Net gun integrated traversing machine structure

Abstract

The utility model relates to the technical field of unmanned aerial vehicle catching net guns, in particular to a net gun integrated crossing machine structure which comprises a machine body, an electric trigger is installed on the top of the machine body, a gas cylinder firing device is placed in the machine body, the head of the machine body is in threaded connection with a flow guide cover, and the side, away from the machine body, of the flow guide cover is in threaded connection with a net spraying gun head. A gun head rear cover is connected to the tail of the net spraying gun head in a clamped mode, four air channels inclining outwards are formed in the net spraying gun head, sealing hammer heads are embedded in the air channels and connected with the four corners of a catching net, and the catching net is placed at the concave position of the middle of the head of the net spraying gun head. The net gun integrated traversing machine is light in structure, light in weight, smoother in aiming operation, capable of aiming and launching in the high-speed advancing process, flexible and simple in operation, high in maneuverability and portability, free of launching a catching net after hovering when facing a more flexible unmanned aerial vehicle, simpler in target catching and higher in success rate.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle capturing net guns, in particular to a net gun integrated through-machine structure. Background Art

[0002] Currently, most drone net guns on the market are mounted type, which requires a large drone with a shaft diameter of 800mm-1500mm to carry the net gun. The overly large size of the drone lacks maneuverability when facing the small-diameter drones on the market, and it is difficult to expand the scope of application to public safety, private protection and other fields; at the same time, the target perspective of the net gun is too different from the target perspective of the camera. When the operator takes off and launches the net, he needs to predict the position of the target drone and launch the net after it hovers, which requires high skills of the operator and stability of the drone. Summary of the invention

[0003] In view of the shortcomings of the prior art, the utility model provides a net-gun integrated crossing machine structure, which solves the technical problems of poor maneuverability of the existing drone capturing net gun and high technical requirements for the operator.

[0004] In order to solve the above-mentioned technical problems, the utility model provides the following technical solutions: a net-gun integrated crossing machine structure, comprising a fuselage, an electric trigger is installed on the top of the fuselage, a gas cylinder trigger is placed in the fuselage, a deflector is threadedly connected to the head of the fuselage, a net-spraying gun head is threadedly connected to the side of the deflector away from the fuselage, a gun head back cover is clamped at the tail of the net-spraying gun head, four air ducts inclined outwards are arranged inside the net-spraying gun head, a sealing hammer head is embedded in the air duct, the sealing hammer head is connected to the four corners of the capture net, and the capture net is placed in the middle depression of the head of the net-spraying gun head.

[0005] Preferably, fuselage connectors are installed on both sides of the bottom of the fuselage, and fuselage arms are embedded in and fixedly connected to the fuselage connectors. The arms include but are not limited to four axes, four axes and eight motors, six axes, eight axes and a Y-shaped structure.

[0006] Preferably, a camera holder is installed on one side of the bottom of the fuselage, and a camera is installed on the camera holder.

[0007] Preferably, the tail portion of the fuselage is threadedly connected to the rear cover of the fuselage.

[0008] Preferably, the gas cylinder firing device comprises a tube shell in the body, one end of which is provided with a firing hole, a spring pin is arranged inside the tube shell near the firing hole, and the other end of the tube shell is arranged inside the compressed gas cylinder.

[0009] Preferably, the mesh spray gun head upper cover is provided with a gun head front cover.

[0010] By means of the above technical solution, the utility model provides a net gun integrated through-machine structure, which has at least the following beneficial effects:

[0011] The structure of the integrated net-gun flying drone is the same as the operation of the general seven-inch long-distance flying drone. The operator only needs to have operating experience of the same type of aircraft. The operation requirements are low. On this basis, it is lighter than the flying drones with the same functions on the market, and the aiming operation is smoother. It can aim and launch while moving at high speed. It is more flexible and simple to operate than similar products on the market, and has higher maneuverability and portability. When facing more flexible drones, there is no need to hover before launching the capture net, which makes capturing targets easier and has a higher success rate. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] The accompanying drawings described herein are used to provide a further understanding of the present invention and constitute a part of this application:

[0013] Figure 1 It is a three-dimensional structural schematic diagram of the utility model from a top view;

[0014] Figure 2 It is a schematic diagram of the three-dimensional structure of the utility model when viewed from above;

[0015] Figure 3 An exploded view of the utility model as a whole;

[0016] Figure 4 It is a structural schematic diagram of the front cross-section of the fuselage of the utility model;

[0017] Figure 5 This is a schematic diagram of the structure of the gas cylinder firing device of the utility model;

[0018] Figure 6 This is a schematic diagram of the structure of the net spraying gun head of the utility model;

[0019] Figure 7 This is a schematic diagram of the structure of the sealing hammer head and the capture net of the utility model;

[0020] Figure 8 It is a schematic diagram of the structure of various structures of the machine arm of the utility model;

[0021] Reference numerals:

[0022] 1. Body; 2. Body connector; 3. Arm; 4. Camera holder; 5. Camera; 6. Gas cylinder trigger; 61. Tube shell; 62. Firing hole; 64. Spring pin; 65. Compressed gas cylinder; 7. Electric trigger; 8. Body rear cover; 9. Air guide cover; 10. Spray net gun head; 101. Air duct; 11. Gun head rear cover; 12. Sealing hammer head; 13. Capture net; 14. Gun head front cover. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] The development of drone capture net 13 guns has grown rapidly in recent years, mainly due to the widespread use of drones and the corresponding increase in security and privacy issues. Net gun drones are usually equipped with a launcher capable of firing a warhead with a net that can be deployed in the air and capture the target drone, rendering it incapable of flight. Example

[0025] Based on the technical defects of the existing technology, please refer to Figure 1-Figure 7 The utility model provides a net-gun integrated crossing machine structure, which is flexible and simple to operate, and has high maneuverability and portability. When facing a more flexible drone, there is no need to hover before launching the capture net, which makes it easier to capture targets and has a higher success rate. It includes a fuselage 1, an electric trigger 7 is installed on the top of the fuselage 1, and the electric trigger 7 is used to fire the spring pin 64 in the gas cylinder firing device 6. The gas cylinder firing device 6 is placed in the fuselage 1, and the gas cylinder firing device 6 can provide power for the launch of the capture net 13. The head of the fuselage 1 is threadedly connected with a guide cover 9, and the guide cover 9 guides the gas sprayed from the gas cylinder firing device 6 to the net spraying gun head 10. The side of the guide cover 9 away from the fuselage 1 is threadedly connected with the net spraying gun head 10, and the net spraying gun head 10 is used to fix and launch the capture net 13. The tail of the net spraying gun head 10 is clamped with a gun head rear cover 11, and the gun head rear cover 11 is used to In order to prevent the capture net 13 from falling and to guide the airflow in the deflector 9, four air passages 101 inclined outward are provided inside the spray gun head 10, and a sealing hammer 12 is embedded in the air passage 101. The sealing hammer 12 is connected to the four corners of the capture net 13, and the capture net 13 is placed in the middle depression of the head of the spray gun head 10; when in use, after the target UAV is found, the electric trigger 7 is used to work and fire the spring needle 64 in the gas cylinder firing device 6, the spring needle 64 breaks the compressed gas cylinder 65 and releases high-pressure gas, and the gas passes through the deflector 9 and enters the air passage 101 in the spray gun head 10, and then the sealing hammer 12 is quickly ejected. Since the air passage 101 is inclined outward, the sealing hammer 12 can be expanded in four directions outward at this time, and the capture net 13 is expanded and the target UAV is captured under the traction of the sealing hammer 12.

[0026] In order to install the power motor, a fuselage connector 2 is installed on both sides of the bottom of the fuselage 1, and an arm 3 is embedded in and fixed to the fuselage connector 2. The arm 3 includes but is not limited to four axes, four axes and eight motors, six axes, eight axes and a Y-shaped structure; the power motor can be installed at the end of the arm 3 for installing the motor to provide power, and the arm 3 can be made of carbon fiber, which is lighter in weight.

[0027] In order to facilitate the shooting of FPV real-time images, a camera holder 4 is installed on one side of the bottom of the fuselage 1, and a camera 5 is installed on the camera holder 4; the camera 5 can be used to shoot the images.

[0028] In order to facilitate the installation or replacement of the gas cylinder trigger 6, a fuselage rear cover 8 is threadedly connected to the rear of the fuselage 1; by providing the fuselage rear cover 8, on the one hand, it can be used to seal the internal gas of the fuselage 1, and on the other hand, it can fix the gas cylinder trigger 6 and facilitate its replacement.

[0029] In order to launch the capture net 13, a gas cylinder trigger 6 can be used as a power source, and the gas cylinder trigger 6 includes a tube shell 61 in the fuselage 1, a firing hole 62 is opened on one end of the tube shell 61, a spring needle 64 is arranged inside the tube shell 61 near the firing hole 62, and a compressed gas cylinder 65 is arranged inside the other end of the tube shell 61; the gas cylinder trigger 6 is equipped with a compressed gas cylinder 65 storing liquefied carbon dioxide for providing an air pressure source, and when the spring needle 64 is triggered, the compressed gas cylinder 65 can be punctured to release the high-pressure gas.

[0030] In order to prevent the capture net 13 from falling during the flight, a gun head front cover 14 is provided on the net spraying gun head 10; the capture net 13 can be fixed in the net spraying gun head 10 by using the gun head front cover 14.

[0031] It can be known from the above embodiments that when in use, after the target UAV is found, the electric trigger 7 is used to work and fire the spring pin 64 in the gas cylinder firing device 6, the spring pin 64 breaks the compressed gas cylinder 65 and releases the high-pressure gas, the gas passes through the deflector 9 and enters the airway 101 in the spray gun head 10, and then the sealing hammer 12 is quickly sprayed out. Since the airway 101 is inclined outward, the sealing hammer 12 can be expanded in four directions outward at this time. Under the traction of the sealing hammer 12, the capture net 13 is expanded and the target UAV can be captured.

[0032] It should be noted that the terms "comprises", "includes" or any other variations thereof are intended to cover non-exclusive inclusion, so that a process, method, article or apparatus that includes a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or apparatus.

[0033] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A net gun integrated through-machine structure, comprising a machine body (1), characterized in that: An electric trigger (7) is installed on the top of the body (1), a gas cylinder trigger (6) is placed in the body (1), a flow deflector (9) is threadedly connected to the head of the body (1), a side of the flow deflector (9) away from the body (1) is threadedly connected to a spray gun head (10), a gun head rear cover (11) is clamped at the tail of the spray gun head (10), four air passages (101) inclined outwardly are arranged inside the spray gun head (10), a sealing hammer head (12) is embedded in the air passage (101), the sealing hammer head (12) is connected to the four corners of the capture net (13), and the capture net (13) is placed in a concave middle part of the head of the spray gun head (10).

2. The net gun integrated through-machine structure according to claim 1 is characterized by: Both sides of the bottom of the fuselage (1) are installed with fuselage connecting parts (2), and the fuselage connecting parts (2) are embedded with and fixedly connected with an arm (3), and the arm (3) includes but is not limited to a four-axis, a four-axis eight-motor, a six-axis, an eight-axis and a Y-shaped structure.

3. The net gun integrated through-machine structure according to claim 1 is characterized by: A camera holder (4) is installed on one side of the bottom of the fuselage (1), and a camera (5) is installed on the camera holder (4).

4. The net gun integrated through-machine structure according to claim 1 is characterized in that: The rear portion of the fuselage (1) is threadedly connected to the fuselage rear cover (8).

5. The net gun integrated through-machine structure according to claim 1 is characterized by: The gas cylinder firing device (6) comprises a tube shell (61) located in the body (1), a firing hole (62) being provided at one end of the tube shell (61), a spring pin (64) being provided inside the tube shell (61) near the firing hole (62), and a compressed gas cylinder (65) being provided inside the other end of the tube shell (61).

6. The net gun integrated through-machine structure according to claim 1, characterized in that: The upper cover of the web spraying gun head (10) is provided with a gun head front cover (14).

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