Net bomb launching assembly and capturing device composed of net bomb launching assembly

Abstract

The utility model discloses a net bomb launching assembly and a catching device formed by the net bomb launching assembly. The net bomb launching assembly comprises a shell, a net bomb launching assembly and a net bomb launching assembly, the net loading cylinder is arranged in the shell and is provided with a cavity for accommodating net bullets; and the multiple launching parts are obliquely arranged, distributed on the side edge of the net loading cylinder in a circumferential array mode, connected to the edge of the net bullets in the net loading cylinder and used for launching the net bullets in the posture of rotating around the axis of the net loading cylinder. According to the utility model, the plurality of launching parts are obliquely arranged and are arranged on the side edge of the net loading cylinder in the circumferential array manner, the plurality of launching parts respectively pull the edges of the net bullets towards different directions of uniform arrangement, and the angular momentum generated by rotation is utilized to resist external interference; therefore, the launched net bomb can be in a rotating posture in the air under the action of centrifugal force, the flying stability of the net bomb is improved, and the capturing success rate of the net bomb is guaranteed.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of capturing, especially relates to a net bomb launching assembly and the capturing device formed by it. BACKGROUND

[0002] In the prior art, the net bomb launching assembly is mostly used in scenes such as unmanned aerial vehicle interception, wild animal protection or special combat, but the existing net bomb launching assembly launching device has some defects, such as single launching angle and poor flight stability of the net bomb, so that it is difficult to guarantee the success rate of capturing the net bomb, and the application effect is seriously affected.

[0003] Therefore, how to improve the stability of the flight of the net bomb to guarantee the success rate of capturing the net bomb is a problem to be solved by the person skilled in the art. CONTENT OF THE UTILITY MODEL

[0004] The utility model embodiment provides a net bomb launching assembly and the capturing device formed by it, aiming at improving the stability of the flight of the net bomb, so as to guarantee the success rate of capturing the net bomb.

[0005] The utility model provides a net bomb launching assembly, which comprises:

[0006] A shell;

[0007] A net loading cylinder is arranged in the shell and is provided with a cavity for accommodating the net bomb;

[0008] A plurality of launching components are arranged obliquely and in a circumferential array on the side of the net loading cylinder and are connected to the edge of the net bomb in the net loading cylinder, and are used for launching the net bomb in a rotating posture around the axis of the net loading cylinder.

[0009] As an implementation mode, the launching component comprises:

[0010] A launching cylinder is arranged obliquely on the side of the net loading cylinder and is used for providing launching power;

[0011] A counterweight is connected to the top of the launching cylinder at one end and is connected to the edge of the net bomb at the other end and is used for launching the net bomb out of the net loading cylinder in a rotating posture around the axis of the net loading cylinder.

[0012] As an implementation mode, the launching component is obliquely arranged in the opposite direction of the axis of the net loading cylinder, and the projection of the axis of the launching component on the horizontal plane and the radial direction of the axis of the net loading cylinder form an angle less than 90°.

[0013] As an implementation mode, the counterweights (32) of a plurality of the launching components (30) are uniformly connected to the edge of the net bomb through traction ropes.

[0014] As an implementation form, the net shooting assembly further comprises a limiting block (40), and the net loading cylinder (20) and the shooting component (30) are arranged on the limiting block (40).

[0015] As an implementation form, the number of the shooting components (30) is at least three.

[0016] As an implementation form, the net shooting assembly further comprises a cylinder plug (50), the lower end of the cylinder plug (50) extends to form a plug-in part (51) which is plugged into the limiting block (40), and the upper end is concave to form a clamping part (52) which is clamped to the bottom of the shooting component (30).

[0017] The limiting block (40) is uniformly provided with a plurality of cylinder plug mounting holes in a circumferential array.

[0018] As an implementation form, the shooting cylinder (31) is provided with a powder cavity and is connected with an ignition device.

[0019] As an implementation form, the net shooting assembly further comprises a net head baffle (60) which is detachably arranged at the top end of the shell (10).

[0020] The utility model further provides a kind of capture device, including the net shooting assembly as any one of the above.

[0021] The utility model embodiment arranges multiple shooting components obliquely, and arranges in circumferential array on the side of net loading cylinder, and multiple shooting components respectively pull the edge of net shooting to different directions arranged uniformly, so that the net shooting can present rotating posture in the air under the action of centrifugal force, utilizes the angular momentum generated by rotation to resist external interference, to improve the stability of net shooting flight, to guarantee the capture success rate of net shooting. BRIEF DESCRIPTION OF DRAWINGS

[0022] In order to more clearly illustrate the technical scheme of the utility model embodiment, the drawings needed in the embodiment description will be briefly introduced below, and obviously, the drawings in the following description are some embodiments of the utility model, and those skilled in the art can also obtain other drawings according to these drawings without creating labor.

[0023] Figure 1 A structure diagram of a net shooting assembly provided by the utility model embodiment is shown in the figure.

[0024] Figure 2 Another structure diagram of a net shooting assembly provided by the utility model embodiment is shown in the figure.

[0025] Figure 3A structure schematic view of a launching component in a net elastic launching assembly provided by the utility model embodiment;

[0026] Figure 4 Another structure schematic view of a launching component in a net elastic launching assembly provided by the utility model embodiment;

[0027] Figure 5 A rotation schematic view of a net elastic in a net elastic launching assembly provided by the utility model embodiment;

[0028] Figure 6 A sectional view of a net elastic launching assembly provided by the utility model embodiment;

[0029] Figure 7 An axis projection view of a launching component in a net elastic launching assembly provided by the utility model embodiment;

[0030] Figure 8 A structure schematic view of a limiting block in a net elastic launching assembly provided by the utility model embodiment;

[0031] Figure 9 A structure schematic view of a barrel plug in a net elastic launching assembly provided by the utility model embodiment.

[0032] Identified in the figure:

[0033] 10, shell; 20, net loading barrel; 30, launching component; 31, launching barrel; 32, counterweight; 40, limiting block; 50, barrel plug; 51, plug-in part; 52, clamping part; 60, net head baffle. DETAILED DESCRIPTION

[0034] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0035] It should be understood that, when used in the description and the appended claims, the terms "comprise" and "include" indicate the existence of described features, integers, steps, operations, elements, and / or components, but do not exclude one or more other features, integers, steps, operations, elements, components, and / or sets thereof.

[0036] It should also be understood that the terms used in the specification of the utility model herein are only for the purpose of describing specific embodiments and are not intended to limit the utility model. As used in the specification of the utility model and the appended claims, the singular forms "a," "an," and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise.

[0037] It should be further understood that the term "and / or" used in the specification of the utility model and the appended claims means any combination of one or more of the associated listed items and all possible combinations, and includes these combinations.

[0038] Please see Figures 1-5 The utility model embodiment provides a net elastic launch assembly, specifically includes:

[0039] The shell 10 is arranged in the shell 10 and is provided with the cavity of containing the net elastic;

[0040] The net loading cylinder 20 is arranged in the shell 10 and is provided with the cavity of containing the net elastic;

[0041] The launch component 30 is arranged in the shell 10 and is provided with the cavity of containing the net elastic;

[0042] In the embodiment, by arranging multiple launch components 30 obliquely and in a circumferential array on the side of the net loading cylinder 20, the multiple launch components 30 respectively pull the edge of the net elastic in different directions arranged uniformly, so that the launched net elastic can present a rotating posture in the air under the action of centrifugal force, and the angular momentum generated by rotation is used to resist external interference, so as to improve the stability of the flight of the net elastic and thus ensure the success rate of capturing the net elastic.

[0043] Specifically, the net elastic generates angular momentum when rotating, and the direction of the rotating shaft is maintained stable through angular momentum conservation. When external factors (such as wind) interfere with the flight of the net elastic, the angular momentum generated by the rotation of the net elastic forms a reverse torque through inertia, so as to correct the motion trajectory and keep it stable. It can be understood that when the multiple launch components 30 are arranged in a circumferential array on the side of the net loading cylinder 20, it is equivalent to that the multiple launch components 30 are arranged in a circumferential array around the axis of the net loading cylinder 20.

[0044] In an embodiment, the launch component 30 includes:

[0045] The launch cylinder 31 is arranged obliquely on the side of the net loading cylinder 20 for providing launch power;

[0046] The counterweight 32 is connected to the top of the launching barrel 31 at one end and to the edge of the net bomb at the other end, and is used to drive the net bomb to be launched in a rotating posture around the axis of the net loading barrel 20.

[0047] In the embodiment, the launching component 30 is composed of the launching barrel 31 and the counterweight 32. The launching barrel 31 is arranged obliquely to provide launching power with an oblique angle, and the counterweight 32 is connected to the launching barrel 31 and the edge of the net bomb respectively, so as to be launched under the driving of the launching power with the oblique angle and drive the net bomb to be launched in a rotating posture around the axis of the net loading barrel 20.

[0048] It can be understood that the plurality of launching components 30 are arranged obliquely and uniformly distributed in a circumferential array on the side of the net loading barrel 20, that is, the plurality of counterweights 32 are uniformly distributed in a circumferential array around the axis of the net loading barrel 20, so that the launching directions of the plurality of counterweights 32 (that is, the directions of the launching power with the oblique angle provided by the launching barrel 31) are also uniformly distributed in a circumferential array on the side of the net loading barrel 20, and since the counterweight 32 is connected to the edge of the net bomb, a plurality of traction forces are formed to launch the net bomb and guide the net bomb to rotate, so as to be launched in a rotating posture around the axis of the net loading barrel 20.

[0049] In combination with FIGS. 1 to 3, Figure 6 and Figure 7 It can be understood that the plurality of launching components 30 are arranged obliquely and uniformly distributed in a circumferential array on the side of the net loading barrel 20, that is, the plurality of counterweights 32 are uniformly distributed in a circumferential array around the axis of the net loading barrel 20, so that the launching directions of the plurality of counterweights 32 (that is, the directions of the launching power with the oblique angle provided by the launching barrel 31) are also uniformly distributed in a circumferential array on the side of the net loading barrel 20, and since the counterweight 32 is connected to the edge of the net bomb, a plurality of traction forces are formed to launch the net bomb and guide the net bomb to rotate, so as to be launched in a rotating posture around the axis of the net loading barrel 20.

[0050] In the embodiment, by limiting the relationship between the axis of the launching component 30 and the axis of the net loading barrel 20, the launching component 30 can provide launching driving force in a specific direction, so as to launch the net bomb in a rotating posture around the axis of the net loading barrel 20.

[0051] Specifically, Figure 6 In the embodiment, the axis of the launching component 30 is represented by a dashed line A, and the axis of the net loading barrel 20 is represented by a dashed line B. The distance between the top of the launching component 30 and the axis of the net loading barrel 20 is greater than the distance between the bottom of the launching component 30 and the axis of the net loading barrel 20. At the same time, the angle between the projection of the axis of the launching component 30 on the horizontal plane and the radial direction of the axis of the net loading barrel 20 is set to be less than 90°. Specifically, Figure 7 In the embodiment, the axis of the launching component 30 is represented by a dashed line A, and the axis of the net loading barrel 20 is represented by a dashed line B. The distance between the top of the launching component 30 and the axis of the net loading barrel 20 is greater than the distance between the bottom of the launching component 30 and the axis of the net loading barrel 20. At the same time, the angle between the projection of the axis of the launching component 30 on the horizontal plane and the radial direction of the axis of the net loading barrel 20 is set to be less than 90°. Specifically, In the embodiment, the axis of the launching component 30 is represented by a dashed line A, and the axis of the net loading barrel 20 is represented by a dashed line B. The distance between the top of the launching component 30 and the axis of the net loading barrel 20 is greater than the distance between the bottom of the launching component 30 and the axis of the net loading barrel 20. At the same time, the angle between the projection of the axis of the launching component 30 on the horizontal plane and the radial direction of the axis of the net loading barrel 20 is set to be less than 90°. Specifically,

[0052] In an embodiment, the plurality of weight blocks 32 of the launching component 30 are evenly connected to the edge of the net launcher through the traction rope.

[0053] In the embodiment, based on the setting mode of the plurality of launching components 30 (inclined setting and evenly arranged in a circumferential array on the side of the net loading cylinder 20), the plurality of weight blocks 32 are also evenly arranged in a circumferential array on the side of the net loading cylinder 20 and evenly distributedly connected to the edge of the net launcher through the traction rope, so that the plurality of evenly distributed launching power with an inclined angle drives the net launcher to be launched in a rotating posture.

[0054] In combination Figure 8 As shown in the figure, in an embodiment, the net launcher launching assembly further comprises a limiting block 40, and the net loading cylinder 20 and the launching component 30 are arranged on the limiting block 40.

[0055] In the embodiment, the limiting block 40 functions to fix the position of the net loading cylinder 20 and the launching component 30 and ensure the stability of each component during launching. For example, when the launching component 30 is provided with launching power by igniting gunpowder, the high-pressure gas formed by the burning of the gunpowder may cause a violent impact on the launching component 30, and the limiting block 40 can effectively prevent the displacement and ensure the accuracy and stability of the launching direction.

[0056] In a specific embodiment, the number of the launching component 30 can be set according to actual needs, but at least three are arranged, so as to ensure that the net launcher launched can be effectively opened, thereby ensuring the success rate of capture.

[0057] In combination Figure 9 As shown in the figure, in an embodiment, the net launcher launching assembly further comprises a cylinder plug 50, the lower end of the cylinder plug 50 extends to form a plug-in part 51 to be plugged into the limiting block 40, and the upper end is concave to form a clamping part 52 to be clamped to the bottom of the launching component 30.

[0058] The limiting block 40 is evenly provided with a plurality of cylinder plug mounting holes in a circumferential array.

[0059] In the embodiment, the cylinder plug 50 is tightly matched through the plug-in part 51 and the clamping part 52, which ensures the stable fixation of the launching component 30 on the limiting block 40. Meanwhile, by evenly arranging a plurality of cylinder plug mounting holes in a circumferential array on the limiting block 40, the number and position of the launching component 30 can be flexibly adjusted by installing different numbers and positions of the cylinder plug 50, so as to meet different launching needs.

[0060] For example, six barrel mounting holes can be arranged on the limiting block 40, so that three or six barrels 50 can be selected and mounted according to actual needs, and the corresponding number of launching components 30 are arranged, so that the launching components 30 can stably launch the netting in a rotating posture, and the layout of the launching components 30 can be flexibly adjusted, thereby improving the applicability of the netting launching assembly.

[0061] In an embodiment, the launching barrel 31 is provided with a propellant cavity, and the ignition device is connected to the propellant cavity.

[0062] In the embodiment, the propellant cavity is arranged in the launching barrel 31 for loading propellant, and the ignition device is connected to the propellant cavity, so that the propellant loaded in the propellant cavity is ignited by the ignition device, thereby generating high-pressure gas in the propellant cavity and pushing the counterweight 32 at the top end of the launching barrel 31 to launch, and then driving the netting to be launched in a predetermined posture. In specific embodiments, the volume of the propellant cavity can be adjusted according to actual needs to adapt to different launching distances and strength requirements. The ignition device can be an electronic detonator or other ignition device, and can be connected to the propellant cavity through a wire.

[0063] In an embodiment, the netting launching assembly further comprises a net head baffle 60 detachably arranged at the top end of the shell 10.

[0064] In the embodiment, the top end of the shell 10 is further provided with a detachable net head baffle 60, and the installation and disassembly of the net head baffle 60 can effectively protect the head of the netting from being damaged during transportation or storage, and facilitate maintenance and replacement, thereby further improving the overall reliability and service life of the launching component 30.

[0065] The embodiment of the utility model further provides a capturing device which comprises the netting launching assembly as described above.

[0066] The embodiments in the specification are described in a progressive manner, and each embodiment focuses on the difference from other embodiments, and the same and similar parts of each embodiment can be referred to each other. For the system disclosed in the embodiments, since it corresponds to the method disclosed in the embodiments, the description is relatively simple, and the related parts can be referred to the method part. It should be pointed out that for ordinary skilled in the art, without departing from the principles of the present application, the present application can be improved and modified, and these improvements and modifications also fall within the protection scope of the claims of the present application.

[0067] It is further noted that the terminology "first", "second" and the like used in the specification are merely used for differentiating one entity or action from another, and do not necessarily imply any actual physical or logical relationship or order between such entities or actions. Moreover, the use of the term "including", "containing" or any other variant thereof is intended to cover non-exclusive inclusion, such that a process, method, article or apparatus that comprises a list of elements is not required to comprise only those elements but can include other elements not expressly listed or inherent to such process, method, article or apparatus. An element preceded by "comprises a..." does not, without further restriction, preclude the existence of additional elements of the same nature as those recited.

Claims

1. A net catapult assembly, characterized by It comprises: a shell (10); a net loading cylinder (20) arranged in the shell (10) and provided with a cavity for accommodating a net bomb; a plurality of launching components (30) arranged obliquely and uniformly in a circumferential array on the side of the net loading cylinder (20) and connected to the edge of the net bomb in the net loading cylinder (20), for launching the net bomb in a rotating posture around the axis of the net loading cylinder (20).

2. The net catapult assembly of claim 1, wherein, The launching component (30) comprises: a launching cylinder (31) arranged obliquely on the side of the net loading cylinder (20) for providing launching power; a counterweight (32) connected to the top of the launching cylinder (31) at one end and to the edge of the net bomb at the other end, for driving the net bomb to be launched out of the net loading cylinder (20) in a rotating posture around the axis of the net loading cylinder (20).

3. The net catapult assembly of claim 2, wherein, The launching component (30) is arranged reversely oblique to the axis of the net loading cylinder (20), and the projection of the axis of the launching component (30) on the horizontal plane is less than 90° with the radial direction of the axis of the net loading cylinder (20).

4. The net catapult assembly of claim 2, wherein, The counterweights (32) of a plurality of the launching components (30) are uniformly connected to the edge of the net bomb through a traction rope.

5. The net catapult assembly of claim 1, wherein, It further comprises a limiting block (40), and the net loading cylinder (20) and the launching component (30) are arranged on the limiting block (40).

6. The net catapult assembly of claim 1, wherein, The number of the launching components (30) is at least three.

7. The net catapult assembly of claim 1, wherein, It further comprises a cylinder plug (50), the lower end of which extends to form a plug-in part (51) for plugging into the limiting block (40), and the upper end of which is recessed to form a clamping part (52) for clamping to the bottom of the launching component (30). A plurality of cylinder plug mounting holes are uniformly arranged in a circumferential array on the limiting block (40).

8. The net catapult assembly of claim 2, wherein, The launching cylinder (31) is provided with a powder cavity and connected to an ignition device.

9. The net catapult assembly of claim 1, wherein, It further comprises a net head baffle (60) detachably arranged at the top end of the shell (10).

10. A capturing device, characterized by It comprises the net bomb launching assembly according to any one of claims 1-9. It comprises the net bomb launching assembly according to any one of claims 1-9.

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