Missile support for simulation training

Abstract

The utility model belongs to military training equipment technical field, concretely is a kind of missile support for simulation training convenient to install, including bottom plate, the bottom plate is provided with support mechanism, the support mechanism includes: adjusting assembly, including the rotating component connection of a group of electric push rod in bottom plate top by setting, the telescopic end of electric push rod is fixedly connected with fixed block, the fixed block is rotatably connected with concave block on through first rotating shaft, a group The concave block top is fixedly connected with rectangular plate, and the rectangular plate top is fixedly connected with the supporting plate;Positioning assembly is set on rectangular plate and is used to position support missile, to solve the angle of traditional support cannot be adjusted, can seriously drag slow training preparation, difficult to switch scene quickly;There is no accurate positioning, naked eye error is big, and the training data is distorted, affect effect evaluation, and cannot adapt to multiple terrain training scene, limit training content, difficult to meet modern simulation training needs problem.

Description

Technical Field

[0001] This utility model belongs to the field of military training equipment technology, specifically a missile support for simulation training that is easy to install. Background Technology

[0002] Simulation training, also known as simulation, involves modeling military scenarios and then using simulation technology to simulate battle situations, strategies, and tactics. This method applies the perspective of systems theory and utilizes various modeling methods such as mathematical modeling. In practice, simulation training plays a significant guiding role in military command. A missile is an aircraft that carries a warhead, is propelled by its own power plant, and is guided and controlled by a guidance system to reach and destroy its target.

[0003] In existing technologies, the angle of traditional supports cannot be adjusted, which will severely slow down training preparation and make it difficult to quickly switch scenes; without precise positioning, the error of visual judgment is large, resulting in distorted training data, affecting the evaluation of the effect, and it cannot be adapted to training scenarios with multiple terrains, limiting training content and making it difficult to meet the needs of modern simulation training.

[0004] Therefore, this utility model provides a missile support for simulation training that is easy to install. Utility Model Content

[0005] To address the shortcomings of existing technologies and solve the problems of traditional support angles not being adjustable, which severely slows down training preparation and makes it difficult to quickly switch scenes; lack of precise positioning, large errors in visual judgment leading to distorted training data, affecting effect evaluation, and inability to adapt to multi-terrain training scenarios, limiting training content and failing to meet the needs of modern simulation training.

[0006] The technical solution adopted by this utility model to solve its technical problem is as follows: The missile support for simulation training that is easy to install according to this utility model includes a base plate, the base plate is provided with a support mechanism, the support mechanism includes: an adjustment component, including a set of electric push rods connected to the top of the base plate through a set rotating component, the telescopic end of the electric push rods is fixedly connected to a fixing block, the fixing block is rotatably connected to a concave block through a first rotating shaft, and a rectangular plate is fixedly connected to the top of the set of concave blocks; a positioning component, set on the rectangular plate for positioning and supporting the missile.

[0007] Preferably, the rotating assembly includes an annular groove on the top of the base plate, a rotating ring rotatably connected in the annular groove, a gear plate fixedly connected to the top of the rotating ring, and the base end of a set of electric actuators fixedly connected to the top of the gear plate.

[0008] Preferably, a first concave frame is fixedly connected to the top of the base plate, a first motor is fixedly connected to the bottom of the first concave frame, a first drive rod is provided at the output end of the first motor, a gear is fixedly connected to the bottom of the first drive rod, and the gear meshes with the gear plate.

[0009] Preferably, the positioning component includes a set of sliding slots opened at the top of the rectangular plate, a sliding block is slidably connected in the sliding slots, and a positioning block is fixedly connected to the top of the sliding block.

[0010] Preferably, a second concave frame is fixedly connected to the bottom of the rectangular plate, a second motor is fixedly connected to the top of the second concave frame in the horizontal direction, a second drive rod is provided at the output end of the second motor, and an adjustment rod is fixedly connected to the top of the second drive rod.

[0011] Preferably, both ends of the adjusting rod are rotatably connected to connecting rods via a second rotating shaft, and a concave strip is rotatably connected to the connecting rod via a third rotating shaft. The concave strip is fixed to the bottom of a pair of sliding blocks.

[0012] The beneficial effects of this utility model are as follows: 1. The missile support for simulation training described in this utility model is easy to install. By controlling the lifting and lowering of a set of electric push rods, it can adapt to different angle adjustments. In conjunction with the rotation of the gear plate, it solves the problems of existing technologies, such as the inability to adjust the angle of traditional supports, which seriously slows down training preparation and makes it difficult to quickly switch scenes; lack of precise positioning, large errors in visual judgment, resulting in distorted training data, affecting effect evaluation, and inability to adapt to multi-terrain training scenarios, limiting training content and failing to meet the needs of modern simulation training.

[0013] 2. The missile support for simulation training described in this utility model, which is easy to install, achieves synchronous lateral movement of the positioning block through a positioning component. The sliding block slides very smoothly within the sliding groove without any jamming. The positioning block and the outer wall of the missile have a high degree of fit, effectively preventing lateral displacement of the missile due to vibration or collision during training, ensuring the missile's positional stability during training. Furthermore, the clamping force of the positioning block can be precisely adjusted by controlling the rotation time of the second motor; the longer the motor rotates forward, the greater the clamping force of the positioning block. This allows it to adapt to simulation training missiles of different diameters, such as small training missiles and medium-sized simulation missiles, improving the support's versatility and eliminating the need for separate supports for different missile models. Attached Figure Description

[0014] The present invention will be further described below with reference to the accompanying drawings.

[0015] Figure 1 This is a perspective view of the present invention; Figure 2This is a schematic diagram of the second motor in this utility model; Figure 3 This is a schematic diagram of the rotating ring in this utility model; Figure 4 This is a schematic diagram of the concave strip in this utility model; In the diagram: 1. Base plate; 2. Electric actuator; 3. Fixing block; 4. Concave block; 5. Rectangular plate; 6. Annular groove; 7. Rotating ring; 8. Gear disc; 9. First concave frame; 10. First motor; 11. First drive rod; 12. Gear; 13. Sliding through groove; 14. Sliding block; 15. Positioning block; 16. Second concave frame; 17. Second motor; 18. Second drive rod; 19. Adjusting rod; 20. Connecting rod; 21. Concave strip. Detailed Implementation

[0016] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.

[0017] like Figures 1 to 4 As shown, an easy-to-install missile support for simulation training according to an embodiment of the present invention includes a base plate 1, which serves as the basic load-bearing component of the entire support and is used to stably place it on the ground or training platform. The base plate 1 is provided with a support mechanism, which includes: an adjustment component, including a set of electric push rods 2 connected to the top of the base plate 1 through a rotating component to adjust the missile pitch angle; a fixing block 3 is fixedly connected to the telescopic end of the electric push rod 2; a concave block 4 is rotatably connected to the fixing block 3 through a first rotating shaft; the fixing block 3 is connected to a rectangular plate 5 to transmit the force of the electric push rod 2 to the rectangular plate 5; and a positioning component, which is provided on the rectangular plate 5 for positioning and supporting the missile.

[0018] The rotating assembly includes an annular groove 6 on the top of the base plate 1, which provides a rotating track for the rotating ring 7. The rotating ring 7 is rotatably connected in the annular groove 6, and a gear plate 8 is fixedly connected to the top of the rotating ring 7. The base end of a set of electric push rods 2 is fixedly connected to the top of the gear plate 8.

[0019] A first concave frame 9 is fixedly connected to the top of the base plate 1. A first motor 10, which is a stepper motor, is fixedly connected to the bottom of the first concave frame 9. The output end of the first motor 10 is provided with a first drive rod 11. A gear 12 is fixedly connected to the bottom of the first drive rod 11. The gear 12 meshes with the gear plate 8.

[0020] During operation, by controlling the lifting and lowering of a set of electric actuators 2, different angles can be adjusted. In conjunction with the rotation of the gear plate 8, this solves the problems in existing technologies, such as the inability to adjust the angle of traditional supports, which seriously slows down training preparation and makes it difficult to quickly switch scenes; the lack of precise positioning and large errors in visual judgment lead to distorted training data, affecting effect evaluation; and the inability to adapt to multi-terrain training scenarios, limiting training content and failing to meet the needs of modern simulation training.

[0021] The positioning component includes a set of sliding slots 13 opened at the top of the rectangular plate 5, which provide a sliding track for the sliding block 14. The sliding block 14 is slidably connected in the sliding slots 13, and a positioning block 15 is fixed to the top of the sliding block 14, which directly contacts the missile. The missile is clamped by the relative movement of the two positioning blocks 15.

[0022] A second concave frame 16 is fixed to the bottom of the rectangular plate 5. A second motor 17 is fixed to the top of the second concave frame 16 in the horizontal direction. As the power source of the positioning component, it is a stepper motor. The output end of the second motor 17 is provided with a second drive rod 18. An adjustment rod 19 is fixed to the top of the second drive rod 18.

[0023] Both ends of the adjusting rod 19 are rotatably connected to the connecting rod 20 via the second rotating shaft. The connecting rod 20 is rotatably connected to the concave strip 21 via the third rotating shaft. The concave strip 21 is fixed to the bottom of a pair of sliding blocks 14.

[0024] During operation, the positioning block 15 moves synchronously laterally via the positioning component. The sliding block 14 slides smoothly within the sliding groove 13 without any jamming. The positioning block 15 maintains a high degree of contact with the missile's outer wall, effectively preventing lateral displacement of the missile due to vibration or collision during training and ensuring positional stability. Furthermore, the clamping force of the positioning block 15 can be precisely adjusted by controlling the rotation time of the second motor 17; the longer the motor rotates forward, the greater the clamping force of the positioning block 15. This allows it to accommodate simulated training missiles of different diameters, such as small and medium-sized missiles, improving the versatility of the support and eliminating the need for separate supports for different missile models.

[0025] Working Principle: The base plate 1 of the support is fixed at a designated position in the simulated training area, such as the ground or a training platform. At this time, the support mechanism is in an initial standby state. The electric push rod 2 in the adjustment component maintains its default initial length, the gear disk 8 and gear 12 of the rotating component are engaged and stationary, and the sliding block 14 of the positioning component is located at both ends of the sliding groove 13, leaving enough space for the missile to be placed later. The rectangular plate 5 also remains horizontal, providing a stable base bearing surface for missile placement. The missile for simulated training is placed smoothly on top of the rectangular plate 5. The rectangular plate 5 is connected together by the concave block 4, the fixing block 3, and the electric push rod 2, and can then move together with the adjustment component. At this time, the missile only relies on the rectangular plate 5 for initial bearing, waiting for the positioning component to further fix it to prevent the missile from shifting during subsequent adjustments.

[0026] After the missile is positioned, the second motor 17 of the positioning assembly is activated. The second motor 17 is mounted on the horizontal top of the second concave bracket 16 at the bottom of the rectangular plate 5. The motor's output drives the second drive rod 18 to rotate. Since the second drive rod 18 and the adjusting rod 19 are fixedly connected, the adjusting rod 19 rotates around its axis along with the second drive rod 18. Both ends of the adjusting rod 19 are connected to connecting rods 20 via a second rotating shaft. When the adjusting rod 19 rotates, the connecting rods 20 at both ends swing synchronously towards the center or sides according to the forward and reverse rotation of the second motor 17. The end of the connecting rod 20 furthest from the adjusting rod 19 is connected to the concave strip 21 via a third rotating shaft. The concave strip 21 is fixed to the bottom of the sliding block 14, so the swinging of the connecting rod 20 is converted into the lateral sliding of the sliding block 14 within the sliding groove 13. When the second motor 17 rotates forward, the adjusting rod 19 drives the connecting rod 20 to swing towards the missile. The sliding block 14 moves towards the center along the sliding groove 13 until the positioning block 15 at the top of the sliding block 14 is tightly fitted against the outer wall of the missile. This completes the lateral positioning support for the missile, preventing lateral deviation during training. If it is necessary to adjust the horizontal angle of the missile, such as simulating the missile turning to aim at different targets, the first motor 10 is activated. The first motor 10 is installed at the bottom of the first concave frame 9 on the top of the base plate 1. The output end of the motor drives the first drive rod 11 to rotate. The gear 12 at the bottom of the first drive rod 11 meshes with the gear disk 8 of the rotating assembly. The gear disk 8 rotates in the annular groove 6 of the base plate 1 through the rotating ring 7. Therefore, the rotation of the gear 12 will drive the gear disk 8 to rotate around the axis of the annular groove 6. The top of the gear disk 8 is fixedly connected to the base end of the electric push rod 2. When the gear disk 8 rotates, it will drive the electric push rod 2, the rectangular plate 5, and the missile to rotate horizontally synchronously until the target direction is adjusted. Then, the first motor 10 is turned off. The meshing structure of gear 12 and toothed disc 8 can maintain the missile's horizontal position stability and avoid angular deviation.

[0027] The terms "front," "back," "left," "right," "top," and "bottom" all refer to the figures in the accompanying drawings. Figure 1 Based on the perspective of the observer, the side of the device facing the observer is defined as the front, the left side of the observer is defined as the left, and so on.

[0028] In the description of this utility model, it should be understood that the terms "center", "longitudinal", "lateral", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limiting the scope of protection of this utility model.

[0029] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A missile support for simulation training that is easy to install, comprising a base plate (1), characterized in that: The base plate (1) is provided with a support mechanism, the support mechanism comprising: The adjustment assembly includes a set of electric push rods (2) connected to the top of the base plate (1) via a rotating assembly. The telescopic end of the electric push rod (2) is fixedly connected to a fixing block (3). A concave block (4) is rotatably connected to the fixing block (3) via a first rotating shaft. A rectangular plate (5) is fixedly connected to the top of the set of concave blocks (4). The positioning component is set on the rectangular plate (5) for positioning and supporting the missile.

2. The missile support for simulation training that is easy to install according to claim 1, characterized in that: The rotating assembly includes an annular groove (6) opened on the top of the base plate (1), a rotating ring (7) is rotatably connected in the annular groove (6), a gear plate (8) is fixedly connected to the top of the rotating ring (7), and the base end of a set of electric push rods (2) is fixedly connected to the top of the gear plate (8).

3. The missile support for simulation training that is easy to install according to claim 2, characterized in that: The top of the base plate (1) is fixedly connected to a first concave frame (9), and the bottom of the first concave frame (9) is fixedly connected to a first motor (10). The output end of the first motor (10) is provided with a first drive rod (11), and the bottom of the first drive rod (11) is fixedly connected to a gear (12). The gear (12) meshes with the gear plate (8).

4. The missile support for simulation training that is easy to install according to claim 1, characterized in that: The positioning component includes a set of sliding slots (13) opened on the top of the rectangular plate (5), a sliding block (14) is slidably connected in the sliding slots (13), and a positioning block (15) is fixedly connected to the top of the sliding block (14).

5. The missile support for simulation training that is easy to install according to claim 1, characterized in that: The bottom of the rectangular plate (5) is fixedly connected to a second concave frame (16), and the top of the second concave frame (16) is fixedly connected to a second motor (17). The output end of the second motor (17) is provided with a second drive rod (18), and the top of the second drive rod (18) is fixedly connected to an adjusting rod (19).

6. The missile support for simulation training that is easy to install according to claim 5, characterized in that: Both ends of the adjusting rod (19) are rotatably connected to the connecting rod (20) via the second rotating shaft. The connecting rod (20) is rotatably connected to the concave strip (21) via the third rotating shaft. The concave strip (21) is fixed to the bottom of a pair of sliding blocks (14).

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