CN214173116U - Simulated shell launching device for actual combat simulated confrontation system - Google Patents
Simulated shell launching device for actual combat simulated confrontation system Download PDFInfo
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- CN214173116U CN214173116U CN202023309644.9U CN202023309644U CN214173116U CN 214173116 U CN214173116 U CN 214173116U CN 202023309644 U CN202023309644 U CN 202023309644U CN 214173116 U CN214173116 U CN 214173116U
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Abstract
The utility model discloses a emulation shell emitter for real soldier's combat simulation confrontation system relates to military training apparatus technical field, including launching tube, spacing section of thick bamboo and drive assembly, inside spacing section of thick bamboo passed through drive assembly and can locate the launching tube through the back-and-forth movement ground cover, and the inner wall and the emulation shell of spacing section of thick bamboo contradict each other. The utility model discloses well spacing section of thick bamboo not only can play the effect of support and fixed emulation shell, can adjust emulation shell transmission position moreover for the use of launching tube is nimble more convenient, is favorable to adjusting the range of emulation shell, and makes the launching tube can extensively be applicable to the emulation shell of various different grade types, and the practicality is strong.
Description
Technical Field
The utility model belongs to the technical field of military training apparatus technique and specifically relates to a emulation shell emitter for real soldier's combat simulation countermeasures system.
Background
The practice ball shooting training is an important project of a real soldier combat simulation countermeasure system, and in order to simulate a battlefield situation and create battlefield atmosphere and effect, a launcher with a launch tube is generally adopted to launch simulated ammunition, for example, a chasing gun is adopted to launch simulated chasing shells, or a grenade launcher mounted below a rifle barrel is adopted to launch simulated grenades. However, the training modes have the problems of complex operation, high potential safety hazard and high training cost.
The chinese patent with application number 201720641674.9 discloses a cylinder pneumatic launcher for launching a simulated training projectile, which is provided with a piston cylinder in the launch cylinder, and a punch for striking the simulated training projectile fuse structure is arranged at the end of the piston rod of the piston cylinder, thereby realizing pneumatic launch and effectively solving the problems existing in the prior art.
However, in the technical scheme, the length of the launching tube cannot be adjusted, the fixed position of the simulated training projectile cannot be adjusted, and in the training process, if the range of the simulated training projectile is adjusted, the simulated training projectile can be achieved only by adjusting the thrust of the air cylinder, so that certain disadvantages exist.
Disclosure of Invention
The utility model provides a emulation shell emitter for real soldier's combat simulation countermeasures system, its main aim at solves above-mentioned problem.
The utility model adopts the following technical scheme:
the utility model provides a simulation shell emitter for real soldier's combat simulation confrontation system, includes the launching tube and sets up the firing mechanism who is used for striking the simulation shell in the launching tube, still includes spacing section of thick bamboo and drive assembly, but inside the launching tube was located to spacing section of thick bamboo through drive assembly back-and-forth movement ground cover, and the inner wall of spacing section of thick bamboo with the simulation shell is contradicted each other.
Further, the driving assembly comprises a movable sleeve and a connecting block; the launching tube is provided with at least one strip-shaped sliding groove along the length direction; the movable sleeve is sleeved outside the launching tube in a manner of moving back and forth, and the connecting blocks connected with the limiting tube are arranged at corresponding positions of the strip-shaped sliding grooves.
Furthermore, a plurality of limiting salient points are symmetrically arranged on two side walls of the strip-shaped sliding groove and used for fixing the connecting block.
Furthermore, a bracket which is mutually abutted with the outer surface of the simulated cannonball is arranged at the end part of the inner side of the limiting cylinder.
Further, the launching mechanism comprises a cylinder, an air duct, an electromagnetic valve and a high-pressure air storage tank; one end of the cylinder body of the air cylinder is fixedly arranged at the end part of the launching tube, and the other end of the cylinder body is connected to the high-pressure air storage tank through an air guide pipe and an electromagnetic valve; a piston rod of the cylinder is arranged in the launching tube in a manner of moving back and forth, and is provided with a punch head for impacting the simulated cannonball.
Furthermore, the end part of the punch is provided with a striking part which is mutually butted with the fuse component of the simulated cannonball.
Compared with the prior art, the utility model discloses the beneficial effect who produces lies in:
the utility model discloses a emulation shell emitter for real soldier's combat simulation confrontation system, including launching tube, a spacing section of thick bamboo and drive assembly, but inside a spacing section of thick bamboo passed through drive assembly back-and-forth movement ground cover and locates the launching tube, and the inner wall and the emulation shell of a spacing section of thick bamboo contradict each other. The utility model discloses well spacing section of thick bamboo not only can play the effect of support and fixed emulation shell, can adjust emulation shell transmission position moreover for the use of launching tube is nimble more convenient, is favorable to adjusting the range of emulation shell, and makes the launching tube can extensively be applicable to the emulation shell of various different grade types, and the practicality is strong.
Drawings
Fig. 1 is a partial sectional view of the launching tube and the launching mechanism of the present invention.
Fig. 2 is a schematic structural view of the middle launching tube of the present invention.
Fig. 3 is an exploded view of the middle launcher of the present invention.
Fig. 4 is a schematic structural view of the middle launching tube and the mounting frame of the present invention.
Detailed Description
The following describes embodiments of the present invention with reference to the drawings. Numerous details are set forth in the following description in order to provide a thorough understanding of the present invention, but it will be apparent to one skilled in the art that the present invention may be practiced without these details.
Referring to fig. 1 to 3, a simulated cannonball launching device for an actual combat simulated confrontation system comprises a launching tube 1 and a launching mechanism 2 arranged in the launching tube 1 and used for impacting a simulated cannonball A, and further comprises a limiting tube 11 and a driving assembly, wherein the limiting tube 11 is sleeved inside the launching tube 1 through the driving assembly in a manner of moving back and forth, and the inner wall of the limiting tube 11 is abutted to the simulated cannonball A. The utility model provides a spacing section of thick bamboo 11 not only can play the effect of support and fixed emulation shell A, can adjust emulation shell A transmission position moreover for the use of launching tube 1 is nimble more convenient, is favorable to adjusting emulation shell A's range, and makes launching tube 1 can extensively be applicable to the emulation shell A of various different grade types, and the practicality is strong.
Referring to fig. 1 to 3, the driving assembly includes a movable sleeve 12 and a connecting block 13; the launching tube 1 is provided with at least one strip-shaped sliding groove 10 along the length direction; the movable sleeve 12 is sleeved outside the launching tube 1 in a manner of moving back and forth, and a connecting block 13 connected to the limiting tube 11 is arranged at a position corresponding to the strip-shaped sliding groove 10. Specifically, the outer side wall of the limiting cylinder 11 is provided with a mounting groove 111 for mounting the connecting block 13. During installation, the limiting cylinder 11 can be installed inside the launching cylinder 1, then one end of the connecting block 13 is installed in the installation groove 111 of the limiting cylinder 11, the movable sleeve 12 is sleeved outside the launching cylinder 1, and the other end of the connecting block 13 is bonded on the inner wall of the sliding sleeve 12 through glue. In addition, can also adopt the connected mode of mortise and tenon structure, also set up the mounting groove at activity sleeve 12 lateral wall promptly, the inside and the outside of launching tube are located to spacing section of thick bamboo 11 and activity sleeve 12 cover respectively during the installation to make spacing section of thick bamboo 11 align each other with the mounting groove of activity sleeve 12, it can in the mounting groove to insert the connecting block again at last. Therefore, the utility model discloses well drive assembly's simple structure, convenient operation is favorable to realizing the regulation of emulation shell A transmission position.
Referring to fig. 1 to 3, two side walls of the strip-shaped chute 10 are symmetrically provided with a plurality of limit bumps 101 for fixing the connecting block 13. The plurality of limiting salient points 101 play a limiting role on the limiting barrel 11, and when the simulated cannonball A is used, the sliding sleeve 12 is pushed forwards and backwards with a little force according to the launching position of the simulated cannonball A, so that the operation is simple and convenient.
Referring to fig. 1 to 3, the inner end of the limiting cylinder 11 is provided with a bracket 110 which is abutted against the outer surface of the simulated cannonball a. The structure of the bracket 110 may be designed according to the specific configuration of the simulated cannonball A.
Referring to fig. 1, the firing mechanism 2 includes a cylinder 21, an air duct 22, an electromagnetic valve 23, and a high-pressure air tank 24; one end of a cylinder body 211 of the cylinder 21 is fixedly arranged at the end part of the launching tube 1, and the other end of the cylinder body 211 is connected with a high-pressure air storage tank 24 through an air duct 22 and an electromagnetic valve 23; a piston rod 212 of the cylinder 21 is arranged in the barrel 1 movably back and forth and is provided with a punch 213 for striking the simulated projectile. In order to fire the artificial shell more precisely, the end of the punch 213 is provided with a striking part 214 which interferes with the fuse member of the artificial shell a. Likewise, the specific configuration of the impact portion 214 can also be designed according to the specific configuration of the simulated shell A.
Referring to fig. 4, the launching device further includes a mounting frame 3 for mounting the launch canister 1; the mounting frame 3 comprises a base 31 and two connecting arms 32 which are symmetrically arranged on two sides of the base 31, and a mounting part is formed between the two connecting arms 32; the launching tube 1 can be vertically arranged in the mounting part in a turnover mode through the connecting assembly. The utility model discloses a launching tube 1 has designed dedicated mounting bracket 3, and this mounting bracket 3 not only can be simple, and is firm stable, can adjust launching tube 1's launch angle wantonly moreover, and it is nimble convenient to use, and the practicality is strong.
Referring to fig. 4, as a specific connection method: the connection assembly includes an adjustment nut 33; the two connecting arms 32 are provided with mounting holes at corresponding positions of the mounting parts; both sides of the launch barrel 1 are vertically and tiltably installed in the installation part by means of the adjusting nut 33 matching with the installation hole. The design of the adjusting nut 33 not only can fully ensure the installation stability of the launch canister 1, but also can make the adjustment of the installation angle of the launch canister 1 more flexible and convenient. In addition, still can be with launch barrel 1 pin joint in the mount pad to set up the cylinder or the electric telescopic handle that are used for driving launch barrel 1 to realize vertical upset. Those skilled in the art can understand and implement the method according to the above description, and thus the detailed description is omitted.
Referring to fig. 4, the base 31 is provided with a storage cabinet 34 for storing the simulated shell a between the two connecting arms 32. The design of the storage cabinet 34 can be used for storing the simulated cannonball A and other articles on one hand, and on the other hand, the stability of the mounting frame 3 can be improved by using the weight of the stored articles, so that the practicability, reliability and convenience of the mounting frame 3 are effectively improved.
Referring to fig. 4, because the launching tube 1 can be vertically turned, in order to facilitate taking the simulated cannonball a quickly in the training process, the front side and the rear side of the 34 of the storage cabinet are hinged with a cabinet door 341 and provided with a handle 342.
Referring to fig. 4, the base 31 is provided with a ramp 35 at the lower edge of the cabinet door. When storing emulation shell A, in order to guarantee safety, place it with dedicated shell case earlier usually, place the shell case in locker 34 again, consequently set up sloping platform 35 and can conveniently pull out the shell case to ground when taking emulation shell A for the design of storage case 34 is more humanized and rationalized.
Referring to fig. 4, as a preferred solution: the two connecting arms 32 are of triangular configuration, whereby the structural stability of the mounting frame 3 is fully ensured.
Referring to fig. 4, as a preferred solution: both connecting arms 32 are provided with lightening holes 321, so that the structural strength of the mounting rack 3 can be ensured, and the self weight of the mounting rack can be properly lightened, so that the mounting rack 3 can be conveniently carried and stored.
The above-mentioned be the utility model discloses a concrete implementation way, nevertheless the utility model discloses a design concept is not limited to this, and the ordinary use of this design is right the utility model discloses carry out immaterial change, all should belong to the act of infringement the protection scope of the utility model.
Claims (6)
1. The utility model provides a emulation shell emitter for real soldier's combat simulation confrontation system, includes the launching tube and sets up the firing mechanism who is used for striking emulation shell in the launching tube, its characterized in that: the simulated projectile shooting device is characterized by further comprising a limiting cylinder and a driving assembly, wherein the limiting cylinder is sleeved inside the launching cylinder in a back-and-forth moving mode through the driving assembly, and the inner wall of the limiting cylinder is abutted to the simulated projectile.
2. The simulated projectile launching device for an actual combat simulated countermeasure system as claimed in claim 1 wherein: the driving assembly comprises a movable sleeve and a connecting block; the launching tube is provided with at least one strip-shaped sliding groove along the length direction; the movable sleeve is sleeved outside the launching tube in a manner of moving back and forth, and the connecting blocks connected with the limiting tube are arranged at corresponding positions of the strip-shaped sliding grooves.
3. The simulated projectile launching device for an actual combat simulated countermeasure system as claimed in claim 2, wherein: and a plurality of limiting convex points are symmetrically arranged on two side walls of the strip-shaped sliding groove and used for fixing the connecting block.
4. The simulated projectile launching device for an actual combat simulated countermeasure system as claimed in claim 1 wherein: and a bracket which is mutually abutted against the outer surface of the simulated cannonball is arranged at the end part of the inner side of the limiting cylinder.
5. The simulated projectile launching device for an actual combat simulated countermeasure system as claimed in claim 1 wherein: the launching mechanism comprises an air cylinder, an air guide pipe, an electromagnetic valve and a high-pressure air storage tank; one end of the cylinder body of the air cylinder is fixedly arranged at the end part of the launching tube, and the other end of the cylinder body is connected to the high-pressure air storage tank through an air guide pipe and an electromagnetic valve; a piston rod of the cylinder is arranged in the launching tube in a manner of moving back and forth, and is provided with a punch head for impacting the simulated cannonball.
6. The simulated projectile launching device for an actual combat simulated countermeasure system as claimed in claim 5, wherein: the end part of the punch is provided with a striking part which is mutually butted with a fuse component of the simulated cannonball.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023309644.9U CN214173116U (en) | 2020-12-31 | 2020-12-31 | Simulated shell launching device for actual combat simulated confrontation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023309644.9U CN214173116U (en) | 2020-12-31 | 2020-12-31 | Simulated shell launching device for actual combat simulated confrontation system |
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| Publication Number | Publication Date |
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| CN214173116U true CN214173116U (en) | 2021-09-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202023309644.9U Active CN214173116U (en) | 2020-12-31 | 2020-12-31 | Simulated shell launching device for actual combat simulated confrontation system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
-
2020
- 2020-12-31 CN CN202023309644.9U patent/CN214173116U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
| CN114485262B (en) * | 2022-01-29 | 2024-03-29 | 重庆零壹空间航天科技有限公司 | System for verifying missile oblique launching reliability |
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