CN206353151U - A kind of water environment monitors aircraft - Google Patents
A kind of water environment monitors aircraft Download PDFInfo
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- CN206353151U CN206353151U CN201621211511.9U CN201621211511U CN206353151U CN 206353151 U CN206353151 U CN 206353151U CN 201621211511 U CN201621211511 U CN 201621211511U CN 206353151 U CN206353151 U CN 206353151U
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- aircraft
- ccd camera
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 44
- 230000007613 environmental effect Effects 0.000 claims abstract description 22
- 238000004891 communication Methods 0.000 claims description 9
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 7
- 239000001301 oxygen Substances 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 238000007789 sealing Methods 0.000 claims description 7
- 239000000498 cooling water Substances 0.000 claims description 6
- 238000012546 transfer Methods 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 4
- 239000007789 gas Substances 0.000 claims 1
- 238000012544 monitoring process Methods 0.000 abstract description 20
- 238000010276 construction Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 5
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003643 water by type Substances 0.000 description 2
- 238000012773 Laboratory assay Methods 0.000 description 1
- 239000005422 algal bloom Substances 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002352 surface water Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
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- Arrangements For Transmission Of Measured Signals (AREA)
- Studio Devices (AREA)
- Testing Or Calibration Of Command Recording Devices (AREA)
Abstract
Aircraft is monitored the utility model discloses a kind of water environment, water environment monitoring aircraft includes aircraft body, the aircraft body carries attitude transducer and digital compass, the top of the aircraft body is provided with control module and wireless transport module, the bottom of the aircraft body is provided with environmental data collecting module and water-proof CCD camera, and the bottom of the aircraft body is also equipped with kickboard；The attitude transducer, digital compass, wireless transport module, environmental data collecting module and water-proof CCD camera are connected with control module, and the water-proof CCD camera is connected with wireless transport module；Barometer is also equipped with the aircraft body, the barometer is connected with control module.The utility model is simple in construction, easy to control, the monitoring for realizing water environment that can efficiently, flexibly, economic.
Description
Technical field
The utility model belongs to environmental monitoring technology field, more particularly to a kind of water environment monitoring aircraft.
Background technology
Water is one of indispensable important substance resource that the mankind depend on for existence and development, but recently as society's warp
Development and industrialization, the quickening of urbanization process of Ji, the activity that human simple pursues economic interests make rivers and lakes just meet with
By severe contamination, aquatic ecosystem is declined by different degrees of destruction, algal bloom, water transparency, aquatic to plant
Thing is gradually withered away, and with serious pollution lake there is also water body nigrescence or wawter bloom occurs.Water environment pollution has had influence on people's life
Every aspect living, and the increasingly enhanced environmental consciousness of people proposes higher requirement to fwaater resources protection, therefore, control source is cut
Dirt, strengthens environment monitoring capability, and lifting rivers and lakes managerial skills ensure the sustainable profit of water resource to safeguard river lake healthy life
With being a urgent vital task.
At this stage, conventional water area monitoring means have：Artificial sample, laboratory assays, remote sensing monitoring technology, aquatic organism
Monitor water quality technology, unmanned plane etc..These monitoring methods respectively have advantage and disadvantage, wherein for artificial sample, lab analysis
Method, has that data acquisition is slow, monitoring process is cumbersome and labor intensity；Remote sensing technology has that detection accuracy is low, expense
The problems such as using high；Aquatic organism monitors, and is only capable of the water quality situation near reaction test website；Unmanned plane, with flexible, motor-driven
Performance, but environmental monitoring can only be carried out from visual angle.
Utility model content
The purpose of this utility model is that there is provided a kind of water environment monitoring aircraft for above-mentioned deficiency.
To solve upper problem, the technical scheme that the utility model is used is：A kind of water environment monitors aircraft, including
Aircraft body, the aircraft body carries attitude transducer and digital compass, and the top of the aircraft body is provided with
Control module and wireless transport module, the bottom of the aircraft body are provided with environmental data collecting module and waterproof shooting
Head, the bottom of the aircraft body is also equipped with kickboard；The attitude transducer, digital compass, wireless transport module, environment
Data acquisition module and water-proof CCD camera are connected with control module, and the water-proof CCD camera is connected with wireless transport module；Institute
State and barometer is also equipped with aircraft body, the barometer is connected with control module.
Further, the wireless transport module is by wireless data transfer module, wireless image-sound transport module and wireless
Communication module is constituted, and the wireless data transfer module and wireless communication module are connected with control module, the wireless image-sound
Transport module is connected with water-proof CCD camera.
Further, the environmental data collecting module includes cooling-water temperature sensor, acidity-basicity sensor and dissolved oxygen sensing
Device.
Further, the control module and wireless transport module are arranged in waterproof sealing cabin, the waterproof sealing cabin
It is fixed on the top of aircraft body.
Further, the environmental data collecting module is connected with water-proof CCD camera by expansion link with aircraft body.
Further, in addition to support, the kickboard is connected by support with the lower end of aircraft body.
Further, LED is housed, the LED is connected with control module around the camera lens of the water-proof CCD camera.
The beneficial effects of the utility model are as follows：The utility model by by environmental data collecting module, water-proof CCD camera,
Wireless transport module, kickboard are combined with quadrotor, and are carried out using the sealed compartment of lightweight at the waterproof of electronic equipment
Reason, the stretching and compression of support structures realize the three-dimensional water environment monitoring of the water surface, underwater all-dimensional.The utility model structure
Simply, it is easy to control, the monitoring for realizing water environment that can efficiently, flexibly, economic.
Brief description of the drawings
Fig. 1 is the utility model structural representation；
Fig. 2 is the schematic diagram that the utility model lands on the ground；
Fig. 3 is system composition structured flowchart of the present utility model；
In figure：It is aircraft body 1, kickboard 2, support 3, environmental data collecting module and water-proof CCD camera 4, expansion link 5, close
Batten down 6.
Embodiment
The utility model is described in further details with reference to specific embodiment and accompanying drawing, but the utility model is not only
It is confined to secondary.
As Figure 1-3, a kind of water environment monitoring aircraft of the utility model offer, including aircraft body 1 (including
Propeller, brshless DC motor, electricity are adjusted), the aircraft body 1 carries attitude transducer and digital compass, the aircraft
The top of main body 1 is provided with control module and wireless transport module, and the bottom of the aircraft body 1 is provided with environmental data and adopted
Collect module and water-proof CCD camera 4, the bottom of the aircraft body 1 is also equipped with kickboard 2；The attitude transducer, digital sieve
Disk, wireless transport module, environmental data collecting module and water-proof CCD camera are connected with control module, the water-proof CCD camera with
Wireless transport module is connected；Barometer is also equipped with the aircraft body, the barometer is connected with control module；The control
Molding block is microcontroller (MCU), can use the product of Fuji Tsu's MB9B120M models, but not limited to this；MCU passes through
I2C buses are connected with attitude transducer, barometer, digital compass；Attitude transducer includes three axis accelerometer, three axis accelerometer
Instrument, can use MPU6050 model chips, but not limited to this；Barometer can use MS5611 model chips, but be not limited to
This；Digital compass can use HMC5883L model chips, but not limited to this；By attitude algorithm, MCU is adjusted to flight by electricity
The brshless DC motor of device is controlled in real time, and receives the pulse position that ground control centre is transmitted by wireless communication module
Signal (PPM) constantly adjustment posture and flight path, realize neatly water area monitoring.
Further, the wireless transport module is by wireless data transfer module, wireless image-sound transport module and wireless
Communication module is constituted, and the wireless data transfer module and wireless communication module are connected with control module, the wireless image-sound
Transport module is connected with water-proof CCD camera；Wherein wireless image-sound transport module is used for the transmission of water-proof CCD camera image, can adopt
With the 2.4G wireless transport modules of ANTEMA brands, but not limited to this；Wireless environment data transmission module be used for cooling-water temperature sensor,
The water quality data transmission that acidity-basicity sensor, dissolved oxygen sensor are measured, can use communications band for 433MHz CC1101
Module, but not limited to this；Wireless communication module is used for ground control centre to the underwater acoustic remote control of aircraft, can use
NRF2401 wireless modules, but not limited to this.
Further, the environmental data collecting module includes cooling-water temperature sensor, acidity-basicity sensor and dissolved oxygen sensing
Device；Wherein cooling-water temperature sensor is connected with MCU common I/O port, can be popped one's head in using the DS18b20 water temperatures of good seal, but not
It is limited to this；The ADC mouths connection of acidity-basicity sensor and dissolved oxygen sensor and MCU, wherein acidity-basicity sensor can use band
The pH value collection sensor of temperature-compensating, dissolved oxygen sensor can use DO sensors, but not limited to this；MCU obtains environment number
After the data gathered according to acquisition module, data are packed and header and the complete packet of telegram end composition is mixed, using without line number
Data are passed back ground control centre according to transport module.
Further, the control module and wireless transport module are arranged in waterproof sealing cabin, the waterproof sealing cabin 6
The top of aircraft body 1 is fixed on, the waterproof sealing cabin 6 is made up of light waterproof material.
Further, the environmental data collecting module passes through expansion link 5 and the phase of aircraft body 1 with water-proof CCD camera
Even；Also include support 3, the kickboard 2 is connected by support 3 with the lower end of aircraft body 1；When aircraft flies in water surface water skiing
During row, kickboard 2 provides certain buoyancy for whole aircraft, reduces system energy consumption, under gravity, in whole system most
Bottom and the position for being less than kickboard；When aircraft lands on ground, expansion link 5 compresses, by environmental data collecting module with taking the photograph
As head is retracted to the position contour with kickboard 2, it is ensured that aircraft can be stopped steadily on the ground.
Further, LED is housed, the LED is connected with control module, just around the camera lens of the water-proof CCD camera
Shooting of the water-proof CCD camera to low light environment under water when aircraft water skiing flight, the pattern of water-proof CCD camera by MCU controls,
When being shot to the water surface, LED is gone out, and when being shot to underwater environment, LED is bright.
As shown in figure 3, the mode of operation of water environment monitoring aircraft is broadly divided into two kinds：
(1) water surface is monitored：When aircraft flight above waters, water-proof CCD camera carries out realtime graphic to the water surface and adopted
Collection, and ground control centre is passed back by wireless image-sound transport module；
(2) underwater monitoring：After aircraft flies to specified waters, it lands in the water surface and water skiing flight, and environmental data is adopted
Collect module and in water-proof CCD camera immersion water, water-proof CCD camera carries out real-time underwater picture collection, and is transmitted by wireless image-sound
Module passes image back control centre, while cooling-water temperature sensor, acidity-basicity sensor and dissolved oxygen sensor carry out water quality data
Collection, and control centre back is passed data by wireless data transfer module.
The utility model is by by environmental data collecting module, water-proof CCD camera, wireless transport module, kickboard and aircraft
It is combined, and the water-proofing treatment of electronic equipment and the stretching and compression of support structures is carried out using the sealed compartment of lightweight, realizes
The three-dimensional water environment monitoring of the water surface, underwater all-dimensional.The utility model is simple in construction, easy to control, can efficiently, flexibly,
The economic monitoring for realizing water environment, it is adaptable to environmental monitoring.
Claims (7)
1. a kind of water environment monitors aircraft, including aircraft body, the aircraft body carries attitude transducer sum
Word compass, it is characterised in that the top of the aircraft body is provided with control module and wireless transport module, the aircraft
The bottom of main body is provided with environmental data collecting module and water-proof CCD camera, and the bottom of the aircraft body is also equipped with floating
Plate；The attitude transducer, digital compass, wireless transport module, environmental data collecting module and water-proof CCD camera with control
Module is connected, and the water-proof CCD camera is connected with wireless transport module；Barometer, the gas are also equipped with the aircraft body
Pressure meter is connected with control module.
2. water environment according to claim 1 monitors aircraft, it is characterised in that the wireless transport module is by wireless
Data transmission module, wireless image-sound transport module and wireless communication module composition, the wireless data transfer module and wireless
Communication module is connected with control module, and the wireless image-sound transport module is connected with water-proof CCD camera.
3. water environment according to claim 2 monitors aircraft, it is characterised in that the environmental data collecting module bag
Include cooling-water temperature sensor, acidity-basicity sensor and dissolved oxygen sensor.
4. water environment according to claim 3 monitors aircraft, it is characterised in that the control module and be wirelessly transferred
Module is arranged in waterproof sealing cabin, and the waterproof sealing cabin is fixed on the top of aircraft body.
5. water environment according to claim 4 monitors aircraft, it is characterised in that the environmental data collecting module with
Water-proof CCD camera is connected by expansion link with aircraft body.
6. water environment according to claim 5 monitors aircraft, it is characterised in that also including support, the kickboard is led to
Support is crossed with the lower end of aircraft body to be connected.
7. water environment according to claim 6 monitors aircraft, it is characterised in that the camera lens week of the water-proof CCD camera
Enclose equipped with LED, the LED is connected with control module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621211511.9U CN206353151U (en) | 2016-11-10 | 2016-11-10 | A kind of water environment monitors aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621211511.9U CN206353151U (en) | 2016-11-10 | 2016-11-10 | A kind of water environment monitors aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206353151U true CN206353151U (en) | 2017-07-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621211511.9U Expired - Fee Related CN206353151U (en) | 2016-11-10 | 2016-11-10 | A kind of water environment monitors aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206353151U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106526116A (en) * | 2016-11-10 | 2017-03-22 | 浙江大学 | Water area environment monitoring aircraft and monitoring method thereof |
| CN108802315A (en) * | 2018-06-15 | 2018-11-13 | 南通航运职业技术学院 | A kind of water environment monitoring device and its monitoring method |
-
2016
- 2016-11-10 CN CN201621211511.9U patent/CN206353151U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106526116A (en) * | 2016-11-10 | 2017-03-22 | 浙江大学 | Water area environment monitoring aircraft and monitoring method thereof |
| CN108802315A (en) * | 2018-06-15 | 2018-11-13 | 南通航运职业技术学院 | A kind of water environment monitoring device and its monitoring method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170725 Termination date: 20191110 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |