CN210323356U - Anti-unmanned aerial vehicle radar slewing mechanism - Google Patents
Anti-unmanned aerial vehicle radar slewing mechanism Download PDFInfo
- Publication number
- CN210323356U CN210323356U CN201920777176.6U CN201920777176U CN210323356U CN 210323356 U CN210323356 U CN 210323356U CN 201920777176 U CN201920777176 U CN 201920777176U CN 210323356 U CN210323356 U CN 210323356U
- Authority
- CN
- China
- Prior art keywords
- shell
- unmanned aerial
- mounting plate
- aerial vehicle
- lower shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Details Of Aerials (AREA)
Abstract
The utility model discloses an anti-unmanned aerial vehicle radar slewing mechanism, include: the device comprises a shell, a receiving antenna, an electromagnetic wave transmitter, a signal control processing unit, a power supply, a camera device and a supporting structure, wherein the supporting structure is provided with the shell and the camera device, and the camera device is embedded in the shell; the shell is composed of an upper shell and a lower shell, wherein the upper shell and the lower shell are of groove structures, and the upper shell and the lower shell are buckled to form a cavity structure; a mounting substrate is arranged at the opening of the upper shell, wherein a receiving antenna is arranged on the mounting substrate; an electromagnetic wave transmitter, a signal control processing unit and a power supply are arranged in the lower shell, and a power supply interface is arranged on one side of the lower shell; and the bottom of the lower shell is provided with a shell connecting plate. The utility model discloses an unmanned aerial vehicle to air flight detects, and adjustment camera device's position carries out real-time snapshot to the unmanned aerial vehicle of control flight, improves the reliability that detects.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to anti-unmanned aerial vehicle radar slewing mechanism.
Background
Drones are unmanned aerial vehicles that are operated by radio remote sensing devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an on-board computer. The unmanned aerial vehicle has wide application, low cost and higher efficiency; no casualty risk; the life ability is strong, the maneuverability is good, the use is convenient, the device plays an extremely important role in modern war and has a wider prospect in the civil field. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft.
Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Along with the rapid development of the unmanned aerial vehicle industry, civil irregular unmanned aerial vehicle flies to cause great potential safety hazard to public safety, so the anti-unmanned aerial vehicle industry that suits with it also develops rapidly. Anti-unmanned aerial vehicle means through technical means and equipment, controls consumer level unmanned aerial vehicle. Generally, anti-unmanned aerial vehicle monitoring device is mostly for surveying discovery, tracking identification, decision-making judgement, a link process of counterattack, through giving background monitor center with detected signal transmission, judges whether unmanned aerial vehicle invades from this, but because aerial other objects flight in addition, only rely on radar electromagnetic signal to judge, causes the erroneous judgement easily, has reduced the reliability that detects.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that to the not enough among the above-mentioned prior art, disclose an anti-unmanned aerial vehicle radar slewing mechanism, monitor the unmanned aerial vehicle of invasion, reach the early warning and for later stage interference and expulsion provide information.
The utility model adopts the technical proposal that: an anti-drone radar slewing mechanism comprising:
the device comprises a shell, a receiving antenna, an electromagnetic wave transmitter, a signal control processing unit, a power supply, a camera device and a supporting structure;
the supporting structure is provided with a shell and a camera device, and the camera device is embedded in the shell;
the shell is composed of an upper shell and a lower shell, wherein the upper shell and the lower shell are of groove structures, and the upper shell and the lower shell are buckled to form a cavity structure;
a mounting substrate is arranged at the opening of the upper shell, wherein a receiving antenna is arranged on the mounting substrate;
an electromagnetic wave transmitter, a signal control processing unit and a power supply are arranged in the lower shell, and a power supply interface is arranged on one side of the lower shell; and the bottom of the lower shell is provided with a shell connecting plate.
As a further technical solution of the utility model is: the utility model discloses a casing, including epitheca opening part, first mount table, second mounting panel, first mount table and second mounting panel, the epitheca opening part outside sets up first mount table, set up first mounting panel on the first mount table, the inferior valve opening part outside sets up the second mount table, set up the second mounting panel on the second mount table, the second mount table corresponds the position with first mounting panel and sets up the second recess, first mount table corresponds the position with the second mounting panel and sets up first recess.
As a further technical solution of the utility model is: and sealing rings are arranged around the first groove and the second groove.
As a further technical solution of the utility model is: the supporting structure comprises a base, an upright post, a horizontal rotating mechanism and a pitch angle rotating mechanism; the stand sets up the top at the base, set up horizontal slewing mechanism and pitch angle slewing mechanism on the stand.
As a further technical solution of the utility model is: the horizontal rotating mechanism comprises a first motor, a speed reducer, a coupler, a first gear, a second gear and a first rotating shaft;
the output end of the first motor is connected with a speed reducer, the output end of the speed reducer is connected with a coupler, a first gear is fixedly arranged at the end part of the coupler and is meshed with a second gear, the second gear is arranged on the outer side of the first rotating shaft and is fixedly connected with the first rotating shaft,
as a further technical solution of the utility model is: the pitch angle rotating mechanism comprises a second motor, a worm wheel and a second rotating shaft;
the output end of the second motor is connected with a worm, the worm is meshed with a worm wheel, the worm wheel is fixedly connected with a second rotating shaft, and the second rotating shaft is connected with the shell connecting plate.
As a further technical solution of the utility model is: the power supply adopts a lithium battery.
Compared with the prior art, the utility model has the following advantage:
1. the utility model discloses electromagnetic wave transmitter in the shell passes through the transmitting antenna and outwards launches the electromagnetic wave, through scanning the detection area comprehensively, when having detected unmanned aerial vehicle, receiving antenna receives electromagnetic wave reflection signal and calculates the distance, speed and the direction that obtain unmanned aerial vehicle according to the Doppler to this reflection electromagnetic wave signal through signal control processing unit, generates control signal from this and controls slewing mechanism, adjusts camera device's position, carries out the candid photograph to the unmanned aerial vehicle that gets into the shooting region.
2. The first mounting platform and the second mounting platform that set up on the shell for the equipment is convenient, can assemble the shaping, simple to operate with epitheca and inferior valve lock through first mounting panel and second mounting panel.
3. The waterproof and rainproof functions of the shell are realized by arranging the sealing ring, so that electronic equipment inside the shell is protected.
4. Set up horizontal slewing mechanism and pitch angle slewing mechanism on the bearing structure, through the unmanned aerial vehicle locating information that signal control processing unit produced, drive horizontal slewing mechanism and pitch angle slewing mechanism drive the shell and rotate, make the camera device that sets up on it aim at unmanned aerial vehicle direction position and shoot, acquire unmanned aerial vehicle picture information.
Drawings
Fig. 1 is a structural diagram of a radar rotating mechanism of an anti-unmanned aerial vehicle provided by the utility model;
fig. 2 is an enlarged view of the housing portion separating structure according to the present invention.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings of the embodiments of the present invention are combined to clearly and completely describe the technical solutions of the embodiments of the present invention, and obviously, the described embodiments are some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise. Unless expressly stated or limited otherwise, the terms "mounted," "connected," "secured," and the like are intended to be inclusive and mean that, for example, they may be fixedly connected or detachably connected or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
Referring to fig. 1 and fig. 2, fig. 1 is a structural diagram of a radar rotating mechanism of an anti-unmanned aerial vehicle according to the present invention; fig. 2 is an enlarged view of the housing portion separating structure according to the present invention.
Example one
As shown in fig. 1 and 2, an anti-drone radar slewing mechanism includes:
the device comprises a shell 1, a receiving antenna 2, an electromagnetic wave transmitter 3, a signal control processing unit 4, a power supply 5, a camera device 6 and a supporting structure 7;
the supporting structure 7 is provided with a shell 1 and a camera device 2, and the camera device 2 is embedded in the shell 1;
the shell 1 is composed of an upper shell 11 and a lower shell 12, wherein the upper shell 11 and the lower shell 12 are groove structures, and the upper shell 11 and the lower shell 12 are buckled to form a cavity structure;
a mounting substrate 111 is arranged at an opening of the upper shell 11, wherein a receiving antenna 2 is arranged on the mounting substrate 111;
the electromagnetic wave transmitter 3, the signal control processing unit 4 and the power supply 5 are arranged in the lower shell 12, and the power supply interface 121 is arranged on one side of the lower shell 12; the bottom of the lower case 12 is provided with a case coupling plate 13.
The embodiment of the utility model provides an in, electromagnetic wave transmitter in the shell launches the electromagnetic wave to the outside, unmanned aerial vehicle through flying in the air detects, when having detected unmanned aerial vehicle, receiving antenna receives electromagnetic wave reflection signal and calculates the distance that obtains unmanned aerial vehicle according to the Doppler to this reflection electromagnetic wave signal through signal control processing unit, speed and direction, it controls slewing mechanism to generate control signal from this, the camera is unanimous with radar received signal direction, the week is rotated, realize the auxiliary image detection function through the camera, the camera adopts the high magnification camera lens, automatic focusing can be realized, take a candid photograph unmanned aerial vehicle to the discovery.
Example two
In this embodiment, the structure of the upper shell and the lower shell is explained on the basis of the first embodiment, specifically: a first mounting table 112 is arranged on the outer side of the opening of the upper shell 11, a first mounting plate 113 is arranged on the first mounting table 112, a second mounting table 121 is arranged on the outer side of the opening of the lower shell 12, a second mounting plate 122 is arranged on the second mounting table 121, a second groove 122 is arranged on the second mounting table 121 corresponding to the first mounting plate 113, and a first groove 114 is arranged on the first mounting table 112 corresponding to the second mounting plate 122;
the first mounting platform and the second mounting platform that set up on the shell for the equipment is convenient, can assemble the shaping, simple to operate with epitheca and inferior valve lock through first mounting panel and second mounting panel.
EXAMPLE III
Because this anti-unmanned aerial vehicle radar installations is installed in outdoor open air environment, in order to avoid the rainwater to radar installations's damage, this embodiment explains the shell structure on the basis of embodiment two, specifically is: sealing rings are arranged around the first groove 113 and the second groove 122. The waterproof and rainproof functions of the shell are realized by arranging the sealing ring, so that electronic equipment inside the shell is protected.
Example four
In the present embodiment, the structure of the upper shell and the lower shell is explained based on the first embodiment, in the present embodiment, the supporting structure 7 includes a base 71, a column 72, a horizontal rotation mechanism 73, and a pitch rotation mechanism 74; the column 72 is disposed above the base 71, and the horizontal rotation mechanism 73 and the pitch rotation mechanism 74 are provided on the column 72.
The horizontal rotation mechanism 73 includes a first motor 731, a reducer 732, a coupling 733, a first gear 734, a second gear 735, and a first rotation shaft 736; the output end of the first motor 721 is connected with a speed reducer 732, the output end of the speed reducer 732 is connected with a coupling 733, the end of the coupling 733 is fixedly provided with a first gear 734, the first gear 734 is meshed with a second gear 735, the second gear 735 is installed on the outer side of the first rotating shaft 736 and is fixedly connected with the first rotating shaft 736,
the pitch angle rotation mechanism 74 includes a second motor 741, a worm 742, a worm wheel 743, and a second rotation shaft 744; the output end of the second motor 741 is connected to a worm 742, the worm 742 is engaged with a worm wheel 743, the worm wheel 743 is fixedly connected to a second rotating shaft 744, and the second rotating shaft 744 is connected to the housing connecting plate 13.
In this embodiment, set up horizontal slewing mechanism and pitch angle slewing mechanism on the bearing structure, through the unmanned aerial vehicle locating information that signal control processing unit produced, drive horizontal slewing mechanism and pitch angle slewing mechanism drive the shell and rotate, make the camera device that sets up on it aim at unmanned aerial vehicle direction position and shoot, acquire unmanned aerial vehicle picture information.
In the embodiment, the first motor is arranged to drive the first gear and the second gear to rotate so as to realize horizontal rotation of the shell, and the second motor is arranged to drive the worm gear to drive the pitch angle of the shell to adjust, wherein the horizontal rotation angle is 0-360 degrees, and the pitch angle rotation angle is 0-90 degrees.
In this embodiment, power 5 adopts the lithium cell, can charge through power source, and the circuit of power supply to first motor and second motor all sets up inside the pole setting, installs the cable inside the pole setting, prevents that the cable from exposing, protects the life of cable.
While the preferred embodiments of the present invention have been described in detail, the present invention is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art.
Many other changes and modifications can be made without departing from the spirit and scope of the invention. It is to be understood that the invention is not to be limited to the specific embodiments, but only by the scope of the appended claims.
Claims (7)
1. An anti-unmanned aerial vehicle radar slewing mechanism, its characterized in that includes: the device comprises a shell, a receiving antenna, an electromagnetic wave transmitter, a signal control processing unit, a power supply, a camera device and a supporting structure;
the supporting structure is provided with a shell and a camera device, and the camera device is embedded in the shell;
the shell is composed of an upper shell and a lower shell, wherein the upper shell and the lower shell are of groove structures, and the upper shell and the lower shell are buckled to form a cavity structure;
a mounting substrate is arranged at the opening of the upper shell, wherein a receiving antenna is arranged on the mounting substrate;
an electromagnetic wave transmitter, a signal control processing unit and a power supply are arranged in the lower shell, and a power supply interface is arranged on one side of the lower shell; and the bottom of the lower shell is provided with a shell connecting plate.
2. The anti-unmanned aerial vehicle radar slewing mechanism of claim 1, characterized in that, a first mounting plate is arranged outside the upper shell opening, a first mounting plate is arranged on the first mounting plate, a second mounting plate is arranged outside the lower shell opening, a second mounting plate is arranged on the second mounting plate, a second groove is arranged at a position of the second mounting plate corresponding to the first mounting plate, and a first groove is arranged at a position of the first mounting plate corresponding to the second mounting plate.
3. An anti-drone radar rotation mechanism according to claim 2, characterised in that sealing rings are provided around the first and second grooves.
4. The anti-drone radar rotation mechanism of claim 1, wherein the support structure includes a base, a column, a horizontal rotation mechanism, and a pitch rotation mechanism; the stand sets up the top at the base, set up horizontal slewing mechanism and pitch angle slewing mechanism on the stand.
5. The anti-drone radar rotation mechanism of claim 4, wherein the horizontal rotation mechanism includes a first motor, a reducer, a coupler, a first gear, a second gear, a first shaft;
the output end of the first motor is connected with the speed reducer, the output end of the speed reducer is connected with the coupler, a first gear is fixedly arranged at the end part of the coupler and meshed with a second gear, and the second gear is installed on the outer side of the first rotating shaft and fixedly connected with the first rotating shaft.
6. The anti-drone radar rotation mechanism of claim 4, wherein the pitch angle rotation mechanism includes a second motor, a worm gear, and a second shaft;
the output end of the second motor is connected with a worm, the worm is meshed with a worm wheel, the worm wheel is fixedly connected with a second rotating shaft, and the second rotating shaft is connected with the shell connecting plate.
7. The anti-drone radar rotation mechanism of claim 1, wherein the power source is a lithium battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920777176.6U CN210323356U (en) | 2019-05-27 | 2019-05-27 | Anti-unmanned aerial vehicle radar slewing mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920777176.6U CN210323356U (en) | 2019-05-27 | 2019-05-27 | Anti-unmanned aerial vehicle radar slewing mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210323356U true CN210323356U (en) | 2020-04-14 |
Family
ID=70140798
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920777176.6U Active CN210323356U (en) | 2019-05-27 | 2019-05-27 | Anti-unmanned aerial vehicle radar slewing mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210323356U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113922917A (en) * | 2021-09-02 | 2022-01-11 | 苏州华诺贝斯技术有限公司 | Unmanned aerial vehicle countercheck device with sensing, monitoring and early warning functions and countercheck method thereof |
-
2019
- 2019-05-27 CN CN201920777176.6U patent/CN210323356U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113922917A (en) * | 2021-09-02 | 2022-01-11 | 苏州华诺贝斯技术有限公司 | Unmanned aerial vehicle countercheck device with sensing, monitoring and early warning functions and countercheck method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3452881B1 (en) | Imaging using multiple unmanned aerial vehicles | |
| US10364044B2 (en) | Combined information for object detection and avoidance | |
| US20160286128A1 (en) | Amphibious vtol super drone camera in a mobile case (phone case) with multiple aerial and aquatic flight modes for capturing panoramic virtual reality views, selfie and interactive video | |
| CN209910515U (en) | Portable anti-unmanned aerial vehicle equipment suitable for campus airspace | |
| US20150232181A1 (en) | Helicopter with multi-rotors and wireless capability | |
| CN112606899A (en) | Chassis, chassis control system and chassis control method | |
| US11721222B2 (en) | Ruggedized autonomous helicopter platform | |
| CN210323356U (en) | Anti-unmanned aerial vehicle radar slewing mechanism | |
| CN107942348B (en) | Road law enforcement system based on unmanned aerial vehicle and robot technique | |
| CN108803633A (en) | A kind of unmanned plane low latitude monitoring system based on mobile communications network | |
| CN108082478B (en) | Early warning type unmanned aerial vehicle monitoring and investigation system | |
| RU2723201C1 (en) | Aircraft-type unmanned aerial vehicle for detection of missing person | |
| CN201334116Y (en) | Hovering police reconnaissance flight vehicle with infra-red range measuring function | |
| WO2017208199A1 (en) | Amphibious vtol super drone camera in mobile case (phone case) with multiple aerial and aquatic flight modes for capturing panoramic virtual reality views, selfie and interactwe video | |
| CN210179228U (en) | Detection device for finding, identifying and early warning unmanned aerial vehicle | |
| CN208165258U (en) | A kind of AGV unmanned plane of laser radar positioning function | |
| US20220238987A1 (en) | Mobile surveillance systems extendable mast control systems and methods | |
| CN214890319U (en) | Tripod head of three-light ball machine | |
| CN214057847U (en) | Surface of water environmental monitoring unmanned aerial vehicle that cruises | |
| KR102334831B1 (en) | Image map making system | |
| CN212685907U (en) | Survey and drawing unmanned aerial vehicle with protector | |
| CN205017462U (en) | Panorama is kept watch on and is used unmanned aerial vehicle | |
| CN214174919U (en) | A rotor unmanned aerial vehicle cluster system for burning explodes calamity early warning and processing | |
| CN213168584U (en) | Unmanned aerial vehicle investigation recognition device | |
| CN210310919U (en) | Unmanned aerial vehicle system with parachute safety arrangement |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |