CN206856980U - A kind of disaster field infrared imaging flying robot - Google Patents
A kind of disaster field infrared imaging flying robot Download PDFInfo
- Publication number
- CN206856980U CN206856980U CN201720487224.9U CN201720487224U CN206856980U CN 206856980 U CN206856980 U CN 206856980U CN 201720487224 U CN201720487224 U CN 201720487224U CN 206856980 U CN206856980 U CN 206856980U
- Authority
- CN
- China
- Prior art keywords
- rotor
- flying robot
- infrared imaging
- disaster field
- camera
- 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.)
- Expired - Fee Related
Links
Landscapes
- Manipulator (AREA)
- Studio Devices (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
The utility model discloses a kind of disaster field infrared imaging flying robot,Including device body,Described device body is by the power set that are arranged at the top of the device body and is arranged on the connecting rod of the power set bottom and spherical camera is formed,The power set are by the wireless launcher that is arranged at the top of the power set and are arranged on the rotor plate of the wireless launcher bottom and motor is formed,This kind of disaster field infrared imaging flying robot,With small,The features such as mobility strong and powerful shooting efficiency,It is particularly suitable for being reconnoitred in disaster field,Take pictures,Operation is even searched in evidence obtaining,Simultaneously,What the rotor of this kind of flying robot used in itself is exactly the rotor of solar energy material,It can work while converting solar energy into electric energy,So as to solve traditional flying robot caused during carrying out long-distance survey flight electricity can not regular supply the shortcomings that.
Description
Technical field
Flying robot's technical field is the utility model is related to, specially a kind of disaster field infrared imaging flying machine
People.
Background technology
The species of flying robot is various, and common Miniature Vehicle robot has mobility good, and takeoff and anding place is small,
Can be in a wide range of the advantages that maneuvering flight, therefore there is quite extensive purposes.In some use occasions, flying robot can
To realize that low latitude monitors in real time, the image clearly and high resolution of acquisition, it goes for the fire prevention in forest field and city
Field, the Scout robots such as tour, aerial shooting are equipped with state-of-the-art information gathering system in the world, available for tracking crime
Violate and public activity of keeping one's watch in secret is easy to carry.Scout and its notebook type control panel can put into a suitcase, be easy to secret
Carry and be also easy to be deployed in any crowd overhead simultaneously, available for the monitoring task of the military, can also carry out commonly monitoring work.
With the rapid development of science and technology, the species of flying robot is also more and more, and function also tends to improvement, existing
Some aircraft easily cause electricity due to the reasonable employment of its uncontrollable electric energy during long-distance survey flight is carried out
Can not regular supply, while existing flying machine human body type is generally bigger than normal, and the help to the prospecting of special disaster field is smaller.
So how to design a kind of disaster field infrared imaging flying robot, turn into that we currently to be solved asks
Topic.
The content of the invention
The purpose of this utility model is to provide a kind of disaster field infrared imaging flying robot, to solve the above-mentioned back of the body
The problem of being proposed in scape technology.
To achieve the above object, the utility model provides following technical scheme：A kind of disaster field infrared imaging flight
Robot, including device body, described device body is by the power set that are arranged at the top of the device body and is arranged on this and moves
The connecting rod and spherical camera of power apparatus bottom are formed, and the power set are by the wireless transmission that is arranged at the top of the power set
Device and it is arranged on the rotor plate of the wireless launcher bottom and motor is formed, the top of the spherical camera is provided with rotating shaft, and
The rotating shaft is fixedly connected with spherical camera, and the bottom of the motor is provided with energy-storage battery, and the connecting rod runs through the energy storage
Battery, and insertion is arranged in motor, and the end of the connecting rod is connected with motor and rotating shaft transmission respectively, the rotor plate
Side surrounds the equally distributed rotor mounting hole of the rotor plate provided with several, and the side of the rotor mounting hole is provided with solar energy
Rotor, and solar energy rotor insertion is arranged in rotor mounting hole, and pressure, the motor are applied to rotor mounting hole
Side be provided with four core MAIL-T628GPU, and four core MAIL-T628GPU insertions are arranged in power set, described four
Core MAIL-T628GPU side is provided with image collector, heat energy imager, DSP process chips and ZigBee communication chip, and
Described image collector, heat energy imager, DSP process chips and ZigBee communication chip are welded in four core MAIL-T628GPU
Top, described image collector, heat energy imager, DSP process chips and ZigBee communication chip with four core MAIL-
T628GPU signals connect, and the side of the spherical camera is provided with rotating disk, and the rotating disk nesting is arranged on spherical camera
On, and be flexibly connected with the spherical camera, the rotating disk is electrically connected with motor.
Further, the side of the solar energy rotor is provided with anticollision frame, and the centre position of the anticollision frame with it is wireless
Transmitter is fixedly connected.
Further, rain cover is installed, and the rain cover is arranged on ball with nested at the top of the spherical camera
On shape camera, and it is fixedly connected with connecting rod.
Further, the top of the wireless launcher is provided with transmitting antenna, and the transmitting antenna and ZigBee communication
Chip is electrically connected with.
Further, the bottom of the spherical camera is provided with IR sensor, and the IR sensor and heat energy
Imager is electrically connected with.
Further, the side of described image collector is provided with internal memory, and the internal memory is connected with image collector signal.
Further, the side of the rotating disk is provided with several full-view cameras, and the full-view camera surrounds rotating disk
It is uniformly distributed.
Further, the full-view camera and image collector are electrically connected with, the solar energy rotor and motor with
Energy-storage battery is electrically connected with.
Compared with prior art, the beneficial effects of the utility model are：This kind of disaster field infrared imaging flying machine
People, have the characteristics that small, mobility strong and shooting efficiency are powerful, be particularly suitable for being reconnoitred in disaster field, take pictures, take
Card even searches operation, meanwhile, what the rotor of this kind of flying robot used in itself is exactly the rotor of solar energy material, Neng Gouyi
Side works while electric energy is converted solar energy into, so as to solve mistake of traditional flying robot in the long-distance survey flight of progress
Caused in journey electricity can not regular supply the shortcomings that, in addition, full-view camera and IR sensor can also enter to disaster field
The careful evidence obtaining of taking pictures of row, and life searching, the labor intensity of staff is greatly reduced, having in future widely makes
Use prospect.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is power set partial structural diagram of the present utility model；
Fig. 3 is spherical camera partial structural diagram of the present utility model；
Fig. 4 is four core MAIL-T628GPU partial structural diagrams of the present utility model；
In figure：1- device bodies；2- power set；3- connecting rods；4- spherical cameras；The core MAIL-T628GPU of 5- tetra-；6-
Anticollision frame；7- solar energy rotors；8- energy-storage batteries；9- multi-directional balls；10- motors；11- rain covers；12- transmitting antennas；13- turns
Axle；14- rotor plates；15- wireless launchers；16- rotor mounting holes；17- full-view cameras；18- IR sensors；At 19-DSP
Manage chip；20-ZigBee communication chips；21- internal memories；22- image collectors；23- heat energy imagers；24- rotating disks.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, 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, belong to the scope of the utility model protection.
Fig. 1-4 are referred to, the utility model provides a kind of technical scheme：A kind of disaster field infrared imaging flying machine
People, including device body 1, described device body 1 are moved by being arranged on the power set 2 at the top of device body 1 and being arranged on this
The connecting rod 3 and spherical camera 4 of the bottom of power apparatus 2 are formed, and the power set 2 are by being arranged on the nothing at the top of the power set 2
Line transmitter 15 and it is arranged on the rotor plate 14 of the bottom of wireless launcher 15 and motor 10 is formed, the spherical camera 4
Top is provided with rotating shaft 13, and the rotating shaft 13 is fixedly connected with spherical camera 4, and the bottom of the motor 10 is provided with energy-storage battery
8, the connecting rod 3 runs through the energy-storage battery 8, and insertion is arranged in motor 10, and the end of the connecting rod 3 respectively with motor
10 and rotating shaft 13 be connected, the side of the rotor plate 14 is provided with several around the 14 equally distributed rotor of rotor plate peace
Hole 16 is filled, the side of the rotor mounting hole 16 is provided with solar energy rotor 7, and the solar energy rotor 7 insertion is arranged on rotor
In mounting hole 16, and pressure being applied to rotor mounting hole 16, the side of the motor 10 is provided with four core MAIL-T628GPU5, and
The four core MAIL-T628GPU5 insertions are arranged in power set 2, and the side of the four core MAIL-T628GPU5 is provided with figure
Picture collector 22, heat energy imager 23, DSP process chips 19 and ZigBee communication chip 20, and described image collector 22, heat
Energy imager 23, DSP process chips 19 and ZigBee communication chip 20 are welded at the top of four core MAIL-T628GPU5, described
Image collector 22, heat energy imager 23, DSP process chips 19 and ZigBee communication chip 20 with four core MAIL-
T628GPU5 signals connect, and the side of the spherical camera 4 is provided with rotating disk 24, and the nesting of the rotating disk 24 is arranged on spherical take the photograph
On first 4, and it is flexibly connected with the spherical camera 4, the rotating disk 24 is electrically connected with motor 10.
Further, the side of the solar energy rotor 7 is provided with anticollision frame 6, and the centre position of the anticollision frame 6 and nothing
Line transmitter 15 is fixedly connected, and the anticollision frame 6 can facilitate to be used in the different broken disaster fields for changing degree, prevent rotor by
Damage.
Further, the top of the spherical camera 4 is provided with rain cover 11, and the rain cover 11 is set with nested
It is fixedly connected on spherical camera 4, and with connecting rod 3, the rain cover 11 mainly prevents the rainwater of spherical camera 4 from Qi Ding
Portion enters, and causes device damage.
Further, the top of the wireless launcher 15 is provided with transmitting antenna 12, and the transmitting antenna 12 with
ZigBee communication chip 20 is electrically connected with, and the transmitting antenna 12 can increase the emission effciency of wireless signal.
Further, the bottom of the spherical camera 4 is provided with IR sensor 18, and the IR sensor 18 with
Heat energy imager 23 is electrically connected with, and the IR sensor 18 effectively can enter live body life of the ground even below ruins
Row imaging.
Further, the side of described image collector 22 is provided with internal memory 21, and the internal memory 21 and image collector 22
Signal is connected, and the internal memory 21 effectively can be preserved the signal that image collector 22 is collected, and facilitate follow-up data
Integrate.
Further, the side of the rotating disk 24 is provided with several full-view cameras 17, and the full-view camera 17 encloses
It is uniformly distributed around rotating disk 24, scene can be carried out pan-shot by the full-view camera 17.
Further, the full-view camera 17 is electrically connected with image collector 22, the solar energy rotor 7 and motor
10 are electrically connected with energy-storage battery 8, and the energy-storage battery 8 at any time can be stored up the electric energy conversion in solar energy rotor 7
Deposit.
Operation principle：Four core MAIL-T628GPU5 are inserted in power set 2 first, it is main due to flying robot
Control device is exactly four core MAIL-T628GPU5, so DSP process chips 19 become remote controllers, subsequent staff is just
Four core MAIL-T628GPU5 can be carried out by remote control on the ground and controlled, carry out disaster field flight operation
When, flying robot can shoot according to instruction to disaster field, because the side of spherical camera 4 is provided with rotating disk 24,
And rotating disk 24 is flexibly connected with spherical camera 4, and be electrically connected with motor 10, at the same the side of rotating disk 24 be provided with it is multiple complete
Scape camera 17 can be shot the multi-faceted information at scene, and transmit signals to image collector 22, at the same time,
Live body life of the ground even below ruins effectively can be imaged by IR sensor 18, and transmit signals to heat energy
Imager 23, final image collector 22 and heat energy imager 23 further can be protected image information by internal memory 21
Deposit, and information from wireless launcher 15 is beamed back by ground receiving wastewater facility by ZigBee communication chip 20, it is important that this kind
What the rotor of flying robot used in itself is exactly the rotor of solar energy material, can be worked while converting solar energy into
Electric energy, and recycled by energy-storage battery 8, for this, staff need not worry very much electric energy of the aircraft without abundance.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (8)
1. a kind of disaster field infrared imaging flying robot, including device body (1), it is characterised in that：Described device sheet
Body (1) is by the power set (2) that are arranged at the top of the device body (1) and the connecting rod (3) for being arranged on power set (2) bottom
Formed with spherical camera (4), the power set (2) are by the wireless launcher (15) that is arranged at the top of the power set (2)
And it is arranged on the rotor plate (14) and motor (10) composition of wireless launcher (15) bottom, the top of the spherical camera (4)
End is provided with rotating shaft (13), and the rotating shaft (13) is fixedly connected with spherical camera (4), and the bottom of the motor (10) is provided with storage
Energy battery (8), the connecting rod (3) runs through the energy-storage battery (8), and insertion is arranged in motor (10), and the connecting rod (3)
End be connected respectively with motor (10) and rotating shaft (13), the side of the rotor plate (14) surrounds the rotation provided with several
The equally distributed rotor mounting hole (16) of wing plate (14), the side of the rotor mounting hole (16) are provided with solar energy rotor (7), and
Solar energy rotor (7) insertion is arranged in rotor mounting hole (16), and applies pressure, the electricity to rotor mounting hole (16)
The side of machine (10) is provided with four core MAIL-T628GPU (5), and the embedded power that is arranged on of the four core MAIL-T628GPU (5) fills
Put in (2), the side of the four core MAIL-T628GPU (5) is provided with image collector (22), heat energy imager (23), at DSP
Manage chip (19) and ZigBee communication chip (20), and described image collector (22), heat energy imager (23), DSP processing core
Piece (19) and ZigBee communication chip (20) are welded at the top of four core MAIL-T628GPU (5), described image collector (22),
Heat energy imager (23), DSP process chips (19) and ZigBee communication chip (20) with four core MAIL-T628GPU (5) signals
Connection, the side of the spherical camera (4) is provided with rotating disk (24), and the rotating disk (24) nesting is arranged on spherical camera
(4) on, and it is flexibly connected with the spherical camera (4), the rotating disk (24) is electrically connected with motor (10).
A kind of 2. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：The sun
The side of energy rotor (7) is provided with anticollision frame (6), and the centre position of the anticollision frame (6) and the fixed company of wireless launcher (15)
Connect.
A kind of 3. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：It is described spherical
Rain cover (11) is installed at the top of camera (4), and the rain cover (11) nesting is arranged on spherical camera (4), and
It is fixedly connected with connecting rod (3).
A kind of 4. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：It is described wireless
The top of transmitter (15) is provided with transmitting antenna (12), and the transmitting antenna (12) electrically connects with ZigBee communication chip (20)
Connect.
A kind of 5. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：It is described spherical
The bottom of camera (4) is provided with IR sensor (18), and the IR sensor (18) and heat energy imager (23) are electrical
Connection.
A kind of 6. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：Described image
The side of collector (22) is provided with internal memory (21), and the internal memory (21) is connected with image collector (22) signal.
A kind of 7. disaster field infrared imaging flying robot according to claim 1, it is characterised in that：The rotating disk
(24) side is provided with several full-view cameras (17), and the full-view camera (17) is uniformly distributed around rotating disk (24).
A kind of 8. disaster field infrared imaging flying robot according to claim 7, it is characterised in that：The panorama
Camera (17) and image collector (22) are electrically connected with, the solar energy rotor (7) and motor (10) with energy-storage battery (8)
It is electrically connected with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720487224.9U CN206856980U (en) | 2017-05-04 | 2017-05-04 | A kind of disaster field infrared imaging flying robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720487224.9U CN206856980U (en) | 2017-05-04 | 2017-05-04 | A kind of disaster field infrared imaging flying robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206856980U true CN206856980U (en) | 2018-01-09 |
Family
ID=60823406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720487224.9U Expired - Fee Related CN206856980U (en) | 2017-05-04 | 2017-05-04 | A kind of disaster field infrared imaging flying robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206856980U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995796A (en) * | 2018-07-16 | 2018-12-14 | 福州日兆信息科技有限公司 | Unmanned plane is used in a kind of prospecting of communication iron tower regional site |
-
2017
- 2017-05-04 CN CN201720487224.9U patent/CN206856980U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995796A (en) * | 2018-07-16 | 2018-12-14 | 福州日兆信息科技有限公司 | Unmanned plane is used in a kind of prospecting of communication iron tower regional site |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104503349A (en) | Monitoring device based on unmanned aerial vehicle | |
| CN204808049U (en) | Communication system with unmanned aerial vehicle | |
| CN104058099A (en) | Unmanned plane electro-optical pod | |
| CN203405206U (en) | Panoramic image unmanned aerial vehicle acquisition system | |
| US20080272233A1 (en) | Method and system for generating renewable energy | |
| CN210391577U (en) | Small-size two optical nacelle of triaxial | |
| CN109510972A (en) | A kind of wild animal intelligent surveillance method based on Internet of Things | |
| CN204810432U (en) | Monitored control system with unmanned aerial vehicle | |
| CN107943084B (en) | Following type electromagnetic interference system and method for civil multi-rotor unmanned aerial vehicle | |
| CN104469283B (en) | The micro-unmanned airborne real-time omnidirectional imaging system of one kind and equipment | |
| CN110341948A (en) | A kind of primary and secondary cooperating type inspection flying robot | |
| CN206856980U (en) | A kind of disaster field infrared imaging flying robot | |
| CN206100310U (en) | Oblique photography monitored control system for unmanned aerial vehicle | |
| CN208070018U (en) | A kind of unmanned plane of taking photo by plane being easily installed camera | |
| CN107082115A (en) | A kind of disaster field infrared imaging flying robot | |
| CN210000581U (en) | physical combined unmanned aerial vehicle cluster | |
| CN206223152U (en) | A kind of remote sensing texture information harvester | |
| CN206060685U (en) | A kind of photovoltaic panel hot spot effect detecting system | |
| CN207036116U (en) | Mark rod for outdoor remote sensing mapping | |
| CN203289576U (en) | Portable 3g wireless solar energy monitoring system | |
| CN113433963B (en) | Unmanned aerial vehicle multi-platform system and method for magnetic suspension track inspection | |
| CN212766734U (en) | Visual target tracking device based on quad-rotor unmanned aerial vehicle | |
| CN105836144B (en) | A kind of airborne power supply system of multi-rotor unmanned aerial vehicle | |
| CN214057847U (en) | Surface of water environmental monitoring unmanned aerial vehicle that cruises | |
| CN204206337U (en) | A kind of micro-unmanned airborne real-time omnidirectional imaging system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180109 Termination date: 20190504 |