Real-time monitoring device for launching parameters of rocket mine arrangement equipment

Abstract

The utility model discloses a real-time monitoring device for launching parameters of rocket mine arrangement equipment, which relates to the technical field of rocket mine arrangement equipment and comprises a protective shell, a mounting block is mounted on the outer wall of one side of the protective shell, an adjusting assembly is mounted in the mounting block, and the adjusting assembly comprises a first gear rotationally connected with the inner wall of the mounting block. The outer wall of one side of the first gear is in meshed connection with a double-sided gear ring, the inner wall of the double-sided gear ring is in meshed connection with a plurality of second gears, and the middle of each second gear is rotationally connected with a rotating shaft; in the utility model, the adjusting structure can be used for adjusting according to gun barrels with different calibers, so that the device can be suitable for various rocket mine arrangement equipment, the requirement on a customized device is reduced, the research and development and production cost is reduced, an operator can quickly disassemble and replace a new device, and the installation time is saved.

Description

TECHNICAL FIELD

[0001] The utility model relates to rocket mine laying equipment technical field, concretely is a kind of rocket mine laying equipment launch parameter real-time monitoring device. BACKGROUND

[0002] The technical origin of rocket mine laying equipment can be traced back to the demand of modern war on efficient and flexible mine laying means, with the rapid development of military science and technology, traditional manual mine laying or mechanical mine laying method has been difficult to meet the demand of modern battlefield, therefore, rocket mine laying equipment emerges as the times require, and gradually becomes the important component of ground defense and tactical maneuver of armies in various countries, and when rocket mine laying equipment is launched in test field experiment, monitoring device is usually needed to detect the launch parameters of rocket, and monitoring data include but are not limited to: the launch speed of rocket, therefore speed monitoring device is used to evaluate the mine laying efficiency and accuracy of rocket mine laying equipment, and speed monitoring device is usually installed at the position that can accurately measure the speed of rocket, including the vicinity of barrel mouth, but in order to avoid high temperature and high pressure and airflow interference, a position slightly away from barrel mouth but still can accurately measure speed is usually selected.

[0003] In prior art, traditional rocket mine laying equipment launch speed monitoring device often needs to be customized according to specific barrel diameter, different types of rocket mine laying equipment can need different speed monitoring devices, which reduces the flexibility and replaceability of equipment, whenever new rocket mine laying equipment is developed or existing equipment is improved, speed monitoring device matching the diameter of barrel needs to be redesigned and produced, which increases the complexity and period of subsequent research and development work, simultaneously causes the rise of production cost, and reduces overall economic benefit. UTILITY MODEL CONTENTS

[0004] The utility model aims at providing a kind of rocket mine laying equipment launch parameter real-time monitoring device to solve the problems raised in the above background.

[0005] To solve the above technical problems, the utility model provides a kind of rocket mine laying equipment launch parameter real-time monitoring device, including protective shell, the side outer wall of protective shell is installed with mounting block, the inside of mounting block is installed with adjusting assembly, adjusting assembly includes the first gear that is rotatably connected with the inner wall of mounting block, the side outer wall of first gear is engagedly connected with double-sided tooth ring, the inner wall of double-sided tooth ring is engagedly connected with a plurality of second gears, the middle part of each second gear is rotatably connected with shaft, the end of each second gear away from double-sided tooth ring is engagedly connected with rack, the end of multiple racks close to each other is installed with push plate, the end of push plate away from rack is fixedly connected with protective pad, when first gear rotates, double-sided tooth ring will rotate synchronously.

[0006] Furthermore, a rotating rod is fixedly connected to the middle of the outer wall of one side of the first gear, a handrail is fixedly connected to the top of the rotating rod, a collar is slidably connected to the outer wall of the rotating rod, and a pin is installed on the outer wall of the end of the collar away from the rotating rod.

[0007] Furthermore, a monitoring mounting housing is installed on one side of the outer wall of the protective housing, and a monitoring probe is installed on one side of the outer wall of the monitoring mounting housing.

[0008] Furthermore, a slot is provided on one side of the outer wall of the protective shell, and the outer wall of one side of the first gear is meshed with the double-sided gear ring through the slot. The outer wall of the double-sided gear ring is rotatably connected to the inner wall of the protective shell, and both ends of the rotating shaft are fixedly connected to the inner wall of the protective shell.

[0009] Furthermore, the outer wall of each rack is slidably connected to the inner wall of the protective shell, and the surface of the pad is covered with an anti-slip texture.

[0010] Furthermore, the bottom of the handrail has multiple finger grooves, and the handrail is made of insulating material.

[0011] Furthermore, a guide rail is provided on one side of the outer wall of the rotating rod, and a protrusion is installed on the inner wall of the collar. The collar is slidably connected to the guide rail provided on the outer wall of the rotating rod through the protrusion, and the end of the pin away from the collar is inserted into the inner wall of the mounting block.

[0012] Compared with the prior art, the beneficial effects of this utility model are: the adjustment component can be adjusted according to different caliber gun barrels, making the device applicable to a variety of rocket mine-laying equipment, reducing the need for customized devices, reducing research and development and production costs, and when the device malfunctions or needs maintenance, operators can quickly disassemble and replace it with a new device, saving installation time and reducing installation errors caused by improper operation. There is no need to worry about caliber mismatch, improving the availability and reliability of the equipment. Furthermore, the same type of device makes spare parts inventory management simpler and reduces inventory costs. Attached Figure Description

[0013] Figure 1 A schematic diagram of the overall structure of a real-time monitoring device for launch parameters of a rocket mine-laying equipment.

[0014] Figure 2 A schematic diagram of the internal structure of the housing in a real-time monitoring device for launch parameters of a rocket mine-laying equipment.

[0015] Figure 3 This is a schematic diagram of the adjustment component in a real-time monitoring device for launch parameters of a rocket mine-laying equipment.

[0016] Figure 4 A schematic diagram of the overall structure of a real-time monitoring device for launch parameters of a rocket mine-laying equipment;

[0017] Figure 5 for Figure 4 Enlarged view of point A in the middle.

[0018] In the picture:

[0019] 1. Protective housing; 2. Mounting block; 3. First gear; 4. Double-sided gear ring; 5. Second gear; 6. Shaft; 7. Rack; 8. Push plate; 9. Protective pad; 10. Rotary rod; 11. Handrail; 12. Collar; 13. Pin; 14. Monitoring mounting housing. Detailed Implementation

[0020] 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.

[0021] Please see Figure 1 - Figure 5 This utility model provides a technical solution for a real-time monitoring device for launch parameters of rocket mine-laying equipment:

[0022] In the embodiments of this utility model, see Figure 1 , Figure 2 , Figure 3 , Figure 4 , Figure 5The system includes a protective outer shell 1. A mounting block 2 is installed on one outer wall of the protective outer shell 1. An adjustment assembly is installed inside the mounting block 2. The adjustment assembly includes a first gear 3 rotatably connected to the inner wall of the mounting block 2. A double-sided gear ring 4 is meshed with one outer wall of the first gear 3. The first gear 3 rotates through the assembly's characteristics, achieving stable synchronous drive of the double-sided gear ring 4. Multiple second gears 5 are meshed with the inner wall of the double-sided gear ring 4. The rotation of the first gear 3 is transmitted to the multiple second gears 5 through the double-sided gear ring 4, ensuring the synchronicity of the multiple second gears 5. A rotating shaft 6 is rotatably connected to the middle of each second gear 5. Both ends of the rotating shaft 6 are fixedly connected to the inner wall of the protective outer shell 1, providing stable support for the second gear 5 and preventing it from shaking during rotation. The offset reduces wear and malfunctions caused by vibration or shaking during rocket launch. Each second gear 5 is connected to a rack 7 at the end furthest from the double-sided gear ring 4. Push plates 8 are installed at the ends of multiple racks 7 that are close to each other. The rack 7 converts the rotation of the second gear 5 into linear motion, and the linear push plates 8 are displaced. By utilizing the meshing characteristics, a smooth transition from rotation to linear motion is achieved, improving the adjustment accuracy between components. A protective pad 9 is fixedly connected to the end of the push plate 8 furthest from the rack 7. The protective pad 9 increases the friction between the push plate 8 and the barrel, preventing the device from sliding and improving the contact stability between the components and the barrel. By utilizing the meshing characteristics of the components, the vibration generated during rocket launch can prevent the components from becoming loose, thus affecting the structure and performance of the adjustment components.

[0023] See Figure 4 , Figure 5 A rotating rod 10 is fixedly connected to the middle of the outer wall of one side of the first gear 3. A handrail 11 is fixedly connected to the top of the rotating rod 10. Multiple finger grooves are provided at the bottom of the handrail 11. The handrail 11 is made of insulating material. The finger grooves increase the contact area between the user and the handrail 11, improving the stability of the operation. A collar 12 is slidably connected to the outer wall of the rotating rod 10. A pin 13 is installed on the outer wall of the collar 12 away from the rotating rod 10. A guide rail is provided on one side of the outer wall of the rotating rod 10. A protrusion is installed on the inner wall of the collar 12. The collar 12 is slidably connected to the guide rail on the outer wall of the rotating rod 10 through the protrusion, so that the collar 12 will only slide along the outer wall of the rotating rod 10 or rotate synchronously with the rotating rod 10. The end of the pin 13 away from the collar 12 is inserted into the inner wall of the mounting block 2. When the pin 13 is inserted into the inner wall of the mounting block 2, it is fixed, thereby fixing the position of the collar 12 and the rotating rod 10.

[0024] See Figure 2A slot is provided on one side of the outer wall of the protective shell 1. The outer wall of the first gear 3 is meshed with the double-sided gear ring 4 through the slot. The slot provides the necessary space for the meshing connection between the first gear 3 and the double-sided gear ring 4. A monitoring mounting shell 14 is installed on one side of the outer wall of the protective shell 1. A monitoring probe is installed on one side of the outer wall of the monitoring mounting shell 14. The monitoring probe itself does not participate in the movement of the components, but allows the monitoring mounting shell 14 to provide data on the speed parameters of the rocket after launch through the monitoring probe.

[0025] Working principle: The user first slides the pin 13 out of the inner wall of the mounting block 2 using the collar 12 to release the limit, then holds the handle 11 and rotates it. Since the rotating rod 10 is fixedly connected to the handle 11, and the bottom end of the rotating rod 10 away from the handle 11 is rotatably connected to the first gear 3, when the handle 11 rotates, the first gear 3 will rotate synchronously. When the first gear 3 rotates, the double-sided toothed ring 4 meshing with the first gear 3 will rotate on the inner wall of the protective shell 1. The rotation of the double-sided toothed ring 4 causes the second gear 5 to rotate, so that the rack 7 meshing with the second gear 5 will convert the rotational motion of the second gear 5 into linear motion, so that multiple racks 7 can slide on the inner wall of the protective shell 1, thereby adjusting the distance between the push plates 8 to adapt to different barrel calibers, making the device applicable to various rocket mine-laying equipment.

Claims

1. A real-time monitoring device for launch parameters of rocket mine-laying equipment, comprising a protective outer shell (1), characterized in that: An installation block (2) is installed on one side of the outer wall of the protective shell (1). An adjustment component is installed inside the installation block (2). The adjustment component includes a first gear (3) rotatably connected to the inner wall of the installation block (2). A double-sided gear ring (4) is meshed with one side of the outer wall of the first gear (3). A plurality of second gears (5) are meshed with the inner wall of the double-sided gear ring (4). A rotating shaft (6) is rotatably connected to the middle of each second gear (5). A rack (7) is meshed with the end of each second gear (5) away from the double-sided gear ring (4). A push plate (8) is installed at the end of the plurality of racks (7) that are close to each other. A pad (9) is fixedly connected to the end of the push plate (8) away from the rack (7). When the first gear (3) rotates, the double-sided gear ring (4) will rotate synchronously.

2. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 1, characterized in that: A rotating rod (10) is fixedly connected to the middle of the outer wall of one side of the first gear (3). A handrail (11) is fixedly connected to the top of the rotating rod (10). A collar (12) is slidably connected to the outer wall of the rotating rod (10). A pin (13) is installed on the outer wall of the collar (12) away from the rotating rod (10).

3. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 2, characterized in that: The outer wall of the protective shell (1) has a slot on one side, and the outer wall of the first gear (3) is meshed with the double-sided gear ring (4) through the slot.

4. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 3, characterized in that: The outer wall of the double-sided toothed ring (4) is rotatably connected to the inner wall of the protective shell (1), and both ends of the rotating shaft (6) are fixedly connected to the inner wall of the protective shell (1).

5. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 4, characterized in that: A monitoring mounting housing (14) is installed on one side of the outer wall of the protective housing (1), and a monitoring probe is installed on one side of the outer wall of the monitoring mounting housing (14).

6. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 5, characterized in that: The outer wall of each of the racks (7) is slidably connected to the inner wall of the protective shell (1), and the surface of the pad (9) is covered with an anti-slip texture.

7. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 6, characterized in that: A guide rail is provided on one side of the outer wall of the rotating rod (10), and a protrusion is installed on the inner wall of the collar (12). The collar (12) is slidably connected to the guide rail provided on the outer wall of the rotating rod (10) through the protrusion. The end of the pin (13) away from the collar (12) is inserted into the inner wall of the mounting block (2).

8. The real-time monitoring device for launch parameters of rocket mine-laying equipment as described in claim 7, characterized in that: The bottom end of the handrail (11) is provided with multiple finger grooves, and the material of the handrail (11) is an insulating material.

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