Missile aircraft adaptation device for improving damage capability of unmanned aerial vehicle
By designing a bullet-machine adapter device for the cylinder and interface plate, the problem of low fragment density and damage probability during UAV dynamic target practice was solved, achieving efficient damage effect for UAV products, simplifying operation and reducing costs.
Patent Information
- Application Number
- CN202423147519.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-19
- Publication Date
- 2025-11-14
- Estimated Expiration
- 2034-12-19
AI Technical Summary
The existing missile-machine interface structure causes some fragments to fail to strike the target perpendicularly when the product explodes during dynamic target practice by drones, resulting in a decrease in the average fragment distribution density and the probability of damage.
A missile-machine adapter device was designed, comprising a cylinder, a connecting plate, and an interface plate. One end of the cylinder has an oblique section. The connecting plate is connected to the UAV, and the interface plate is connected to the product. By adjusting the attack angle of the UAV, the product is made to explode vertically on the target, thereby increasing the fragment distribution density and the probability of damage.
It achieves uniform distribution of product fragments within the dispersion angle range under dynamic target firing conditions, significantly improving the damage efficiency of UAVs. It is easy to operate and highly versatile, reducing manpower requirements and testing costs.
Smart Images
Figure CN223546467U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of drone accessories technology, and specifically discloses a missile-machine adapter device to improve the destructive capability of drones. Background Technology
[0002] Drones can be used to destroy targets. When delivering products to the attack location, the safety and ignition control devices activate to detonate the products. The explosion generates a shock wave and a high-speed fragmentation group, which damages the target.
[0003] If existing missile adaptation structures are used, such as Figure 1 As shown in the experiment, when the drone dynamically targets, the product explodes at an angle due to the drone's attack angle. The product is not perpendicular to the target, and at the time of explosion, some of the target fragments are outside the product's scattering angle range. Figure 2 As shown, this results in a decrease in the average fragment density and probability of damage to the target within the product's scattering angle range.
[0004] The existing product missile-machine adapter structure cannot effectively address the average distribution density of the maximum fragments and the probability of damage within the target area during dynamic target practice by UAVs. Therefore, it is necessary to improve the design of the product missile-machine adapter structure to further enhance the dynamic damage capability of the product. Utility Model Content
[0005] This utility model is achieved through the following technical solution:
[0006] This utility model provides a missile-machine adapter device to improve the damage capability of UAVs, including a cylinder 1, a connecting plate 2 and an interface plate 3;
[0007] The cylinder 1 is a truncated cylindrical shell with a flat surface at one end and an inclined cross-section at the other end. The cross-section forms an angle of β° with the cylinder axis; β = 90 - α, where α is the UAV's attack angle.
[0008] The outer side of the inclined section port is provided with a circular connecting plate 2; the surface of the connecting plate 2 is provided with a drone connection hole for connecting to the drone body;
[0009] The inner side of the cylindrical body 1 is provided with an interface disk 3 that matches the interface of the drone attack product. The interface disk 3 has a through hole in the middle and a drone attack product connection hole on its surface.
[0010] Preferably, the connecting plate 2 is a flange.
[0011] Furthermore, the flange is provided with bolt holes on its periphery that correspond to the screw holes of the drone attack product, and the drone adapter is connected to the product by bolts.
[0012] Preferably, the interface disk 3 and its intermediate through hole are in the shape of a two-stage stepped cylinder, with the smaller diameter first-stage cylinder protruding axially from the side of the cylinder 1.
[0013] Preferably, the UAV attack product connection hole of the interface disk 3 is a threaded hole, and the missile adapter is connected to the UAV attack product by screws.
[0014] Preferably, the projectile adapter is made of metal.
[0015] Preferably, the diameter of the cylinder 1 is the same as the diameter of the drone attack product.
[0016] The beneficial effects of this utility model are:
[0017] This invention can be configured with connectors suitable for various drone attack angles, allowing for use on multiple product types. It is simple to operate and convenient to use. The actual operation is not limited by the environment, requires minimal manpower, is simple to operate, highly operable and versatile, and economical. It greatly improves the efficiency of product testing, installation, and successful testing, and has been well-appointed in actual testing, significantly improving the damage efficiency of drone products. Attached Figure Description
[0018] Figure 1 A two-dimensional schematic diagram of the adaptation structure for the currently used missile launcher;
[0019] Figure 2 A schematic diagram showing the fragmentation distribution during a dynamic explosion using a current bomb-machined structure adapted to the product.
[0020] Figure 3 This is a two-dimensional connection diagram of the present invention;
[0021] Figure 4 This is a three-dimensional structural front view schematic diagram of the present invention;
[0022] Figure 5 This is a schematic cross-sectional view of the structure of this utility model;
[0023] Figure 6 This is a schematic diagram showing the distribution of fragments during a dynamic explosion after using this invention. Detailed Implementation
[0024] To better illustrate the purpose, technical solution, and advantages of this utility model, further explanation is provided below in conjunction with the accompanying drawings and embodiments. It should be understood that the embodiments are only used to illustrate the technical effects of this utility model and are not intended to limit the scope of protection of this utility model.
[0025] Example 1
[0026] A missile-machine adapter for improving the destructive capability of unmanned aerial vehicles (UAVs) includes a cylinder 1, a connecting plate 2, and an interface plate 3;
[0027] The cylinder 1 is a truncated cylindrical shell with a flat surface at one end and an inclined cross-section at the other end. The cross-section forms an angle of β° with the cylinder axis; β = 90 - α, where α is the UAV's attack angle.
[0028] A circular connecting plate 2 is provided on the outer side of the inclined section port; the connecting plate 2 has a drone connection hole on its surface for connection to the drone body; the connecting plate 2 is a flange. The flange has bolt holes on its periphery corresponding to the screw holes of the drone attack product, and the drone adapter is connected to the product by bolts.
[0029] The inner side of the cylindrical body 1 is provided with an interface plate 3 that matches the interface of the UAV attack product. The interface plate 3 has a through hole in the middle and a UAV attack product connection hole on its surface. The interface plate 3 and its middle through hole are in the shape of a two-stage stepped cylinder, with the smaller diameter first-stage cylinder protruding axially from the side of the cylindrical body 1. The UAV attack product connection hole of the interface plate 3 is a threaded hole, and the missile-machine adapter is connected to the UAV attack product by screws.
[0030] The missile adapter is made of metal. The diameter of the cylinder 1 is the same as the diameter of the UAV attack product.
[0031] In use, first insert the thin-walled cylindrical portion of the connector into the product, aligning the upward-facing through-holes on the interface plate with the threaded holes on the product, and then secure it firmly with screws. After the product is assembled inside the drone, tilt the product and drone at a certain angle β. When the drone attacks the target at an attack angle α, the drone's internal compensation angle β + the drone's attack angle α equals 90°, achieving the optimal attack posture for the drone against the target. Figure 6 As shown, when the drone explodes at the target location, a large number of product fragments can be distributed within the scattering angle range, greatly increasing the average density of fragment distribution and the probability of damage within the scattering angle range, thus effectively damaging the target.
[0032] The specific structure described in this utility model can be selected and used as appropriate, but is not limited to the structure described above. Obviously, different structural changes can be made under the concept of this utility model, but all of them are within the protection scope of this utility model.
Claims
1. A missile-aircraft adapter for improving the destructive capability of unmanned aerial vehicles (UAVs), characterized in that, It includes a cylinder (1), a connecting plate (2), and an interface plate (3); The cylinder (1) is a truncated cylindrical shell with a flat surface at one end and a sloping cross section at the other end. The cross section forms an angle of β° with the cylinder axis; β = 90 - α, where α is the attack angle of the UAV. The outer side of the inclined section port is provided with a circular connecting plate (2); the surface of the connecting plate (2) is provided with a drone connection hole for connection with the drone body; The inner side of the cylindrical body (1) is provided with an interface disk (3) that matches the interface of the UAV attack product. The interface disk (3) has a through hole in the middle and a UAV attack product connection hole on its surface.
2. The missile-aircraft adaptation device for improving the destructive capability of unmanned aerial vehicles according to claim 1, characterized in that, The connecting plate (2) is a flange.
3. The missile-aircraft adaptation device for improving the destructive capability of unmanned aerial vehicles according to claim 2, characterized in that, The flange is provided with bolt holes on its periphery that correspond to the screw holes of the drone attack product, and the drone adapter is connected to the product by bolts.
4. The missile-aircraft adaptation device for improving the destructive capability of unmanned aerial vehicles according to claim 1, characterized in that, The interface disk (3) and its intermediate through hole are two-stage stepped cylinders, with the smaller diameter first-stage cylinder protruding axially from the side of the cylinder (1).
5. The missile-aircraft adaptation device for improving the damage capability of unmanned aerial vehicles according to claim 4, characterized in that, The interface plate (3) has a threaded hole for connecting the drone attack product, and the drone adapter is connected to the drone attack product by screws.
6. The missile-aircraft adaptation device for improving the destructive capability of unmanned aerial vehicles according to claim 1, characterized in that, The missile adapter is made of metal.
7. The missile-aircraft adaptation device for improving the destructive capability of unmanned aerial vehicles according to claim 1, characterized in that, The diameter of the cylinder (1) is the same as the diameter of the drone attack product.