Individual portable air defense missile actual combat simulation trainer launching mechanism

Abstract

The utility model relates to the technical field of model missiles, and discloses an individual portable air defense missile actual combat simulation training device launching mechanism which comprises a device body, a launching mechanism body is arranged on one side of the device body, an anti-skid mechanism is arranged outside the device body, a replacement mechanism is arranged inside the device body, the launching mechanism body comprises a shell, and the shell is provided with an anti-skid mechanism. The shell is arranged on one side of the device body, and a trigger is arranged on one side of the shell. According to the single-soldier portable air-defense missile actual combat simulation training device launching mechanism, the launching mechanism is arranged, in the working process of the single-soldier portable air-defense missile actual combat simulation training device launching mechanism, in order to prevent a trigger from being touched by mistake, an electronic fuse is arranged below the launching mechanism, and the launching mechanism can be powered on to work only when the electronic fuse is turned on; therefore, sufficient safety and reliability are provided. In the launching mechanism, a socket, a large and small target switch, a rear-end collision meeting and attacking switch and a safety switch are consistent with real devices and can replace the real devices to be used for daily training.

Description

Technical Field

[0001] This utility model relates to the field of model missile technology, specifically a launch mechanism for a man-portable air defense missile combat simulation training device. Background Technology

[0002] A model missile is a prototype missile used to simulate the shape and specific functions of a missile. Model missiles are generally divided into two categories: scale model missiles and full-size model missiles. Scale model missiles are often used to simulate the aerodynamic shape of a missile and for wind tunnel testing during missile development to obtain aerodynamic data. There are also cases where launch propulsion devices are installed on scale model missiles to simulate launches and explore the feasibility of launch schemes.

[0003] A search revealed an existing patent (publication number: CN203981012U) that discloses a launching mechanism. This mechanism comprises a main body with an open-end launching channel and a closed-end air intake channel. The launching channel includes a feed inlet, a narrow end, and a wide end. A rod-shaped piston is housed within the launching channel. The rear end of the rod-shaped piston is engaged with the narrow end of the corresponding launching channel by at least one O-ring. A gas storage space is located in front of the wide end of the launching channel. A rear air intake channel communicates with the air intake channel at the narrow end of the launching channel. The air intake channel has an air inlet to deliver the introduced gas to the gas storage space. The main body includes a switch. The rearward pushing area of ​​the rod-shaped piston at the front air intake channel is greater than the forward pushing area at the rear air intake channel. The advantages of this invention are: a more streamlined structure compared to existing launching mechanisms, better meeting practical needs; and the elimination of the need for reloading and pullback after the launched object is fired, making it more convenient to use and achieving rapid degassing firing.

[0004] However, current training methods for single-handed operation of striking weapons cannot solve the problem of conditioned reflexes in shooters through live-fire training. This results in low first-shot hit rates for high-value ammunition, which in turn creates negative conditioned reflexes and fear of the shooter, forming a vicious cycle and a "deadlock." Simulated training should be gradual and scientifically address the adverse reactions caused by conditioned reflexes in shooters. Only with appropriate and targeted training equipment can the negative consequences of conditioned reflexes be overcome in a shorter period of time, rapidly improving the adaptability of the shooter and equipment, increasing hit rates, and enhancing combat effectiveness.

[0005] Therefore, a launch mechanism for a man-portable air defense missile combat simulation training device is proposed to address the above problems. Utility Model Content

[0006] (a) Technical problems to be solved

[0007] To address the shortcomings of existing technologies, this utility model provides a launch mechanism for a man-portable air defense missile combat simulation training device. This solves the problem mentioned in the background that current training for single-handed, single-soldier combat weapons cannot resolve the shooter's conditioned reflex issues through live-fire training. This results in low first-shot hit rates for high-value ammunition, and subsequently, negative conditioned reflexes and fear of the shooter, creating a vicious cycle and a "deadlock." Simulation training should be gradual and scientifically address the adverse reactions caused by conditioned reflexes. Appropriate and targeted training equipment is essential to overcome the negative consequences of conditioned reflexes in a short period, rapidly improving the adaptability of the operator and equipment, increasing hit rates, and enhancing combat effectiveness.

[0008] (II) Technical Solution

[0009] To achieve the above objectives, this utility model provides the following technical solution: a man-portable air defense missile combat simulation training device launching mechanism, including a body, a launching mechanism provided on one side of the body, an anti-slip mechanism provided on the outside of the body, and a replacement mechanism provided inside the body;

[0010] The launching mechanism includes a housing, which is disposed on one side of the device body. A trigger is disposed on one side of the housing. A rechargeable lithium battery is disposed inside the housing. An electronic fuse is disposed on one side of the rechargeable lithium battery. A lithium battery charging interface is disposed on one side of the electronic fuse. A socket is provided on the surface of the housing. An attack / rear-end switch and a target size switch are disposed inside the housing. A safety switch is disposed on one side of the housing.

[0011] As a preferred embodiment, the anti-slip mechanism includes a hinge, which is disposed on the outer wall surface of the device, and a fixing plate is provided on one side of the hinge.

[0012] As a preferred embodiment, a spring a is provided at one end of the fixing plate, the spring a is provided on the outer wall surface of the device body, and a fixing bolt is provided at the other end of the fixing plate.

[0013] As a preferred embodiment, a protective pad is provided on one side of the fixing bolt, and an anti-slip pad is provided on one side of the protective pad, with the anti-slip pad being disposed on the outer wall surface of the device.

[0014] As a preferred embodiment, the replacement mechanism includes a slide groove, which is formed on the inner wall surface of the vessel, and a slider is provided on the inner side of the slide groove.

[0015] As a preferred embodiment, the surface of the slider is provided with a magazine, and the surface of the magazine is provided with a spring b.

[0016] As a preferred embodiment, a limiting rod is provided on one side of the spring b, and a limiting groove is provided on one side of the limiting rod, with the limiting groove being formed on the inner wall surface of the device.

[0017] This utility model provides a launch mechanism for a man-portable air defense missile combat simulation training device. It has the following beneficial effects:

[0018] (1) The launch mechanism of this man-portable air defense missile combat simulation trainer is equipped with an electronic safety device at the bottom of the launch mechanism to prevent accidental triggering during operation. The launch mechanism will only be powered on and operated when the electronic safety device is opened, thus providing sufficient safety and reliability. In the launch mechanism, the socket, target size switch, attack and pursuit switch, and safety switch are consistent with the actual equipment and can replace the actual equipment for daily training. Attached Figure Description

[0019] Figure 1 This is a side view of the appearance structure of this utility model;

[0020] Figure 2 This is a schematic diagram of the launching mechanism structure of this utility model;

[0021] Figure 3 This is a schematic diagram of the anti-slip mechanism of this utility model;

[0022] Figure 4 This is a schematic diagram of the replacement mechanism of this utility model.

[0023] The components are as follows: 1. Body; 2. Launching mechanism; 201. Outer shell; 202. Trigger; 203. Rechargeable lithium battery; 204. Electronic fuse; 205. Lithium battery charging interface; 206. Socket; 207. Attack and rear-end collision switch; 208. Large and small target switch; 209. Safety switch; 3. Anti-slip mechanism; 301. Hinge; 302. Fixing plate; 303. Spring a; 304. Fixing bolt; 305. Protective pad; 306. Anti-slip pad; 4. Replacement mechanism; 401. Slide groove; 402. Slider; 403. Magazine; 404. Spring b; 405. Limiting rod; 406. Limiting groove. Detailed Implementation

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] Please see Figure 1 and Figure 4This utility model provides a technical solution: a man-portable air defense missile combat simulation training device launching mechanism, including a body 1, a launching mechanism 2 provided on one side of the body 1, an anti-slip mechanism 3 provided on the outside of the body 1, and a replacement mechanism 4 provided inside the body 1. The replacement mechanism 4 includes a slide groove 401, which is formed on the inner wall surface of the body 1. A slider 402 is provided on the inner side of the slide groove 401. A magazine 403 is provided on the surface of the slider 402. A spring b 404 is provided on the surface of the magazine 403. A limit rod 405 is provided on one side of the spring b 404, and a limit groove 406 is provided on one side of the limit rod 405. The limit groove 406 is formed on the inner wall surface of the body 1.

[0026] Among them: During the operation of the man-portable air defense missile combat simulation training device launch mechanism, the replacement mechanism 4 is provided. Under the action of the slide 401 and the slider 402, the bullets inside the magazine 403 can be easily replaced. Under the action of the spring b404, the spring b404 drives the limiting rod 405 into the inner side of the limiting groove 406 to fix the magazine 403.

[0027] Please see Figure 2 A man-portable air defense missile combat simulation training device launch mechanism 2 includes a housing 201, which is located on one side of the device body 1. A trigger 202 is located on one side of the housing 201. A rechargeable lithium battery 203 is located inside the housing 201. An electronic fuse 204 is located on one side of the rechargeable lithium battery 203. A lithium battery charging interface 205 is located on one side of the electronic fuse 204. A socket 206 is opened on the surface of the housing 201. An attack and pursuit switch 207 is located inside the housing 201. A large and small target switch 208 is located inside the housing 201. A safety switch 209 is located on one side of the housing 201.

[0028] Specifically: During the operation of the man-portable air defense missile combat simulation training device launch mechanism, in order to prevent accidental triggering 202, an electronic safety 204 is installed below the launch mechanism 2. Only when the electronic safety 204 is opened will the launch mechanism 2 be powered on to work, so as to provide sufficient safety and reliability. In the launch mechanism 2, the socket 206, the large and small target switch 208, the attack and pursuit switch 207, and the safety switch 209 are the same as those in the actual equipment and can replace the actual equipment for daily training.

[0029] Please see Figure 3A man-portable air defense missile combat simulation training device launch mechanism includes an anti-slip mechanism 3 comprising a hinge 301, which is disposed on the outer wall surface of the device body 1. A fixing plate 302 is disposed on one side of the hinge 301. A spring a303 is disposed on one end of the fixing plate 302, which is disposed on the outer wall surface of the device body 1. A fixing bolt 304 is disposed on the other end of the fixing plate 302. A protective pad 305 is disposed on one side of the fixing bolt 304. An anti-slip pad 306 is disposed on one side of the protective pad 305, which is disposed on the outer wall surface of the device body 1.

[0030] In the operation of the man-portable air defense missile combat simulation training device, an anti-slip mechanism 3 is provided. Under the action of the anti-slip pad 306, the anti-slip pad 306 can be used to prevent the device body 1 from slipping. Under the action of the hinge 301, the hinge 301 drives the fixing plate 302 to rotate. At the same time, under the action of the spring a303, one end of the fixing plate 302 is driven to extend and retract to reset. Then, the fixing plate 302 can be used to install the anti-slip pad 306.

[0031] The working principle of this utility model is as follows: During the operation of the launch mechanism of the man-portable air defense missile combat simulation training device, in order to prevent accidental triggering 202, an electronic safety 204 is installed below the launch mechanism 2. Only when the electronic safety 204 is opened will the launch mechanism 2 be powered on to operate, providing sufficient safety and reliability. In the launch mechanism 2, the socket 206, target size switch 208, attack and pursuit switch 207, and safety switch 209 are consistent with the actual device and can replace the actual device for daily training. Secondly, by setting up an anti-slip mechanism 3, under the action of the anti-slip pad 306, the anti-slip pad 306 can be used to make the anti-slip pad 306 work. The 6-pair mechanism provides an anti-slip effect for the body 1. Under the action of the hinge 301, the hinge 301 drives the fixing plate 302 to rotate. At the same time, under the action of the spring a303, one end of the fixing plate 302 is driven to extend and return to its original position. The anti-slip pad 306 can then be installed using the fixing plate 302. Finally, through the provision of the replacement mechanism 4, the bullets inside the magazine 403 can be easily replaced under the action of the slide groove 401 and the slider 402. Under the action of the spring b404, the spring b404 drives the limiting rod 405 into the inner side of the limiting groove 406 to fix the magazine 403.

[0032] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A man-portable air defense missile combat simulation training device launching mechanism, comprising a body (1), characterized in that: The device (1) is provided with a launching mechanism (2) on one side, an anti-slip mechanism (3) is provided on the outside of the device (1), and a replacement mechanism (4) is provided inside the device (1). The launching mechanism (2) includes a housing (201), which is located on one side of the device body (1). A trigger (202) is located on one side of the housing (201). A rechargeable lithium battery (203) is located inside the housing (201). An electronic fuse (204) is located on one side of the rechargeable lithium battery (203). A lithium battery charging interface (205) is located on one side of the electronic fuse (204). A socket (206) is provided on the surface of the housing (201). An attack and rear-end collision switch (207) is located inside the housing (201). A large and small target switch (208) is located inside the housing (201). A safety switch (209) is located on one side of the housing (201).

2. The launching mechanism of a man-portable air defense missile combat simulation training device according to claim 1, characterized in that: The anti-slip mechanism (3) includes a hinge (301), which is disposed on the outer wall surface of the body (1), and a fixing plate (302) is provided on one side of the hinge (301).

3. The launching mechanism of a man-portable air defense missile combat simulation training device according to claim 2, characterized in that: A spring a (303) is provided at one end of the fixing plate (302), the spring a (303) is provided on the outer wall surface of the body (1), and a fixing bolt (304) is provided at the other end of the fixing plate (302).

4. The launching mechanism of a man-portable air defense missile combat simulation trainer according to claim 3, characterized in that: A protective pad (305) is provided on one side of the fixing bolt (304), and an anti-slip pad (306) is provided on one side of the protective pad (305). The anti-slip pad (306) is provided on the outer wall surface of the body (1).

5. The launching mechanism of a man-portable air defense missile combat simulation training device according to claim 1, characterized in that: The replacement mechanism (4) includes a slide (401), which is formed on the inner wall surface of the body (1), and a slider (402) is provided on the inner side of the slide (401).

6. The launching mechanism of a man-portable air defense missile combat simulation trainer according to claim 5, characterized in that: The surface of the slider (402) is provided with a magazine (403), and the surface of the magazine (403) is provided with a spring b (404).

7. The launching mechanism of a man-portable air defense missile combat simulation trainer according to claim 6, characterized in that: A limiting rod (405) is provided on one side of the spring b (404), and a limiting groove (406) is provided on one side of the limiting rod (405). The limiting groove (406) is opened on the inner wall surface of the body (1).

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