CN206584484U - It is a kind of can solar recharging intelligent patrol detection flying robot - Google Patents
It is a kind of can solar recharging intelligent patrol detection flying robot Download PDFInfo
- Publication number
- CN206584484U CN206584484U CN201720296262.6U CN201720296262U CN206584484U CN 206584484 U CN206584484 U CN 206584484U CN 201720296262 U CN201720296262 U CN 201720296262U CN 206584484 U CN206584484 U CN 206584484U
- Authority
- CN
- China
- Prior art keywords
- output end
- electrically connected
- fuselage
- input
- processing unit
- 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.)
- Active
Links
Landscapes
- Burglar Alarm Systems (AREA)
Abstract
The utility model discloses it is a kind of can solar recharging intelligent patrol detection flying robot, including fuselage, the fuselage both sides are symmetrically installed with wing, infrared thermal imagery probe and gas probe are separately installed with the wing of the fuselage both sides, rotor arm is installed on the wing, and the two ends of rotor arm are symmetrically installed with propeller, the inside of the fuselage is provided with control panel, central processing unit is installed on the centre position of the control panel, it is electrically connected between the input of the central processing unit and the output end of data transmission module, the output end of the input of the central processing unit respectively with timer, it is electrically connected between the output end of path planning module and the output end for flying control processor, it is electrically connected between the output end of the central processing unit and the input of alarm.The utility model structure is novel, easy to control, and capacity of will is strong, and intelligence degree is high, and intelligent patrol detection can be achieved.
Description
Technical field
The utility model is related to unmanned plane equipment technical field, specially it is a kind of can solar recharging intelligent patrol detection flight
Robot.
Background technology
At present, it is a kind of can solar recharging intelligent patrol detection flying robot can be widely used in need it is unattended big
Type open storage, parking lot, inflammable and explosive region, military restricted zone etc. needs to carry out the region patrolled and nursed in real time, without consumption
Take a large amount of manpowers.The equipment can voluntarily start by set date, voluntarily flight arrives designated area, voluntarily patrolled in specified altitude range
Look into, by the self-contained multiple sensors of flying robot, to swarmed into institute's region of patrolling and examining people, larger animal, Huo Zhehuo
Calamity, gas abnormal leakage situation carry out backstage real-time video transmission, while the entrained sensor of triggering sends alarm to backstage,
Intervention manual intervention is required to remind.Monitoring time typically be may be provided at 10-30 minutes, and inspection is finished, and flying robot is certainly
It is dynamic to return berth, charging continuation of the journey is automatically begun to, charging is finished, receive second of inspection task.It is all daily according to backstage design
And renew and take off, inspection is returned, charging.
The content of the invention
The purpose of this utility model be provide it is a kind of can solar recharging intelligent patrol detection flying robot, with solution
The problem of being proposed in background technology is stated, is had an advantageous effect in that：The apparatus structure is novel, easy to control, and capacity of will is strong,
Intelligence degree is high, and intelligent patrol detection can be achieved.
To achieve the above object, the utility model provides following technical scheme：It is a kind of can solar recharging intelligent patrol detection
Flying robot, including fuselage, the fuselage both sides are symmetrically installed with wing, the wing of the fuselage both sides and are separately installed with
Infrared thermal imagery is popped one's head in and gas probe, and rotor arm is provided with the wing, and the two ends of rotor arm are symmetrically installed with propeller,
It is provided between rotary electric machine, and rotary electric machine and camera clamp device and is connected by axis of rotation on the lower position of the fuselage
Connect, the surface of the fuselage is provided with solar photovoltaic assembly, and the fuselage side is provided with reception of wireless signals transmitter, institute
The inside for stating fuselage is provided with control panel, the control panel lower position and is provided with battery, the control panel
Central processing unit is installed on centre position, it is electric between the input of the central processing unit and the output end of data transmission module
Property connection, between the input of the data transmission module and the output end of data conversion module be electrically connected with, the data turn
Change the mold the output end of the input of block respectively with the output end, the output end of gas probe and night vision cam of infrared thermal imagery probe
Between be electrically connected with, the input of central processing unit output end respectively with timer, the output end of path planning module,
Fly to be electrically connected between the output end of control processor and GPS output end, the output end of the central processing unit and alarm
It is electrically connected between input, the central processing unit and wireless signal receive electric connection, the wireless communication between transmitter
Number receive to be electrically connected between transmitter and control terminal.
It is preferred that, it is symmetrically installed with below the fuselage on supporting leg, and supporting leg and damping device is installed.
It is preferred that, output end, the real-time range of the winged input for controlling processor respectively with path planning module are predicted
It is electrically connected between the output end of module and the output end of fault detection module.
It is preferred that, it is provided between charging inlet, and charging inlet and battery and is electrically connected with the control panel, institute
State and be electrically connected between the output end of battery and the input of central processing unit, and between battery and solar photovoltaic assembly
It is electrically connected with by wire.
It is preferred that, it is electrically connected between the output end of the central processing unit and the input of power controller, and power
It is electrically connected between the output end of controller and the input of battery.
Compared with prior art, the beneficial effects of the utility model are：The device structure is novel, the ripe nothing of technical backstopping
People's machine platform, timer and fly control processor installation, make the device device Intelligent fixed time is taken off, fault detection module with
Fly control processor to use cooperatively, enable the device to handle many failure problems, and can independently return mooring basin independently to fill
The installation of electricity, solar photovoltaic assembly and charging inlet, makes the device charge power supply by solar photovoltaic assembly and battery
To provide, can also civil power, photovoltaic complementary pair battery charged, moreover, can nurse what is required according to region of patrolling and examining
Difference, the different sensor of UAV flight, in order to prevent stranger from swarming into, the device carries infrared thermal imagery probe, night vision camera
Head, in order to prevent dangerous material from revealing or on fire, the device carries related gas probe, and control terminal can set inspection to prohibit
Area, cruise track, cruising altitude, flight time and interval, the function, easy to control, autonomous energy such as flight weather monitoring and early warning
Power is strong, and intelligence degree is high, and intelligent patrol detection can be achieved.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the internal structure schematic diagram of the utility model fuselage；
Fig. 3 is the utility model control panel structural representation；
Fig. 4 is the utility model night vision cam structural representation；
Fig. 5 is the utility model control system figure.
In figure：1- propellers；2- wings；3- infrared thermal imageries are popped one's head in；4- solar photovoltaic assemblies；5- reception of wireless signals is sent out
Emitter；6- gas probes；7- rotor arms；8- supporting legs；9- night vision cams；10- fuselages；11- control panels；12- wires；
13- batteries；14- alarms；15- fault detection modules；16- central processing units；17- charging inlets；18- rotary electric machines；19-
Camera clamp device；20- data conversion modules；21- data transmission modules；22- timers；23- path planning modules；24- flies
Control processor；25- control terminals；26- real-time range prediction modules；27-GPS；28- power controllers.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Refer to Fig. 1-5, a kind of embodiment that the utility model is provided：It is a kind of can solar recharging intelligent patrol detection flight
Robot, including fuselage 10, the both sides of fuselage 10 be symmetrically installed with wing 2, the wing 2 of the both sides of fuselage 10 be separately installed with it is infrared
Rotor arm 7 is installed on thermal imagery probe 3 and gas probe 6, wing 2, and the two ends of rotor arm 7 are symmetrically installed with propeller 1, machine
It is provided with the lower position of body 10 between rotary electric machine 18, and rotary electric machine 18 and camera clamp device 19 and passes through axis of rotation
Connection, the surface of fuselage 10 is provided with solar photovoltaic assembly 4, and the side of fuselage 10 is provided with reception of wireless signals transmitter 5, machine
The inside of body 10 is provided with control panel 11, the lower position of control panel 11 and is provided with battery 13, control panel 11
Between central processing unit 16 is installed on position, it is electric between the input of central processing unit 16 and the output end of data transmission module 21
Property connection, between the input of data transmission module 21 and the output end of data conversion module 20 be electrically connected with, data conversion mould
The output of the input of block 20 respectively with the output end, the output end of gas probe 6 and night vision cam 9 of infrared thermal imagery probe 3
Be electrically connected between end, the input of central processing unit 16 output end respectively with timer 22, path planning module 23 it is defeated
Go out end, fly to be electrically connected between the output end of control processor 24 and GPS27 output end, the output end and report of central processing unit 16
It is electrically connected between the input of alert device 14, central processing unit 16 and wireless signal receive electric connection between transmitter 5, wirelessly
Signal receives to be electrically connected between transmitter 5 and control terminal 25, and the lower section of fuselage 10 is symmetrically installed with supporting leg 8, and support
Damping device is installed on leg 8, flies output end, the real-time range of the input of control processor 24 respectively with path planning module 23
It is electrically connected between the output end of prediction module 26 and the output end of fault detection module 15, charging is provided with control panel 11
It is electrically connected between interface 17, and charging inlet 17 and battery 13, the output end of battery 13 is defeated with central processing unit 16
Enter and be electrically connected between end, and be electrically connected between battery 13 and solar energy electroplax 4 by wire, central processing unit 16 it is defeated
Go out between end and the input of power controller 28 and be electrically connected with, and output end and the input of battery 13 of power controller 28
It is electrically connected between end.
Operation principle：In use, propeller 1 provides power resources, during the device is patrolled, infrared thermal imagery is visited
Head, gas probe 6 and night vision cam 9 catch external information, and are converted into central processing unit 16 by data conversion module 20
The signal that can be recognized, central processing unit 16 is transferred to by signal transmission module 21, is carried out by central processing unit 16 to data
Processing, if it find that abnormal, control alarm 14 sends alarm signal, and receives transmitter 5 by wireless signal and be transmitted to
Control terminal 25, in flight course, solar photovoltaic assembly 4 converts solar energy into electric energy, and is transferred to by wire 12
Battery 13 is stored, GPS27 real-time capture positional informations, and by wireless signal receive transmitter 5 be transmitted to control eventually
End 25, aircraft is obtained data information transfer by path planning module 23, real-time range prediction module 26 and fault detection module 15
To winged control processor 24, corresponding processing is independently made by flying control processor 24.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Claims (5)
1. it is a kind of can solar recharging intelligent patrol detection flying robot, including fuselage（10）, it is characterised in that：The fuselage
（10）Both sides are symmetrically installed with wing（2）, the fuselage（10）The wing of both sides（2）On be separately installed with infrared thermal imagery probe
（3）And gas probe（6）, the wing（2）On rotor arm is installed（7）, and rotor arm（7）Two ends be symmetrically installed with spiral
Oar（1）, the fuselage（10）Lower position on rotary electric machine is installed（18）, and rotary electric machine（18）With camera clamp device
（19）Between connected by axis of rotation, the fuselage（10）Surface solar energy electroplax photovoltaic module is installed（4）, the machine
Body（10）Side is provided with reception of wireless signals transmitter（5）, the fuselage（10）Inside control panel is installed（11）, institute
State control panel（11）Battery is installed on lower position（13）, the control panel（11）Centre position on be provided with
Central processor（16）, the central processing unit（16）Input and data transmission module（21）Output end between electrically connect
Connect, the data transmission module（21）Input and data conversion module（20）Output end between be electrically connected with, the number
According to modular converter（20）Input respectively with infrared thermal imagery pop one's head in（3）Output end, gas probe（6）Output end and night vision
Camera（9）Output end between be electrically connected with, the central processing unit（16）Input respectively with timer（22）It is defeated
Go out end, path planning module（23）Output end, fly control processor（24）Output end and GPS（27）Output end between electrically
Connection, the central processing unit（16）Output end and alarm（14）Input between be electrically connected with, it is described center processing
Device（16）Receive transmitter with wireless signal（5）Between be electrically connected with, the wireless signal receives transmitter（5）With control terminal
（25）Between be electrically connected with.
2. it is according to claim 1 it is a kind of can solar recharging intelligent patrol detection flying robot, it is characterised in that：It is described
Fuselage（10）Lower section be symmetrically installed with supporting leg（8）, and supporting leg（8）On damping device is installed.
3. it is according to claim 1 it is a kind of can solar recharging intelligent patrol detection flying robot, it is characterised in that：It is described
Fly control processor（24）Input respectively with path planning module（23）Output end, real-time range prediction module（26）It is defeated
Go out end and fault detection module（15）Output end between be electrically connected with.
4. it is according to claim 1 it is a kind of can solar recharging intelligent patrol detection flying robot, it is characterised in that：It is described
Control panel（11）On be provided with charging inlet（17）, and charging inlet（17）With battery（13）Between be electrically connected with, it is described
Battery（13）Output end and central processing unit（16）Input between be electrically connected with, and battery（13）With solar energy
Lie prostrate component（4）Between be electrically connected with by wire.
5. it is according to claim 1 it is a kind of can solar recharging intelligent patrol detection flying robot, it is characterised in that：It is described
Central processing unit（16）Output end and power controller（28）Input between be electrically connected with, and power controller（28）'s
Output end and battery（13）Input between be electrically connected with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720296262.6U CN206584484U (en) | 2017-03-24 | 2017-03-24 | It is a kind of can solar recharging intelligent patrol detection flying robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720296262.6U CN206584484U (en) | 2017-03-24 | 2017-03-24 | It is a kind of can solar recharging intelligent patrol detection flying robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206584484U true CN206584484U (en) | 2017-10-24 |
Family
ID=60113930
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720296262.6U Active CN206584484U (en) | 2017-03-24 | 2017-03-24 | It is a kind of can solar recharging intelligent patrol detection flying robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206584484U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108594820A (en) * | 2018-05-04 | 2018-09-28 | 中国矿业大学 | A kind of crawler type Intelligent Mobile Robot active obstacle system and its control method |
| CN110165765A (en) * | 2018-11-12 | 2019-08-23 | 浙江大学山东工业技术研究院 | Outdoor moving robot charging system and charging method |
| CN113148188A (en) * | 2021-06-10 | 2021-07-23 | 宁波阿瑞斯自动化技术有限公司 | Dual-power vertical take-off and landing fixed-wing unmanned aerial vehicle |
| CN113794149A (en) * | 2021-08-14 | 2021-12-14 | 国家电网有限公司 | Underground cable conduit is with patrolling and examining robot |
| CN117438943A (en) * | 2023-10-24 | 2024-01-23 | 湖北顺安伟业科技有限公司 | Intelligent security device based on thing networking |
-
2017
- 2017-03-24 CN CN201720296262.6U patent/CN206584484U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108594820A (en) * | 2018-05-04 | 2018-09-28 | 中国矿业大学 | A kind of crawler type Intelligent Mobile Robot active obstacle system and its control method |
| CN110165765A (en) * | 2018-11-12 | 2019-08-23 | 浙江大学山东工业技术研究院 | Outdoor moving robot charging system and charging method |
| CN113148188A (en) * | 2021-06-10 | 2021-07-23 | 宁波阿瑞斯自动化技术有限公司 | Dual-power vertical take-off and landing fixed-wing unmanned aerial vehicle |
| CN113794149A (en) * | 2021-08-14 | 2021-12-14 | 国家电网有限公司 | Underground cable conduit is with patrolling and examining robot |
| CN113794149B (en) * | 2021-08-14 | 2023-04-07 | 国家电网有限公司 | Underground cable conduit is with patrolling and examining robot |
| CN117438943A (en) * | 2023-10-24 | 2024-01-23 | 湖北顺安伟业科技有限公司 | Intelligent security device based on thing networking |
| CN117438943B (en) * | 2023-10-24 | 2024-05-31 | 湖北顺安伟业科技有限公司 | Intelligent security device based on thing networking |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206584484U (en) | It is a kind of can solar recharging intelligent patrol detection flying robot | |
| CN105292398B (en) | A kind of unmanned boat-carrying unmanned plane hybrid system | |
| CA2929254C (en) | Unmanned aerial vehicle (uav) having vertical takeoff and landing (vtol) capability | |
| CN106887161B (en) | Unmanned aerial vehicle automatic take-off and landing management station, unmanned aerial vehicle automatic take-off and landing management system and method | |
| CN108230678B (en) | Traffic road monitoring system using unmanned aerial vehicle for monitoring | |
| CN108466567B (en) | Multi-functional unmanned plane moors steady charging platform and method | |
| CN206348665U (en) | A kind of heat distribution pipe network UAV Intelligent cruising inspection system based on Beidou navigation | |
| CN204808049U (en) | Communication system with unmanned aerial vehicle | |
| CN106909169A (en) | A kind of full automatic power patrol UAV system | |
| CN208367220U (en) | Nuclear pollution region nuclear radiation monitoring system based on unmanned plane | |
| CN106143821A (en) | A kind of unmanned boat boat-carrying hangar system | |
| CN204822097U (en) | Anti -jamming unmanned aerial vehicle system | |
| CN204373696U (en) | Based on the urban environment detection system of quadrotor | |
| CN104058099A (en) | Unmanned plane electro-optical pod | |
| CN204810432U (en) | Monitored control system with unmanned aerial vehicle | |
| CN106814752A (en) | A kind of round-the-clock City Surveillance System based on unmanned plane cluster | |
| CN204895881U (en) | Unmanned aerial vehicle system with thermal imaging system | |
| CN107014971B (en) | Underwater hiding-machine buoy base station with efficient charging and remote data transmission function | |
| CN104683759B (en) | Inner wall of stack corrosion condition wireless video monitoring apparatus and method for based on aircraft | |
| CN108762307A (en) | Skyscraper natural gas standpipe safety pre-warning system based on unmanned machine testing | |
| CN110480645A (en) | Cable duct of substation crusing robot based on temperature self-adaptation control | |
| CN205931243U (en) | Alert unmanned aerial vehicle that uses | |
| CN108803633A (en) | A kind of unmanned plane low latitude monitoring system based on mobile communications network | |
| CN204846371U (en) | Can keep away unmanned aerial vehicle system of barrier | |
| CN108082478B (en) | Early warning type unmanned aerial vehicle monitoring and investigation system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |