CN106114860A - A kind of air quality detection system based on UAS - Google Patents
A kind of air quality detection system based on UAS Download PDFInfo
- Publication number
- CN106114860A CN106114860A CN201610547208.4A CN201610547208A CN106114860A CN 106114860 A CN106114860 A CN 106114860A CN 201610547208 A CN201610547208 A CN 201610547208A CN 106114860 A CN106114860 A CN 106114860A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- module
- air quality
- detection device
- automatic pilot
- 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.)
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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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- 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
Abstract
The invention discloses a kind of air quality detection system based on UAS, including fuselage and wing, described fuselage interior stage casing is provided with interconnective detection device and power supply, fuselage interior back segment is provided with fuel tank and automatic pilot, afterbody is provided with electromotor, and automatic pilot connects electromotor；Described detection device includes gas detection cell, amplification circuit module, A/D conversion module and data transmission module, gas detection cell gathers air quality information, and by the signal that collects after amplification circuit module is amplified, being transferred to A/D conversion module, final signal is through the server of data transmission module transmission to ground base station；The position that described fuselage bottom is corresponding with detection device offers hatch door, and detection device is connected with fuselage by expansion bracket；Described automatic pilot includes central processing unit, and be connected with central processing unit respectively six axle gyroscopes, barometer, pitot meter, GPS module, command receiver.
Description
Technical field
The present invention relates to field of Environment Protection, particularly relate to a kind of air quality detection system based on UAS.
Background technology
With growth in the living standard, people pay attention to all the more the air quality of place living environment.Existing air quality is examined
Survey device mainly include industrial and directly display type.Wherein, industrial air quality detecting device is incited somebody to action by industrial transmitter
The air quality that gas detection probe is detected is converted to digital signal, voltage signal and the current signal that can be identified.Industry
Type air quality detecting device cannot be used by vast unprofessional user, does not the most possess domestic function.Directly display type air
Quality detection device is to be incorporated into by gas detection module in the circuit possessing digital displaying function, makes gas detecting value directly show
Show, it is simple to use.But the type air quality detecting device of directly displaying needs configuration instruction book to instruct user operation, and shows number
Value needs data that user consults in description thus judges air quality, thereby results in inconvenience.
Summary of the invention
The invention aims to solve shortcoming present in prior art, and the one proposed is based on UAS
Air quality detection system.
To achieve these goals, present invention employs following technical scheme: a kind of air matter based on UAS
Amount detection systems, including fuselage and wing, described fuselage interior stage casing is provided with interconnective detection device and power supply, in fuselage
Portion's back segment is provided with fuel tank and automatic pilot, and afterbody is provided with electromotor, and automatic pilot connects electromotor；
Described detection device includes gas detection cell, amplification circuit module, A/D conversion module and data transmission module, gas
Detector unit gathers air quality information, and by the signal that collects after amplification circuit module is amplified, is transferred to A/D and converts
Module, final signal is through the server of data transmission module transmission to ground base station；Described fuselage bottom and detection device pair
The position answered offers hatch door, and detection device is connected with fuselage by expansion bracket；
Described automatic pilot includes central processing unit, and be connected with central processing unit respectively six axle gyroscopes, barometer,
Pitot meter, GPS module, command receiver.
Preferably, described electromotor is connected with fuel tank by oil pipe.
Preferably, the bottom of described fuselage is respectively equipped with nose-gear and rear undercarriage.
Compared with prior art, the invention has the beneficial effects as follows:
1, being located on unmanned plane by air detecting device of the present invention, it is possible to achieve the detection to altitude air quality, expands sky
The range of gas detection device.
2, detection device is accommodated in fuselage, it is to avoid detect device when not working and damage.
3, unmanned plane is provided with automatic pilot, it is achieved automatic Pilot, and practicality is higher.
Accompanying drawing explanation
Fig. 1 is the principle schematic of a kind of based on UAS the air quality detection system that the present invention proposes；
Fig. 2 is the structural representation of a kind of based on UAS the air quality detection system that the present invention proposes.
In figure: 1, fuselage, 2, nose-gear, 3, rear undercarriage, 4, hatch door, 5, power supply, 6, fuel tank, 7, electromotor, 8, from
Dynamic pilot, 9, detection device.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.
With reference to Fig. 1-2, a kind of air quality detection system based on UAS, including fuselage 1 and wing, described machine
The internal stage casing of body 1 is provided with interconnective detection device 9 and power supply 5, and the internal back segment of fuselage 1 is provided with fuel tank 6 and automatic pilot
8, fuselage 1 afterbody is provided with electromotor 7, and automatic pilot 8 connects electromotor 7, and electromotor 7 is connected with fuel tank 6 by oil pipe.
Described detection device 9 includes gas detection cell, amplification circuit module, A/D conversion module and data transmission module,
Gas detection cell gathers air quality information, and by the signal that collects after amplification circuit module is amplified, is transferred to A/D
Conversion module, final signal is through the server of data transmission module transmission to ground base station.With detection dress bottom described fuselage 1
The position putting 9 correspondences offers hatch door 4, and detection device 9 is connected with fuselage 1 by expansion bracket, and when unmanned plane takes off, hatch door 4 closes
Closing, it is internal that detection device 9 is accommodated in fuselage 1, and when unmanned plane arrives high-altitude, hatch door 4 is opened, and detection device 9 stretches out with expansion bracket,
Start working.Detection device 9 is accommodated in fuselage 1, it is to avoid detect device 9 when not working and damage.
Described automatic pilot 8 includes central processing unit, and be connected with central processing unit respectively six axle gyroscopes, gas
Pressure meter, pitot meter, GPS module, command receiver, described six axle gyroscopes are used for obtaining attitude information and send central authorities' process to
Device, exports to aviation mechanism, to ensure this unmanned plane smooth flight after process；Described barometer is used for obtaining atmospheric pressure height
Information sends central processing unit to, exports to aviation mechanism after process, controls unmanned plane during flying height；Described pitot meter is used for
Obtain aerial effective wind speed information and send central processing unit to, exporting to aviation mechanism after process, making flight more stable,
Increase the stability of unmanned plane airline operation aloft；Described GPS module is used for positional information to be transferred to central processing unit, with
Latitude and longitude coordinates information is provided in real time to central processing unit；Described command receiver is used for receiving the instruction that ground base station sends,
Control the flight path of unmanned plane.
Preferably, the bottom of described fuselage 1 is respectively equipped with nose-gear 2 and rear undercarriage 3.
The above, the only present invention preferably detailed description of the invention, but protection scope of the present invention is not limited thereto,
Any those familiar with the art in the technical scope that the invention discloses, according to technical scheme and
Inventive concept equivalent or change in addition, all should contain within protection scope of the present invention.
Claims (3)
1. an air quality detection system based on UAS, including fuselage (1) and wing, it is characterised in that described
The internal stage casing of fuselage (1) is provided with interconnective detection device (9) and power supply (5), and the internal back segment of fuselage (1) is provided with fuel tank (6)
With automatic pilot (8), fuselage (1) afterbody is provided with electromotor (7), and automatic pilot (8) connects electromotor (7)；
Described detection device (9) includes gas detection cell, amplification circuit module, A/D conversion module and data transmission module, gas
Body detector unit gathers air quality information, and by the signal that collects after amplification circuit module is amplified, is transferred to A/D and turns
Changing module, final signal is through the server of data transmission module transmission to ground base station；Described fuselage (1) bottom and detection dress
Putting position corresponding to (9) and offer hatch door (4), detection device (9) is connected with fuselage (1) by expansion bracket；
Described automatic pilot (8) includes central processing unit, and be connected with central processing unit respectively six axle gyroscopes, air pressure
Meter, pitot meter, GPS module, command receiver.
A kind of air quality detection system based on UAS the most according to claim 1, it is characterised in that described
Electromotor (7) is connected with fuel tank (6) by oil pipe.
A kind of air quality detection system based on UAS the most according to claim 1, it is characterised in that described
The bottom of fuselage (1) is respectively equipped with nose-gear (2) and rear undercarriage (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610547208.4A CN106114860A (en) | 2016-07-13 | 2016-07-13 | A kind of air quality detection system based on UAS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610547208.4A CN106114860A (en) | 2016-07-13 | 2016-07-13 | A kind of air quality detection system based on UAS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114860A true CN106114860A (en) | 2016-11-16 |
Family
ID=57283935
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610547208.4A Pending CN106114860A (en) | 2016-07-13 | 2016-07-13 | A kind of air quality detection system based on UAS |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114860A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106527490A (en) * | 2017-01-18 | 2017-03-22 | 青岛欧森系统技术有限公司 | Oil-powered multi-rotor unmanned aerial vehicle autopilot |
| CN108216626A (en) * | 2017-12-27 | 2018-06-29 | 湖州品创孵化器有限公司 | A kind of intelligent driving unmanned plane for Detection of Air Quality |
| CN108593842A (en) * | 2018-03-26 | 2018-09-28 | 山东大学 | Based on explosion-proof unmanned aerial vehicle platform tunnel gas automatic monitoring system and method |
| CN109720563A (en) * | 2019-02-28 | 2019-05-07 | 南京邮电大学 | Intelligent quadrotor gliding unmanned plane and its flight control method |
| CN111846223A (en) * | 2020-07-23 | 2020-10-30 | 东莞理工学院 | Machine bird with air quality monitoring function |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2501051Y (en) * | 2001-11-15 | 2002-07-17 | 何燕文 | Gas detector |
| CN2804861Y (en) * | 2005-06-15 | 2006-08-09 | 上海西叶电子科技有限责任公司 | Device for testing air quality |
| CN101876717A (en) * | 2009-12-16 | 2010-11-03 | 中国科学院大气物理研究所 | Pilotless aircraft airborne atmospheric environment detection system |
| CN202481315U (en) * | 2011-11-15 | 2012-10-10 | 中科宇图天下科技有限公司 | Multifunctional unmanned aerial vehicle (UAV) system for environment emergency monitoring |
| CN104133042A (en) * | 2014-08-01 | 2014-11-05 | 江苏恒创软件有限公司 | Unmanned plane based air quality monitoring device and monitoring method |
-
2016
- 2016-07-13 CN CN201610547208.4A patent/CN106114860A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2501051Y (en) * | 2001-11-15 | 2002-07-17 | 何燕文 | Gas detector |
| CN2804861Y (en) * | 2005-06-15 | 2006-08-09 | 上海西叶电子科技有限责任公司 | Device for testing air quality |
| CN101876717A (en) * | 2009-12-16 | 2010-11-03 | 中国科学院大气物理研究所 | Pilotless aircraft airborne atmospheric environment detection system |
| CN202481315U (en) * | 2011-11-15 | 2012-10-10 | 中科宇图天下科技有限公司 | Multifunctional unmanned aerial vehicle (UAV) system for environment emergency monitoring |
| CN104133042A (en) * | 2014-08-01 | 2014-11-05 | 江苏恒创软件有限公司 | Unmanned plane based air quality monitoring device and monitoring method |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106527490A (en) * | 2017-01-18 | 2017-03-22 | 青岛欧森系统技术有限公司 | Oil-powered multi-rotor unmanned aerial vehicle autopilot |
| CN108216626A (en) * | 2017-12-27 | 2018-06-29 | 湖州品创孵化器有限公司 | A kind of intelligent driving unmanned plane for Detection of Air Quality |
| CN108593842A (en) * | 2018-03-26 | 2018-09-28 | 山东大学 | Based on explosion-proof unmanned aerial vehicle platform tunnel gas automatic monitoring system and method |
| CN109720563A (en) * | 2019-02-28 | 2019-05-07 | 南京邮电大学 | Intelligent quadrotor gliding unmanned plane and its flight control method |
| CN111846223A (en) * | 2020-07-23 | 2020-10-30 | 东莞理工学院 | Machine bird with air quality monitoring function |
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Application publication date: 20161116 |