CN206734624U - Atmosphere environment supervision unmanned plane - Google Patents
Atmosphere environment supervision unmanned plane Download PDFInfo
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- CN206734624U CN206734624U CN201720298854.1U CN201720298854U CN206734624U CN 206734624 U CN206734624 U CN 206734624U CN 201720298854 U CN201720298854 U CN 201720298854U CN 206734624 U CN206734624 U CN 206734624U
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- China
- Prior art keywords
- unmanned plane
- mechanical arm
- atmosphere environment
- main body
- environment supervision
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- 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.)
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- 230000005611 electricity Effects 0.000 claims abstract description 17
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 11
- 239000000523 sample Substances 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims abstract description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 6
- 230000005540 biological transmission Effects 0.000 claims description 12
- 230000003416 augmentation Effects 0.000 claims description 6
- 239000000835 fiber Substances 0.000 abstract description 5
- 238000011160 research Methods 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 abstract description 3
- 238000012544 monitoring process Methods 0.000 description 8
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 239000000809 air pollutant Substances 0.000 description 1
- 231100001243 air pollutant Toxicity 0.000 description 1
- 230000034303 cell budding Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000005416 organic matter Substances 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 239000012855 volatile organic compound Substances 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
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Abstract
The utility model discloses a kind of atmosphere environment supervision unmanned plane, including one or more sensor probes, a pair of undercarriages, unmanned plane mechanical arm, big torsion steering wheel, dynamic lithium battery, body electricity She areas, unmanned plane main body and remote control.The utility model can possess the cruising time for being longer than 50 minutes, and ultimate load is up to more than 7kg, execution task that can be in the longer time or the self-defined more research equipments of carrying;It is made of carbon fibre material, has the advantages that heat-resist, structural strength is high, hardness is higher, is not susceptible to deformation;By real-time return data and draw a diagram, so that technical staff uses.
Description
Technical field
It the utility model is related to a kind of unmanned machine equipment, more particularly to a kind of atmosphere environment supervision unmanned plane.
Background technology
Four rotor wing unmanned aerial vehicles are a kind of widely used at present, and hover stable and easy to use, the unmanned plane to save space,
At this stage, China's air quality and the monitoring of waste gas emission source are set by artificial sample and analysis costly mostly
It is standby.However, under the increasingly serious background of air environmental pollution problem, this means are limited by time and cost, it is difficult to
Realize the long-term purpose for effectively monitoring atmosphere quality in real time.Fixed-wing unmanned plane requires higher to site requirements and operation,
It can not hover, and it is not readily portable.
Armed unmanned plane is still in the budding stage at present, and unmanned plane mechanical arm is used only for capturing object and tests rank
Section.
Utility model content
The purpose of this utility model:A kind of atmosphere environment supervision unmanned plane is provided, based on the real-time of atmosphere quality
Monitoring prevention, using advantages such as the low cost of unmanned plane, intellectuality, high accuracy, it is flat to build a moveable monitoring in real time
Platform, the point or non point source of pollution larger for some monitoring difficulty, accomplish effective air quality monitoring and data transfer in real time.Together
When supporting analysis system, analysis in real time is carried out to Monitoring Data and is drawn, is that state enterprise and scientific research institutions' reply are various complicated big
Compression ring border provides effective data supporting.
To achieve these goals, the technical solution of the utility model is:
A kind of atmosphere environment supervision unmanned plane, including one or more sensor probes, a pair of undercarriages, unmanned plane machinery
Arm, big torsion steering wheel, dynamic lithium battery, body electricity She areas, unmanned plane main body and remote control;Described body electricity She areas installation
In described unmanned plane main body, described dynamic lithium battery is hung on the bottom of described unmanned plane main body, described a pair
Undercarriage is symmetrically arranged at the both ends of described unmanned plane main body;Described unmanned plane mechanical arm is carbon fibre materials system
Into described unmanned plane mechanical arm is provided with hollow-out parts, and the wheelbase of described unmanned plane mechanical arm is 640mm;Described nobody
One end of machine mechanical arm is connected wherein on the undercarriage described in one by described big torsion steering wheel, described unmanned plane machine
Tool arm is located at the lower section of described undercarriage, and is flipped to the outside by described big torsion steering wheel, described one or more
Sensor probe is separately positioned on the other end of described unmanned plane mechanical arm;Described remote control includes remote control and reception
Machine, described receiver are arranged in described unmanned plane main body, described remote control and described receiver wireless connection.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, described unmanned plane mechanical arm is provided with 4K levels video camera and three
Axle increases steady brushless head.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, described unmanned plane main body is provided with image transmission, described
Image transmission include that figure passes transmitting terminal, figure passes ground receiver end and OSD devices, described figure passes transmitting terminal, figure passes ground
Face receiving terminal and OSD devices are connected with described 4K levels video camera and the brushless head of three-axis stability augmentation.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, the total length of described unmanned plane mechanical arm is 1m.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, described body electricity She areas include brushless electric machine, motor cabinet and nothing
Brush electricity is adjusted, and described brushless electric machine, motor cabinet and brushless electricity are adjusted and be connected respectively with described unmanned plane mechanical arm, and by described
Dynamic lithium battery is powered.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, it is provided with data processing software and number in described unmanned plane main body
According to transmitting device.
Above-mentioned atmosphere environment supervision unmanned plane, wherein, described data transmission device includes sensor and GPRS data
Transmitter.
The utility model can possess the cruising time for being longer than 50 minutes, and ultimate load, can be when longer up to more than 7kg
Between execution task or self-defined carry more research equipments;It is made of carbon fibre material, there is heat-resist, structure
Intensity is high, hardness is higher, is not susceptible to the advantages that deformation;By real-time return data and draw a diagram, so that technical staff makes
With.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model atmosphere environment supervision unmanned plane.
Fig. 2 is the structural representation of the unmanned plane mechanical arm expansion of the utility model atmosphere environment supervision unmanned plane.
Embodiment
Embodiment of the present utility model is further illustrated below in conjunction with accompanying drawing.
Refer to shown in accompanying drawing 1 and accompanying drawing 2, a kind of atmosphere environment supervision unmanned plane, including one or more sensors are visited
First 1, a pair of undercarriages 2, unmanned plane mechanical arm 3, big torsion steering wheel 4, dynamic lithium battery 5, body electricity She areas 6, unmanned plane main body 7
And remote control;Described body electricity She areas 6 are arranged in described unmanned plane main body 7, and described dynamic lithium battery 5 is hung on
The bottom of described unmanned plane main body 7, described a pair of undercarriages 2 are symmetrically arranged at the two of described unmanned plane main body 7
End;Described unmanned plane mechanical arm 3 is made up of carbon fibre materials, and described unmanned plane mechanical arm 3 is provided with hollow-out parts, described
The wheelbase of unmanned plane mechanical arm 3 is 640mm;One end of described unmanned plane mechanical arm 3 is connected by described big torsion steering wheel 4
Wherein on the undercarriage 2 described in one, described unmanned plane mechanical arm 3 is located at the lower section of described undercarriage 2, and passes through institute
The big torsion steering wheel 4 stated flips to the outside, and described one or more sensor probes 1 are separately positioned on described unmanned plane machine
The other end of tool arm 3;Described remote control includes remote control and receiver, and described receiver is arranged on described unmanned plane
In main body 7, described remote control and described receiver wireless connection.
Described unmanned plane mechanical arm 3 is provided with 4K levels video camera and the brushless head of three-axis stability augmentation, and 4K levels can be controlled to take the photograph
360 degree of camera verts and ensures that camera image stabilization is without friction, can also coordinate the brushless head of three-axis stability augmentation by remote control system
Control focal length, shooting and the video recording of camera.
The total length of described unmanned plane mechanical arm 3 is 1m, the kg of maximum capacity 1, highest can bearing temperature 1500 it is Celsius
Degree, cruising time is up to 50 more than min.
Described unmanned plane main body 7 is provided with image transmission, described image transmission include figure pass transmitting terminal,
Figure passes ground receiver end and OSD devices, and described figure passes transmitting terminal, figure passes ground receiver end and OSD devices and described 4K levels
Video camera and the brushless head connection of three-axis stability augmentation, the no-delay figure biography ground of passing back of the image of 4K levels video camera shooting can be connect
Receiving end, and every flying quality of unmanned plane is enclosed, it is easy to pilot operator to read;Control is flown using standard-sized sheet source, voluntarily write winged
Line program, can designed, designed OSD interfaces, self-defining various functions, OSD is screen menu type regulative mode, is usually pressed
The rectangle menu for the display items reconciling items information that screen ejects after Menu keys, can be by the menu to display items work
Make index to be adjusted including color, pattern, geometry etc., so as to reach optimal use state.
Described body electricity She areas 6 include brushless electric machine, motor cabinet and brushless electricity and adjusted, described brushless electric machine, motor cabinet
And brushless electricity is adjusted and is connected respectively with described unmanned plane mechanical arm 3, and powered by described dynamic lithium battery 5.It can use
The brushless electric machines of MARATHON 4108 and the brushless electricity of 40A are adjusted, and coordinate the 1555 complete positive and negative oars of carbon fiber, rotating speed is 600 revs/min, single
Motor maximum pull 2kg.
Data processing software and data transmission device are provided with described unmanned plane main body 7, can be to by sensor and number
The data passed back according to transport module are recompiled and taxonomic revision, make its easily readable, and can be with automatically generated data
Record and statistical table.
Described data transmission device includes sensor and GPRS data transmitter, sensor probe 1 can be collected into
Data transmitted in a manner of GPRS signals to each terminal.The air quality data of collection is transmitted by GPRS data, and in office
Meaning terminal reads analyze data in real time.
The utility model can change frequency range and transmission power according to demand by remote control, and unmanned plane is controlled
System, the flight control system of unmanned plane main body 7 are independently edited entirely, and are connected with power facility dynamic lithium battery 5 and remote control
Connect, the offline mode and flight auxiliary, built-in 3 axle, 16 high accuracy gyroscope instrument, 3 14, axle high accuracy that can support various kinds add
Speedometer/magnetometer, 6 axis accelerometers/magnetometer, MS5611 high accuracy barometers.
Sensor probe 1 can measure the scope of particulate matter:PM1.0 (0 ~ 999 μ g/m3), PM2.5(0~999μg/m3),
PM10 (0 ~ 999 μ g/m3), operating ambient temperature are -10 ~ 650C, humidity:0-99%RH.Volatile organic matter(VOCs)Survey
Amount scope is 0-500 ppm, resolution ratio:1 ppm, measurement error:3%FS, response time<6min.The utility model can be taken simultaneously
Band various air pollutants sensor probe 1, it is accurate to determine every atmosphere pollution numerical value under complex environment.
Unmanned plane mechanical arm 3 can meet light weight, the high requirement of intensity.Common unmanned plane mechanical arm is using such as
PP1120HF materials are made, and its tensile strength is 50kg/cm2, and carbon fiber is then up to 2 × 10^7kg/cm2.PP1120HF's
Heat distortion temperature is 150 degrees Celsius, and carbon fiber is then up to more than 1500 degrees Celsius.High temperature resistant mechanical arm designs, and binds simultaneously
Sensor probe 1, it can accurately determine every pollutant numerical value of the point.
The utility model has easy to use, full-featured, security compared with traditional atmosphere environment supervision unmanned plane
The four big outstanding advantages such as height, advanced technology, can be to putting accurate monitoring because the utility model is equipped with mechanical arm, and can be with
The environment that can not go deep into for a variety of unmanned planes, its supporting data processing software can also be such that researcher is read in multiple terminals
Take it to return in real time and have been subjected to the data of processing, eliminate cumbersome manual analysis step.The atmosphere environment supervision unmanned plane
The requirements of the industry to atmosphere environment supervision such as environmental administration, scientific research institutions, all kinds of gases discharge enterprise will be met.
The utility model can carry ultrasonic wave module, coordinate winged control to possess automatic obstacle-avoiding and complete intelligent automatic cruising function.
In summary, the utility model can possess the cruising time for being longer than 50 minutes, and ultimate load, can up to more than 7kg
With in the execution task of longer time or the self-defined more research equipments of carrying;It is made, is had resistance to of carbon fibre material
It is hot it is good, structural strength is high, hardness is higher, is not susceptible to the advantages that deformation;By real-time return data and draw a diagram, so as to
Technical staff uses.
Preferred embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model,
Every equivalent structure transformation made using the utility model description, or it is directly or indirectly related with other are attached to
The technical field of product, similarly it is included in scope of patent protection of the present utility model.
Claims (7)
- A kind of 1. atmosphere environment supervision unmanned plane, it is characterised in that:Including one or more sensor probes, a pair of undercarriages, Unmanned plane mechanical arm, big torsion steering wheel, dynamic lithium battery, body electricity She areas, unmanned plane main body and remote control;Described body Electricity She areas are arranged in described unmanned plane main body, and described dynamic lithium battery is hung on the bottom of described unmanned plane main body, A pair of described undercarriages are symmetrically arranged at the both ends of described unmanned plane main body;Described unmanned plane mechanical arm is that carbon is fine Dimension material is made, and described unmanned plane mechanical arm is provided with hollow-out parts, and the wheelbase of described unmanned plane mechanical arm is 640mm;Institute The one end for the unmanned plane mechanical arm stated is connected wherein on the undercarriage described in one by described big torsion steering wheel, described Unmanned plane mechanical arm is located at the lower section of described undercarriage, and is flipped to the outside by described big torsion steering wheel, and described one Individual or multiple sensor probes are separately positioned on the other end of described unmanned plane mechanical arm;Described remote control includes remote control Device and receiver, described receiver are arranged in described unmanned plane main body, described remote control and described receiver without Line connects.
- 2. atmosphere environment supervision unmanned plane according to claim 1, it is characterised in that:Set on described unmanned plane mechanical arm There are 4K levels video camera and the brushless head of three-axis stability augmentation.
- 3. atmosphere environment supervision unmanned plane according to claim 2, it is characterised in that:Described unmanned plane main body is provided with Image transmission, described image transmission includes figure and passes transmitting terminal, figure biography ground receiver end and OSD devices, described Figure passes transmitting terminal, figure passes ground receiver end and OSD devices are connected with described 4K levels video camera and the brushless head of three-axis stability augmentation.
- 4. atmosphere environment supervision unmanned plane according to claim 1, it is characterised in that:Described unmanned plane mechanical arm it is total Length is 1m.
- 5. atmosphere environment supervision unmanned plane according to claim 1, it is characterised in that:Described body electricity She areas include nothing Brush motor, motor cabinet and brushless electricity are adjusted, and it is mechanical with described unmanned plane respectively that described brushless electric machine, motor cabinet and brushless electricity are adjusted Arm connects, and is powered by described dynamic lithium battery.
- 6. atmosphere environment supervision unmanned plane according to claim 1, it is characterised in that:It is provided with described unmanned plane main body Data processing software and data transmission device.
- 7. atmosphere environment supervision unmanned plane according to claim 6, it is characterised in that:Described data transmission device includes Sensor and GPRS data transmitter.
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CN201720298854.1U CN206734624U (en) | 2017-03-26 | 2017-03-26 | Atmosphere environment supervision unmanned plane |
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CN201720298854.1U CN206734624U (en) | 2017-03-26 | 2017-03-26 | Atmosphere environment supervision unmanned plane |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108646784A (en) * | 2018-06-21 | 2018-10-12 | 河南天腾航空科技有限公司 | A kind of unmanned plane night Regional Atmospheric Environment monitoring method |
GB2569219A (en) * | 2017-10-13 | 2019-06-12 | Alti Velo Industrial Uav Rental Ltd | Non-destructive testing apparatus and method of use |
-
2017
- 2017-03-26 CN CN201720298854.1U patent/CN206734624U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2569219A (en) * | 2017-10-13 | 2019-06-12 | Alti Velo Industrial Uav Rental Ltd | Non-destructive testing apparatus and method of use |
CN108646784A (en) * | 2018-06-21 | 2018-10-12 | 河南天腾航空科技有限公司 | A kind of unmanned plane night Regional Atmospheric Environment monitoring method |
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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: 20171212 Termination date: 20200326 |