CN105882950A - Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity - Google Patents
Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity Download PDFInfo
- Publication number
- CN105882950A CN105882950A CN201610235784.5A CN201610235784A CN105882950A CN 105882950 A CN105882950 A CN 105882950A CN 201610235784 A CN201610235784 A CN 201610235784A CN 105882950 A CN105882950 A CN 105882950A
- Authority
- CN
- China
- Prior art keywords
- arm
- main body
- micro
- body edge
- strip
- 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.)
- Withdrawn
Links
- 238000007689 inspection Methods 0.000 title claims abstract description 24
- 230000005611 electricity Effects 0.000 title abstract description 5
- 238000004891 communication Methods 0.000 claims abstract description 26
- 238000005192 partition Methods 0.000 claims abstract description 7
- 230000005855 radiation Effects 0.000 claims description 33
- 238000001514 detection method Methods 0.000 claims description 15
- 230000003071 parasitic effect Effects 0.000 claims description 4
- 230000002035 prolonged effect Effects 0.000 claims description 2
- 238000000926 separation method Methods 0.000 abstract 1
- 230000005684 electric field Effects 0.000 description 5
- 238000002955 isolation Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 230000002547 anomalous effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 208000002925 dental caries Diseases 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000004297 night vision Effects 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/06—Helicopters with single rotor
-
- 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
- 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
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The invention discloses an electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity. The electricity grid inspection UAV comprises a main UAV body, wherein a propeller enabling the UAV to fly is arranged at the top end of the main UAV body, a drive motor is arranged in the main UAV body and used for driving the propeller to rotate; a battery cavity is formed in the main UAV body through separation of two transverse partition boards, and a rechargeable battery is arranged in the battery cavity; a longitudinal partition board is arranged below the battery cavity and divides the lower part of the main UAV body into a communication cavity and a circuit cavity; a camera is arranged on the UAV, so that manual inspection on foot can be effectively replaced, and inspection is realized by the UAV; besides, the three cavities are formed in the UAV, the communication, the power supply and the battery are separated in three independent cavities, and accordingly, more reasonable distribution without mutual influence is realized.
Description
Technical field
The present invention relates to a kind of electromagnetism intensity detection patrol unmanned machine of electric power network.
Background technology
At present, patrolling and examining mainly by patrolling and examining the most on foot of electric power network, the manual inspection when of running into complicated landform
The most extremely difficult, poor effect, efficiency is the lowest；And human use's unmanned air vehicle technique reaches its maturity at present, UAV
Being called for short " unmanned plane ", english abbreviation is " UaV ", is to utilize radio robot and the presetting apparatus provided for oneself to handle not
Manned aircraft.Unmanned plane is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition: nobody goes straight up to
These several big classes of machine, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol.Without driving on unmanned plane
Cabin, but the equipment such as automatic pilot, presetting apparatus is installed；On ground, naval vessels or machine tool remote control station personnel pass through radar
Deng equipment, it be tracked, position, remote control, remote measurement and Digital Transmission.Unmanned plane is utilized to carry out the various power equipments transmitted electricity
Check and patrol and examine, in order to power monitoring department pinpoints the problems and safeguards in time, it is ensured that power transmission network properly functioning；Unmanned plane
Test mode has efficient, quick, reliable, low cost, not by the advantage of regional impact.
Summary of the invention
It is an object of the invention to overcome disadvantages described above, it is provided that a kind of electromagnetism intensity detection electric power network patrols and examines nothing
Man-machine.
For achieving the above object, the concrete scheme of the present invention is as follows: a kind of electromagnetism intensity detection electric power network is patrol unmanned
Machine, includes unmanned plane main body, and described unmanned plane main body top is provided with the propeller making unmanned plane during flying, described unmanned plane main body
Inside it is provided with driving motor, is used for driving propeller to rotate；It is separated out an electricity by two lateral partitions in described unmanned plane main body
Cell cavity, is provided with rechargeable battery in described battery cavities；Being provided with a longitudinal baffle below described battery cavities, described longitudinal baffle will be unmanned
Communication chamber and circuit chamber it is separated into below owner's body；
Described circuit intracavity is provided with circuit box, is provided with routing inspection circuit in described circuit box, and described routing inspection circuit includes master control
CPU, also includes the night-viewable photographic head being connected respectively and the communication module for communication with master cpu signal；Described can night
Being located at unmanned plane main body bottom depending on photographic head, described communication module includes communication antenna, and described communication antenna is located at communication chamber
In.
Wherein, described communication antenna includes a pcb board, described pcb board be provided with the first micro-strip oscillator unit and and
First micro-strip oscillator cell configuration is the most identical with size and symmetrically arranged second micro-strip oscillator unit；First micro-strip oscillator unit
Include a hexagonal micro-strip main body；It is main that six limits starting number clockwise from angle, top of micro-strip main body are followed successively by first
Body limit, the second body edge, the 3rd body edge, the 4th body edge, the 5th body edge, the 6th body edge；Described second body edge is prolonged
Being extended with the first feed arm of L-shaped, described first feed arm is provided with the second feed arm away from one end of micro-strip main body, and described second
Feed arm is parallel with the 3rd body edge；Angle between described first body edge and the 6th body edge has extended upward tip
Radiation arm；Being provided with the first arc notch between described 5th body edge and the 6th body edge, described first arc notch is to extension
It is extended with the first parasitic radiation arm of triangle；Described micro-strip main body is provided with the main aperture of circle, includes in described main aperture
There are two the first fan-shaped sector arms and the second sector arm；It is equipped with one group first on described first sector arm and the second sector arm
Hollow out combines, and described first hollow out combination includes three parallel hollow out bars；First sector arm is respectively by the first linking arm
It is connected with micro-strip main body with the second linking arm；Second sector arm is respectively by the 3rd linking arm and the 4th linking arm and micro-strip main body
Connect；The obstruction breach of a V-arrangement it is equipped with on described first linking arm and the 3rd linking arm；
Between the first linking arm and the second linking arm, described micro-strip main body is extended to the first sector arm the first arc of arcuation
Shape radiation arm；
Between the 3rd linking arm and the 4th linking arm, described micro-strip main body is extended to the second sector arm side the of arcuation
Two arc radiation arms；Described pcb board is provided with for the power feed hole with the second feed arm feed.
Wherein, between the first body edge and the 6th body edge, between the second main body and the 3rd body edge, the 3rd main body and the
It is equipped with one between four body edge, between the 4th main body and the 5th body edge and circular obstructs hole.
Wherein, micro-strip main body, what it was equipped with a rectangle at the 5th body edge and the second body edge obstructs hollow out
Unit；The described hollow-out unit that obstructs includes from obstructing F shape radiation arm that hollow-out unit top margin downwardly extends out and from obstructing
The F shape radiation arm that hollow-out unit base extends upward.
Wherein, the inner arc limit of described first arc radiation arm and the inner arc limit of the second arc radiation arm are equipped with a rectangle
Rectangular radiation arm.
Described routing inspection circuit also includes the heat detector being connected with master cpu signal, and described heat detector is located at
The lateral wall of unmanned plane main body；
Described routing inspection circuit also includes the storage recording equipment being connected with master cpu signal；
Described routing inspection circuit also includes the electric field intensity detector being connected with master cpu signal, described electric field intensity detector
It is located at the lateral wall of unmanned plane main body；
Described routing inspection circuit also includes the magnetic field intensity detector being connected with master cpu signal, described magnetic field intensity detector
It is located at the lateral wall of unmanned plane main body；
Described routing inspection circuit also includes the Anticollision Radar being connected with master cpu signal, and described Anticollision Radar is located at unmanned owner
The lateral wall of body；
The invention have the benefit that by arranging photographic head on unmanned plane, it is possible to the effective manpower that replaces is patrolled and examined on foot, real
Patrolling and examining of existing unmanned plane, additionally arranges three cavitys in body, is three independences by machine intra-body communication, power supply, cell partition
Chamber, it is achieved relatively reasonably distribution does not affects mutually.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the theory diagram of the routing inspection circuit of the present invention；
Fig. 3 is the top view of the communication antenna of the present invention；
Fig. 4 is the top view of the first micro-strip oscillator unit of the present invention；
Fig. 5 is the partial enlarged drawing of this Fig. 4；
Fig. 6 is the return loss test figure of this antenna；
Fig. 7 is the isolation performance test figure of this antenna；
Fig. 8 is directional diagram during this antenna 2.4GHz；
Fig. 9 is directional diagram during this antenna 5.0GHz；
Description of reference numerals in Fig. 1 to Fig. 9:
1-unmanned plane main body；11-propeller；12-drives motor；The night-viewable photographic head of 2-；3-communication antenna；41-circuit chamber；
42-communicates chamber；5-circuit box；51-electric field intensity detector；52-heat detector；53-magnetic field intensity detector；54-is crashproof
Radar；6-battery cavities；
A1-PCB plate；A2-power feed hole；
B1-micro-strip main body；B21-the first feed arm；B22-the second feed arm；B3-tip radiation arm；B4-the first parasitic radiation
Arm；The main aperture of b5-；B61-the first sector arm；B62-the second sector arm；B63, b64-first hollow out combination；B65-first connects
Arm；B66-the 3rd linking arm；B67-the 4th linking arm；B68-the second linking arm；B71-the first arc radiation arm；B72-the second arc
Shape radiates；B73, b74-rectangular radiation arm；
B8-obstructs hole；B9-obstructs hollow-out unit；B91-F shape radiation arm.
Detailed description of the invention
The present invention is further detailed explanation with specific embodiment below in conjunction with the accompanying drawings, is not the reality of the present invention
The scope of executing is confined to this.
As shown in Figures 1 to 9, a kind of electromagnetism intensity detection patrol unmanned machine of electric power network described in the present embodiment, including
Unmanned plane main body 1, described unmanned plane main body 1 top is had to be provided with the propeller 11 making unmanned plane during flying, in described unmanned plane main body 1
It is provided with driving motor 12, is used for driving propeller 11 to rotate；It is separated out one by two lateral partitions in described unmanned plane main body 1
Battery cavities 6, is provided with rechargeable battery in described battery cavities 6；A longitudinal baffle, described longitudinal baffle it is provided with below described battery cavities 6
Communication chamber 42 and circuit chamber 41 will be separated into below unmanned plane main body 1；Circuit box 5, described circuit it is provided with in described circuit chamber 41
Being provided with routing inspection circuit in box 5, described routing inspection circuit includes master cpu, also include be connected with master cpu signal respectively can
Night vision cam 2 and the communication module for communicating；Described night-viewable photographic head 2 is located at unmanned plane main body 1 bottom, described communication
Module includes communication antenna 3, and described communication antenna 3 is located in communication chamber 42；By arranging photographic head on unmanned plane, it is possible to
The effective manpower that replaces is patrolled and examined on foot, it is achieved patrolling and examining of unmanned plane, additionally arranges three cavitys in body, by logical in body
Letter, power supply, cell partition are three independent chambeies, it is achieved relatively reasonably distribution does not affects mutually.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network described in the present embodiment, described communication antenna 3 includes
One pcb board a1, described pcb board a1 be provided with the first micro-strip oscillator unit and and the first micro-strip oscillator cell configuration and size equal
Identical and symmetrically arranged second micro-strip oscillator unit；First micro-strip oscillator unit includes a hexagonal micro-strip main body
b1；The six articles of limits starting number clockwise from angle, top of micro-strip main body b1 are followed successively by the first body edge, the second body edge, the 3rd master
Body limit, the 4th body edge, the 5th body edge, the 6th body edge；Described second body edge extends the first feed arm having L-shaped
B21, described first feed arm b21 is provided with the second feed arm b22, described second feed arm b22 away from one end of micro-strip main body b1
Parallel with the 3rd body edge；Angle between described first body edge and the 6th body edge has extended upward most advanced and sophisticated radiation arm
b3；Being provided with the first arc notch between described 5th body edge and the 6th body edge, described first arc notch extends outward
There is the first parasitic radiation arm b4 of triangle；Described micro-strip main body b1 is provided with main aperture b5 of circle, in described main aperture b5
Include two the first fan-shaped sector arm b61 and the second sector arm b62；Described first sector arm b61 and the second sector arm b62
On be equipped with one group of first hollow out combination b63, b64, described first hollow out combination b63, b64 includes three parallel hollow outs
Bar；First sector arm b61 is connected with micro-strip main body b1 by the first linking arm b65 and the second linking arm b68 respectively；Second is fan-shaped
Arm b62 is connected with micro-strip main body b1 by the 3rd linking arm b66 and the 4th linking arm b67 respectively；Described first linking arm b65 with
The obstruction breach of a V-arrangement it is equipped with on 3rd linking arm b66；Between the first linking arm b65 and the second linking arm b68, institute
State micro-strip main body b1 and extend the first arc radiation arm b71 having arcuation to the first sector arm b61；At the 3rd linking arm b66 and
Between 4th linking arm b67, described micro-strip main body b1 extends the second arc radiation having arcuation to the second sector arm b62 side
B72 arm；Described pcb board a1 is provided with for power feed hole a2 with the second feed arm b22 feed.
Designed by substantial amounts of microstrip circuit structure, and under substantial amounts of l-G simulation test and parameter adjustment, finally determine
Above-mentioned antenna structure；This antenna after feeding coupling by multiple antenna stacks simultaneously, and it shows excellence at 2.4GHz and 5.0GHz
Electric property, specifically such as Fig. 6, averagely reaches 9.65dBi near this frequency range under bandwidth；And other electric properties also have the most excellent
Different result, its return loss the return loss of 2.4-2.48GHz frequency range and 5.15-5.875GHz frequency range be superior to-
15dB；Such as Fig. 7, isolation is better than-20dB at the isolation loss of 2.4-2.48GHz and 5.15-5.875GHz frequency range.Proving should
Antenna itself possesses preferable performance；It addition, its directivity of this antenna, as shown in Figure 8 and Figure 9, under two frequency all
For omni-directional antenna.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network described in the present embodiment, the first body edge and the 6th main body
Between limit, between the second main body and the 3rd body edge, between the 3rd main body and the 4th body edge, the 4th main body and the 5th body edge
Between be equipped with one and circular obstruct hole b8.Be provided with obstructs hole b8, can increase the length of electric current flowing, increases radioactivity
Energy.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network described in the present embodiment, micro-strip main body b1, it is near the
Be equipped with a rectangle at five body edge and the second body edge obstructs hollow-out unit b9；Described hollow-out unit b9 that obstructs includes
From obstructing F shape radiation arm b91 that hollow-out unit b9 top margin downwardly extends out and upwardly extending from obstructing hollow-out unit b9 base
The F shape radiation arm b91 gone out.Obstructing the setting of hollow-out unit b9, found by the experimental data of gyroscope, it can effectively increase
In the case of adding radiation characteristic, moreover it is possible to effectively reduce isolation loss, increase bandwidth.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network described in the present embodiment, described first arc radiation arm
The inner arc limit of the inner arc limit of b71 and the second arc radiation b72 arm is equipped with rectangular radiation arm b73, b74 of a rectangle.
Described routing inspection circuit also includes the heat detector 52 being connected with master cpu signal, described heat detector 52
It is located at the lateral wall of unmanned plane main body 1；For quick detection ignition point, find thermal source, prevent fire from expanding.
Described routing inspection circuit also includes the storage recording equipment being connected with master cpu signal；Real time record patrols and examines information.
Described routing inspection circuit also includes the electric field intensity detector 51 being connected with master cpu signal, described electric field intensity
Detector 51 is located at the lateral wall of unmanned plane main body 1；For detecting anomalous electric field.
Described routing inspection circuit also includes the magnetic field intensity detector 53 being connected with master cpu signal, described magnetic field intensity
Detector 53 is located at the lateral wall of unmanned plane main body 1；For detecting anomalous field.
Described routing inspection circuit also includes the Anticollision Radar 54 being connected with master cpu signal, and described Anticollision Radar 54 is located at
The lateral wall of unmanned plane main body 1；Prevent unmanned plane from smashing.
The above is only a preferred embodiment of the present invention, therefore all according to the structure described in present patent application scope
Make, equivalence change that feature and principle are done or modify, be included in the protection domain of present patent application.
Claims (5)
1. the electromagnetism intensity detection patrol unmanned machine of electric power network, it is characterised in that: include unmanned plane main body (1), described
Unmanned plane main body (1) top is provided with the propeller (11) making unmanned plane during flying, is provided with driving motor in described unmanned plane main body (1)
(12), it is used for driving propeller (11) to rotate；It is separated out a battery cavities by two lateral partitions in described unmanned plane main body (1)
(6), it is provided with rechargeable battery in described battery cavities (6)；Described battery cavities (6) lower section is provided with a longitudinal baffle, described longitudinal baffle
Unmanned plane main body (1) lower section is separated into communication chamber (42) and circuit chamber (41)；It is provided with circuit box in described circuit chamber (41)
(5), being provided with routing inspection circuit in described circuit box (5), described routing inspection circuit includes master cpu, also include respectively with master control
The night-viewable photographic head (2) that cpu signal connects and the communication module for communicating；Described night-viewable photographic head (2) is located at unmanned
Owner's body (1) bottom, described communication module includes communication antenna (3), and described communication antenna (3) is located in communication chamber (42)；
Described routing inspection circuit also includes the magnetic field intensity detector (53) being connected with master cpu signal, and described magnetic field intensity is visited
Survey device (53) and be located at the lateral wall of unmanned plane main body (1).
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network the most according to claim 1, it is characterised in that: described logical
Letter antenna (3) includes a pcb board (a1), and described pcb board (a1) is provided with the first micro-strip oscillator unit and and the first micro-strip
Oscillator unit shapes and sizes are the most identical and symmetrically arranged second micro-strip oscillator unit；First micro-strip oscillator unit includes one
Individual hexagonal micro-strip main body (b1)；It is main that six limits starting number clockwise from angle, top of micro-strip main body (b1) are followed successively by first
Body limit, the second body edge, the 3rd body edge, the 4th body edge, the 5th body edge, the 6th body edge；Described second body edge is prolonged
Being extended with first feed arm (b21) of L-shaped, described first feed arm (b21) is provided with second away from one end of micro-strip main body (b1)
Feed arm (b22), described second feed arm (b22) is parallel with the 3rd body edge；Described first body edge and the 6th body edge it
Between angle extended upward most advanced and sophisticated radiation arm (b3)；It is provided with the first arc between described 5th body edge and the 6th body edge
V notch v, described first arc notch extends outward the first parasitic radiation arm (b4) of triangle；Described micro-strip main body
(b1) it is provided with first sector arm (b61) of circle, in described main aperture (b5), includes two the first fan-shaped sector arms
(b61) and the second sector arm (b62)；It is equipped with one group first on described first sector arm (b61) and the second sector arm (b62) to engrave
Idle pattern (b63, b64), described first hollow out combination (b63, b64) includes three parallel hollow out bars；First sector arm
(b61) it is connected with micro-strip main body (b1) by the first linking arm (b65) and the second linking arm (b68) respectively；Second sector arm
(b62) it is connected with micro-strip main body (b1) by the 3rd linking arm (b66) and the 4th linking arm (b67) respectively；Described first connects
The obstruction breach of a V-arrangement it is equipped with on arm (b65) and the 3rd linking arm (b66)；
Between the first linking arm (b65) and the second linking arm (b68), described micro-strip main body (b1) is to the first sector arm (b61)
Extend the first arc radiation arm (b71) having arcuation；Three
Between the 3rd linking arm (b66) and the 4th linking arm (b67), described micro-strip main body (b1) is to the second sector arm (b62)
Second arc radiation (b72) arm having arcuation is extended in side；Described pcb board (a1) be provided with for the second feed arm
(b22) power feed hole (a2) fed.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network the most according to claim 2, it is characterised in that: first is main
Between body limit and the 6th body edge, between the second main body and the 3rd body edge, between the 3rd main body and the 4th body edge, the 4th main
It is equipped with one between body and the 5th body edge and circular obstructs hole (b8).
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network the most according to claim 2, it is characterised in that: micro-strip master
Body (b1), what it was equipped with a rectangle at the 5th body edge and the second body edge obstructs hollow-out unit (b9)；Described resistance
Disturb hollow-out unit (b9) to include from obstructing F shape radiation arm (b91) that hollow-out unit (b9) top margin downwardly extends out and from resistance
Disturb F shape radiation arm (b91) that hollow-out unit (b9) base extends upward.
A kind of electromagnetism intensity detection patrol unmanned machine of electric power network the most according to claim 2, it is characterised in that: described the
The inner arc limit of the inner arc limit of one arc radiation arm (b71) and the second arc radiation (b72) arm is equipped with the rectangular radiation of a rectangle
Arm (b73, b74).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610235784.5A CN105882950A (en) | 2016-04-15 | 2016-04-15 | Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610235784.5A CN105882950A (en) | 2016-04-15 | 2016-04-15 | Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105882950A true CN105882950A (en) | 2016-08-24 |
Family
ID=56704929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610235784.5A Withdrawn CN105882950A (en) | 2016-04-15 | 2016-04-15 | Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105882950A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106553755A (en) * | 2016-11-04 | 2017-04-05 | 朱怀新 | A kind of power patrol unmanned machine of independently putting out a fire |
| CN106564597A (en) * | 2016-11-04 | 2017-04-19 | 朱怀新 | Electric power polling unmanned aerial vehicle |
| WO2018036093A1 (en) * | 2016-08-25 | 2018-03-01 | 凌企芳 | Smart unmanned aerial vehicle utilized in power line inspection |
| CN108061827A (en) * | 2017-11-21 | 2018-05-22 | 中国人民解放军陆军工程大学 | Unmanned plane Electromgnetic seat situation monitoring method, terminal device and system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140263819A1 (en) * | 2012-06-08 | 2014-09-18 | Phoenix Products, Inc. | Helicopter drip pan |
| CN105235907A (en) * | 2015-11-26 | 2016-01-13 | 李万 | Electric power circuit detection unmanned aerial vehicle with heat source detector |
| CN105258723A (en) * | 2015-09-18 | 2016-01-20 | 江健良 | High-voltage station detection device |
| CN105292470A (en) * | 2015-11-26 | 2016-02-03 | 李万 | Unmanned aerial vehicle for power line detection |
| CN105292471A (en) * | 2015-11-26 | 2016-02-03 | 欧志洪 | Solar electric power line detection unmanned aerial vehicle |
-
2016
- 2016-04-15 CN CN201610235784.5A patent/CN105882950A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140263819A1 (en) * | 2012-06-08 | 2014-09-18 | Phoenix Products, Inc. | Helicopter drip pan |
| CN105258723A (en) * | 2015-09-18 | 2016-01-20 | 江健良 | High-voltage station detection device |
| CN105235907A (en) * | 2015-11-26 | 2016-01-13 | 李万 | Electric power circuit detection unmanned aerial vehicle with heat source detector |
| CN105292470A (en) * | 2015-11-26 | 2016-02-03 | 李万 | Unmanned aerial vehicle for power line detection |
| CN105292471A (en) * | 2015-11-26 | 2016-02-03 | 欧志洪 | Solar electric power line detection unmanned aerial vehicle |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018036093A1 (en) * | 2016-08-25 | 2018-03-01 | 凌企芳 | Smart unmanned aerial vehicle utilized in power line inspection |
| CN106553755A (en) * | 2016-11-04 | 2017-04-05 | 朱怀新 | A kind of power patrol unmanned machine of independently putting out a fire |
| CN106564597A (en) * | 2016-11-04 | 2017-04-19 | 朱怀新 | Electric power polling unmanned aerial vehicle |
| CN106564597B (en) * | 2016-11-04 | 2019-01-29 | 江苏锦程航空科技有限公司 | A kind of power patrol unmanned machine |
| CN106553755B (en) * | 2016-11-04 | 2019-02-22 | 广州三飞航空科技有限公司 | A kind of power patrol unmanned machine of independently putting out a fire |
| CN108061827A (en) * | 2017-11-21 | 2018-05-22 | 中国人民解放军陆军工程大学 | Unmanned plane Electromgnetic seat situation monitoring method, terminal device and system |
| CN108061827B (en) * | 2017-11-21 | 2018-11-02 | 中国人民解放军陆军工程大学 | Unmanned plane Electromgnetic seat situation monitoring method, terminal device and system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105882950A (en) | Electricity grid inspection UAV (unmanned aerial vehicle) capable of detecting electromagnetism intensity | |
| CN105973235B (en) | For there are the rotor wing unmanned aerial vehicles of no-fly zone polygonal region to cover search path planning method | |
| US10040547B1 (en) | Unmanned aerial vehicle | |
| CN105790439A (en) | Real-time recording power grid patrol-inspection unmanned aerial vehicle | |
| CN105292471B (en) | A kind of solar electric power wireline inspection unmanned plane | |
| CN105235907B (en) | It is provided with the power circuit detection unmanned plane of thermal source detector | |
| CN102183955A (en) | Transmission line inspection system based on multi-rotor unmanned aircraft | |
| CN103116360A (en) | Unmanned aerial vehicle obstacle avoidance controlling method | |
| EP2828164B1 (en) | Device for detecting critical states of a surface | |
| CN106218873B (en) | A kind of anti-crash protection structure of unmanned plane | |
| CN105914641A (en) | Heat-source-detector-included unmanned aerial vehicle for power grid polling | |
| CN105292470B (en) | A kind of electric power circuit detects without man-machine | |
| CN205792528U (en) | Portable unmanned machine interference unit | |
| CN105836117A (en) | Unmanned aerial vehicle for night vision tour inspection of electric power network | |
| CN112357078A (en) | Unmanned aerial vehicle and method for patrol operation of earth-rock dam in abnormal seepage area | |
| WO2018036093A1 (en) | Smart unmanned aerial vehicle utilized in power line inspection | |
| CN106741875A (en) | A kind of flight search and rescue system and method | |
| CN105882949A (en) | Electricity grid inspection UAV (unmanned aerial vehicle) | |
| CN106240822A (en) | It is provided with the power patrol unmanned machine of magnetic field intensity detector | |
| CN204368419U (en) | A kind of Novel inclined four rotor wing unmanned aerial vehicle | |
| CN110626500A (en) | Unmanned aerial vehicle | |
| CN204998768U (en) | Unmanned aerial vehicle protects trigger device | |
| CN106275399A (en) | A kind of patrol unmanned machine of intelligent electric power being provided with storage device | |
| CN207000827U (en) | Aircraft, earth station and RF detection system | |
| CN106275398A (en) | One can position power patrol unmanned machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20160824 |
|
| WW01 | Invention patent application withdrawn after publication |