Flying object capturing device

Abstract

The utility model discloses a flyer capturing device, which particularly relates to the field of flyer capturing and comprises a flying body mounted on a launching gun. The capturing group comprises guide pipes, plummets, a net and an emitter, the guide pipes are distributed in the flying body in a horn shape, one plummet is slidably placed in each guide pipe, the plummets are connected through the net, and the emitter is embedded in the flying body and used for pushing the plummets in the guide pipes to fly outwards along the guide pipes; the time delay module comprises a microcontroller, a timer circuit and a battery, the length of a countdown section of the time delay module is reasonably preset during the flying period of the whole device which is separated from a launching gun for the first time, the capturing group can be launched for the second time in the air, and the use distance of the capturing group can be at least doubled by combining the two sections of aerial displacements of the capturing group; and the whole process is high in response speed, easy to operate by a user and high in flyer capturing efficiency.

Description

Technical Field

[0001] The utility model relates to the field of flying object capture, and more specifically, the utility model relates to a flying object capture device. Background Art

[0002] Whether it is a flying creature or a flying machine, it is necessary to capture it when necessary to prevent it from causing harm to land activities.

[0003] Taking drones as an example, the existing methods for capturing drones mostly use electromagnetic interference. By interfering with the control system of the drone, the drone loses its original flight path instructions. However, this operation method is expensive, has a small working range, is inconvenient to use, and cannot directly capture the drone itself.

[0004] In some cases, a net gun is also used. Although the net gun is easy to carry, its effective capture range is only about 20m. Due to its low kinetic energy, the process of covering the target is relatively slow. Summary of the Utility Model

[0005] In order to overcome the above-mentioned defects of the prior art, an embodiment of the utility model provides a flying object capture device. The technical problem to be solved by the utility model is: how to quickly and efficiently capture the drone itself.

[0006] To achieve the above object, the utility model provides the following technical solution: a flying object capture device, including a flying body installed on a launching gun; a capture group including a guiding tube, a weight, a net and a launcher. A plurality of guiding tubes are arranged in a horn shape in the flying body. A weight is slidably placed in each guiding tube. A plurality of weights are connected by a net. The launcher is buried in the flying body and is used to push the weight in the guiding tube to fly out along the guiding tube; a delay module including a microcontroller, a timer circuit and a battery, and the launcher, the timer circuit, the microcontroller and the battery are electrically connected.

[0007] In a preferred embodiment, a through groove is formed on the side wall of the guiding tube.

[0008] In a preferred embodiment, the delay module and an external control platform are electrically connected through wireless transmission.

[0009] In a preferred embodiment, the delay module is equipped with a control button for manually inputting the countdown duration.

[0010] In a preferred embodiment, the flying body includes a housing, a warhead catcher, a tail wing and an end cap. The housing is a hollow structure. The capture group is arranged in the housing. The housing and the end cap are snap-connected. The delay module is buried in the housing. The housing and the warhead catcher are detachably connected. The tail wing is fixed on the warhead catcher.

[0011] In a preferred embodiment, the warhead catcher and the housing are connected by a snap structure.

[0012] In a preferred embodiment, the warhead catcher and the housing are threadedly connected.

[0013] Technical effects and advantages of the present utility model:

[0014] By reasonably presetting the length of the countdown period of the delay module during the first flight of the entire device away from the launch gun, the capture group can be launched a second time in the air. The combined two air displacements of the capture group can at least double the usage distance of the capture group, and the response speed of the entire process is fast, easy for users to operate, and the efficiency of capturing flying objects is high. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The drawings are used to provide a further understanding of the technical solutions of the present utility model, and constitute a part of the present utility model. The embodiments of the present utility model and their descriptions are used to explain the present utility model and do not constitute an improper limitation to the present utility model.

[0016] Figure 1 It is a structural diagram of the flying object capture device of the present utility model.

[0017] Figure 2 It is a structural diagram of the flying body in the present utility model.

[0018] Figure 3 It is a structural diagram of the capture group in the present utility model.

[0019] Figure 4 It is a structural diagram of the opened net of the present utility model.

[0020] The reference numerals in the drawings are: 1, flying body; 11, housing; 12, warhead catcher; 13, tail fin; 14, end cap; 2, capture group; 21, guide tube; 22, weight; 23, net; 24, launcher; 3, delay module. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0021] Now, the exemplary embodiments will be described more fully with reference to the accompanying drawings. However, the exemplary embodiments can be implemented in various forms and should not be construed as limited to the examples set forth herein; rather, these exemplary embodiments are provided so that the present disclosure will be more thorough and complete, and will fully convey the concept of the exemplary embodiments to those skilled in the art. The drawings are only schematic illustrations of the present disclosure and are not necessarily drawn to scale. The same reference numerals in the drawings denote the same or similar parts, and thus their repeated description will be omitted.

[0022] In addition, the described features, structures or characteristics may be combined in one or more example embodiments in any suitable manner. In the following description, many specific details are provided to provide a full understanding of the example embodiments of the present disclosure. However, those skilled in the art will appreciate that the technical solutions of the present disclosure may be practiced while omitting one or more of the specific details, or other methods, components, steps, etc. may be adopted. In other cases, well-known structures, methods, implementations or operations are not shown or described in detail to avoid obscuring various aspects of the present disclosure.

[0023] Example

[0024] like Figures 1 - 4 A flying object capturing device comprises a flying object 1, a capturing group 2 and a delay module 3. The flying object 1 is connected to a launching gun, the capturing group 2 is placed inside the flying object 1, and the delay module 3 is used to control the capturing group 2 to detach from the flying object 1 at an appropriate time, thereby extending the running time and trajectory of the capturing group 2 in the air.

[0025] The flying body 1 includes a shell 11, a warhead catcher 12, a tail fin 13 and an end cover 14. The capture group 2 is placed in the shell 11. The shell 11 and the head of the warhead catcher 12 are connected by threads. The tail fin 13 is fixed on the rear side of the warhead catcher 12 to extend the flight time of the entire device. One end of the shell 11 is open, which is convenient for the user to assemble the flying body 1 and the capture group 2. After the assembly is completed, the end cover 14 can be closed. The opening of the shell 11 and the end cover 14 are snap-fitted and connected.

[0026] The bullet catcher 12 is used to connect with the launch gun, and the user controls the launch timing of the launch gun to launch the entire capture device to a designated location. It should be noted that the working principle of the launch gun is to store energy and then release it in a short period of time to transfer the energy to the object so that the object can obtain sufficient speed to overcome external resistance and reach the predetermined target. Different types of launch guns may use different energy forms and mechanisms to achieve this process. Since the launch gun itself is a prior art, it will not be described in detail in this embodiment.

[0027] The capture group 2 includes a guide tube 21, a sinker 22, a net 23 and a launcher 24. A plurality of guide tubes 21 are fixed in the shell 11. The plurality of guide tubes 21 are arranged in a trumpet shape. The large end of the trumpet shape is in the same direction as the opening of the shell 11, and the small ends are in contact with the launcher 24. A sinker 22 is slidably placed in each guide tube 21. Under normal conditions, the sinker 22 will not detach from the guide tube 21.

[0028] Preferably, the emitter 24 is driven by gunpowder power. Under the control of the delay module 3, the gas pressure generated by the explosion of gunpowder is transmitted to the guide tube 21 through the emitter 24. Under the restraint and guiding action of the guide tube 21, the weight 22 is pushed to accelerate and be launched along the axial trajectory of the guide tube 21. As the time of the parabolic-like motion of several weights 22 in the air extends, the several weights 22 move away from each other, and the net 23 used to connect the several weights 22 is gradually unfolded and captures the flying target. Similarly, the emitter 24 can also be of other power drive types. Since it is prior art, it will not be elaborated here.

[0029] It should be noted that

[0030] Preferably, the side surface of the guide tube 21 is provided with a through groove, and a part of the net 23 connected to the weight 22 is located in the through groove.

[0031] The delay module 3 includes a timer circuit and a microcontroller. The timer circuit presets a specific time interval, that is, the countdown period. When the timer circuit detects the end of the preset time interval, the microcontroller receives the corresponding signal and activates the ignition mechanism of the emitter 24, thereby starting the entire launch process.

[0032] Preferably, the timer circuit is connected to an external control platform through wireless transmission technology. The user can remotely modify the length of the countdown period of the timer circuit through the external control platform. The wireless transmission technology can be WiFi, Bluetooth, satellite communication, etc. This embodiment only gives examples and does not make specific limitations.

[0033] Preferably, the delay module 3 is equipped with a regulation button. The user can input the required countdown duration into the microcontroller by manually operating the regulation button, so as to accurately control the subsequent ignition timing, which is particularly applicable in occasions with poor communication environments.

[0034] It should be noted that the above-mentioned delay module 3 refers to an integrated entity that can be embedded in the housing 11.

[0035] The working principle of the present utility model:

[0036] By reasonably presetting the length of the countdown period of the delay module 3 during the first flight of the entire device away from the launch gun, the capture group 2 can be launched a second time in the air. The combined two air displacements of the capture group 2 can at least double the use distance of the capture group 2, and the entire process has a fast response speed, is easy for users to operate, and has a high efficiency in capturing flying objects.

[0037] The above only describes some exemplary embodiments of the present utility model by way of illustration. Without doubt, for those of ordinary skill in the art, the described embodiments can be modified in various different ways without departing from the spirit and scope of the present utility model. Therefore, the above drawings and description are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present utility model.

[0038] Finally, the following points should be noted: First, in the description of this application, it should be noted that unless otherwise specified and defined, the terms "installation", "connection", and "coupling" should be understood in a broad sense. It can be a mechanical connection or an electrical connection, or it can be the communication inside two components. It can be directly connected. "Up", "down", "left", "right", etc. are only used to represent the relative position relationship. When the absolute position of the object being described changes, the relative position relationship may change.

[0039] Second: In the drawings of the disclosed embodiments of the present utility model, only the structures related to the disclosed embodiments are involved. For other structures, reference can be made to the usual designs. Without conflict, the same embodiment and different embodiments of the present utility model can be combined with each other.

[0040] Finally: The above are only the preferred embodiments of the present utility model and are not used to limit the present utility model. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A flying object capturing device, characterized in that Including: A flying object (1), installed on a launching gun; A capture group (2), including a guiding tube (21), a weight (22), a net (23) and a launcher (24). A number of guiding tubes (21) are arranged in a horn shape inside the flying object (1). A weight (22) is slidably placed in each guiding tube (21). A number of weights (22) are connected by a net (23). The launcher (24) is buried inside the flying object (1), and the launcher (24) is used to push the weight (22) in the guiding tube (21) to fly out along the guiding tube (21); A delay module (3), including a microcontroller, a timer circuit and a battery. The launcher (24), the timer circuit, the microcontroller and the battery are electrically connected.

2. The flying object capturing device according to claim 1, characterized in that: A through groove is formed on the side wall of the guiding tube (21).

3. The flying object capturing device according to claim 1, characterized in that: The delay module (3) and an external control platform are electrically connected through wireless transmission.

4. A flying object capturing device according to claim 1 or 3, characterized in that: The delay module (3) is equipped with a control button for manually inputting the countdown duration.

5. The flying object capturing device according to claim 1, wherein: The flying object (1) includes a housing (11), a warhead catcher (12), a tail fin (13) and an end cap (14). The housing (11) is a hollow structure. The capture group (2) is arranged inside the housing (11). The housing (11) and the end cap (14) are snap-connected. The delay module (3) is buried in the housing (11). The housing (11) and the warhead catcher (12) are detachably connected. The tail fin (13) is fixed on the warhead catcher (12).

6. The flying object capturing device according to claim 5, characterized in that: The warhead catcher (12) and the housing (11) are connected by a snap structure.

7. The flying object capturing device according to claim 5, wherein: The warhead catcher (12) and the housing (11) are threadedly connected.

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