CN205931244U - Emergent unmanned aerial vehicle of fire control - Google Patents
Emergent unmanned aerial vehicle of fire control Download PDFInfo
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- CN205931244U CN205931244U CN201620879581.5U CN201620879581U CN205931244U CN 205931244 U CN205931244 U CN 205931244U CN 201620879581 U CN201620879581 U CN 201620879581U CN 205931244 U CN205931244 U CN 205931244U
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- unmanned plane
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- fire
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- data acquisition
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Abstract
The utility model discloses an emergent unmanned aerial vehicle of fire control, including rotor, unmanned aerial vehicle body, three -axis pan -tilt, data acquisition module and MC 51 the singlechip, the side of unmanned aerial vehicle body is fixed with rotor installation arm, but and zoom camera and infrared thermal imager's output all with image sensor's input electric connection, the internally mounted of unmanned aerial vehicle body has a GPS orientation module, GPS orientation module and image sensor's output all with data acquisition module's input electric connection, data acquisition module's output and MC 51 the input electric connection of singlechip, MC 51 the singlechip passes through data transfer module and remote control device electric connection. The utility model discloses a but zoom camera shoots the scene of fire, investigates the disaster of conflagration position, searches for ands rescue personnel through infrared thermal imager, and the accessible speaker is propagandaed directed to communicate simultaneously, through the relieve disaster delivery of article of air -drop device, and convenient to use, the practicality is strong.
Description
Technical field
This utility model is related to unmanned plane equipment technical field, specially a kind of fire-fighting emergent unmanned plane.
Background technology
UAV abbreviation unmanned plane, is to be manipulated with the presetting apparatus provided for oneself using radio robot
Not manned aircraft.Can be divided into from technical standpoint definition:Depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, no
People's dirigible, unmanned parasol etc.;Unmanned plane presses application, can be divided into military and civilian.When there is fire, all can set out to disappear
Anti- car is put out a fire, but fire fighting truck fire fighting limitation larger it is impossible to understand the situation within fire in depth, thus cannot make
Rescue method the most appropriate.
Utility model content
The purpose of this utility model is to provide a kind of fire-fighting emergent unmanned plane, to solve proposition in above-mentioned background technology
Problem, is had an advantageous effect in that:By varifocal camera, scene of fire is shot, the condition of a disaster of fire location is carried out
Personnel are searched and rescued by infrared thermography, can be propagandaed directed to communicate by speaker simultaneously, carried out by dropping gear by investigation
The delivery of disaster relief article, easy to use, practical.
For achieving the above object, this utility model provides following technical scheme:A kind of fire-fighting emergent unmanned plane, including rotation
The wing, unmanned plane body, three axle heads, data acquisition module and MC-51 single-chip microcomputer, the side of described unmanned plane body is fixed with rotation
Wing installing arm, the other end of rotor installing arm is provided with coupling, and the top of described coupling is provided with rotor, described unmanned plane
The bottom of body is fixed with two undercarriages, and is provided with three axle heads and dropping gear between two undercarriages, described three axle clouds
Varifocal camera or infrared thermography be provided with platform, and the outfan of varifocal camera and infrared thermography is all and image
The input of sensor is electrically connected with, and the inside of described unmanned plane body is provided with d GPS locating module, d GPS locating module and figure
As sensor outfan all with the electric connection of the input of data acquisition module, the outfan of described data acquisition module and
The input of MC-51 single-chip microcomputer is electrically connected with, the outfan of MC-51 single-chip microcomputer respectively with dropping gear controller and unmanned plane this
The input of the speaker of body front end is electrically connected with, and it is electrical with remote control device that described MC-51 single-chip microcomputer passes through digital transmission module
Connect.
Preferably, the side of described no human body is provided with four rotor installing arms, and four rotor installing arms are positioned at same
In one plane, the angle between adjacent rotor installing arm is 90 degree.
Preferably, the inside of described unmanned plane body is provided with memory module, and the input of memory module is mono- with MC-51
The outfan of piece machine is electrically connected with.
Preferably, it is provided with data transmission set and graphic transmission equipment in described digital transmission module.
Compared with prior art, the beneficial effects of the utility model are:This equipment passes through varifocal camera to scene of fire
Shot, the condition of a disaster of fire location is carried out investigations, by infrared thermography, personnel is searched and rescued, simultaneously can be by raising
Sound device is propagandaed directed to communicate, and carries out the delivery of disaster relief article by dropping gear, easy to use, practical.
Brief description
Fig. 1 installs the structural representation of varifocal camera for this utility model;
Fig. 2 installs portion's structural representation of thermal infrared imager for this utility model;
Fig. 3 is system block diagram of the present utility model.
In figure:1- rotor;2- coupling;3- rotor installing arm;4- unmanned plane body;5- speaker;6- undercarriage;7- is empty
Throw device;8- tri- axle head;The varifocal camera of 9-;10- infrared thermography;11- imageing sensor;12-GPS module;13- number
According to acquisition module;14-MC-51 single-chip microcomputer;14- dropping gear controller;16- digital transmission module;17- Remote terminal.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely description is it is clear that described embodiment is only a part of embodiment of this utility model rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of making creative work
The every other embodiment being obtained, broadly falls into the scope of this utility model protection.
Refer to Fig. 1-3, a kind of embodiment that this utility model provides:A kind of fire-fighting emergent unmanned plane, including rotor 1,
Unmanned plane body 4, three axle heads 8, data acquisition module 13 and MC-51 single-chip microcomputer 14, the side of unmanned plane body 4 is fixed with rotation
Wing installing arm 3, the side of no human body 4 is provided with four rotor installing arms 3, and four rotor installing arms 3 are generally aligned in the same plane
Interior, the angle between adjacent rotor installing arm 3 is 90 degree, and the other end of rotor installing arm 3 is provided with coupling 2, coupling 2
Top is provided with rotor 1, and the bottom of unmanned plane body 4 is fixed with two undercarriages 6, and is provided with three axles between two undercarriages 6
Head 8 and dropping gear 7, three axle heads 8 are provided with varifocal camera 9 or infrared thermography 10, and varifocal camera 9 He
The outfan of infrared thermography 10 is all electrically connected with the input of imageing sensor 11, and the inside of unmanned plane body 4 is installed
There is a d GPS locating module 12, the outfan of d GPS locating module 12 and imageing sensor 11 input all with data acquisition module 13
It is electrically connected with, the outfan of data acquisition module 13 is electrically connected with the input of MC-51 single-chip microcomputer 14, unmanned plane body 4
Inside is provided with memory module, and the input of memory module is electrically connected with the outfan of MC-51 single-chip microcomputer 14, and MC-51 is mono-
The outfan of piece machine 14 is electrically connected with the input of dropping gear controller 15 and the speaker 5 of unmanned plane body 4 front end respectively
Connect, MC-51 single-chip microcomputer 14 is electrically connected with remote control device 17 by digital transmission module 16, be provided with data in digital transmission module 16 and pass
Transfer device and graphic transmission equipment.
Operation principle:During use, first pass through remote control unit and control unmanned plane during flying to appointed place, then pass through variable
Burnt camera 9 carries out investigations to scene of fire, by infrared thermography 10, personnel is searched and rescued, and can pass through speaker 4 simultaneously
Propagandaed directed to communicate, carried out the delivery of disaster relief article, the picture that varifocal camera 9 is gathered with infrared thermography 10 by dropping gear 7
Face is transmitted to data acquisition module 13 by imageing sensor 11, is then sent to Remote eventually by digital transmission module 16
End.
It is obvious to a person skilled in the art that this 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, this practicality can be realized in other specific forms new
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, this practicality is new
The scope of type is limited by claims rather than described above, it is intended that the containing of equivalency that will fall in claim
All changes in justice and scope are included in this utility model.Any reference in claim should not be considered as limiting
Involved claim.
Claims (4)
1. a kind of fire-fighting emergent unmanned plane, including rotor(1), unmanned plane body(4), three axle heads(8), data acquisition module
(13)With MC-51 single-chip microcomputer(14)It is characterised in that:Described unmanned plane body(4)Side be fixed with rotor installing arm(3),
Rotor installing arm(3)The other end coupling is installed(2), described coupling(2)Top rotor is installed(1), described nothing
Man-machine body(4)Bottom be fixed with two undercarriages(6), and two undercarriages(6)Between three axle heads are installed(8)And air-drop
Device(7), described three axle heads(8)On varifocal camera is installed(9)Or infrared thermography(10), and varifocal camera
(9)And infrared thermography(10)Outfan all and imageing sensor(11)Input be electrically connected with, described unmanned plane this
Body(4)Inside d GPS locating module is installed(12), d GPS locating module(12)With imageing sensor(11)Outfan all with
Data acquisition module(13)Input be electrically connected with, described data acquisition module(13)Outfan and MC-51 single-chip microcomputer
(14)Input be electrically connected with, MC-51 single-chip microcomputer(14)Outfan respectively with dropping gear controller(15)And unmanned plane
Body(4)The speaker of front end(5)Input be electrically connected with, described MC-51 single-chip microcomputer(14)By digital transmission module(16)With
Remote control device(17)It is electrically connected with.
2. a kind of fire-fighting emergent unmanned plane according to claim 1 it is characterised in that:Described no human body(4)Side
Four rotor installing arms are installed(3), and four rotor installing arms(3)In being generally aligned in the same plane, adjacent rotor installing arm(3)It
Between angle be 90 degree.
3. a kind of fire-fighting emergent unmanned plane according to claim 1 it is characterised in that:Described unmanned plane body(4)Interior
Portion is provided with memory module, and the input of memory module and MC-51 single-chip microcomputer(14)Outfan be electrically connected with.
4. a kind of fire-fighting emergent unmanned plane according to claim 1 it is characterised in that:Described digital transmission module(16)In be provided with
Data transmission set and graphic transmission equipment.
Priority Applications (1)
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CN201620879581.5U CN205931244U (en) | 2016-08-15 | 2016-08-15 | Emergent unmanned aerial vehicle of fire control |
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CN201620879581.5U CN205931244U (en) | 2016-08-15 | 2016-08-15 | Emergent unmanned aerial vehicle of fire control |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107145146A (en) * | 2017-04-21 | 2017-09-08 | 成都梵辰科技有限公司 | The unmanned plane and its rescue method searched and rescued for disaster area |
CN107218970A (en) * | 2017-05-24 | 2017-09-29 | 中国矿业大学 | Unmanned aerial vehicle for monitoring distribution and combustion situation of coal field fire area and method thereof |
CN108583882A (en) * | 2018-04-16 | 2018-09-28 | 钱文娟 | A kind of fire-fighting and rescue unmanned plane |
CN110065633A (en) * | 2019-04-11 | 2019-07-30 | 东华大学 | Multi-source Information Fusion search and rescue system based on multi-rotor unmanned aerial vehicle |
CN113835116A (en) * | 2020-06-24 | 2021-12-24 | 河南铭视科技股份有限公司 | Disaster situation position determining system |
WO2022110242A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Firefighting unmanned aerial vehicle |
-
2016
- 2016-08-15 CN CN201620879581.5U patent/CN205931244U/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107145146A (en) * | 2017-04-21 | 2017-09-08 | 成都梵辰科技有限公司 | The unmanned plane and its rescue method searched and rescued for disaster area |
CN107218970A (en) * | 2017-05-24 | 2017-09-29 | 中国矿业大学 | Unmanned aerial vehicle for monitoring distribution and combustion situation of coal field fire area and method thereof |
CN108583882A (en) * | 2018-04-16 | 2018-09-28 | 钱文娟 | A kind of fire-fighting and rescue unmanned plane |
CN110065633A (en) * | 2019-04-11 | 2019-07-30 | 东华大学 | Multi-source Information Fusion search and rescue system based on multi-rotor unmanned aerial vehicle |
CN113835116A (en) * | 2020-06-24 | 2021-12-24 | 河南铭视科技股份有限公司 | Disaster situation position determining system |
CN113835116B (en) * | 2020-06-24 | 2024-05-17 | 河南铭视科技股份有限公司 | Disaster situation position determining system |
WO2022110242A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Firefighting unmanned aerial vehicle |
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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: 20170208 Termination date: 20210815 |
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CF01 | Termination of patent right due to non-payment of annual fee |