A mine simulator
Patent Information
- Application Number
- CN202522096205.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-09-29
- Publication Date
- 2026-11-03
- Estimated Expiration
- 2035-09-29
AI Technical Summary
Traditional simulated landmines are susceptible to environmental interference, causing the ignition device to fail in humid or low-temperature environments, and there is a safety hazard of accidental activation during transportation.
The design incorporates an inner shell, propellant grain, ignition assembly, and firing stop mechanism. The ignition assembly ignites the propellant grain, and the firing stop mechanism prevents accidental ignition during transportation. Combined with the stable installation of the outer shell, this enhances safety.
It improves the safety and stability of simulated landmines, reduces the probability of accidental explosions during transportation, and enhances the reliability of training simulations.
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Figure CN224933362U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of military teaching and training equipment, and in particular to a simulated landmine. Background Technology
[0002] In the field of military teaching and training, simulated landmines are important training tools used to simulate the triggering and explosion effects of landmines in real combat environments, so as to improve soldiers' battlefield identification, bomb disposal and tactical response capabilities. Simulated landmines in existing technologies are usually composed of a shell, explosive charge, ignition device and triggering mechanism. Their core requirements are safety and reliability, simulation realism and ease of operation.
[0003] However, traditional ignition methods are easily affected by environmental conditions. Humid environments may cause poor circuit contact, and low temperatures may reduce the sensitivity of the ignition charge. For example, exposed firing pins are easily damaged by impacts. Furthermore, during transportation, storage, or pre-training preparation, if subjected to vibration, accidental activation, or environmental interference, the ignition device may be accidentally activated and ignite the charge, causing the simulated explosion to occur prematurely, posing a safety hazard to operators and training sites. Therefore, these methods have certain shortcomings. Utility Model Content
[0004] The purpose of this invention is to provide a simulated landmine to solve the problems mentioned in the background section.
[0005] To achieve the above objectives, this utility model provides the following technical solution: a simulated landmine, comprising:
[0006] Inner shell;
[0007] A propellant grain, which is fitted inside the inner shell;
[0008] An end cap is installed on the top of the inner housing and is used to shield and protect the propellant column.
[0009] An ignition assembly is disposed on the inner housing and is used to ignite the propellant column;
[0010] A firing stop mechanism is disposed between the ignition assembly and the propellant column;
[0011] The outer casing is threaded onto the outside of the inner casing.
[0012] Preferably, the bottom of the end cap is provided with a circular part, which is slidably sleeved between the inner shell and the propellant column. A limiting sleeve is fixedly connected to the outer wall of the circular part, and a limiting groove is formed in the top of the inner shell. The outer wall of the limiting sleeve is slidably engaged with the inner cavity of the limiting groove.
[0013] Preferably, the ignition assembly includes:
[0014] The bottom of the inner shell has a mounting groove, and the bottom plate is slidably sleeved inside the mounting groove;
[0015] A heating resistor is fixedly installed on the top of the base plate, and the top of the inner wall of the mounting groove is provided with a mounting hole corresponding to the heating resistor.
[0016] The ignition charge is disposed inside the mounting hole and is wrapped around the heating resistor.
[0017] Preferably, the ignition assembly further includes:
[0018] The electrode sheet is fixedly connected to the bottom of the base plate and is electrically connected to the leads of the heating resistor.
[0019] A conductive sheet is fixedly installed inside the outer casing, and the conductive sheet is pressed together with the electrode sheet.
[0020] An arc-shaped pad is fixedly connected to the inner wall of the bearing groove, and the outer wall of the arc-shaped pad is slidably engaged with the base plate.
[0021] Preferably, the generator blocking mechanism includes:
[0022] The partition has a connecting hole on one side of the inner shell, and the outer wall of the partition is slidably inserted into the inner cavity of the connecting hole. The partition is located between the propellant column and the ignition powder.
[0023] The restraint assembly has a mounting groove corresponding to the restraint assembly on one side of the inner shell. The restraint assembly is used to limit and restrain the partition.
[0024] Preferably, the restraint assembly includes:
[0025] A connecting block, the top of which is fixedly connected to a partition, and a notch is provided at the bottom of the connecting block;
[0026] The first magnet and the second magnet are fixedly embedded in the connecting block and the inner shell, respectively, with opposite magnetic poles facing each other.
[0027] Preferably, the restraint assembly includes:
[0028] A connecting frame, the top of which is fixedly connected to the partition;
[0029] A locking rod, the outer wall of which is slidably inserted into the connecting frame, and a locking groove is provided at the bottom of the inner wall of the mounting groove, and the bottom of the outer wall of the locking rod is slidably engaged with the inner cavity of the locking groove;
[0030] A connecting plate, which is fixedly connected to the top of the locking rod.
[0031] Preferably, the restraint assembly further includes:
[0032] A handle, which is fixedly connected to the top of the connecting plate;
[0033] A guide rod is fixedly connected inside the connecting frame, and the outer wall of the guide rod is slidably inserted into the connecting plate.
[0034] A limiting spring is slidably sleeved on the outside of the guide rod, and the limiting spring is located at the top of the connecting plate.
[0035] The technical effects and advantages of this utility model are as follows:
[0036] This invention utilizes the combined use of an inner shell, a propellant charge, an ignition assembly, a detonation blocking mechanism, and an outer shell. The ignition assembly ignites and launches the propellant charge, causing it to propel out and simulate an explosion above the ground, thereby improving the safety of training simulations. Furthermore, the detonation blocking mechanism enhances safety during transportation and reduces the probability of spontaneous explosion of the propellant charge. Attached Figure Description
[0037] Figure 1 This is a schematic diagram of the overall structure of this utility model;
[0038] Figure 2 This is a schematic diagram of the internal structure of the front of this utility model;
[0039] Figure 3 This utility model Figure 2 Enlarged structural diagram at point A in the middle;
[0040] Figure 4 This is a schematic diagram of the internal structure of the inner shell portion in Embodiment 1 of this utility model.
[0041] Figure 5 This is a schematic diagram of the internal structure of the inner shell portion on the side of Embodiment 2 of this utility model.
[0042] In the diagram: 1. Inner shell; 2. Propellant column; 3. End cap; 4. Ignition assembly; 41. Base plate; 42. Heating resistor; 43. Ignition charge; 44. Electrode plate; 45. Conductive plate; 46. Arc pad; 5. Ignition blocking mechanism; 51. Partition plate; 521. Connecting block; 522. First magnet; 523. Second magnet; 524. Connecting frame; 525. Locking rod; 526. Connecting plate; 527. Handle; 528. Guide rod; 529. Limiting spring; 6. Outer shell; 7. Circular part; 8. Limiting sleeve. Detailed Implementation
[0043] 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.
[0044] Example 1: This utility model provides the following... Figures 1-4 The simulated landmine shown includes an inner shell 1, a propellant charge 2, an end cap 3, an ignition assembly 4, a detonation blocking mechanism 5, and an outer shell 6. The propellant charge 2 is fitted inside the inner shell 1, and the end cap 3 is installed on the top of the inner shell 1. The end cap 3 is used to shield and protect the propellant charge 2. The propellant charge 2 is composed of a shell, gunpowder, sawdust, black powder, and a fuse. The gunpowder, sawdust, black powder, and fuse are arranged from top to bottom inside the shell. Figure 2 As shown, the fuse corresponds to the ignition assembly 4. The propellant charge 2 operates on the same principle as fireworks. When the fuse is lit, it ignites the black powder. The ignition of the black powder gives the casing a thrust, causing the propellant charge 2 to eject from the inner casing 1. The black powder ignites the gunpowder through sawdust, causing the propellant charge 2 to explode. This is existing technology and will not be discussed in detail here. This simulates a landmine explosion. The ignition assembly 4 is located on the inner casing 1 and is used to ignite the propellant charge 2. The detonation blocking mechanism 5 is located between the ignition assembly 4 and the propellant charge 2. During transportation and storage, the detonation blocking mechanism 5 can prevent the ignition assembly 4 from igniting the propellant charge 2, thereby improving the safety of the propellant charge 2 during transportation and storage. The outer casing 6 is threaded onto the outside of the inner casing 1. The outer casing 6 can ensure the stability of the installation of the ignition assembly 4 and the detonation blocking mechanism 5.
[0045] Specifically, the bottom of the end cap 3 is provided with a circular ring 7, which is slidably sleeved between the inner shell 1 and the propellant charge 2. The outer wall of the circular ring 7 is fixedly connected to a limiting sleeve 8. A limiting groove is opened at the top inside the inner shell 1. The outer wall of the limiting sleeve 8 is slidably engaged with the inner cavity of the limiting groove. The limiting sleeve 8 can improve the stability of the connection between the circular ring 7 and the inner shell 1. Furthermore, the friction between the limiting sleeve 8 and the inner shell 1 is greater than the weight of the propellant charge 2 and much less than the lifting force when the propellant charge 2 is launched, thereby improving the stability of the end cap 3 in shielding and protecting the propellant charge 2.
[0046] Furthermore, the ignition assembly 4 includes a base plate 41, a heating resistor 42, and an ignition charge 43. The bottom of the inner housing 1 is provided with a mounting groove, and the base plate 41 is slidably fitted into the inside of the mounting groove. The heating resistor 42 is fixedly installed on the top of the base plate 41. The top of the inner wall of the mounting groove is provided with a mounting hole corresponding to the heating resistor 42. The ignition charge 43 is placed inside the mounting hole and is wrapped around the outside of the heating resistor 42. When the heating resistor 42 is energized or generates heat, it ignites the ignition charge 43, which in turn ignites the propellant column 2.
[0047] Furthermore, the ignition assembly 4 also includes an electrode plate 44, a conductive plate 45, and an arc-shaped pad 46. The electrode plate 44 is fixedly connected to the bottom of the base plate 41 and is electrically connected to the pins of the heating resistor 42. The conductive plate 45 is fixedly installed inside the outer casing 6. The conductive plate 45 and the electrode plate 44 are pressed together and adhered to each other. The two electrode plates 44 are respectively in the shape of a ring and a disk. So when the outer casing 6 and the inner casing 1 are rotated together, the two conductive plates 45 can contact the two electrode plates 44 individually, thereby avoiding short circuits or open circuits. The arc-shaped pad 46 is fixedly connected to the inner wall of the bearing groove. The outer wall of the arc-shaped pad 46 is slidably engaged with the base plate 41. The arc-shaped pad 46 can improve the stability of the base plate 41 installed inside the bearing groove.
[0048] In particular, the detonation mechanism 5 includes a partition 51 and a restraint assembly. A connection hole is provided on one side of the inner housing 1. The outer wall of the partition 51 is slidably inserted into the inner cavity of the connection hole. The partition 51 is located between the propellant column 2 and the ignition powder 43. The partition 51 is made of a material with good heat insulation performance to reduce the chance of the ignition powder 43 accidentally igniting the propellant column 2. When the propellant column 2 is in use, the outer housing 6 needs to be disassembled and the partition 51 needs to be pulled out. A mounting groove corresponding to the restraint assembly is provided on one side of the inner housing 1. The restraint assembly is used to limit and restrain the partition 51.
[0049] Furthermore, the restraint assembly includes a connecting block 521, a first magnet 522, and a second magnet 523. The top of the connecting block 521 is fixedly connected to the partition 51, and a notch is provided at the bottom of the connecting block 521. The first magnet 522 and the second magnet 523 are respectively fixedly embedded in the connecting block 521 and the inner shell 1. The opposite magnetic poles of the first magnet 522 and the second magnet 523 are opposite to each other. The first magnet 522 and the second magnet 523 can limit the position of the connecting block 521, thereby improving the stability of the partition 51 installation. Moreover, the connecting block 521 and the partition 51 can be directly pulled out using the notch at the bottom of the connecting block 521.
[0050] Example 2: Unlike Example 1, as follows... Figure 5As shown, the restraint assembly includes a connecting frame 524, a locking rod 525, a connecting plate 526, a handle 527, a guide rod 528, and a limiting spring 529. The top of the connecting frame 524 is fixedly connected to the partition plate 51. The outer wall of the locking rod 525 is slidably inserted into the connecting frame 524. A locking groove is provided at the bottom of the inner wall of the mounting groove. The bottom of the outer wall of the locking rod 525 is slidably engaged with the inner cavity of the locking groove. The connecting plate 526 is fixedly connected to the top of the locking rod 525. The handle 527 is fixedly connected to the top of the connecting plate 526. The handle 527 can be used to move the rod. The connecting plate 526 and the locking rod 525 rise, thereby separating the locking rod 525 from the inner housing 1, and thus pulling out the partition 51. The guide rod 528 is fixedly connected to the inside of the connecting frame 524. The outer wall of the guide rod 528 is slidably inserted into the connecting plate 526. The limiting spring 529 is slidably sleeved on the outside of the guide rod 528. The limiting spring 529 is located at the top of the connecting plate 526. Under the action of the limiting spring 529, the connecting plate 526 can drive the locking rod 525 to be in a stable state and locked with the inner housing 1, thereby ensuring the stability of the partition 51 installation.
[0051] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.
Claims
1. A simulated landmine, characterized in that, include: Inner shell (1); Propellant column (2), which is fitted inside the inner shell (1); End cap (3), the end cap (3) is installed on the top of the inner shell (1), the end cap (3) is used to shield and protect the propellant column (2); Ignition assembly (4), which is disposed on the inner shell (1) and is used to ignite the propellant column (2); A firing blocking mechanism (5) is disposed between the ignition assembly (4) and the propellant column (2); The outer shell (6) is threaded onto the outside of the inner shell (1).
2. The simulated landmine according to claim 1, characterized in that, The bottom of the end cap (3) is provided with a ring part (7), which is slidably sleeved between the inner shell (1) and the propellant column (2). The outer wall of the ring part (7) is fixedly connected with a limiting sleeve (8). A limiting groove is opened at the top inside the inner shell (1), and the outer wall of the limiting sleeve (8) is slidably engaged with the inner cavity of the limiting groove.
3. The simulated landmine according to claim 1, characterized in that, The ignition assembly (4) includes: The bottom plate (41) has an installation groove at the bottom of the inner shell (1), and the bottom plate (41) is slidably sleeved inside the installation groove; Heating resistor (42) is fixedly installed on the top of the base plate (41), and the top of the inner wall of the mounting groove is provided with mounting holes corresponding to the heating resistor (42); Ignition charge (43) is disposed inside the mounting hole and is wrapped around the heating resistor (42).
4. The simulated landmine according to claim 2, characterized in that, The ignition assembly (4) also includes: Electrode sheet (44), the electrode sheet (44) is fixedly connected to the bottom of the base plate (41), and the electrode sheet (44) is electrically connected to the pin of the heating resistor (42); A conductive sheet (45) is fixedly installed inside the outer shell (6), and the conductive sheet (45) is pressed together with the electrode sheet (44); The arc pad (46) is fixedly connected to the inner wall of the bearing groove, and the outer wall of the arc pad (46) is slidably engaged with the bottom plate (41).
5. The simulated landmine according to claim 4, characterized in that, The signal blocking mechanism (5) includes: The partition (51) has a connecting hole on one side of the inner shell (1). The outer wall of the partition (51) is slidably inserted into the inner cavity of the connecting hole. The partition (51) is located between the propellant column (2) and the ignition powder (43). The restraint assembly has a mounting groove corresponding to the restraint assembly on one side of the inner shell (1). The restraint assembly is used to limit and restrain the partition (51).
6. The simulated landmine according to claim 5, characterized in that, The restraint component includes: A connecting block (521) is fixedly connected to a partition plate (51) at its top and has a notch at its bottom. The first magnet (522) and the second magnet (523) are respectively fixedly embedded in the connecting block (521) and the inner shell (1), and the opposite magnetic poles of the first magnet (522) and the second magnet (523) are opposite to each other.
7. The simulated landmine according to claim 5, characterized in that, The restraint component includes: A connecting frame (524), the top of which is fixedly connected to a partition (51); Locking rod (525), the outer wall of the locking rod (525) is slidably inserted into the connecting frame (524), the bottom of the inner wall of the mounting groove is provided with a locking groove, and the bottom of the outer wall of the locking rod (525) is slidably engaged with the inner cavity of the locking groove; A connecting plate (526) is fixedly connected to the top of the locking rod (525).
8. The simulated landmine according to claim 7, characterized in that, The restraint assembly also includes: A handle (527) is fixedly connected to the top of a connecting plate (526); Guide rod (528), the guide rod (528) is fixedly connected to the inside of the connecting frame (524), and the outer wall of the guide rod (528) is slidably inserted and sleeved with the connecting plate (526); A limiting spring (529) is slidably sleeved on the outside of the guide rod (528) and is located on the top of the connecting plate (526).
