CN108569393A - A kind of Multifunctional pre-warning counter unmanned plane - Google Patents
A kind of Multifunctional pre-warning counter unmanned plane Download PDFInfo
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- CN108569393A CN108569393A CN201710142366.6A CN201710142366A CN108569393A CN 108569393 A CN108569393 A CN 108569393A CN 201710142366 A CN201710142366 A CN 201710142366A CN 108569393 A CN108569393 A CN 108569393A
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- control box
- microcomputerized controllers
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- plc microcomputerized
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- 239000011248 coating agent Substances 0.000 claims abstract description 4
- 238000000576 coating method Methods 0.000 claims abstract description 4
- 239000002184 metal Substances 0.000 claims abstract description 4
- 238000004891 communication Methods 0.000 claims description 10
- 238000005516 engineering process Methods 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000003245 working effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/60—Jamming involving special techniques
- H04K3/62—Jamming involving special techniques by exposing communication, processing or storing systems to electromagnetic wave radiation, e.g. causing disturbance, disruption or damage of electronic circuits, or causing external injection of faults in the information
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/181—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K2203/00—Jamming of communication; Countermeasures
- H04K2203/10—Jamming or countermeasure used for a particular application
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Signal Processing (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Computer Networks & Wireless Communication (AREA)
- Multimedia (AREA)
- Remote Sensing (AREA)
- Emergency Alarm Devices (AREA)
Abstract
The invention discloses a kind of Multifunctional pre-warnings to break through unmanned plane, including crossbearer and control box, and crossbearer surface is coated with wear-resistant coating, crossbearer top is equipped with supporting rack, crossbearer is welded with supporting rack, and supporting rack is bolted to connection with control box, control box top is provided with the connecting plate of metal, connecting plate top is equipped with loop bar, loop bar top is equipped with strut, strut is flexibly connected with loop bar, strut top is provided with motor cabinet, motor cabinet is welded with strut, motor cabinet top is provided with motor, motor top is equipped with propeller, accumulator is installed inside control box, accumulator side is equipped with PLC microcomputerized controllers, PLC microcomputerized controllers are electrically connected with motor；PLC microcomputerized controllers side is equipped with take photo by plane camera and infrared camera, and take photo by plane camera and infrared camera are electrically connected with PLC microcomputerized controllers；Accumulator side is equipped with suppressor, and suppressor is electrically connected with PLC microcomputerized controllers.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of Multifunctional pre-warning breaks through unmanned plane.
Background technology
Unmanned plane has been used in life every aspect at present, even improve quality, aspect people life for us；And
Nearly more than 30 years have been developed in domestic unmanned plane market, and consumer field is gradually expanded to from initial military domain.Domestic and international nothing
Man-machine the relevant technologies rapid development, UAV system type is various, the wide distinct characteristics of purposes, causes it in size, quality, boat
Journey, endurance, flying height, flying speed, task dispatching various aspects have larger difference.Due to the diversity of unmanned plane, for not
Same considering has different sorting techniques：By flying platform configuration classify, unmanned plane can be divided into fixed-wing unmanned plane, rotor without
Man-machine, unmanned airship, umbrella wing unmanned plane, flapping wing unmanned plane etc..Unmanned plane generally all has a single function at present, can only give certain some ring
Border individually services, and especially near airport, since weather changes at any time, birds fly and more caused seriously to aircraft flight wantonly
It influences, it is huge additionally, due to inlet flow rate, it is easy to unexpected fire is caused, is increased additionally, due to unmanned plane, enemy's unmanned plane
It may threaten, interfere to us, therefore, we should wait if necessary sanctions enemy plane, can be allowed by breaking through enemy plane
Enemy is feared, so, we are badly in need of unmanned plane that is a kind of multi-functional and can breaking through enemy plane and escort for us.
So how to design a kind of Multifunctional pre-warning counter unmanned plane, becoming us will currently solve the problems, such as.
Invention content
The purpose of the present invention is to provide a kind of Multifunctional pre-warnings to break through unmanned plane, to solve to propose in above-mentioned background technology
Unmanned plane the problem of easily being interfered.
To achieve the above object, the present invention provides the following technical solutions：
A kind of Multifunctional pre-warning counter unmanned plane, including crossbearer and control box, and the crossbearer surface is coated with wear-resistant coating,
It is characterized in that：The crossbearer top is equipped with supporting rack, and the crossbearer is welded with supporting rack, and support frame as described above and control box
It is bolted to connection, the control box top is provided with the connecting plate of metal, and the connecting plate top is equipped with loop bar, institute
State loop bar top and strut be installed, the strut is flexibly connected with loop bar, and strut top is provided with motor cabinet, the motor cabinet with
Strut welds, and the motor cabinet top is provided with motor, and the motor top is equipped with propeller, is arranged inside the connecting plate
There is rivet, accumulator is installed inside the control box, the accumulator side is equipped with PLC microcomputerized controllers, and the PLC is micro-
Machine controller is electrically connected with motor；
PLC microcomputerized controllers side is equipped with take photo by plane camera and infrared camera, the camera and red of taking photo by plane
Outer camera is electrically connected with PLC microcomputerized controllers, and PLC microcomputerized controllers are collected and analyze take photo by plane camera and infrared photography
The collected data of head institute；
The accumulator side is equipped with suppressor, and the PLC microcomputerized controllers send according to its analysis result and instruct
To suppressor, its working condition is controlled.
Further, PLC microcomputerized controllers side is equipped with GPS locator, and the PLC microcomputerized controllers are by its point
Analysis result is sent to GPS locator, and the GPS locator carries out analyzing and positioning, and location information is fed back to the PLC microcomputers
Controller is equipped with offline mode controller, the letter that PLC microcomputerized controllers are fed back according to GPS locator inside the control box
Cease to send to offline mode controller and instruct, the offline mode controller receive the instructions of the PLC microcomputerized controllers into
And control the operating status of motor.
Further, the control box top is equipped with wireless communication module, and the wireless communication module and the PLC are micro-
Machine controller signal connects, and is used for and ground staff's information exchange.
Further, the wireless communication module side is equipped with counter electromagnetic device, and the PLC microcomputerized controllers are according to it
Analysis result sends instruction to counter electromagnetic device, and controls the operating status of counter electromagnetic device.
Compared with prior art, the beneficial effects of the invention are as follows：This kind of intelligent early-warning counter unmanned plane be provided with high definition and
The comprehensive shooting specific region of infrared camera, provides exact information, routine use can be used for surrounding for ground control
Early warning is shot, by concentrating different function combination that can complete multiple-task；In addition, again can place is right by suppressor
Our interference eliminations break through the use of electromagnetic device to protect oneself, can break through some enemy planes, reduce the threat to us, lead to
This upgrading is crossed, different task requirement can be completed, substantially met demand not of the same race.
Description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is local control box's structural schematic diagram of the present invention；
In figure：1- crossbearers；2- supporting racks；3- motor cabinets；4- struts；5- loop bars；6- motors；7- propellers；8- channel radios
Interrogate module；9- breaks through electromagnetic device；10- rivets；11- connecting plates；12- control box；13- accumulators；14- takes photo by plane camera；17- flies
Row mode controller；18-GPS locators；19-PLC microcomputerized controllers；20- infrared cameras；21- suppressors.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of Multifunctional pre-warning counter unmanned plane, including crossbearer 1
With control box 12, and 1 surface of the crossbearer is coated with wear-resistant coating, it is characterised in that：1 top of the crossbearer is equipped with supporting rack 2,
The crossbearer 1 is welded with supporting rack 2, and support frame as described above 2 is bolted to connection with control box 12, and the control box 12 is pushed up
End is provided with the connecting plate 11 of metal, and 11 top of the connecting plate is equipped with loop bar 5, and 5 top of the loop bar is equipped with strut 4,
The strut 4 is flexibly connected with loop bar 5, and 4 top of strut is provided with motor cabinet 3, and the motor cabinet 3 is welded with strut 4, the electricity
3 top of engine base is provided with motor 6, and 6 top of the motor is equipped with propeller 7, and the connecting plate 11 is internally provided with rivet 10,
Accumulator 13 is installed, 13 side of the accumulator is equipped with PLC microcomputerized controllers 19, the PLC inside the control box 12
Microcomputerized controller 19 is electrically connected with motor 6；
19 side of PLC microcomputerized controllers is equipped with take photo by plane camera 14 and infrared camera 20, the camera shooting of taking photo by plane
First 14 and infrared camera 20 be electrically connected with PLC microcomputerized controllers 19, PLC microcomputerized controllers 19 are collected and analyze to take photo by plane and take the photograph
As 20 collected data of head 14 and infrared camera；
13 side of the accumulator is equipped with suppressor 21, and the PLC microcomputerized controllers 19 are sent out according to its analysis result
It send instruction to suppressor 21, controls its working condition.When the analysis of PLC microcomputerized controllers 19 determines the camera 14 and infrared of taking photo by plane
When the data that the equipment such as camera 20 are acquired are unfavorable to us, PLC microcomputerized controllers 19 send out signal control suppressor work
Make, avoids interference unmanned plane normal work.
Further, 19 side of PLC microcomputerized controllers is equipped with GPS locator 18, the PLC microcomputerized controllers 19
Its analysis result is sent to GPS locator 18, the GPS locator 18 carries out analyzing and positioning, and location information is fed back to
The PLC microcomputerized controllers 19 are equipped with offline mode controller 17, PLC microcomputerized controllers 19 inside the control box 12
It sends and instructs to offline mode controller 17 according to 18 feedack of GPS locator, the offline mode controller 17 receives
The instruction of the PLC microcomputerized controllers 19 and then the operating status for controlling motor 6.It can be accurately to barrier using GPS locator 18
Object etc. is hindered to be positioned, so that PLC microcomputerized controllers 19 control other component workings, and control offline mode controller 17 is adjusted
The offline mode of whole unmanned plane.
For ease of with ground carry out information exchange, and convenient for ground handling operator control unmanned plane various actions, institute
It states 12 top of control box and wireless communication module 8, the wireless communication module 8 and 19 signal of PLC microcomputerized controllers is installed
Connection is used for and ground staff's information exchange.8 side of the wireless communication module is equipped with counter electromagnetic device 9, the counter electricity
Chinaware 9 is connect with 19 signal of PLC microcomputerized controllers.When being broken through, the controllable counter of PLC microcomputerized controllers 19
Electromagnetic device 9 works, and generates interference wave.
Operation principle：First, fully charged to accumulator 13, it is full to control 6 rotating speed of each motor using PLC microcomputerized controllers 19
Foot flight needs, and by 14 captured in real-time ground of camera of taking photo by plane, can be detected using infrared camera 20 and be blocked by barrier
Region, secondly can utilize take photo by plane camera 14 and take photo by plane camera 14 acquire information, be transmitted to PLC microcomputerized controllers 19,
It can be positioned, then analyzed by PLC microcomputerized controllers 19, then result is fed back to wireless telecommunications in real time by GPS locator 18
Module 8, wireless communication module 8 can filter by suppressor 21 with ground staff's information exchange, shield enemy nobody
Machine or the interference wave of other equipment transmitting with our aircraft of protection, the analysis of PLC microcomputerized controllers 19 obtain whether be enemy nobody
Then consequential signal is transferred to counter electromagnetic device 9 by machine, the counter transmitting interference wave of electromagnetic device 9 breaks through enemy plane, meanwhile, by PLC
Microcomputerized controller 19 analyzes 18 signal of GPS locator, can change the unmanned plane work using offline mode controller 17
Operation mode and offline mode meet basic requirement by arrangement above.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (4)
1. a kind of Multifunctional pre-warning breaks through unmanned plane, including crossbearer (1) and control box (12), and the crossbearer (1) surface is coated with
Wear-resistant coating, it is characterised in that：Crossbearer (1) top is equipped with supporting rack (2), and the crossbearer (1) is welded with supporting rack (2)
It connects, and support frame as described above (2) is bolted to connection with control box (12), control box (12) top is provided with metal
Connecting plate (11), connecting plate (11) top are equipped with loop bar (5), and loop bar (5) top is equipped with strut (4), described
Strut (4) is flexibly connected with loop bar (5), and strut (4) top is provided with motor cabinet (3), and the motor cabinet (3) is welded with strut (4)
It connects, motor cabinet (3) top is provided with motor (6), and motor (6) top is equipped with propeller (7), the connecting plate
(11) it is internally provided with rivet (10), accumulator (13), accumulator (13) side are installed inside the control box (12)
PLC microcomputerized controllers (19) are installed, the PLC microcomputerized controllers (19) are electrically connected with motor (6)；
PLC microcomputerized controllers (19) side is equipped with camera of taking photo by plane (14) and infrared camera (20), and described take photo by plane is taken the photograph
Picture head (14) and infrared camera (20) are electrically connected with PLC microcomputerized controllers (19), and PLC microcomputerized controllers (19) are collected simultaneously
Analyze the collected data of camera (14) and infrared camera (20) institute of taking photo by plane；
Accumulator (13) side is equipped with suppressor (21), and the PLC microcomputerized controllers (19) are according to its analysis result
Suppressor (21) is sent a command to, its working condition is controlled.
2. a kind of Multifunctional pre-warning according to claim 1 breaks through unmanned plane, it is characterised in that：The PLC microcomputers control
Device (19) side is equipped with GPS locator (18), its analysis result is sent to GPS positioning by the PLC microcomputerized controllers (19)
Device (18), the GPS locator (18) carries out analyzing and positioning, and location information is fed back to the PLC microcomputerized controllers (19),
Offline mode controller (17) is installed inside the control box (12), PLC microcomputerized controllers (19) are according to GPS locator (18)
Feedack sends to offline mode controller (17) and instructs, and it is micro- that the offline mode controller (17) receives the PLC
The instruction of machine controller (19) and then the operating status for controlling motor (6).
3. a kind of Multifunctional pre-warning according to claim 1 breaks through unmanned plane, it is characterised in that：Control box (12) top
End is equipped with wireless communication module (8), and the wireless communication module (8) connect with PLC microcomputerized controllers (19) signal, uses
In with ground staff's information exchange.
4. Multifunctional pre-warning according to claim 3 breaks through unmanned plane, it is characterised in that：The wireless communication module (8)
Side is equipped with counter electromagnetic device (9), and the PLC microcomputerized controllers (19) are sent out according to its analysis result to counter electromagnetic device (9)
Instruction is sent, and controls the operating status of counter electromagnetic device (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710142366.6A CN108569393A (en) | 2017-03-10 | 2017-03-10 | A kind of Multifunctional pre-warning counter unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710142366.6A CN108569393A (en) | 2017-03-10 | 2017-03-10 | A kind of Multifunctional pre-warning counter unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108569393A true CN108569393A (en) | 2018-09-25 |
Family
ID=63577270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710142366.6A Pending CN108569393A (en) | 2017-03-10 | 2017-03-10 | A kind of Multifunctional pre-warning counter unmanned plane |
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| Country | Link |
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| CN (1) | CN108569393A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111787216A (en) * | 2019-04-04 | 2020-10-16 | 南京非空航空科技有限公司 | Anti-unmanned aerial vehicle device based on many cameras |
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| CN104133483A (en) * | 2014-07-08 | 2014-11-05 | 遵义师范学院 | Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof |
| CN104943858A (en) * | 2015-07-03 | 2015-09-30 | 广西大学 | Multifunctional coaxial double-rotor-wing four-shaft aircraft |
| CN205345314U (en) * | 2016-01-13 | 2016-06-29 | 谈智 | Portable rotor unmanned aerial vehicle |
| CN205615720U (en) * | 2016-04-15 | 2016-10-05 | 杨维国 | Unmanned aerial combustible gas listens thermal imaging ware of taking photo by plane |
| CN106025921A (en) * | 2016-06-29 | 2016-10-12 | 国网山东省电力公司济南市历城区供电公司 | Aerial-shooting line inspection device for unmanned aerial vehicle |
| CN206590111U (en) * | 2017-03-10 | 2017-10-27 | 中交遥感载荷（北京）科技有限公司 | A kind of Multifunctional pre-warning breaks through unmanned plane |
-
2017
- 2017-03-10 CN CN201710142366.6A patent/CN108569393A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2012108021A (en) * | 2012-03-05 | 2013-09-10 | Александр Викторович Багров | METHOD FOR SHOCK IMPACT ON DANGEROUS SPACE OBJECTS AND DEVICE FOR ITS IMPLEMENTATION |
| CN104133483A (en) * | 2014-07-08 | 2014-11-05 | 遵义师范学院 | Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof |
| CN104943858A (en) * | 2015-07-03 | 2015-09-30 | 广西大学 | Multifunctional coaxial double-rotor-wing four-shaft aircraft |
| CN205345314U (en) * | 2016-01-13 | 2016-06-29 | 谈智 | Portable rotor unmanned aerial vehicle |
| CN205615720U (en) * | 2016-04-15 | 2016-10-05 | 杨维国 | Unmanned aerial combustible gas listens thermal imaging ware of taking photo by plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111787216A (en) * | 2019-04-04 | 2020-10-16 | 南京非空航空科技有限公司 | Anti-unmanned aerial vehicle device based on many cameras |
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