiments of the present invention may be combined with each other.
As shown in fig. 1 to 6, the vertical projectile disk kinetic energy launching system comprises a launching device system, an air supply system and a control system, wherein the launching device system comprises a launching tube 13, a quick-opening valve, a high-pressure air chamber and a projectile feeding mechanism.
The utility model discloses a launcher system is the main part of launch system, is a high overload kinetic energy launch system, according to the similar principle of dynamics, uses compressed air to replace the high-pressure gas that traditional gunpowder burning produced to accomplish the transmission to the shot. When the projectile is launched, the quick opening valve is quickly opened, the gas pressure is directly applied to the bottom of the projectile, and the projectile is accelerated to obtain certain kinetic energy and then is ejected from a muzzle. The design of this scheme has fully combined 25mm bore principle model machine design experience in the past, simultaneously according to the requirement of using under the space environment to satisfy the muzzle initial velocity that the index required and be the design basis, accomplish structural security, reliability simultaneously, and accomplish the best optimization of structure on this basis again, with lightweight, the miniaturization, the modularization of guaranteeing the product.
The quick-opening valve is arranged between the high-pressure air chamber and the inner cavity of the bullet supply section 6 and used for closing the front-end outlet of the high-pressure air chamber to isolate air or quickly opening the front-end outlet of the high-pressure air chamber to communicate the high-pressure air chamber with the inner cavity of the bullet supply section 6.
Specifically, the launching tube is mainly used for completing a launching task of the projectile, and the projectile is pushed by air pressure after being opened through the quick opening valve and accelerated in the gun tube until certain projectile kinetic energy is obtained, and then is ejected from a gun muzzle to complete a launching action. The launching tube is made of high-strength aluminum alloy materials, the bearing in the bore is considered, and the wall thickness of the barrel is reasonable. As shown in fig. 11 and 12, the launching tube 13 includes a launching barrel and a bore barrel, one end of the launching barrel is connected with the ammunition feeding section 6 of the ammunition feeding mechanism, the other end of the launching barrel is connected with the bore barrel, two reinforcing sections are arranged in the middle of the launching barrel, the whole wall thickness is reasonably reduced while the bearing pressure and the strength rigidity of the barrel are ensured, so that the barrel mass is reduced, and the barrel interface adopts a large-size rectangular threaded connection interface; in order to improve the hitting precision of the launching system, the system is also provided with a line-chamber barrel, and the wall of the inner chamber guide part of the line-chamber barrel is provided with a plurality of spiral bulges and grooves which form a certain inclination angle with the axis of the barrel, so that the line-chamber barrel has the function of endowing the shot with a certain rotating speed when the shot goes out of the chamber, and the stability of the shot in the flying process is ensured. Meanwhile, the interfaces of the line-bore barrel and the launching barrel are kept consistent, so that the line-bore barrel and the launching barrel have interchangeability conditions.
Specifically, a quick-opening valve, which serves to isolate gas and open quickly, is usually installed at the front end of the high-pressure chamber. When gas is injected, the quick-opening valve is in a closed state, so that the gas is only injected into the high-pressure gas chamber and does not leak to the emission barrel section; when in deflation, the quick-opening valve can be quickly opened, so that a large amount of gas in the high-pressure gas chamber immediately acts on the bottom of the projectile positioned in the projectile feeding section. The quick-opening valve in the scheme preferably adopts a piston type pressure release mechanism so as to improve the design optimization of the structure, control the pressure of the air chamber and realize the high-speed movement of the piston rod, thereby realizing the function of quick opening, and the opening speed is about 10ms.
The high-pressure air chamber is used for storing high-pressure air and providing energy for accelerating the shot. In this embodiment, its volume design is 1L, satisfies the bullet supply initial velocity requirement by interior ballistic trajectory calculation, and the high-pressure gas chamber internal diameter is 70mm, and high light aluminum alloy processing is adopted on the high-pressure gas chamber wholly, designs according to 15 MPa's overload pressure, guarantees certain factor of safety.
The gas supply system is connected with the high-pressure gas chamber, is used for providing inert gas for the high-pressure gas chamber, is a power source for ensuring normal work of the launching system, and particularly is peripheral equipment essential to the launching system and consists of a gas storage tank, a regulating valve and a conveying pipeline. The gas storage tank is internally provided with a gas medium, the output pressure value is adjusted by an adjusting valve, the function of supplying gas to the high-pressure gas chamber is realized through a conveying pipeline, and the gas storage tank has the main task of ensuring the storage and release of high-pressure gas.
The control system is connected to the launching device system and the air supply system, respectively, and is configured to control a launching process of the launching device system and an operation of the air supply system, as shown in fig. 13, which is a control flow chart of a launching program. The control system mainly controls and feeds back the execution action of the transmitting system and detects and controls the state parameters of the transmitting system according to the application requirements in the space environment, and the core of the whole control box lies in the power supply and distribution, remote control and remote measurement, control of an ammunition supply mechanism, control of a valve switch, control of inflation pressure and the like of the system.
Specifically, the control system comprises a motor rotary transformer control system, a pressure control system, a sensor control system and a communication system. The motor rotation control system is connected with the bullet supply motor 11, and controls the composite bullet supply mechanism for synchronously rotating the poking elastic teeth 4 and the bullet drum isolation cover 5 through a single motor control mode; the pressure control system is respectively connected with the quick opening valve and the regulating valve; the sensor control system is connected to the rotary encoder 12 for detecting the feeding status of the projectiles.
The control system further comprises a ground test system, and the ground test system tests the overall performance of the launching system under the ground environment and comprises indexes such as launching speed, initial speed of the projectile, striking precision and the like. Specifically, the ground test system comprises a recovery chamber, a target plate and a speed measurement system, wherein the recovery chamber is used for recovering shot shots.
As shown in fig. 14, the velocity measurement system is used to measure the muzzle initial velocity of the projectile. At the moment when the projectile is shot out of the muzzle, the projectile has obtained a certain initial velocity kinetic energy. At the moment when the projectile starts to move, the shading quantity is changed through an infrared screen of a first launch correlation ballistic trajectory screen sensor, a first square wave generated by the first sensor is fed back to a controller, the projectile moves through a second launch correlation ballistic trajectory screen sensor, a second square wave generated by the second sensor is fed back to the controller, and the launch time is calculated through the time difference between the first square wave and the second square wave, so that the muzzle initial speed of the projectile is calculated according to a formula.
As shown in fig. 2 to 6, ammunition feed mechanism includes drum 1 and holds a plurality of shots 2 in drum 1 magazine be provided with play bullet mouth 3 on drum 1 be provided with in drum 1 and be used for dialling out the bullet tooth 4 of playing 3 with shot 2 drum 1 outside drum 1 is provided with and dials 4 synchronous revolution's drum cage 5, drum cage 5 is used for pushing away the shot 2 of dialling bullet tooth 4 and pushes away to the position of waiting to launch of the 6 inner chambers of bullet section, and seals up shot 2 in bullet section 6 through drum cage 5. The utility model discloses in, for the ammunition feed that can be rapid accurate when making the magazine ammunition feed to alleviate whole weight simultaneously, this scheme adopts the ammunition feed structure of single motor control multistage combined type motion, and its magazine capacity is 30 shots, and can accomplish automatic continuous loading.
Specifically, a plurality of shots 2 are perpendicularly placed in a fixed motion track formed by a fixed guide rail 7 in the drum magazine 1, the shots 2 move along a fixed track in the drum magazine 1 under the action of the poking bullet teeth 4 and are sequentially pulled out from a bullet outlet 3 formed in the drum magazine 1, the bullet outlet 3 formed in the drum magazine 1 corresponds to the open end of the bullet supply section 6, a plurality of partition plates 8 correspondingly matched with the tooth portions of the poking bullet teeth 4 are arranged on the drum partition cover 5, the partition plates 8 on the drum partition cover 5 are arranged at the back in the rotation direction relative to the corresponding tooth portions of the poking bullet teeth 4, the shots 2 are pushed into the to-be-launched position inside the bullet supply section 6 through the partition plates 8 arranged at the back after the poking bullet outlet 3 of the poking bullet teeth 4, the partition plates 8 on the drum partition cover 5 are rotated to the open end of the bullet supply section 6 and are in butt joint sealing with the bullet supply section 6, so that the inner cavity of the bullet supply section 6 filled with the shots 2 forms a relatively sealed space. Wherein, the main effect of drum cage on the one hand is for having dialled out the bullet of play mouth and continue to provide group bullet thrust and make it move to the feed magazine position, on the other hand is that the bullet arrives the feed magazine position after, seal the bullet in the inside position of waiting to launch of feed section, the thrust that the drum was dialled out to the bullet promptly is provided by dialling the bullet tooth, after the drum was dialled out to the bullet, when waiting to launch the position motion to the feed magazine, its thrust is provided by the division board of drum cage, dial bullet tooth and drum cage synchronous rotation motion, only the tooth portion of dialling the bullet tooth is slightly leaned on in the drum cage.
As shown in fig. 7 and 8, bosses 9 are arranged on two sides of a partition plate 8 on the drum magazine 5, a clamping groove 10 corresponding to the boss 9 on the partition plate 8 is arranged at the opening end of the cartridge feeding section 6, and when the partition plate 8 of the drum magazine 5 rotates to the opening end of the cartridge feeding section 6, the boss 9 on the partition plate 8 is clamped into the clamping groove 10 at the opening end of the cartridge feeding section 6 to form a buckle-stopping type butt joint structure. The design of knot formula butt joint structure, the accuracy of guaranteeing the division board rotational position is guaranteed to the division board on the one hand, guarantees that the division board can be better with bullet supply section upper shed sealed, and on the other hand is in the twinkling of an eye in order to guarantee the shot transmission, and bullet supply section inner chamber pressure increases suddenly, avoids inner chamber pressure to the pressure impact of drum magazine, lets pressure undertake by the butt joint boss.
As shown in fig. 9 and 10, the drum magazine is vertically installed on the upper end of the cartridge feeding section in the whole lateral direction, the drum magazine 1 is provided with a cartridge feeding motor 11, the cartridge feeding motor 11 is used for driving the cartridge shifting teeth 4 and the drum magazine 5 to synchronously rotate, specifically, the cartridge feeding motor is a 320V dc motor, the output torque is 20n.m, the power output shaft of the cartridge feeding motor 11 is provided with a rotary encoder 12, and whether the cartridge feeding of the monitoring projectile is in place or not is controlled by detecting the rotation angle of the motor.
The launching system optimizes the structural strength and the interface strength while considering the realization of structural functional performance, carries out structural optimization on a local weak structure according to the environmental and mechanical requirements under the space application environment, and leads the whole ammunition supply mechanism to pass the environmental and mechanical requirements required by a space carrying platform.
The launching system controls and releases the high-pressure inert gas, thereby realizing the accelerated launching process of the projectile. As the inert gas with high molecular weight is adopted, compared with the traditional gunpowder launching, the gas medium is more single, and the converted kinetic energy is more sufficient due to the high mole number. Meanwhile, the corresponding impact on the launching recoil is small, and the impact on the posture of the system carrying platform is small.
The launching system adopts inert gas as driving energy, the whole launching process can be considered as a cold launching process, and the launching system does not contain an initiating explosive device and has higher reliability and safety.
The launching system adopts the bullet feeding mechanism of the vertical bullet disk, the bullet feeding mechanism controls the compound action of the bullet poking teeth, the bullets and the bullet drum isolation cover of the bullet drum through the output of the single motor, and the functions of bullet feeding, bullet distribution and bore internal sealing of the bullet feeding mechanism are realized.
The launching system carries out real-time signal detection on the bullet feeding action of the bullet through the design of the bullet drum and the sensor, monitors and counts whether the bullet is fed in place or not and the position number of the bullet feeding bullet, and can feed back the telemetering signal of the bullet feeding state in time.
The above description is only for the preferred embodiment of the present invention and should not be taken as limiting the invention, and any modifications, equivalent replacements, and improvements made within the spirit and principle of the present invention should be included within the protection scope of the present invention.
Claims (10)
1. The utility model provides a vertical bullet dish kinetic energy transmitting system, includes emitter system, air feed system and control system, its characterized in that: the launching device system comprises a launching tube (13), a quick opening valve, a high-pressure air chamber and a bullet supply mechanism;
the two ends of the inner cavity of the ammunition feeding section (6) of the ammunition feeding mechanism are respectively connected with the launching tube (13) and the high-pressure air chamber, and the quick-opening valve is arranged between the high-pressure air chamber and the inner cavity of the ammunition feeding section (6) and is used for closing the front-end outlet of the high-pressure air chamber to isolate gas or quickly opening the front-end outlet of the high-pressure air chamber to communicate the high-pressure air chamber with the inner cavity of the ammunition feeding section (6);
the gas supply system is connected with the high-pressure gas chamber and is used for supplying inert gas to the high-pressure gas chamber;
and the control system is respectively connected with the transmitting device system and the gas supply system and is used for controlling the transmitting process of the transmitting device system and the action of the gas supply system.
2. The vertical sabot kinetic energy launching system of claim 1, further comprising: ammunition feed mechanism includes barrate (1) and holds a plurality of shots (2) in barrate (1) magazine be provided with play bullet mouth (3) on barrate (1) be provided with in barrate (1) and be used for dialling group bullet tooth (4) of play bullet mouth (3) with shot (2) barrate drum (1) outside is provided with and dials bullet tooth (4) synchronous revolution's barrate cage (5), barrate cage (5) are used for pushing away shot (2) of dialling bullet tooth (4) and push away to the pending launch position of ammunition feed section (6) inner chamber, and seal up shot (2) in ammunition feed section (6) through barrate cage (5).
3. The vertical projectile disk kinetic energy launching system of claim 2, wherein: the projectile bodies (2) are placed in a fixed motion track formed by a fixed guide rail (7) in the drum magazine (1), and the projectile bodies (2) move along the fixed track in the drum magazine (1) under the action of the poking teeth (4) and are sequentially poked out through projectile outlets (3) formed in the drum magazine (1).
4. The vertical sabot kinetic energy launching system of claim 3, further comprising: the play bullet mouth (3) of seting up on barrage (1) corresponds with the open end of ammunition feed section (6) be provided with a plurality ofly on barrage cage (5) and dial bullet tooth (4) tooth and correspond complex division board (8), division board (8) on barrage cage (5) lean on the back to arrange for the corresponding tooth portion of dialling bullet tooth (4) in the direction of rotation, behind bullet (2) dial play bullet mouth (3) through dialling bullet tooth (4), push to the inside position of awaiting the launch of ammunition feed section (6) through division board (8) that set up by the back again.
5. The vertical projectile disk kinetic energy launching system of claim 4, wherein: and the isolating plate (8) on the drum isolating cover (5) is rotated to the opening end of the bullet supply section (6) and is in butt joint sealing with the bullet supply section (6), so that a relatively sealed space is formed in the inner cavity of the bullet supply section (6) filled with the bullets (2).
6. The vertical projectile disk kinetic energy launching system of claim 5, wherein: division board (8) both sides on barrage cage (5) are provided with boss (9) the open end of ammunition feed section (6) be provided with division board (8) go up boss (9) and correspond complex joint groove (10), when division board (8) of barrage cage (5) are rotatory to the open end of ammunition feed section (6), boss (9) card on division board (8) are gone into and are formed in joint groove (10) of ammunition feed section (6) open end and end knot formula butt joint structure.
7. The vertical projectile disk kinetic energy launching system of claim 2, wherein: the drum magazine is characterized in that a cartridge feed motor (11) is arranged on the drum magazine (1), the cartridge feed motor (11) is used for driving the poking elastic teeth (4) and the drum magazine isolating cover (5) to synchronously rotate, and a rotary encoder (12) is arranged on a power output shaft of the cartridge feed motor (11).
8. The vertical projectile disk kinetic energy launching system of claim 1, wherein: launch barrel (13) are including launching barrel and line thorax barrel, launch barrel one end links to each other with ammunition feed section (6) of ammunition feed mechanism, and its other end links to each other with the line thorax barrel the launch barrel middle part is provided with at least one and strengthens the section be provided with a plurality of spiral archs and the recess that become certain inclination with the barrel axis on the bore guide part pipe wall of line thorax barrel.
9. The vertical projectile disk kinetic energy launching system of claim 7, wherein: the control system comprises a motor rotary transformer control system, a pressure control system, a sensor control system and a communication system;
the motor rotating transformer control system is connected with a bullet supply motor (11), and a composite bullet supply mechanism for synchronously rotating the poking elastic teeth (4) and the drum isolating cover (5) is controlled through a single motor control mode;
the pressure control system is respectively connected with the quick-opening valve and the regulating valve;
the sensor control system is connected with the rotary encoder (12) and used for detecting the feeding state of the shot.
10. The vertical projectile disk kinetic energy launching system of claim 9, wherein: the control system further comprises a ground test system, the ground test system comprises a recovery chamber, a target plate and a speed measurement system, the recovery chamber is used for recovering the shot to be shot, and the speed measurement system is used for measuring the muzzle initial speed of the shot.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222314084.9U CN218120756U (en) | 2022-08-31 | 2022-08-31 | Vertical bullet dish kinetic energy transmitting system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222314084.9U CN218120756U (en) | 2022-08-31 | 2022-08-31 | Vertical bullet dish kinetic energy transmitting system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN218120756U true CN218120756U (en) | 2022-12-23 |
Family
ID=84529453
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202222314084.9U Active CN218120756U (en) | 2022-08-31 | 2022-08-31 | Vertical bullet dish kinetic energy transmitting system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN218120756U (en) |
-
2022
- 2022-08-31 CN CN202222314084.9U patent/CN218120756U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1102022B1 (en) | Automatic weapon with recoiling barrel | |
US3491650A (en) | Firearm | |
RU2363908C2 (en) | "tyamack" artillery piece with floating recoil | |
CN218120756U (en) | Vertical bullet dish kinetic energy transmitting system | |
CN218120754U (en) | Vertical bullet disk ammunition feed mechanism | |
RU2571837C2 (en) | Two-medium automatic sniper gun and cartridges for shooting from v.a. kushchenko gun | |
CN213932207U (en) | Micro-sound sniper gun structure | |
CN110631412B (en) | Automatic piston long-stroke air guide backseat system of medium-large-diameter high-precision automatic rifle | |
US2581395A (en) | Gas piston operated firearm | |
CN114894041B (en) | High-speed shelling no-force gun bullet capable of being launched in limited space | |
CN114963865B (en) | Capacity-increasing type gun initial speed serialization device and control method | |
CN114777566B (en) | Chemical-amplification type gun initial speed serialization device and control method | |
US4084480A (en) | Lightweight small craft gun system | |
RU180703U1 (en) | Air rifle automatic reload device | |
RU2545185C2 (en) | Biathlon pneumatic spring-piston rifle of kushchenko v.a. and bullet for rifle shooting (versions) | |
CN114027289B (en) | Titanium radium bullet bird repellent device with compressed air as power | |
CN117663896A (en) | Vertical spring plate kinetic energy emission system | |
US11346621B2 (en) | Recoilless apparatus for guns | |
CN215909748U (en) | Firearm without recoil or with low recoil | |
CN218120755U (en) | Ammunition supply mechanism and rotating wheel type kinetic energy launching system | |
CN218455416U (en) | Ammunition feed disc and ammunition feed mechanism | |
CN218443521U (en) | Double-elastic-disc kinetic energy launching system | |
CN112524995A (en) | Attached ammunition firing speed adjusting device and working method thereof | |
US20070251133A1 (en) | Method of firing of firearms | |
CN117804273A (en) | Double-spring-disc kinetic energy emission system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |