CN107554767A - Power patrol unmanned machine - Google Patents
Power patrol unmanned machine Download PDFInfo
- Publication number
- CN107554767A CN107554767A CN201710672960.6A CN201710672960A CN107554767A CN 107554767 A CN107554767 A CN 107554767A CN 201710672960 A CN201710672960 A CN 201710672960A CN 107554767 A CN107554767 A CN 107554767A
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- China
- Prior art keywords
- battery bag
- main body
- group
- unmanned machine
- power patrol
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- 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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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The present invention provides a kind of power patrol unmanned machine, including:Main body；The support arm for being connected and being disposed below with main body；In the flight component that support arm tail end is set；It is arranged on the landing chassis of bottom part body；It is arranged on the positioning component of body top；The battery bag bag of bottom part body is arranged on, for being powered for unmanned plane, battery bag has first group of electrode slice for being used for being connected to unmanned plane, is connected with second group of electrode slice on unmanned plane to realize the operation such as power supply and detection.The power patrol unmanned machine of the present invention, using the integrated design of battery bag and unmanned plane body, radiator structure and fixed structure are rationally designed inside battery bag simultaneously, so that the structure inside battery bag is more reasonable, the realization more easily radiated, Optimal Structure Designing is carried out to the on-off circuit inside battery bag simultaneously, realizes radiating and fixed double optimization.
Description
Technical field
The present invention relates to unmanned plane cruising inspection system field, in particular to a kind of power patrol unmanned machine and system.
Background technology
With economic and science and technology continuous development, various power systems have also obtained perfect.In recent years, unmanned plane exists
Application among power system is more and more extensive, and effective application of unmanned plane promotes the sustainable development of power industry.
The application of power system is than wide, therefore traditional electrical power management architecture can not meet current power row gradually
The growth requirement of industry.And the application of unmanned plane then solves relevant issues, power construction difficulty is reduced, solves regional patrol
Problem.
Power patrol unmanned machine (UAV) can carry the special equipments such as visible ray, infrared thermal imaging and carry out height to power circuit
The tour of precision, most of type can realize spot hover, so as to carry out more careful depth to doubtful hidden danger or trouble point
The video analysis entered.Using unmanned plane line walking, substantially increase operating efficiency and make an inspection tour the accuracy of result, also save simultaneously
Substantial amounts of human cost.It is contemplated that the prospect that unmanned plane is applied to power circuit patrolling is boundless.
But power patrol unmanned machine also has some defects in all many-sides of load-carrying, radiating, such as carrying is detachable
The charge-discharge circuit that rechargeable battery contains inside easy to fall off, battery bag is arranged on casing, not easy heat radiation, is easily loosened, battery
Cell heat dissipation problem inside bag, causes heat to gather, especially in altitude high temperature flight, it is easier to these occur
Problem.
The content of the invention
Present invention aims at a kind of power patrol unmanned machine of offer, including：
Main body；
The support arm for being connected and being disposed below with main body；
In the flight component that support arm tail end is set；
It is arranged on the landing chassis of bottom part body；
It is arranged on the positioning component of body top；
The battery bag of bottom part body is arranged on, for being powered for unmanned plane, battery bag, which has, to be used to be connected to unmanned plane
First group of electrode slice；
Wherein, the support arm is 4, is centered around the uniform setting of main body surrounding, corresponding four flight crews of 4 support arms
Part, each flight component drive the rotor of rotation to form by a motor and by motor, and motor is connected to one
In individual circuit control mainboard, circuit control mainboard is arranged in main body；
The battery bag is fixed to the bottom of the main body, and the bottom of the main body is provided with to be installed in the battery bag
During position and battery bag second group of electrode slice being mutually inserted of first group of electrode slice, second group of electrode slice and the circuit control
Mainboard connection processed；At least one set is additionally provided with the battery bag by multiple rechargeable batteries battery pack in series, it is adjacent
Battery pack between be provided with heat dissipation grid, the outside of each rechargeable cell be also wrapped on phase-change heat material layer and
The plastic packaging layer of plastic packaging phase-change material layers, the switching circuit board of control battery charging and discharging, switching circuit board are additionally provided with battery bag
It is connected with first group of electrode slice；
Connected to form series connection on the whole, gone here and there by alloying metal piece before the both positive and negative polarity of the multiple rechargeable battery
The switching circuit board is connected to after connection, the switching circuit board is fixed on the heat dissipation grid, also, on-off circuit
One is provided between plate and heat dissipation grid has porous plastic septum, and plastic septum both sides are pasted with damping sheet material.
Further, the landing chassis bottom is provided with Wireless charging coil, and is arranged on the main body by cable and one
Interior master control charging circuit connection, master control charging circuit are connected to second group of electrode slice and are used to charge to battery bag.
Further, electric quantity monitoring circuit is additionally provided with the battery bag, is connected with the battery pack and switching circuit board,
For monitoring the residual charge state of battery bag.
Further, the landing chassis bottom is additionally provided with switch module, via first group of electrode slice and second group of electricity
Pole piece is connected with the electric quantity monitoring circuit, is triggered when sending the first signal and landing for being triggered in unmanned plane raising
Secondary signal is sent, to control electric quantity monitoring circuit to work.
Further, wireless network transmissions component and memory are also integrated with the circuit control mainboard in the main body,
The memory is used to store the data that the collecting device of unmanned plane is gathered, and wireless network transmissions component is used for long-range prison
Central transmission data are controlled, the wireless network transmissions component is connected with switch module, is configured to control according to the secondary signal
Stop data transfer.
Further, the rechargeable cell is 18650 type lithium batteries, and is arranged to metal in heat dissipation grid and dissipates
Heat grate.
Further, the damping sheet material includes rubber sheet.
Further, the phase-change heat material layer only covers not surpassing along the extension of mediad both sides for rechargeable cell
Cross the part of cell length 1/2.
Further, the positioning component includes at least one of GPS or Big Dipper positioning component.
Further, there are multiple field-effect transistors on the switching circuit board, switched as charge and discharge control.
By above technical scheme, power patrol unmanned machine of the invention, using the integration of battery bag and unmanned plane body
Design, while radiator structure and fixed structure are rationally designed inside battery bag so that the structure inside battery bag is more reasonable,
The realization more easily radiated, while Optimal Structure Designing is carried out to the on-off circuit inside battery bag, realize radiating and fix
Double optimization.
It should be appreciated that as long as all combinations of aforementioned concepts and the extra design described in greater detail below are at this
Sample design it is not conflicting in the case of can be viewed as the disclosure subject matter a part.In addition, required guarantor
All combinations of the theme of shield are considered as a part for the subject matter of the disclosure.
Can be more fully appreciated from the following description with reference to accompanying drawing present invention teach that foregoing and other aspect, reality
Apply example and feature.The feature and/or beneficial effect of other additional aspects such as illustrative embodiments of the present invention will be below
Description in it is obvious, or by according to present invention teach that embodiment practice in learn.
Brief description of the drawings
Accompanying drawing is not intended to drawn to scale.In the accompanying drawings, each identical or approximately uniform group shown in each figure
It can be indicated by the same numeral into part.For clarity, in each figure, not each part is labeled.
Now, by example and the embodiment of various aspects of the invention will be described in reference to the drawings, wherein：
Fig. 1 is the schematic diagram of the power patrol unmanned machine of the present invention.
Fig. 2 is the electric-control system schematic diagram of the power patrol unmanned machine of the present invention.
Fig. 3 is the circuit diagram inside the battery bag of the power patrol unmanned machine of the present invention.
Fig. 4 is the battery structure schematic diagram inside the battery bag of the power patrol unmanned machine of the present invention.
Fig. 5 is the schematic diagram of the heat dissipation grid of the battery bag of the power patrol unmanned machine of the present invention.
Fig. 6 is the schematic diagram of the monomer rechargeable battery of the battery bag of the power patrol unmanned machine of the present invention.
Embodiment
In order to know more about the technology contents of the present invention, especially exemplified by specific embodiment and institute's accompanying drawings are coordinated to be described as follows.
Each side with reference to the accompanying drawings to describe the present invention in the disclosure, shown in the drawings of the embodiment of many explanations.
It is not intended to cover all aspects of the invention for embodiment of the disclosure.It should be appreciated that a variety of designs presented hereinbefore and reality
Apply example, and those designs described in more detail below and embodiment can in many ways in any one come it is real
Apply, because design disclosed in this invention and embodiment are not limited to any embodiment.In addition, disclosed by the invention one
A little aspects can be used alone, or otherwise any appropriately combined be used with disclosed by the invention.
With reference to shown in Fig. 1-Fig. 6, the present invention proposes a kind of power patrol unmanned machine, for being flown on power circuit
Inspection, the collecting device carried using it gather information, early to have found that it is likely that existing risk and problem.
The power patrol unmanned machine 100 of the present invention is multi-rotor unmanned aerial vehicle, including main body 101, the branch that is connected with main body 101
Brace 102, the flight component (103,104) set in support arm tail end, it is arranged on symmetrically arranged a pair of the bottom of main body 101
Landing chassis 105, camera assembly 106, battery bag 109 and the positioning component 108 for being arranged on body top.
In embodiments of the invention, the support arm 102 is 4, the corresponding four flight components of 4 support arms, Mei Gefei
Row component drives the rotor 104 of rotation to form by a motor 103 and by motor 103, and motor 103 is connected to
In one circuit control mainboard.
Circuit control mainboard is arranged in main body, is integrated with flight controller, motor-drive circuit, wireless network thereon and is received
Send out module, 6 axle gyroscopes, acceleration transducer, local storage, Temperature Humidity Sensor, camera assembly image-forming assembly and
Main control processor.Foregoing flight controller, motor-drive circuit, wireless network transceiver module, 6 axle gyroscopes, acceleration sensing
Device, local storage, Temperature Humidity Sensor, the image-forming assembly of camera assembly are all connected to main control processor.
6 axle gyroscopes, acceleration transducer are respectively used to the flight attitude data of collection unmanned plane in real time, and are transferred to master
Control processor.
Flight controller is used for the flight for adjusting unmanned plane with control according to flight attitude data controlled motor drive circuit
Posture.Flight controller can use the drive circuit and type of drive of existing unmanned plane.
Temperature Humidity Sensor is used to gather the data of the Temperature and Humidity module of unmanned plane location in real time and is transferred to main control processor.
Camera assembly, including lens assembly 107 and the image-forming assembly positioned at camera lens rear, image-forming assembly are handled with master control
Device connects, image-forming assembly be used to receiving the image that is gathered from lens assembly 107 and by video conversion into electric signal output to
Main control processor.
Positioning component 108, such as Big Dipper positioning component or GPS location component etc., for obtaining the ground of unmanned plane in real time
Position data is managed, and is transferred to main control processor.
Battery bag 109, using rechargeable battery pack, such as lithium battery pack, there are multiple chargeable lithium cells, for nothing
Man-machine power supply.Battery bag is also connected with wireless charging circuit, for being charged by wireless charging circuit to battery bag.Battery bag has
Have for being connected to the first of unmanned plane group of electrode slice 1091.
Wireless charging circuit, has multiple micro radio charge coils, and multiple micro radio charge coils are separately mounted to
In foregoing 2 landing chassis, charged by the magnetic coupling with the external world.Multiple micro radio charge coils pass through wired line
Road such as cable are connected to the master control charging circuit being integrated in circuit control mainboard, and main control processor connects more than master control charging circuit
Connect.Master control charging circuit, it is connected to second group of electrode slice and is used to charge to battery bag 109.
In some instances, the bottom of landing chassis 105 is additionally provided with switch module, via first group of electrode slice and second group of electricity
Pole piece is connected with the electric quantity monitoring circuit, is triggered when sending the first signal and landing for being triggered in unmanned plane raising
Secondary signal is sent, to control electric quantity monitoring circuit to work.
Wireless network transceiver module, such as including 4G or 5G wireless communication modules, for unmanned plane to be accessed into network, make
Unmanned plane is able to carry out data interaction with remote monitoring center.
With reference to Fig. 3, battery bag 109 is fixed on the bottom of main body 101, such as is carried out by buckle, or the component such as neck
Fixed, the bottom of main body is provided with when battery bag 109 is installed in place and first group of electrode slice 1091 of battery bag is mutually inserted
Second group of electrode slice 1011, second group of electrode slice 1011 be connected with circuit control mainboard, is connected to the master of circuit control mainboard
Control processor.
With reference to Fig. 2-6, at least one set is additionally provided with battery bag 109 by multiple rechargeable batteries 1092 electricity in series
Pond group 1093, as illustrated, having battery pack as three groups, heat dissipation grid is provided between adjacent battery pack, radiate lattice
Grid be fixed to battery bag shell on each rechargeable cells of outside be also wrapped on phase-change heat material layer 1095 and
The plastic packaging layer of plastic packaging phase-change material layers, the switching circuit board 1096 of control battery charging and discharging, switch electricity are additionally provided with battery bag
Road plate 1096 is connected with first group of electrode slice 1091.In optional example, switching circuit board 1096 has multiple effects
Transistor is answered, is switched as charge and discharge control.
Connected to form series connection on the whole, gone here and there by alloying metal piece before the both positive and negative polarity of multiple rechargeable batteries 1092
The switching circuit board 1096 is connected to after connection, the switching circuit board is fixed on the heat dissipation grid 1094, also,
One is provided between switching circuit board and heat dissipation grid has porous plastic septum 1098, and plastic septum both sides are pasted with damping
Sheet material, such as rubber sheet, on the one hand to the insulation between circuit control mainboard and heat dissipation grid, on the other hand play damping and
Strengthen the effect of fastening.
In certain embodiments, landing chassis bottom is additionally provided with switch module, is connected with electric quantity monitoring circuit, in nothing
It is triggered to send the first signal and be triggered when landing during man-machine raising and sends secondary signal, controls electric quantity monitoring circuit work
Make.In this way, when unmanned plane takes off or lands, the detection of an electricity can be directly carried out, it is not necessary to individually designed
Electric power detection switchs, it is not required that electricity is monitored always, so as to which the electricity for producing unnecessary persistently consumes.
Maintenance for the ease of electricity and unmanned plane is caused to be able to the continuation of the journey of long period, our circuits in main body
Wireless network transmissions component and memory are also integrated with control mainboard, and is set by the collection of memory storage unmanned plane
The standby data gathered, such as the data of the collection such as Temperature Humidity Sensor, camera assembly, gyroscope and acceleration transducer.
Wireless network transmissions component is used to long-range Surveillance center transmit these data, the wireless network transmissions component with
Switch module connects, and is configured to control stopping data transfer according to the secondary signal.In this way, when unmanned plane is landing,
We, which just suspend, is transmitted, and saves electricity.Also, now can is realized by way of directly transmitting, or can be with
The time by way of a transmission is charged on one side, avoid the data fault caused by unexpected power-off in transmitting procedure.
We are preferably 18650 type lithium batteries in the rechargeable cell of the solution of the present invention, and in heat dissipation grid
It is arranged to heat dissipation metal grid, such as aluminium alloy or copper alloy heat dissipation grid.
Due to 18650 batteries or the electrode of other batteries, i.e. both positive and negative polarity is typically all disposed within end positions, in order to prevent
The problems such as corroding caused by the leakage of phase-change material, we by phase-change heat material layer only cover rechargeable cell along
Mediad both sides extend not more than the part of cell length 1/2.
Although the present invention is disclosed above with preferred embodiment, so it is not limited to the present invention.Skill belonging to the present invention
Has usually intellectual in art field, without departing from the spirit and scope of the present invention, when can be used for a variety of modifications and variations.Cause
This, the scope of protection of the present invention is defined by those of the claims.
Claims (10)
- A kind of 1. power patrol unmanned machine, it is characterised in that including:Main body；The support arm for being connected and being disposed below with main body；In the flight component that support arm tail end is set；It is arranged on the landing chassis of bottom part body；It is arranged on the positioning component of body top；The battery bag of bottom part body is arranged on, for being powered for unmanned plane, battery bag, which has, to be used to be connected to the first of unmanned plane Group electrode slice；Wherein, the support arm is 4, is centered around the uniform setting of main body surrounding, and 4 support arms correspond to four flight components, Each flight component drives the rotor of rotation to form by a motor and by motor, and motor is connected to an electricity In the control mainboard of road, circuit control mainboard is arranged in main body；The battery bag is fixed to the bottom of the main body, and the bottom of the main body is provided with when the battery bag is installed in place Second group of electrode slice being mutually inserted with first group of electrode slice of battery bag, second group of electrode slice are led with circuit control Plate connects；At least one set is additionally provided with the battery bag by multiple rechargeable batteries battery pack in series, adjacent electricity Heat dissipation grid is provided between the group of pond, heat dissipation grid is fixed on the shell of battery bag, the outside of each rechargeable cell The plastic packaging layer of phase-change heat material layer and plastic packaging phase-change material layers is also wrapped on, control battery charge and discharge is additionally provided with battery bag The switching circuit board of electricity, switching circuit board are connected with first group of electrode slice；Connected before the both positive and negative polarity of the multiple rechargeable battery by alloying metal piece to form series connection on the whole, after series connection Be connected to the switching circuit board, the switching circuit board is fixed on the heat dissipation grid, also, switching circuit board with One is provided between heat dissipation grid has porous plastic septum, and plastic septum both sides are pasted with damping sheet material.
- 2. power patrol unmanned machine according to claim 1, it is characterised in that the landing chassis bottom is provided with wireless charging Electric coil, and be connected by cable with the master control charging circuit that one is arranged in the main body, master control charging circuit is connected to Two groups of electrode slices are used to charge to battery bag.
- 3. power patrol unmanned machine according to claim 1, it is characterised in that electricity prison is additionally provided with the battery bag Slowdown monitoring circuit, it is connected with the battery pack and switching circuit board, for monitoring the residual charge state of battery bag.
- 4. power patrol unmanned machine according to claim 1, it is characterised in that the landing chassis bottom is additionally provided with switch Component, it is connected via first group of electrode slice and second group of electrode slice with the electric quantity monitoring circuit, for being risen in unmanned plane It is triggered to send the first signal and be triggered when landing when rising and sends secondary signal, controls electric quantity monitoring circuit to work.
- 5. power patrol unmanned machine according to claim 4, it is characterised in that in the circuit control mainboard in the main body Wireless network transmissions component and memory are also integrated with, what the memory was gathered for storing the collecting device of unmanned plane Data, wireless network transmissions component are used to transmit data, the wireless network transmissions component and switches set to long-range Surveillance center Part connects, and is configured to control stopping data transfer according to the secondary signal.
- 6. power patrol unmanned machine according to claim 1, it is characterised in that the rechargeable cell is 18650 Type lithium battery, and it is arranged to heat dissipation metal grid in heat dissipation grid.
- 7. power patrol unmanned machine according to claim 1, it is characterised in that the damping sheet material includes rubber sheet.
- 8. power patrol unmanned machine according to claim 1, it is characterised in that the phase-change heat material layer only covers list The part that cell length 1/2 is extended not more than along mediad both sides of body rechargeable battery.
- 9. power patrol unmanned machine according to claim 1, it is characterised in that the positioning component includes GPS or north Struggle against at least one of positioning component.
- 10. power patrol unmanned machine according to claim 1, it is characterised in that have on the switching circuit board multiple Field-effect transistor, switched as charge and discharge control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710672960.6A CN107554767A (en) | 2017-08-09 | 2017-08-09 | Power patrol unmanned machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710672960.6A CN107554767A (en) | 2017-08-09 | 2017-08-09 | Power patrol unmanned machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554767A true CN107554767A (en) | 2018-01-09 |
Family
ID=60974384
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710672960.6A Withdrawn CN107554767A (en) | 2017-08-09 | 2017-08-09 | Power patrol unmanned machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107554767A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110269540A (en) * | 2018-03-15 | 2019-09-24 | 谢苏琨 | A kind of UAV system of cleaning of buildings metope |
| CN112478186A (en) * | 2020-12-17 | 2021-03-12 | 石家庄嘉诚联信科技开发有限公司 | Power distribution network inspection unmanned aerial vehicle based on vehicle-mounted system |
-
2017
- 2017-08-09 CN CN201710672960.6A patent/CN107554767A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110269540A (en) * | 2018-03-15 | 2019-09-24 | 谢苏琨 | A kind of UAV system of cleaning of buildings metope |
| CN112478186A (en) * | 2020-12-17 | 2021-03-12 | 石家庄嘉诚联信科技开发有限公司 | Power distribution network inspection unmanned aerial vehicle based on vehicle-mounted system |
| CN112478186B (en) * | 2020-12-17 | 2022-10-18 | 石家庄嘉诚联信科技开发有限公司 | Power distribution network inspection unmanned aerial vehicle based on vehicle-mounted system |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180109 |
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| WW01 | Invention patent application withdrawn after publication |