CN107241158A - Unmanned plane breaks through device - Google Patents
Unmanned plane breaks through device Download PDFInfo
- Publication number
- CN107241158A CN107241158A CN201710207819.9A CN201710207819A CN107241158A CN 107241158 A CN107241158 A CN 107241158A CN 201710207819 A CN201710207819 A CN 201710207819A CN 107241158 A CN107241158 A CN 107241158A
- Authority
- CN
- China
- Prior art keywords
- antenna
- unmanned plane
- fixed mount
- housing
- breaks
- 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.)
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Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/80—Jamming or countermeasure characterized by its function
- H04K3/90—Jamming or countermeasure characterized by its function related to allowing or preventing navigation or positioning, e.g. GPS
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/80—Jamming or countermeasure characterized by its function
- H04K3/82—Jamming or countermeasure characterized by its function related to preventing surveillance, interception or detection
- H04K3/825—Jamming or countermeasure characterized by its function related to preventing surveillance, interception or detection by jamming
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/80—Jamming or countermeasure characterized by its function
- H04K3/92—Jamming or countermeasure characterized by its function related to allowing or preventing remote control
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Selective Calling Equipment (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Device is broken through the invention provides a kind of unmanned plane, including housing, it is installed with the housing on control circuit board, the control circuit board and is provided with the electric power management circuit being sequentially connected, scanning circuit, voltage controlled oscillator, radio frequency power amplification modules and aerial radiation circuit；The front end of the housing is provided with the first fixed mount, first fixed mount and is fixedly connected with first antenna, the second antenna and third antenna；The first antenna, the second antenna, third antenna are connected with the aerial radiation circuit respectively.The present invention is installed with three antennas by the removable fixed mount of housing forward end, realize all standing of tranmitting frequency, the management and control to different unmanned plane working frequency range has been effectively ensured, and landing can be remotely controlled to it after guiding unmanned plane during flying to certain position, so as to improve the effect of management and control.In addition, the present invention has the advantages that small volume, carrying and folding and unfolding are convenient.
Description
Technical field
Break through technology the present invention relates to unmanned plane, and in particular to be a kind of unmanned plane counter device.
Background technology
In recent years, with the fast development of unmanned air vehicle technique, unmanned plane industry development is swift and violent, has been widely used in public
The fields such as safety, fire-fighting, traffic, military affairs and business.
Unmanned plane is brought convenience in high-altitude shooting, aerial carry etc. on to user, but also gives the masses and law enforcement
Personnel bring very big trouble and potential safety hazard.Spy on other people privacy, the unmanned planes brought by unmanned plane reequips cargo transport, nothing privately
A series of unsafe problems such as the man-machine too drastic word vertically hung scroll of carrying, the smuggling of unmanned plane border have caused various countries to unmanned plane hidden danger
Worry.Corresponding unmanned plane during flying rule is limited for this various countries, and has set up regulatory authorities, but this is simultaneously
The infringement of strick precaution unmanned plane not yet in effect to social safety.In Jin Liangnian various countries, unmanned plane rushes into government area, airport landing
The hazard events such as course line, landmark, military base still emerge in an endless stream.
Although existing market is there is also the product of some counter unmanned planes, such product generally existing volume is greatly, again
Amount weight, working time are short, in the case of non-transformer, the problem of unsatisfactory to the unmanned plane management and control in long-distance flight；Especially
It is management and control of this kind of product to unmanned plane, is largely to force it to land by disturbing its work, once unmanned plane is losing
Dropped in the case of control and easily damage or even hurt innocent persons.
The content of the invention
Therefore, it is an object of the invention to provide a kind of management and control effect it is good, can work long hours, small-sized gun barrel it is portable
Unmanned plane breaks through device.
The purpose of the present invention is achieved through the following technical solutions.
A kind of unmanned plane breaks through in device, including housing, the housing and is installed with control circuit board, the control circuit
The electric power management circuit being sequentially connected, scanning circuit, voltage controlled oscillator, radio frequency power amplification modules and aerial radiation electricity are provided with plate
Road；The front end of the housing is provided with the first fixed mount, first fixed mount and is fixedly connected with first antenna, the second antenna
And third antenna；The first antenna, the second antenna, third antenna are connected with the aerial radiation circuit respectively.
Preferably, a link slot is provided with the downside of the front end of the housing, the rear end of first fixed mount is provided with one
The contiguous block being placed in the link slot can be corresponded to.
Preferably, the lower end of first fixed mount is provided with the pipe and fast-assembling base for being used to connect A-frame,
Locked after in the pipe correspondence insertion fast-assembling base by a lock.
Preferably, second antenna is located above first antenna, and the two front end is fixedly connected by the second fixed mount.
Preferably, second fixed mount includes being placed on the upper retainer ring of the second antenna front ends and is placed on first antenna
On lower retainer ring, be fixedly connected between fixed ring and lower retainer ring by lock-screw.
Preferably, fixed ring upper end is provided with hinge, and the lower retainer ring lower end is provided with down hinge.
Preferably, the first fixed mount side is provided with a connecting plate, and the third antenna passes through an articulated elements and institute
Connecting plate connection is stated, and third antenna can be rotated by the articulated elements and deploy or be folded in the first fixed mount side.
Preferably, the hull outside is also equipped with radiator and fan for being radiated to control circuit board.
Preferably, the housing rear end is provided with the first battery being connected with the electric power management circuit；Under the housing
End is provided with removable the second standby battery.
Preferably, the first antenna be GPS GLONASS Galileo Beidou navigation L band antennas；Described second day
Line is BDStar navigation system S band antennas；The third antenna is remote control band antenna.
The unmanned plane counter device that the present invention is provided, three antennas are installed with by the removable fixed mount of housing forward end,
The all standing of tranmitting frequency is realized, the management and control to different unmanned plane working frequency range has been effectively ensured, and fly in guiding unmanned plane
Landing can be remotely controlled to it by going to after certain position, so as to improve the effect of management and control.In addition, three antennas of the invention pass through
Two fixed mounts are removable to be fixedly mounted, and battery is removable is fixed on housing, and can change reserve battery, therefore greatly side
Carrying and folding and unfolding.
Brief description of the drawings
Fig. 1 is unmanned plane of the present invention counter device schematic diagram one；
Fig. 2 is unmanned plane of the present invention counter device schematic diagram two；
Fig. 3 is unmanned plane of the present invention counter device schematic diagram three；
Fig. 4 is unmanned plane of the present invention counter device schematic diagram four；
Fig. 5 is that unmanned plane of the present invention breaks through the structure chart that device is provided with tripod.
Identifier declaration in figure：Housing 10, the first battery 11, the second battery 12, radiator 13, fan 14, neck 15, instruction
Lamp 16, buckle switch 17, link slot 18, the first fixed mount 20, contiguous block 21, pipe 22, lock 23, articulated elements 24, fast-assembling bottom
Seat 25, first antenna 30, the second antenna 40, third antenna 50, the second fixed mount 60, upper retainer ring 61, lower retainer ring 62, locking
Screw 63, down hinge 64, upper hinge 65.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
Refer to shown in Fig. 1~Fig. 5, the present invention is to provide a kind of easy to carry, unmanned plane counter that management and control effect is good
Device.
Wherein unmanned plane counter device includes housing 10, and the housing 10 is the good metal-back of thermal diffusivity, inside it
Control circuit board is installed with, the control worked whole counter device system is realized by control circuit board.
The corresponding outside of housing 1 of control circuit board is provided with radiator 13 and fan 14, in control circuit board work
When making, the heat produced in time to it is effectively radiated, to ensure the normal work of control circuit board.
The rear end of housing 10, which is detachably fixed, is provided with the first battery 11, after the first battery 11 is installed, and its correspondence can be with
Control circuit board is connected, to realize the power supply to control circuit board.And it is also equipped with one detachably in the lower end of housing 10 correspondence
The second battery 12, the second battery 12 be reserve battery, wherein the first battery 11, the second battery 12 pass through latch realize and shell
The fast assembling-disassembling of body 10.When entirely counter device normal work, powered by the first battery 11, and work as the electricity of the first battery 11 not
When sufficient, then the first battery 11 can be switched to by control circuit board and is powered, the first battery 11 and the second battery 12 are high poly-
Compound lithium battery, it has the characteristics of capacity is big, stability is high.
Buckle switch 17 is additionally provided with the lower end of housing 10, buckle switch 17 is connected with control circuit board, for opening
Work that is dynamic or closing whole system, and buckle switch 17 uses waterproofing design, a knob of key trigger action water proof switch can start.
For the ease of unmanned plane break through device can, observation distant to high-altitude more difficult black winged unmanned plane manage
Control, also sets up gun sight on body, and its correspondence is fixedly mounted on neck 15 on the housing 10, and neck 15 is that pick up fourth Buddhist nun leads
Rail, to improve its operating efficiency.
In addition, the indicator lamp 16 being connected with control circuit board is additionally provided with housing 10, for the Working mould to breaking through device
Formula and working condition are indicated.
The electric power management circuit being sequentially connected electrically, scanning circuit are wherein provided with control circuit board, voltage controlled oscillator, is penetrated
Frequency power amplifier module and aerial radiation circuit；Electric power management circuit correspondence is connected with first battery 11, passes through the first battery 11
Power and be correspondingly managed；Scanning circuit (Sweep Source circuit module) is by astatic multivibrator and source follower circuit
Composition, when power switch is opened, capacitor produces a certain size sawtooth voltage through resistance and IC discharge and recharge
Signal output, the source follower being connected is exported with multivibrator and is inputted, source follower is increased using field-effect transistor
Its strong load-carrying ability, can produce the voltage signal output of different frequency sawtooth waveforms；Voltage controlled oscillator input and frequency sweep
The output end connection of source circuit module, the voltage signal control that can be produced according to Sweep Source circuit module exports various random frequencies
Spectrum；The spectrum signal that RF power amplification circuit module exports the voltage controlled oscillator received amplifies, while its output end and antenna
Sending-end impedance matched design.
The front end of housing 10 is installed with the first fixed mount 20, and is fixedly connected with first antenna on the first fixed mount 20
30th, the second antenna 40 and third antenna 50；The first antenna be GPS GLONASS Galileo Beidou navigation L frequency ranges day
Line；Second antenna is BDStar navigation system S band antennas；The third antenna is remote control band antenna；And it is described
First antenna 30, the second antenna 40, third antenna 50 are connected with the aerial radiation circuit respectively.Wherein described antenna electric magnetic wave
With multiband characteristic, and the bandwidth of each wave band, thus can realize tranmitting frequency by unmanned plane alignment system frequency and
Remote control system frequency all standing.
Due to the antenna for three kinds of different frequency ranges that counter device is used, with high directivity, the characteristic such as bandwidth, gain height,
Correspondence can launch multiband electromagnetic wave, therefore can select the working condition of different mode when being used according to actual conditions,
The mode of operation that single band or multiband electromagnetic wave are launched simultaneously may be selected.
Be provided with a link slot 18 on the downside of the front end of housing 10, and the rear end of the first fixed mount 20 be provided with one can
Correspondence is placed in the contiguous block 21 in the link slot 18；The can be realized by being placed in by the correspondence of contiguous block 21 in link slot 18
One fixed mount 20 is detachably connected with housing 10.
The front end of first fixed mount 20 is installed with the antenna 40 of first antenna 30 and second, and the second antenna 40 is located at first
The top of antenna 30, and the fore-end of the two is fixedly connected by the second fixed mount 60.Second fixed mount 60 is Same Part,
Its both sides is symmetrically installed, and is specifically included and is placed on the upper retainer ring 61 of the front end of the second antenna 40 and is placed in the middle of first antenna 30
Partial lower retainer ring 62, is fixedly connected between fixed ring 61 and lower retainer ring 62 by lock-screw 63.Upper fixation
The upper end of ring 61 is provided with hinge 65, and the lower lower end of retainer ring 62 is provided with down hinge 64.
The side of first fixed mount 20 is provided with a connecting plate, and third antenna 50 passes through an articulated elements 24 and the company
Fishplate bar is connected, and articulated elements 24 is the hinge with damping, and third antenna 50 can be rotated by the articulated elements 24 and deploy or fold
In the side of the first fixed mount 20.
Unmanned plane breaks through the working stability of device for convenience, unmanned plane counter device can be fixedly mounted on into A-frame 70
On, therefore the fast-assembling base that a pipe 22 can be provided with the lower end of the first fixed mount 20 and is fixedly connected with the pipe 22
25, pipe 22 can be inserted into the corresponding groove of fast-assembling base 25, after fast-assembling base 25 is connected with A-frame, can pass through lock 23
It is locked.
Multiband electromagnetic wave power that unmanned plane of the present invention counter device is launched is big, power consumption is relatively small, longevity of service etc.
Characteristic, effectively fast shut-off remote control and unmanned plane can be contacted, and rapid pipe connecting unmanned plane and guide its flight to a positioning
Postpone, make unmanned plane rapid descent, therefore avoid unmanned plane and dropped in the case of out of hand and damage and hurt innocent persons
The problem of.
In addition, present invention counter device meeting small volume, it is detachable, portable the characteristics of, while multiple batteries can also be used
Module for power supply, other battery module is automatically switched to when a certain battery module electricity is low to system power supply, in the feelings not powered off
Ensure the work of counter device for a long time under condition.Implementing effective management and control to unmanned plane in-flight for counter device, there is provided more may be used
The guarantee leaned on.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.
Claims (10)
1. a kind of unmanned plane breaks through device, including housing (10), it is characterised in that be installed with control line in the housing (10)
The electric power management circuit being sequentially connected, scanning circuit, voltage controlled oscillator, radio frequency work(are provided with road plate, the control circuit board
Amplification module and aerial radiation circuit；The front end of the housing (10) is provided with the first fixed mount (20), first fixed mount
(20) first antenna (30), the second antenna (40) and third antenna (50) are fixedly connected with；The first antenna (30), second
Antenna (40), third antenna (50) are connected with the aerial radiation circuit respectively.
2. unmanned plane as claimed in claim 1 breaks through device, it is characterised in that be provided with one on the downside of the front end of the housing (10)
Link slot (18), the rear end of first fixed mount (20), which is provided with one, can correspond to the connection being placed in the link slot (18)
Block (21).
3. unmanned plane as claimed in claim 2 breaks through device, it is characterised in that the lower end of first fixed mount (20) is provided with
In one pipe (22) and fast-assembling base (25) for connecting A-frame, pipe (22) the correspondence insertion fast-assembling base (25)
Locked afterwards by a lock (23).
4. unmanned plane as claimed in claim 2 breaks through device, it is characterised in that second antenna (40) is located at first antenna
(30) above, and the two front end is fixedly connected by the second fixed mount (60).
5. unmanned plane as claimed in claim 4 breaks through device, it is characterised in that second fixed mount (60) includes being placed on the
The upper retainer ring (61) of two antennas (40) front end and the lower retainer ring (62) being placed in first antenna (30), fixed ring
(61) it is fixedly connected between lower retainer ring (62) by lock-screw (63).
6. unmanned plane as claimed in claim 5 breaks through device, it is characterised in that fixed ring (61) upper end is provided with hinge
Axle (65), lower retainer ring (62) lower end is provided with down hinge (64).
7. unmanned plane as claimed in claim 2 breaks through device, it is characterised in that the first fixed mount (20) side is provided with one
Connecting plate, the third antenna (50) is connected by an articulated elements (24) with the connecting plate, and third antenna (50) can pass through
The articulated elements (24) rotates and deploys or be folded in the first fixed mount (20) side.
8. unmanned plane as claimed in claim 2 breaks through device, it is characterised in that be also equipped with being used on the outside of the housing (10) pair
The radiator (13) and fan (14) of control circuit board radiating.
9. unmanned plane as claimed in claim 8 breaks through device, it is characterised in that housing (10) rear end is provided with and the electricity
The first battery (11) of power management circuits connection；Housing (10) lower end is provided with removable standby the second battery (12).
10. unmanned plane as claimed in claim 2 breaks through device, it is characterised in that the first antenna (30) be GPS
GLONASS Galileo Beidou navigation L band antennas；Second antenna (40) is BDStar navigation system S frequency ranges day
Line；The third antenna (50) is remote control band antenna.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710207819.9A CN107241158B (en) | 2017-03-31 | 2017-03-31 | Unmanned aerial vehicle reverse controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710207819.9A CN107241158B (en) | 2017-03-31 | 2017-03-31 | Unmanned aerial vehicle reverse controller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107241158A true CN107241158A (en) | 2017-10-10 |
| CN107241158B CN107241158B (en) | 2023-07-21 |
Family
ID=59983164
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710207819.9A Active CN107241158B (en) | 2017-03-31 | 2017-03-31 | Unmanned aerial vehicle reverse controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107241158B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108282244A (en) * | 2018-02-05 | 2018-07-13 | 深圳科立讯通信有限公司 | Portable unmanned machine jamming equipment |
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| CN108282244A (en) * | 2018-02-05 | 2018-07-13 | 深圳科立讯通信有限公司 | Portable unmanned machine jamming equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107241158B (en) | 2023-07-21 |
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