Electromagnetic confrontation device applied to multi-unmanned aerial vehicle cluster game

Abstract

The utility model provides an electromagnetic confrontation device applied to a multi-unmanned aerial vehicle cluster game, relates to the field of electromagnetic confrontation devices, and solves the problems that when an existing electromagnetic confrontation device is used, due to the fact that maneuverability of an unmanned aerial vehicle is high, and when the traditional electromagnetic confrontation device is arranged, the maneuverability of the unmanned aerial vehicle is not high. The utility model discloses a confrontation device for an unmanned aerial vehicle, and aims to solve the problems that the confrontation device can be mounted only by manually assembling the confrontation device by virtue of ground personnel, but the confrontation of the unmanned aerial vehicle is influenced due to low assembling efficiency of a traditional bolt fixing mode and the like. The structure of a supporting mechanism, a supporting leg assembly, a side plate assembly, a connecting assembly and a telescopic rod is adopted; and the rapid and stable supporting function of the device under different terrains is achieved. Compared with a traditional assembly mode of fixing through bolts, device deployment can be rapidly completed by unfolding the supporting leg assemblies and adjusting the telescopic rods, the assembly efficiency is greatly improved, the device can cope with rapid maneuvering of the unmanned aerial vehicle in time, and the timeliness of confrontation to the unmanned aerial vehicle is enhanced.

Description

TECHNICAL FIELD

[0001] The utility model belongs to electromagnetic countermeasure device field, especially relate to a kind of electromagnetic countermeasure device applied to multi-unmanned aerial vehicle cluster game. BACKGROUND

[0002] At present, in modern war and some complex security protection scene, multi-unmanned aerial vehicle cluster exhibits strong fighting capacity and application potential by its cooperative combat capability, high mobility and flexibility. However, this also brings serious security challenges. Enemy multi-unmanned aerial vehicle cluster can carry out reconnaissance, attack or interference to key facilities, area, seriously threatens our security and interests.

[0003] However, when the existing electromagnetic countermeasure device is used, due to the strong mobility of unmanned aerial vehicle, the traditional electromagnetic countermeasure device needs to be manually assembled by ground personnel before installation, but the traditional bolt fixing mode has low assembly efficiency, which affects the countermeasure for unmanned aerial vehicle.

[0004] Therefore, in view of the above scheme in actual production and implementation use The defect is corrected, improved, and the spirit and concept of seeking good are followed, and the help of professional knowledge and experience, as well as the trial of many parties, is used to create the utility model, and a kind of electromagnetic countermeasure device applied to multi-unmanned aerial vehicle cluster game is provided, to solve the problem that the existing electromagnetic countermeasure device is used, due to the strong mobility of unmanned aerial vehicle, the traditional electromagnetic countermeasure device needs to be manually assembled by ground personnel before installation, but the traditional bolt fixing mode has low assembly efficiency, which affects the countermeasure for unmanned aerial vehicle. UTILITY MODEL CONTENTS

[0005] The utility model provides a kind of electromagnetic countermeasure device applied to multi-unmanned aerial vehicle cluster game, solve the problem that the existing electromagnetic countermeasure device is used, due to the strong mobility of unmanned aerial vehicle, the traditional electromagnetic countermeasure device needs to be manually assembled by ground personnel before installation, but the traditional bolt fixing mode has low assembly efficiency, which affects the countermeasure for unmanned aerial vehicle.

[0006] The technical scheme of the utility model is realized as follows: a kind of electromagnetic countermeasure device applied to multi-unmanned aerial vehicle cluster game, including support mechanism, the top end surface of the support mechanism is fixedly connected with sleeve assembly, the top end surface of the sleeve assembly is fixedly connected with seat body mechanism;

[0007] The top end of the seat body mechanism is provided with an annular groove, the outer side of the seat body mechanism is fixedly connected with a support plate assembly, the support plate assembly is provided with two parts, the two support plate assemblies are fixedly connected at the left and right sides of the outer circumferential surface of the seat body mechanism, a servo motor A is installed on the bottom end surface of each of the two support plate assemblies, a driving gear is coaxially installed on the top end output shaft of the servo motor A, a guide seat assembly is rotatably connected in the annular groove at the top end of the seat body mechanism, a top opening U-shaped support assembly is fixedly connected to the top end surface of the guide seat assembly, a guide gear assembly in mesh transmission with the driving gear is fixedly connected in an annular array on the outer circumferential surface of the support assembly, a servo motor B is installed on the outer side of the support assembly, an electromagnetic generator is installed on the left side output shaft of the servo motor B, an electromagnetic module, a radar module and a monitoring module are fixedly connected in the front end groove of the electromagnetic generator, the sleeve assembly has a hollow structure, a support leg assembly is hingedly connected in the support mechanism, a guide rod mechanism in a cylindrical structure is inserted into the sleeve assembly, a connecting assembly for counterweight is fixedly connected to the bottom end surface of the guide rod mechanism, a telescopic rod is rotatably connected in the slot in the connecting assembly, and the side of the telescopic rod away from the connecting assembly is hingedly connected with a side plate assembly.

[0008] As a preferred embodiment, the support leg assembly is provided with three parts, and the three support leg assemblies are installed in an annular array on the inner side of the support mechanism.

[0009] As a preferred embodiment, the connecting assembly has a disc-shaped structure.

[0010] As a preferred embodiment, a blocking plate assembly with a circular cross section is fixedly connected to the top end surface of the guide rod mechanism.

[0011] As a preferred embodiment, two side plate assemblies are fixedly connected to the inner side of each of the three support leg assemblies.

[0012] As a preferred embodiment, the blocking plate assembly is used to limit the longitudinal position of the guide rod mechanism in the sleeve assembly.

[0013] After the above technical scheme is used, the beneficial effects of the present application are as follows:

[0014] 1、In the present application, by adopting the structure of the support mechanism, the support leg assembly, the side plate assembly, the connecting assembly and the telescopic rod, the rapid and stable support function of the device under different terrains is realized. Compared with the traditional assembly method relying on bolts, this structure can quickly complete the device deployment by unfolding the support leg assembly and adjusting the telescopic rod, greatly improving the assembly efficiency, so that the device can timely respond to the rapid maneuvering of the unmanned aerial vehicle, and the timeliness of the confrontation with the unmanned aerial vehicle is enhanced.

[0015] 2. The utility model discloses, through adopting the structure combination of seat body mechanism, support plate subassembly, servo motor A, drive gear, guide seat subassembly, support subassembly and guide tooth subassembly, realized electromagnetic countermeasure assembly multi -angle quick adjustment function. Compared with the electromagnetic countermeasure device of traditional fixed angle, this structure can control servo motor A, utilize the angle of gear drive accurate adjustment support subassembly to the direction of quick adjustment electromagnetic generator, electromagnetic module etc. component, improved the adaptability to different direction unmanned aerial vehicle cluster, enhanced the flexibility and effectiveness of electromagnetic countermeasure. BRIEF DESCRIPTION OF DRAWINGS

[0016] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, below will to the drawing needed to use in the embodiment or prior art description simple introduction, obviously, the drawing in the following description only some embodiments of the utility model, for those skilled in the art, under the premise of not paying the creativity labor intensity, can also obtain other drawings according to these drawings.

[0017] Figure 1 It is the front side view structural schematic diagram of the electromagnetic countermeasure device of the utility model after part structure dissection;

[0018] Figure 2 It is the front view structural schematic diagram of the electromagnetic countermeasure device of the utility model;

[0019] Figure 3 It is the connecting assembly and telescopic rod combination structural schematic diagram of the electromagnetic countermeasure device of the utility model;

[0020] Figure 4 It is the overhead view structural schematic diagram of the electromagnetic countermeasure device of the utility model;

[0021] Figure 5 It is the support subassembly and guide tooth subassembly combination structural schematic diagram of the electromagnetic countermeasure device of the utility model;

[0022] Figure 6 It is the left view structural schematic diagram of the electromagnetic countermeasure device of the utility model;

[0023] In the drawing, 1, support mechanism;101, sleeve subassembly;1011, foot subassembly;1012, side plate subassembly;2, guide rod mechanism;201, blocking plate subassembly;2011, connecting assembly;2012, telescopic rod;3, seat body mechanism;301, support plate subassembly;3011, servo motor A;3012, drive gear;3013, guide seat subassembly;3014, support subassembly;3015, guide tooth subassembly;3016, servo motor B;3017, electromagnetic generator;3018, electromagnetic module;3019, radar module;3020, monitoring module. DETAILED DESCRIPTION

[0024] 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.

[0025] like Figures 1-6 As shown, an electromagnetic countermeasure device for multi-drone swarm gaming includes: a support mechanism 1, a sleeve assembly 101 fixedly connected to the top surface of the support mechanism 1, and a base mechanism 3 fixedly connected to the top surface of the sleeve assembly 101.

[0026] The top of the seat mechanism 3 has an annular groove. A support plate assembly 301 is fixedly connected to the outer side of the seat mechanism 3. There are two support plate assemblies 301, fixedly connected to the left and right sides of the outer circumference of the seat mechanism 3 respectively. A servo motor A3011 is mounted on the bottom surface of each support plate assembly 301. A drive gear 3012 is coaxially mounted on the top output shaft of the servo motor A3011. A guide seat assembly 3013 is rotatably connected inside the annular groove at the top of the seat mechanism 3. A U-shaped support assembly 3014 with a top opening is fixedly connected to the top surface of the guide seat assembly 3013. Guide gear assemblies 3015, meshing with the drive gear 3012, are fixedly connected in a circular array on the outer circumference of the support assembly 3014. A servo motor B3016 is installed on the outside of 014. An electromagnetic generator 3017 is installed on the left output shaft of the servo motor B3016. An electromagnetic module 3018, a radar module 3019, and a monitoring module 3020 are fixedly connected inside the front groove of the electromagnetic generator 3017. The sleeve assembly 101 has an internal hollow structure. A support leg assembly 10111 is hinged inside the support mechanism 1. A cylindrical guide rod mechanism 2 is inserted inside the sleeve assembly 101. A connecting assembly 2011 for counterweight is fixedly connected to the bottom end face of the guide rod mechanism 2. A telescopic rod 2012 is rotatably connected inside the notch opened in the connecting assembly 2011. The side of the telescopic rod 2012 away from the connecting assembly 2011 is hinged to the side plate assembly 1012.

[0027] Among them, there are three support leg components 10111, which are arranged in a ring array and installed on the inner side of the support mechanism 1. The connecting component 2011 has a disc-shaped structure.

[0028] The top end surface of the guide rod mechanism 2 is fixedly connected with a blocking plate assembly 201 with a circular cross section, and the inner side of each of the three supporting leg assemblies 1011 is fixedly connected with two side plate assemblies 1012 in opposition, and the blocking plate assembly 201 is used to limit the longitudinal position of the guide rod mechanism 2 in the sleeve assembly 101.

[0029] In use, when the electromagnetic countermeasure device needs to be used, first place the supporting mechanism 1 at a suitable position, and expand the three supporting leg assemblies 10111 that are hingedly and annularly arranged inside the supporting mechanism 1 to provide stable support for the entire device, and the side plate assemblies 1012 fixedly connected to the inner side of the supporting leg assemblies 10111 can assist in stabilizing the supporting legs and enhancing the stability of the support, and at the same time, the guide rod mechanism 2 inserted into the sleeve assembly 101, with the telescopic rod 2012 in the bottom end connecting assembly 2011 hingedly connected to the side plate assembly 1012, can further adjust the supporting structure by adjusting the length of the telescopic rod 2012 to adapt to different terrains and ensure the stability of the device.

[0030] Then when the angle of the electromagnetic countermeasure assembly needs to be adjusted, start the servo motor A3011 at the bottom end of the two supporting plate assemblies 301, and the output shaft at the top end drives the driving gear 3012 to rotate, since the guide tooth assembly 3015 is in meshing transmission with the driving gear 3012 and the guide tooth assembly 3015 is fixed in an annular array on the outer peripheral surface of the supporting assembly 3014, the supporting assembly 3014 will rotate on the guide seat assembly 3013 in the annular groove at the top end of the seat body mechanism 3, thereby achieving adjustment of the overall angle of the electromagnetic generator 3017, the electromagnetic module 3018, the radar module 3019 and the monitoring module 3020, so that they can be aligned in the direction of the target UAV cluster.

[0031] When the target direction is determined, start the servo motor B3016, and the left output shaft drives the electromagnetic generator 3017 to rotate to adjust the emission angle of the electromagnetic generator 3017, and the electromagnetic module 3018 starts to work to emit electromagnetic signals of specific frequency and intensity to interfere with the communication, navigation and other systems of the enemy UAV cluster, the radar module 3019 continuously scans and monitors the target area to obtain real-time information such as the position, speed and flight attitude of the UAV cluster, and transmits the data to the monitoring module 3020, and the monitoring module 3020 analyzes and processes the data and feeds back the analysis results to the operator or cooperates with other systems to adjust the electromagnetic countermeasure strategy in a timely manner.

[0032] During the operation of the device, the blocking plate assembly 201 fixed at the top end of the guide rod mechanism 2 limits the longitudinal position of the guide rod mechanism 2 in the sleeve assembly 101 to prevent excessive displacement of the guide rod mechanism 2 due to external force or vibration and other factors, and to ensure the stability of the overall structure of the device and the continuous and stable operation of the electromagnetic countermeasure operation.

[0033] The above merely describes the preferred embodiments of the present application, and is not intended to limit the present application, and any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. An electromagnetic countermeasure device for multi-UAV swarm gaming, comprising a support mechanism (1), wherein a sleeve assembly (101) is fixedly connected to the top surface of the support mechanism (1), characterized in that, A seat mechanism (3) is fixedly connected to the top surface of the sleeve assembly (101). The top of the seat mechanism (3) is provided with an annular groove. A support plate assembly (301) is fixedly connected to the outer side of the seat mechanism (3). There are two support plate assemblies (301). The two support plate assemblies (301) are fixedly connected to the left and right sides of the outer circumference of the seat mechanism (3). A servo motor A (3011) is installed on the bottom end surface of the two support plate assemblies (3011). A drive gear (3012) is coaxially installed on the top output shaft of the servo motor A (3011). A guide seat assembly (3013) is rotatably connected inside the annular groove at the top of the seat mechanism (3). A U-shaped support assembly (3014) with a top opening is fixedly connected to the top surface of the guide seat assembly (3013). A guide gear assembly (3015) that meshes with the drive gear (3012) is fixedly connected in an annular array on the outer circumference of the support assembly (3014). A servo motor B (3016) is installed on the outside. An electromagnetic generator (3017) is installed on the left output shaft of the servo motor B (3016). An electromagnetic module (3018), a radar module (3019), and a monitoring module (3020) are fixedly connected inside the front groove of the electromagnetic generator (3017). The sleeve assembly (101) has an internal hollow structure. A support leg assembly (1011) is hinged inside the support mechanism (1). A cylindrical guide rod mechanism (2) is inserted inside the sleeve assembly (101). A connecting assembly (2011) for counterweight is fixedly connected to the bottom end face of the guide rod mechanism (2). A telescopic rod (2012) is rotatably connected inside the notch opened in the connecting assembly (2011). The side of the telescopic rod (2012) away from the connecting assembly (2011) is hinged to the side plate assembly (1012).

2. The electromagnetic countermeasure device for multi-UAV swarm gaming as described in claim 1, characterized in that, The support leg assembly (1011) is provided in three places, and the three support leg assemblies (1011) are installed in a ring array on the inner side of the support mechanism (1).

3. The electromagnetic countermeasure device for multi-UAV swarm gaming as described in claim 1, characterized in that, The connecting component (2011) has a disc-shaped structure.

4. The electromagnetic countermeasure device for multi-UAV swarm gaming as described in claim 1, characterized in that, The guide rod mechanism (2) has a circular cross-section baffle assembly (201) fixedly connected to its top surface.

5. The electromagnetic countermeasure device for multi-UAV swarm gaming according to claim 1, characterized in that, The inner sides of the three support leg assemblies (1011) are fixedly connected to two side plate assemblies (1012) in opposite directions.

6. The electromagnetic countermeasure device for multi-UAV swarm gaming according to claim 4, characterized in that, The baffle assembly (201) is used to limit the longitudinal position of the guide rod mechanism (2) in the sleeve assembly (101).

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