CN108528718A - Atmospheric environment monitors aircraft and monitoring method automatically - Google Patents
Atmospheric environment monitors aircraft and monitoring method automatically Download PDFInfo
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- CN108528718A CN108528718A CN201810284678.5A CN201810284678A CN108528718A CN 108528718 A CN108528718 A CN 108528718A CN 201810284678 A CN201810284678 A CN 201810284678A CN 108528718 A CN108528718 A CN 108528718A
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- atmospheric environment
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 19
- 238000000034 method Methods 0.000 title claims abstract description 14
- 239000007789 gas Substances 0.000 claims abstract description 44
- 230000006641 stabilisation Effects 0.000 claims abstract description 25
- 239000001307 helium Substances 0.000 claims abstract description 11
- 229910052734 helium Inorganic materials 0.000 claims abstract description 11
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000005070 sampling Methods 0.000 claims abstract description 11
- 238000013519 translation Methods 0.000 claims abstract description 4
- 238000001514 detection method Methods 0.000 claims description 10
- 239000011162 core material Substances 0.000 claims description 5
- 239000000945 filler Substances 0.000 claims description 5
- 229910002114 biscuit porcelain Inorganic materials 0.000 claims description 4
- 239000002245 particle Substances 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims description 3
- 238000011105 stabilization Methods 0.000 abstract description 3
- 238000012360 testing method Methods 0.000 abstract description 3
- 230000001360 synchronised effect Effects 0.000 abstract description 2
- 238000005457 optimization Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 230000007613 environmental effect Effects 0.000 description 3
- 238000009790 rate-determining step (RDS) Methods 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N1/00—Sampling; Preparing specimens for investigation
- G01N1/02—Devices for withdrawing samples
- G01N1/22—Devices for withdrawing samples in the gaseous state
- G01N1/2273—Atmospheric sampling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N1/00—Sampling; Preparing specimens for investigation
- G01N1/02—Devices for withdrawing samples
- G01N1/22—Devices for withdrawing samples in the gaseous state
- G01N1/2273—Atmospheric sampling
- G01N2001/2279—Atmospheric sampling high altitude, e.g. rockets, balloons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Biomedical Technology (AREA)
- Molecular Biology (AREA)
- Physics & Mathematics (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention relates to a kind of atmospheric environments to monitor aircraft and monitoring method automatically.This kind of atmospheric environment monitors aircraft automatically, including UAV flight's platform, air sampler, UAV flight's platform includes electric drive system, gas bag systems stabilisation and power control system, the electric drive system provides drive force UAV flight lifting platform and translation by battery, which includes one being installed on the helium packet for providing buoyancy on UAV flight's platform for UAV flight's platform when high aerial for unmanned plane.Above-mentioned atmospheric environment monitors aircraft automatically, increase the hang time of UAV flight's platform, it can realize and acquisition is synchronized to the pollution condition of air in flight or stagnant null process, under the premise of ensureing various Testing index, data stabilization, shorten the sampling time；The control mode that this kind of atmospheric environment monitors aircraft automatically is various, and different weather conditions can be coordinated to work.
Description
Technical field
The invention belongs to environmental science and environmental project, remote sensing science and technology, aviation and communication technology crossing domain, tools
Body is related to a kind of atmospheric environment and monitors aircraft and monitoring method automatically.
Background technology
With the continuous development of global economy, industrial and domestic pollutant air total emission volumn is continuously increased, range is held
Continuous to expand, haze or local atmosphere contamination phenomenon are on the rise, it has also become Chinese and many rapid economic development countries or region
Environmental concern focus, this contamination phenomenon will gradually influence global atmosphere environment.Currently, PM2.5 mainly passes through ground environment
Monitoring station net obtains, and website covering is limited, and can not provide vertical distribution data.Satellite remote sensing coverage area is big, lacks near-earth
Face detecting vertical distribution data.
To solve the above-mentioned problems, it discloses one kind application No. is the application for a patent for invention of CN201610762798.2 and is used for
The aircraft of environment monitoring, which is characterized in that including drone body, detecting module, gas-monitoring module, wireless network transmitting-receiving
Module, central control system；The detecting module is set to below drone body, and detecting module includes for acquiring cromogram
Communication unit as the camera of information and for color image information to be sent to central control system；The gas-monitoring mould
Block is used for through the atmospheric condition in Sensor monitoring specific region, and the data of monitoring are sent out by the wireless network transceiver module
It send to central control system.Existing unmanned plane is usually rotary wind type, and the flight time is usually at 15-30 minutes, and needle
The time of air environment detection is typically required and ensures certain hang time and detects highly higher therefore existing
The aircraft of environment monitoring is typically only capable to the detection of short time such as carry out quick laser, take pictures, and detection numerical value is passed through nothing
Line network transceiving module is fed back in central control system, and can not be sampled to air, is referred to the air in atmospheric environment
Mark is effectively detected, and detection range is small, data are unstable.
Invention content
To overcome deficiency in the prior art, a kind of atmospheric environment of present invention offer to monitor aircraft and monitoring side automatically
Method.
To achieve the above object, the technical solution adopted by the present invention is as follows：A kind of atmospheric environment monitors aircraft automatically,
It is characterized in that：Including UAV flight's platform, at least one air sampler being set on UAV flight's platform, the nothing
Man-machine carrying platform includes electric drive system, gas bag systems stabilisation and power control system, and the electric drive system is by electricity
Pond provides drive force UAV flight lifting platform and translation, the gas bag systems stabilisation are installed on UAV flight including one
The helium packet of buoyancy, power control system difference are provided when high aerial for UAV flight's platform on platform for unmanned plane
It is connect with electric drive system and gas bag systems stabilisation to switch or make electric drive system and gas bag systems stabilisation to cooperate.
Optimization, further include timing control apparatus, which connect with power control system to control nobody
Machine carrying platform starts or stops in the time range of setting.
Optimization, further include position control device, which connect with power control system to specify nobody
Machine carrying platform flies to specific region.
Optimization, electric drive system includes battery component, blade assembly and driving mechanism, driving mechanism band movable vane piece
Component rotates, which provides electric power for driving mechanism.
Optimization, gas bag systems stabilisation includes rack platform and self-filler, which is set to blade group
It is set in rack platform and is connect with battery component for the support helium packet after branch inflation, the self-filler above part.
Optimization, air sampler includes that gas gathering mask, sampling core material and holder, the gas gathering mask are installed on nobody by holder
Machine carries in sample platform, which is installed in gas gathering mask.
Optimization, the inlet end and blade assembly of gas gathering mask are positioned opposite, when which rotates into collection gas shield
It is sent into air.
Atmospheric environment automatic monitoring method monitors aircraft automatically using above-mentioned atmospheric environment, and rate-determining steps are as follows：
Step 1, when detection zone environment, power control system switches or makes electric drive system and gas bag stability series respectively
System cooperates, and UAV flight's platform is sent to the height and position into area to be tested；
Step 2, air sampler acquires the bisque in air during unmanned plane during flying or during the stagnant sky of certain height
Particle；
Step 3, after the completion of acquisition, power control system switches or makes electric drive system and gas bag systems stabilisation phase respectively
Mutually cooperation, UAV flight's platform is sent back to.
Further, the automatic flight time is set, the automatic aircraft that monitors starts automatically in the flight time of setting, completes
Collecting work.
Further, automatic flight range is set, the automatic aircraft that monitors flies in the flight range of setting, completes to adopt
Collect work.
By the above-mentioned description of this invention it is found that compared with prior art, atmospheric environment provided by the invention monitors automatically
Aircraft can be increased the hang time of UAV flight's platform by electric drive system and gas bag systems stabilisation, make unmanned plane
Carrying platform can be realized synchronizes acquisition in flight or stagnant null process to the pollution condition of air, atmosphere sampler and
Blade assembly matches, and improves and is passed through air quantity in gas gathering mask within the unit interval, and then is ensureing that Testing index is various, data
Under the premise of stabilization, shorten the sampling time；The control mode that this kind of atmospheric environment monitors aircraft automatically is various, can coordinate difference
Weather condition work.
Description of the drawings
Fig. 1 is the structural schematic diagram that atmospheric environment monitors that aircraft helium is undertaken to perform work within a time limit and according to specifications when making automatically.
Fig. 2 is that atmospheric environment monitors structural schematic diagram when aircraft helium packet does not work automatically.
Fig. 3 is that atmospheric environment monitors aircraft air sampler structural schematic diagram automatically.
Fig. 4 is the structural schematic diagram that atmospheric environment monitors aircraft air sampler gas gathering mask automatically.
Fig. 5 is the internal structure schematic diagram that atmospheric environment monitors aircraft air sampler gas gathering mask automatically.
Specific implementation mode
Below by way of specific implementation mode, the invention will be further described.
Shown in Fig. 5, a kind of atmospheric environment monitors aircraft, including UAV flight's platform 1, air automatically
Sampler 2, timing control apparatus 3, position control device 4；
UAV flight's platform 1 includes electric drive system 11, gas bag systems stabilisation 12 and power control system 13,
The electric drive system 1 provides 1 lifting of drive force UAV flight platform and translation, electronic drive by battery
Dynamic system 11 includes battery component 111, blade assembly 112 and driving mechanism 113, which drives blade assembly 112
Rotation, the battery component 111 are that driving mechanism 113 provides electric power,
The gas bag systems stabilisation 12 includes rack platform 121, helium packet 122, self-filler 123, the rack platform
121 are set to for the support helium packet 122 after branch inflation above blade assembly, and it is flat which is set to holder
It is connect in platform 121 and with battery component, which connect with helium packet 122, and helium packet 121 is used for unmanned plane
Buoyancy is provided for UAV flight's platform when high aerial,
The power control system 13 is connect with electric drive system 11 and gas bag systems stabilisation 12 to switch or make electricity respectively
Dynamic drive system 11 and gas bag systems stabilisation 12 cooperate；
Air sampler 2 includes that gas gathering mask 21, sampling core material 22 and holder 23, the gas gathering mask 21 are installed on by holder 23
In UAV flight's sample platform 1, which is installed in gas gathering mask 21, and the both ends of gas gathering mask 21 are provided with stomata, inlet end
211 is positioned opposite with blade assembly 112, and air, the air of feeding are sent into collection gas shield 21 when which rotates
It quickly circulates in sampling core material 22, sampling green wood is enable quickly to intercept the information in air；
Timing control apparatus 3, the timing control apparatus 3 are connect with power control system 11 to control UAV flight's platform
1 starts or stops in the time range of setting；
Position control device 4, the position control device are connect with power control system 13 to specify UAV flight's platform
It flies to specific region, which has the navigation chip based on the Big Dipper or GPS.
Atmospheric environment automatic monitoring method monitors aircraft automatically using above-mentioned atmospheric environment, and rate-determining steps are as follows：
Step 1, the automatic flight time is set, by 4 automatic movement area of position control device by timing control apparatus 3
Domain, the automatic aircraft that monitors starts automatically in flight time time of setting, and can fly in the flight range of setting, carries out
Collecting work；
Step 2, when detection zone environment, power control system switches or makes electric drive system and gas bag stability series respectively
System cooperates, and UAV flight's platform is sent to the height and position into area to be tested；
Step 3, air sampler is according to detection needs, when atmosphere pollution situation in detection zone during unmanned plane during flying
It is synchronous to carry out atmospheric sampling, it is extremely examined in the stagnant sky of UAV flight's platform when detecting the atmospheric condition of specific position or certain height
The bisque particle in air is acquired when location is set；
Step 4, after the completion of acquisition, power control system switches or makes electric drive system and gas bag systems stabilisation phase respectively
Mutually cooperation, UAV flight's platform is sent back to.
11, atmospheric environment automatic monitoring method, it is characterised in that：Aircraft is monitored automatically using above-mentioned atmospheric environment,
Its rate-determining steps is as follows：
Step 1, when detection zone environment, power control system switches or makes electric drive system and gas bag stability series respectively
System cooperates, and UAV flight's platform is sent to the height and position into area to be tested；
Step 2, air sampler acquires the bisque in air during unmanned plane during flying or during the stagnant sky of certain height
Particle；
Step 3, after the completion of acquisition, power control system switches or makes electric drive system and gas bag systems stabilisation phase respectively
Mutually cooperation, UAV flight's platform is sent back to.
By the above-mentioned description of this invention it is found that compared with prior art, a kind of atmospheric environment provided by the invention is automatic
Aircraft is monitored, the hang time of UAV flight's platform can be increased by electric drive system and gas bag systems stabilisation, make nothing
Man-machine carrying platform can be realized synchronizes acquisition, atmospheric sampling dress in flight or stagnant null process to the pollution condition of air
Set and matched with blade assembly, improve and be passed through air quantity in gas gathering mask within the unit interval, so ensure Testing index it is various,
Under the premise of data stabilization, shorten the sampling time；The control mode that this kind of atmospheric environment monitors aircraft automatically is various, can coordinate
Different weather conditions work.
A kind of specific implementation mode of the present invention is above are only, but the design concept of the present invention is not limited thereto, all profits
The change for carrying out unsubstantiality to the present invention with this design, should all belong to the behavior for invading the scope of the present invention.
Claims (10)
1. atmospheric environment monitors aircraft automatically, it is characterised in that：Including UAV flight's platform, to be set to UAV flight flat
At least one air sampler on platform, UAV flight's platform include electric drive system, gas bag systems stabilisation and move
Force control system, the electric drive system provide drive force UAV flight lifting platform and translation, the gas by battery
It is that UAV flight's platform carries when high aerial that packet systems stabilisation, which is installed on UAV flight's platform including one and is used for unmanned plane,
For the helium packet of buoyancy, which connect with electric drive system and gas bag systems stabilisation to switch or make electricity respectively
Dynamic drive system and gas bag systems stabilisation cooperate.
2. atmospheric environment according to claim 1 monitors aircraft automatically, it is characterised in that：It further include timing controlled dress
It sets, which connect with power control system is started with controlling UAV flight's platform in the time range of setting
Or stop.
3. atmospheric environment according to claim 1 or 2 monitors aircraft automatically, it is characterised in that：It further include location control
Device, the position control device are connect with power control system with specified UAV flight's platform flight to specific region.
4. atmospheric environment according to claim 1 monitors aircraft automatically, it is characterised in that：The electric drive system packet
Battery component, blade assembly and driving mechanism are included, it is driving mechanism which, which drives blade assembly rotation, the battery component,
Electric power is provided.
5. atmospheric environment according to claim 4 monitors aircraft automatically, it is characterised in that：The gas bag systems stabilisation packet
Rack platform and self-filler are included, which is set to above blade assembly for the support helium packet after branch inflation,
The self-filler is set in rack platform and is connect with battery component.
6. atmospheric environment according to claim 1 or 4 monitors aircraft automatically, it is characterised in that：The air sampler
It is installed in UAV flight's sample platform by holder including gas gathering mask, sampling core material and holder, the gas gathering mask, sampling core material peace
Loaded in gas gathering mask.
7. atmospheric environment according to claim 6 monitors aircraft automatically, it is characterised in that：The inlet end of the gas gathering mask
It is positioned opposite with blade assembly, when which rotates air is sent into collection gas shield.
8. atmospheric environment automatic monitoring method, it is characterised in that：Aircraft is monitored automatically using above-mentioned atmospheric environment, is controlled
Steps are as follows：
Step 1, when detection zone environment, power control system switches or makes electric drive system and gas bag systems stabilisation phase respectively
UAV flight's platform, is sent the height and position into area to be tested by mutually cooperation；
Step 2, air sampler acquires the bisque particle in air during unmanned plane during flying or during the stagnant sky of certain height；
Step 3, after the completion of acquisition, power control system switches or makes electric drive system and gas bag systems stabilisation phase interworking respectively
It closes, UAV flight's platform is sent back to.
9. atmospheric environment automatic monitoring method according to claim 8, it is characterised in that：The automatic flight time is set, from
Dynamic monitoring aircraft starts automatically in the flight time of setting, completes collecting work.
10. atmospheric environment automatic monitoring method according to claim 8 or claim 9, it is characterised in that：Set automatic movement area
Domain, the automatic aircraft that monitors fly in the flight range of setting, complete collecting work.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810284678.5A CN108528718A (en) | 2018-04-02 | 2018-04-02 | Atmospheric environment monitors aircraft and monitoring method automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810284678.5A CN108528718A (en) | 2018-04-02 | 2018-04-02 | Atmospheric environment monitors aircraft and monitoring method automatically |
Publications (1)
| Publication Number | Publication Date |
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| CN108528718A true CN108528718A (en) | 2018-09-14 |
Family
ID=63482854
Family Applications (1)
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| CN201810284678.5A Pending CN108528718A (en) | 2018-04-02 | 2018-04-02 | Atmospheric environment monitors aircraft and monitoring method automatically |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110646250A (en) * | 2019-08-22 | 2020-01-03 | 湖南国康检验检测技术有限公司 | Sampling device for environment detection |
| CN113092190A (en) * | 2021-03-17 | 2021-07-09 | 王晓雪 | Atmospheric pollution monitoring sampling device based on unmanned aerial vehicle remote control |
| JP7001878B1 (en) | 2020-06-30 | 2022-01-24 | 楽天グループ株式会社 | Aircraft, suction system and suction method |
| US11619570B1 (en) * | 2020-06-02 | 2023-04-04 | United States Of America As Represented By The Secretary Of The Air Force | Filter-based air sampler capable of integration into small unmanned aerial vehicles |
| WO2023063828A1 (en) * | 2021-10-14 | 2023-04-20 | Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno | Method of acquisition of analytes with an unmanned mobile platform, mobile delivery platform, assembly and use |
| CN117890165A (en) * | 2024-03-14 | 2024-04-16 | 徐州智航智能科技有限公司 | High-altitude air body collector based on unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2327626A1 (en) * | 2009-11-27 | 2011-06-01 | Universita' Degli Studi di Napoli Parthenope | Air pollutants monitoring by a continuous process in real time and at different altitudes |
| CN104777014A (en) * | 2015-04-27 | 2015-07-15 | 中国气象局气象探测中心 | Atmosphere collecting device for inflatable unmanned helicopter and altitude gas collecting method |
| CN106153403A (en) * | 2016-08-05 | 2016-11-23 | 中国科学院遗传与发育生物学研究所农业资源研究中心 | A kind of Atmospheric particulates sampling system |
| KR101716868B1 (en) * | 2015-11-12 | 2017-03-27 | 울산과학기술원 | Unmanned flight apparatus for sampling chemical substances |
| CN107765346A (en) * | 2017-11-03 | 2018-03-06 | 河北科技大学 | A kind of eight-rotary wing aircraft for weather environment measurement |
| CN208198829U (en) * | 2018-04-02 | 2018-12-07 | 威洁（石狮）中水回用技术有限公司 | A kind of atmospheric environment monitors aircraft automatically |
-
2018
- 2018-04-02 CN CN201810284678.5A patent/CN108528718A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2327626A1 (en) * | 2009-11-27 | 2011-06-01 | Universita' Degli Studi di Napoli Parthenope | Air pollutants monitoring by a continuous process in real time and at different altitudes |
| CN104777014A (en) * | 2015-04-27 | 2015-07-15 | 中国气象局气象探测中心 | Atmosphere collecting device for inflatable unmanned helicopter and altitude gas collecting method |
| KR101716868B1 (en) * | 2015-11-12 | 2017-03-27 | 울산과학기술원 | Unmanned flight apparatus for sampling chemical substances |
| CN106153403A (en) * | 2016-08-05 | 2016-11-23 | 中国科学院遗传与发育生物学研究所农业资源研究中心 | A kind of Atmospheric particulates sampling system |
| CN107765346A (en) * | 2017-11-03 | 2018-03-06 | 河北科技大学 | A kind of eight-rotary wing aircraft for weather environment measurement |
| CN208198829U (en) * | 2018-04-02 | 2018-12-07 | 威洁（石狮）中水回用技术有限公司 | A kind of atmospheric environment monitors aircraft automatically |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110646250A (en) * | 2019-08-22 | 2020-01-03 | 湖南国康检验检测技术有限公司 | Sampling device for environment detection |
| CN110646250B (en) * | 2019-08-22 | 2022-06-17 | 湖南国康检验检测技术有限公司 | Sampling device for environment detection |
| US11619570B1 (en) * | 2020-06-02 | 2023-04-04 | United States Of America As Represented By The Secretary Of The Air Force | Filter-based air sampler capable of integration into small unmanned aerial vehicles |
| JP7001878B1 (en) | 2020-06-30 | 2022-01-24 | 楽天グループ株式会社 | Aircraft, suction system and suction method |
| JP2022024215A (en) * | 2020-06-30 | 2022-02-09 | 楽天グループ株式会社 | Flying body, suction system and suction method |
| CN113092190A (en) * | 2021-03-17 | 2021-07-09 | 王晓雪 | Atmospheric pollution monitoring sampling device based on unmanned aerial vehicle remote control |
| CN113092190B (en) * | 2021-03-17 | 2024-02-06 | 陕西国臻实业集团有限公司 | Atmospheric pollution monitoring sampling device based on unmanned aerial vehicle remote control |
| WO2023063828A1 (en) * | 2021-10-14 | 2023-04-20 | Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno | Method of acquisition of analytes with an unmanned mobile platform, mobile delivery platform, assembly and use |
| CN117890165A (en) * | 2024-03-14 | 2024-04-16 | 徐州智航智能科技有限公司 | High-altitude air body collector based on unmanned aerial vehicle |
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Application publication date: 20180914 |