Individual portable air defense missile actual combat simulation training device magazine
By designing a man-portable air defense missile combat simulation training device with a missile magazine, the problem of the lack of live-fire launches in existing simulators has been solved, enabling high-accuracy training under low-cost and low-field conditions, and simulating the physiological condition reflexes of real launches.
Patent Information
- Application Number
- CN202520030248.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-07
- Publication Date
- 2025-11-18
- Estimated Expiration
- 2035-01-07
AI Technical Summary
Existing man-portable air defense missile simulators lack live-fire capabilities, leading to aiming distortion and decreased hit rate due to conditioned reflexes. Furthermore, live-fire training is costly, has high site requirements, and cannot generate physiological conditioned reflexes in humans.
Design a man-portable air defense missile combat simulation training device magazine, including a magazine shell, cover assembly, stop block assembly, locking component and rotating assembly, to ensure that the simulated missile is stably fixed during the launch process, and to achieve simulated launch by connecting to the launch mechanism through a conductive pin.
The simulator's magazine can generate conditioned reflexes under low-cost and low-site-requirement conditions, improving hit rate, reducing psychological pressure, and providing a realistic firing experience.
Smart Images
Figure CN223564861U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of combat simulation training technology for air defense missiles, specifically to a man-portable air defense missile combat simulation training device magazine. Background Technology
[0002] Man-portable air defense missile combat simulation training device, hereinafter referred to as simulator.
[0003] Currently, domestic simulators all use AR simulators and laser simulators for training, and do not have the function of firing simulated live ammunition for training, so they do not have ammunition magazines.
[0004] During equipment training, when a shooter operates the firing mechanism, due to conditioned reflexes, they may blink or shift their shoulder at the moment of impact, causing distorted movements, altering the aiming direction, changing the original aiming axis, and reducing hit efficiency. This conditioned reflex cannot be elicited by indoor training methods such as laser or VR, meaning it's impossible to produce a physiological protective response in the human body. Only when using a realistic scenario simulating missile launch can a physiological conditioned reflex be generated.
[0005] Live ammunition is expensive, requires sophisticated training grounds, and is difficult to maintain. Simulated training rounds, on the other hand, meet the basic conditions for inducing conditioned reflexes and have lower requirements for training grounds; firing training can be conducted in ordinary training grounds where there is no danger within visual range. The HN6B, as a new type of man-portable air defense missile, is a combined missile and ammunition system, distributed and stored as ammunition. Before firing live ammunition, the shooter has no opportunity to experience the feeling of firing, resulting in immense psychological pressure and a high likelihood of developing strong conditioned reflexes. Therefore, there is an urgent need to design a man-portable air defense missile combat simulation training device with a missile magazine to solve these problems. Utility Model Content
[0006] The purpose of this invention is to provide a man-portable air defense missile combat simulation training device magazine to address the aforementioned shortcomings in the prior art.
[0007] To achieve the above objectives, this utility model provides the following technical solution:
[0008] A man-portable air defense missile combat simulation training device magazine includes a magazine shell and a simulated missile installed inside the magazine shell. The rear end of the magazine shell is provided with an openable sealing cover assembly, which is used at least to seal the rear end of the magazine shell after the simulated missile is installed.
[0009] The front end of the magazine housing is provided with a stop assembly that extends into the interior of the magazine housing. The stop assembly is used at least to simulate the limiting of the projectile inside the magazine housing.
[0010] A locking member is provided above the cover assembly and is connected to the magazine housing. The locking member is used at least for the fixed connection between the magazine housing and the cover assembly.
[0011] Below the cover assembly is a rotating assembly installed at the rear end of the magazine housing. The rotating assembly is used at least for opening and closing the cover assembly at the rear end of the magazine housing.
[0012] Preferably, the front end of the magazine housing is provided with a slot, the stop assembly is disposed inside the slot, and the front end of the simulated bullet is engaged with the stop assembly.
[0013] Preferably, a slot is provided above the tail end of the magazine housing, and a sealing groove is provided at the tail end of the magazine housing, and the cover assembly is fastened in the sealing groove.
[0014] Preferably, the stop assembly includes a protrusion located inside the magazine housing, and a guide rod is fixedly disposed on the top of the protrusion. A baffle is fixedly disposed on the top of the guide rod. A mounting plate fixed to the outer wall of the magazine housing is slidably sleeved on the outside of the guide rod. A return spring located between the mounting plate and the protrusion is sleeved on the outside of the guide rod.
[0015] Preferably, the cover assembly includes an insulating plate, an ammunition magazine access cover is provided on the outer side of the insulating plate, and a rubber cover is provided on the outer side of the ammunition magazine access cover.
[0016] Preferably, a plurality of spring pins are provided on one outer wall of the insulating plate, and the end of the simulated bullet is provided with a connection port that is electrically connected to the spring pins.
[0017] Preferably, the locking member includes a mounting groove above the cover assembly, and a compression spring is provided inside the mounting groove. The cover assembly is provided with a liner plate outside, and a button is provided in the middle of the liner plate. A tongue plate located inside the mounting groove is provided between the compression spring and the button, and a hook is provided at the end of the tongue plate.
[0018] Preferably, the rotating assembly includes a first hinge plate disposed on the bottom outer wall of the magazine housing and a second hinge plate fixed on the bottom outer wall of the cover assembly. A pivot is provided between the first hinge plate and the second hinge plate, and a notch for mounting the pivot is provided below the tail end of the magazine housing.
[0019] In the above technical solution, the man-portable air defense missile combat simulation training magazine provided by this utility model has the following beneficial effects:
[0020] This invention features a design where, after the simulated projectile is placed into the magazine at the rear of the barrel, the cover assembly is closed and the locking mechanism is pressed to secure it. This ensures that the simulated projectile is firmly fixed inside the magazine, preventing displacement or detachment due to changes in the barrel angle that could lead to launch failure. The conductive pin (spring pin) in the cover assembly is connected to the launching mechanism. When the trigger of the launching mechanism is pulled, the simulated projectile inside the magazine is energized (the spring pin and the connector are connected) and begins to operate. Attached Figure Description
[0021] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in this utility model. For those skilled in the art, other drawings can be obtained based on these drawings.
[0022] Figure 1 This is a structural schematic diagram of the ammunition magazine of a man-portable air defense missile combat simulation training device according to the present invention.
[0023] Figure 2 This is an exploded view of the tail structure of the missile magazine, which is provided for an embodiment of the missile magazine of a man-portable air defense missile combat simulation training device of this utility model.
[0024] Figure 3 This is a partial structural cross-sectional view of the ammunition magazine of a man-portable air defense missile combat simulation training device according to the present invention.
[0025] Figure 4 This is a schematic diagram of the open state structure of the cover assembly provided in an embodiment of the man-portable air defense missile combat simulation training device of this utility model.
[0026] Figure 5 This is an enlarged view of the locking mechanism structure provided in an embodiment of the missile magazine of a man-portable air defense missile combat simulation training device of this utility model.
[0027] Figure 6 This is an enlarged view of the rotating component structure provided in an embodiment of the man-portable air defense missile combat simulation training device of this utility model.
[0028] 1. Magazine housing; 11. Groove; 12. Slot; 13. Sealing groove; 2. Stop assembly; 21. Protrusion; 22. Guide rod; 23. Baffle; 24. Mounting plate; 25. Return spring; 3. Cover assembly; 31. Insulating plate; 32. Spring pin; 33. Connection port; 4. Locking element; 41. Mounting groove; 42. Liner; 43. Compression spring; 44. Tongue plate; 45. Hook; 46. Button; 5. Rubber cover; 6. Magazine access cover; 7. Rotating assembly; 71. Hinge plate one; 72. Hinge plate two; 73. Shaft; 74. Notch; 8. Simulated cartridge. Detailed Implementation
[0029] To enable those skilled in the art to better understand the technical solution of this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings.
[0030] like Figure 1-6 As shown in the figure, the present invention provides a man-portable air defense missile combat simulation training device magazine, including a magazine shell 1 and a simulated missile 8 installed inside the magazine shell 1. The rear end of the magazine shell 1 is provided with an openable cover assembly 3, which is used at least to seal the rear end of the magazine shell 1 after the simulated missile 8 is installed. The front exterior of the magazine shell 1 is provided with a stop assembly 2 that penetrates into the interior of the magazine shell 1, which is used at least to limit the simulated missile 8 inside the magazine shell 1. A locking member 4 connected to the magazine shell 1 is provided above the cover assembly 3, which is used at least to fix the magazine shell 1 and the cover assembly 3. A rotating assembly 7 installed at the rear end of the magazine shell 1 is provided below the cover assembly 3, which is used at least to open and close the cover assembly 3 at the rear end of the magazine shell 1.
[0031] In this embodiment, there are a magazine housing 1 and a simulated missile 8 installed inside the magazine housing 1;
[0032] Specifically, a slot 11 is provided on the front exterior of the magazine housing 1, and a stop assembly 2 is provided inside the slot 11. The front end of the simulated projectile 8 is engaged with the stop assembly 2, and the stop assembly 2 floats inside the slot 11. When the simulated projectile 8 is loaded into the magazine housing 1, the stop assembly 2 limits the simulated projectile 8. When the simulated projectile 8 is launched, the simulated projectile 8 generates thrust, causing the stop assembly 2 to push out and allowing the simulated projectile 8 to move inside the launch channel.
[0033] Specifically, a slot 12 is provided above the tail end of the magazine housing 1, and the hook 45 of the locking member 4 is engaged inside the slot 12 to fix the cover assembly 3 at the tail end of the magazine housing 1. A sealing groove 13 is provided at the tail end of the magazine housing 1, and the cover assembly 3 is fastened in the sealing groove 13.
[0034] In this embodiment, an openable cover assembly 3 is provided at the tail end of the magazine housing 1. The cover assembly 3 is used at least to seal the tail end of the magazine housing 1 after the simulated missile 8 is installed.
[0035] Specifically, the cover assembly 3 includes an insulating plate 31, an ammunition magazine inspection cover 6 is provided on the outside of the insulating plate 31, and a rubber cover 5 is provided on the outside of the ammunition magazine inspection cover 6. The rubber cover 5 can be removed from the ammunition magazine inspection cover 6, and then the ammunition magazine inspection cover 6 can be removed to enable the repair of the circuit board inside the insulating plate 31.
[0036] Specifically, a number of spring pins 32 are provided on one outer wall of the insulating plate 31, and the end of the simulated projectile 8 is provided with a connection port 33 that is electrically connected to the spring pins 32. The spring pins 32 are inserted into the connection port 33, and when the launching mechanism is energized, the circuit is connected, thereby realizing the launching of the simulated projectile 8.
[0037] In this embodiment, a stop assembly 2 is provided on the front exterior of the magazine housing 1, extending into the interior of the magazine housing 1. The stop assembly 2 is used at least to simulate the limiting of the projectile 8 inside the magazine housing 1.
[0038] Specifically, the stop assembly 2 includes a protrusion 21 located inside the magazine housing 1, with a guide rod 22 fixedly mounted on the top of the protrusion 21. A baffle 23 is fixedly mounted on the top of the guide rod 22. A mounting plate 24 fixed to the outer wall of the magazine housing 1 is slidably sleeved on the outside of the guide rod 22. A return spring 25 located between the mounting plate 24 and the protrusion 21 is sleeved on the outside of the guide rod 22. Under the action of the return spring 25, the protrusion 21 is inserted into the inside of the magazine housing 1, forming a blocking structure in the magazine housing 1, allowing the simulated ammunition to pass through. The simulated missile 8 can be stably installed inside the magazine housing 1 without instability caused by angle changes. When the simulated missile 8 is fired, it generates thrust, which pushes the protrusion 21 out of the magazine housing 1. At this time, the guide rod 22 and the baffle 23 move together. The guide rod 22 slides out inside the mounting plate 24. At this time, the return spring 25 is compressed. After the simulated missile 8 is fired, the protrusion 21 returns to its original position under the action of the return spring 25, which facilitates the loading of the next simulated missile 8.
[0039] In this embodiment, a locking member 4 connected to the magazine housing 1 is provided above the cover assembly 3. The locking member 4 is used at least for the fixed connection between the magazine housing 1 and the cover assembly 3.
[0040] Specifically, the locking component 4 includes a mounting groove 41 above the cover assembly 3, and a compression spring 43 is provided inside the mounting groove 41. A liner 42 is provided outside the cover assembly 3, and a button 46 is provided in the middle of the liner 42. A tongue plate 44 is provided between the compression spring 43 and the button 46, located inside the mounting groove 41. A hook 45 is provided at the end of the tongue plate 44. When the cover assembly 3 is fastened to the tail end of the magazine housing 1, the tongue plate 44 drives the hook 45 to engage inside the slot 12, thereby fixing the cover assembly 3 at the tail end of the magazine housing 1. When the cover assembly 3 needs to be opened, the operator needs to press the button 46 to move the tongue plate 44 and the hook 45, allowing the hook 45 to be pulled out from inside the slot 12, thereby quickly opening the cover.
[0041] In this embodiment, a rotating assembly 7 is provided below the cover assembly 3 and installed at the tail end of the magazine housing 1. The rotating assembly 7 is used at least for opening and closing the cover assembly 3 at the tail end of the magazine housing 1.
[0042] Specifically, the rotating assembly 7 includes a first hinge plate 71 disposed on the bottom outer wall of the magazine housing 1 and a second hinge plate 72 fixed on the bottom outer wall of the cover assembly 3. A pivot 73 is disposed between the first hinge plate 71 and the second hinge plate 72. A notch 74 is provided at the lower end of the magazine housing 1 for mounting the pivot 73. When the cover assembly 3 is closed and opened, the pivot 73 causes the first hinge plate 71 and the second hinge plate 72 to rotate relative to each other, and the pivot 73 can enter the interior of the notch 74 to avoid motion interference.
[0043] Operating steps: 1. Insert the simulated missile 8 into the interior of the magazine housing 1;
[0044] Second, under the limiting action of the stop assembly 2 at the front end of the magazine housing 1, the simulated missile 8 is stably installed inside the magazine housing 1;
[0045] Third, the operator then attaches the cover assembly 3 to the rear end of the magazine housing 1 by rotating the assembly 7 and secures it using the locking component 4.
[0046] Fourth, the spring pin 32 in the cover assembly 3 is connected to the launching mechanism. When the trigger of the launching mechanism is pulled and the power is turned on, the simulated missile 8 inside the magazine housing 1 is powered on and works to realize the launch of the simulated missile 8.
[0047] The foregoing description only illustrates certain exemplary embodiments of the present invention. Undoubtedly, those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.
Claims
1. A man-portable air defense missile combat simulation training device magazine, comprising a magazine housing (1) and a simulated missile (8) installed inside the magazine housing (1), characterized in that, The rear end of the magazine housing (1) is provided with an openable cover assembly (3), which is used at least to seal the rear end of the magazine housing (1) after the simulated bullet (8) is installed. The front end of the magazine housing (1) is provided with a stop assembly (2) that extends into the interior of the magazine housing (1). The stop assembly (2) is used at least to simulate the limiting of the projectile (8) inside the magazine housing (1). The cover assembly (3) is provided with a locking member (4) connected to the magazine housing (1) above it. The locking member (4) is used at least for the fixed connection between the magazine housing (1) and the cover assembly (3). Below the cover assembly (3) is a rotating assembly (7) installed at the tail end of the magazine housing (1). The rotating assembly (7) is used at least for opening and closing the cover assembly (3) at the tail end of the magazine housing (1).
2. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, The front end of the magazine housing (1) is provided with a slot (11), the stop assembly (2) is located inside the slot (11), and the front end of the simulated bullet (8) is engaged with the stop assembly (2).
3. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, A slot (12) is provided above the tail end of the magazine housing (1), and a sealing groove (13) is provided at the tail end of the magazine housing (1), and the cover assembly (3) is fastened in the sealing groove (13).
4. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, The stop assembly (2) includes a protrusion (21) located inside the magazine housing (1), and a guide rod (22) is fixedly provided on the top of the protrusion (21). A baffle (23) is fixedly provided on the top of the guide rod (22). An installation plate (24) fixed on the outer wall of the magazine housing (1) is slidably sleeved on the outside of the guide rod (22). A return spring (25) located between the installation plate (24) and the protrusion (21) is sleeved on the outside of the guide rod (22).
5. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, The cover assembly (3) includes an insulating plate (31), an ammunition magazine maintenance cover (6) is provided on the outside of the insulating plate (31), and a rubber cover (5) is provided on the outside of the ammunition magazine maintenance cover (6).
6. The magazine of a man-portable air defense missile combat simulation trainer according to claim 5, characterized in that, A plurality of spring pins (32) are provided on one side of the outer wall of the insulating plate (31), and the end of the simulated bullet (8) is provided with a connection port (33) that is electrically connected to the spring pins (32).
7. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, The locking member (4) includes a mounting groove (41) above the cover assembly (3), and a compression spring (43) is provided inside the mounting groove (41). A liner (42) is provided outside the cover assembly (3), and a button (46) is provided in the middle of the liner (42). A tongue plate (44) located inside the mounting groove (41) is provided between the compression spring (43) and the button (46), and a hook (45) is provided at the end of the tongue plate (44).
8. The magazine of a man-portable air defense missile combat simulation trainer according to claim 1, characterized in that, The rotating assembly (7) includes a first hinge plate (71) disposed on the bottom outer wall of the magazine housing (1) and a second hinge plate (72) fixed on the bottom outer wall of the cover assembly (3). A rotating shaft (73) is provided between the first hinge plate (71) and the second hinge plate (72). A notch (74) for the installation position of the rotating shaft (73) is provided below the tail end of the magazine housing (1).