CN205959072U - Unmanned aerial vehicle power line inspection device - Google Patents
Unmanned aerial vehicle power line inspection device Download PDFInfo
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- CN205959072U CN205959072U CN201620807430.9U CN201620807430U CN205959072U CN 205959072 U CN205959072 U CN 205959072U CN 201620807430 U CN201620807430 U CN 201620807430U CN 205959072 U CN205959072 U CN 205959072U
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- unmanned plane
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Abstract
The utility model provides an unmanned aerial vehicle power line inspection device includes at least: by unmanned aerial vehicle (1), wireless data chain machine carries module (2), visual detection module (3), aircraft end (U) that satellite signal reception module (4) and autopilot module (5) constitute and the ground station side (G) who constitutes by wireless data chain ground face mould piece (6) and computer (7), autopilot module (5) are by electron compass (51), the gesture detects sensor (52), height sensor (53) and flight controller (54) constitute, its characterized in that: wireless data chain machine carry module (2), visual detection module (3), satellite signal reception module (4) and autopilot module (5) setting on unmanned aerial vehicle (1), the utility model discloses can realize power line's autonomic high -efficient the detection.
Description
Technical field：
The present invention relates to a kind of unmanned plane power circuit polling device, belong to polling transmission line technical field.
Background technology：
Unmanned plane is the unmanned vehicle that a kind of utilization radio robot and itself presetting apparatus manipulate,
Have the advantages that simple to operate, easily controllable, be widely used in take photo by plane photography, electric inspection process, environment measuring, forest fire protection, calamity
The fields such as feelings inspection, anti-terrorism lifesaving, military surveillance.With the continuous development of microelectric technique and micro mechanical system technology, unmanned
Machine constantly strides forward to miniaturization and intelligent direction, is widely used in electric inspection process field in recent years, and
Become a kind of development trend.
But, at this stage during unmanned plane power circuit polling device aerial work, mostly adopt manual remote control or according to people
The working method being detected for the course line setting.Independently patrolling and examining for how realizing unmanned plane, technically studying phase further
Close less, thus the efficient detection to power circuit can not be realized well.
For the problems referred to above, the present invention proposes a kind of unmanned plane power circuit polling device, realizes power circuit is carried out
Autonomous detection, significant to the detection efficiency improving power circuit.
Content of the invention：
The purpose of the present invention：Propose a kind of unmanned plane power circuit polling device, realize power circuit is independently examined
Survey.
In order to realize the purpose of the present invention, intend employing the following technical solutions：
1st, the present invention at least includes：Connect by unmanned plane, wireless data chain onboard modules, vision-based detection module, satellite-signal
The aircraft end of receipts module and automatic Pilot module composition and the ground being made up of wireless data chain earth module and computer
Stand end it is characterised in that：Described automatic Pilot module is by electronic compass, attitude detecting sensor, height sensor and flight
Controller is constituted, wireless data chain onboard modules, vision-based detection module, satellite signal reception module and the setting of automatic Pilot module
On unmanned plane, above-mentioned unmanned plane is rotor wing unmanned aerial vehicle or fixed-wing unmanned plane.
Brief description：
Fig. 1 illustrates the composition of the present invention.
Fig. 2 illustrates the using method of the present invention.
1st, unmanned plane；2nd, wireless data chain onboard modules；3rd, vision-based detection module；4th, satellite signal reception module；5th, certainly
Dynamic driving module；6th, wireless data chain earth module；7th, computer；8th, electric force pole tower I；9th, electric force pole tower II；10th, electric lines of force；
11st, patrol and examine direction I；12nd, electric force pole tower III；13rd, patrol and examine direction II；14th, electric force pole tower IV；51st, electronic compass；52nd, attitude inspection
Survey sensor；53rd, height sensor；54th, flight controller；U, aircraft end；G, earth station end.
Specific embodiment：
The present invention at least includes：Connect by unmanned plane 1, wireless data chain onboard modules 2, vision-based detection module 3, satellite-signal
Receive the module 4 and automatic Pilot module 5 aircraft end U constituting and be made up of wireless data chain earth module 6 and computer 7
Earth station end G it is characterised in that：Described automatic Pilot module 5 is passed by electronic compass 51, attitude detecting sensor 52, height
Sensor 53 and flight controller 54 are constituted, wireless data chain onboard modules 2, vision-based detection module 3, satellite signal reception module 4
It is arranged on unmanned plane 1 with automatic Pilot module 5, upper described unmanned plane 1 is rotor wing unmanned aerial vehicle or fixed-wing unmanned plane.
When power circuit polling is carried out using the present invention, the first step, artificial control aircraft end U flies to electric force pole tower II9
Overhead, shoot electric lines of force 10, electric force pole tower I8, electric force pole tower II9 and electric force pole tower III12 using vision-based detection module 3
Image, and the number that satellite signal reception module 4, electronic compass 51, attitude detecting sensor 52, height sensor 53 are detected
According to this and electric lines of force 10, electric force pole tower I8, electric force pole tower II9 and electric force pole tower III12 image information pass through wireless data chain
Onboard modules 2 and wireless data chain earth module 6 transmit to the computer 7 of earth station end G, and computer 7 determines electric force pole tower
The positional information of I8, electric force pole tower II9 and electric force pole tower III12 simultaneously stores it on computer 7；Second step, computer 7 is known
Behind the direction of other electric lines of force 10, direction I11 is patrolled and examined in artificial determination, and aircraft end U patrols and examines in the control lower edge of automatic Pilot module 5
Direction I11 flies to electric force pole tower III12 automatically, and by the image of electric lines of force 10 and satellite signal reception module 4, electronic compass
51st, the data that attitude detecting sensor 52, height sensor 53 detect passes through wireless data chain onboard modules 2 and wireless data
Chain earth module 6 transmits to the computer 7 of earth station end G, and computer 7 judges whether circuit is abnormal, and abnormal information is deposited
Storage is on computer 7；3rd step, when aircraft end U flies to space-time on electric force pole tower III12, by the airborne mould of wireless data chain
The image information of electric lines of force 10, electric force pole tower IV14 is transmitted to the meter of earth station end G by block 2 and wireless data chain earth module 6
On calculation machine 7, computer 7 according to the relative position of electric force pole tower II9, electric force pole tower III12 and electric force pole tower IV14 and is patrolled and examined
Direction I11 automatically determines and patrols and examines direction II13, and aircraft end U patrols and examines direction II13 certainly in the control lower edge of automatic Pilot module 5
Move and fly to electric force pole tower IV14, and the image of electric lines of force 10, satellite signal reception module 4, electronic compass 51, attitude detection are passed
Sensor 52, the information of height sensor 53 are transmitted to ground by wireless data chain onboard modules 2 and wireless data chain earth module 6
On the computer 7 of face station end G, computer 7 judges whether circuit is abnormal, and abnormal information is stored on computer 7, class according to this
Push away, with reference to the 3rd step, realize patrolling and examining of power circuit.
Claims (2)
1. a kind of unmanned plane power circuit polling device, at least includes：By unmanned plane (1), wireless data chain onboard modules (2),
Aircraft end (U) that vision-based detection module (3), satellite signal reception module (4) and automatic Pilot module (5) are constituted and by no
Earth station end (G) that line Data-Link earth module (6) and computer (7) are constituted it is characterised in that：Described automatic Pilot module
(5) it is made up of electronic compass (51), attitude detecting sensor (52), height sensor (53) and flight controller (54), wirelessly
Data-Link onboard modules (2), vision-based detection module (3), satellite signal reception module (4) and automatic Pilot module (5) are arranged on
On unmanned plane (1).
2. a kind of unmanned plane power circuit polling device according to claim 1 it is characterised in that：Described unmanned plane
(1) it is rotor wing unmanned aerial vehicle or fixed-wing unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620807430.9U CN205959072U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle power line inspection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620807430.9U CN205959072U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle power line inspection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205959072U true CN205959072U (en) | 2017-02-15 |
Family
ID=57973343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620807430.9U Expired - Fee Related CN205959072U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle power line inspection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205959072U (en) |
-
2016
- 2016-07-22 CN CN201620807430.9U patent/CN205959072U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170215 Termination date: 20210722 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |