CN206114693U - Unmanned aerial vehicle carries remote sensing wind-force monitoring devices - Google Patents
Unmanned aerial vehicle carries remote sensing wind-force monitoring devices Download PDFInfo
- Publication number
- CN206114693U CN206114693U CN201620595836.5U CN201620595836U CN206114693U CN 206114693 U CN206114693 U CN 206114693U CN 201620595836 U CN201620595836 U CN 201620595836U CN 206114693 U CN206114693 U CN 206114693U
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- wind
- air velocity
- aerial vehicle
- unmanned aerial
- transducer
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Abstract
The utility model provides an airborne remote sensing wind power monitoring device of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, a rotor wing, a shock absorption rod, an undercarriage, a wireless communication device, a bracket, an installation bottom plate, a wind ring, a wind speed sensor, a wind vane, a wind direction sensor and an information acquisition chip; the four corners of the top end of the unmanned aerial vehicle body are provided with rotor wings, and the undercarriage is arranged at the bottom end of the unmanned aerial vehicle body through shock-absorbing rods; the central authorities position on unmanned aerial vehicle body top is equipped with the support, the top of support is equipped with mounting plate, mounting plate's the height that highly is higher than the rotor, the last air velocity transducer that is equipped with of mounting plate, wind direction sensor, the last wind ring that is equipped with of air velocity transducer, the last weather vane that is equipped with of wind direction sensor, still be equipped with the information acquisition chip on the mounting plate, the input and the air velocity transducer of information acquisition chip, wind direction sensor are connected, the output and the wireless communication device of information acquisition chip are connected. The beneficial effects of the utility model are that but real-time supervision wind direction, wind speed.
Description
Technical field
This utility model belongs to remote sensing technology field, fills more particularly, to a kind of monitoring of pilotless aircraft airborne remote sensing wind-force
Put.
Background technology
Existing wind force monitoring device is assembled into greatly fixed website, can only monitor some region of wind speed and direction letter
Breath, physical resources utilization rate bottom is a kind of can solving this problem, monitoring wind force monitoring device being mounted on unmanned plane
System needs further to research and develop.
Utility model content
It is distant that the purpose of this utility model is to provide the high pilotless aircraft airborne of a kind of simple structure, simple to operate, stability
Sense wind force monitoring device.
The technical solution of the utility model is：A kind of pilotless aircraft airborne remote sensing wind force monitoring device of the present utility model,
Including unmanned plane body, rotor, decoupling rod, undercarriage, radio communication device, support, mounting base, vane, air velocity transducer,
Weathercock, wind transducer, information gathering chip；
Four edges on the unmanned plane body top are provided with rotor, and the undercarriage is arranged on nobody by decoupling rod
The bottom of machine body；
The middle position on the unmanned plane body top is provided with support, and the top of the support is provided with mounting base, described
The height of mounting base is higher than the height of rotor, and the mounting base is provided with air velocity transducer, wind transducer, the wind speed
Covers disposed on sensor has vane, and the wind transducer is provided with weathercock, and information gathering chip, the letter are additionally provided with mounting base
The input of breath acquisition chip is connected with air velocity transducer, wind transducer, the outfan and nothing of described information acquisition chip
Line communicator is connected.
The top of the unmanned plane body is additionally provided with solar energy photovoltaic panel, electrical storage device, the solar energy photovoltaic panel and storage
The input of electric installation is connected, the outfan and radio communication device of the electrical storage device, air velocity transducer, wind direction sensing
Device, information gathering chip are connected.
This utility model has the advantages and positive effects that：
1st, due to adopting above-mentioned technical proposal, wind speed, wind direction real-time monitoring it is convenient；With simple structure, operation
Simply, the advantages of wind-force information of different regions can be gathered.
2nd, system run all right is high, and gathered data reliability is high.
Description of the drawings
Fig. 1 is structural representation of the present utility model.
In figure：
1- unmanned plane bodies, 2- rotors, 3- decoupling rods, 4- undercarriages, 5- solar energy photovoltaic panels, 6- electrical storage devices, 7- without
Line communicator, 8- supports, 9- mounting bases, 10- vanes, 11- air velocity transducers, 12- weathercocks, 13- wind transducers, 14-
Information gathering chip.
Specific embodiment
This utility model is elaborated below in conjunction with the accompanying drawings.
As shown in figure 1, a kind of pilotless aircraft airborne remote sensing wind force monitoring device of the present utility model, including unmanned plane body
1st, rotor 2, decoupling rod 3, undercarriage 4, solar energy photovoltaic panel 5, electrical storage device 6, radio communication device 7, support 8, mounting base
9th, vane 10, air velocity transducer 11, weathercock 12, wind transducer 13, information gathering chip 14；
Four edges on the top of unmanned plane body 1 are provided with rotor 2, and undercarriage 4 is arranged on unmanned plane sheet by decoupling rod 3
The bottom of body 1；
The middle position on the top of unmanned plane body 1 is provided with support 8, and the top of support 8 is provided with mounting base 9, mounting base 9
Height higher than rotor 2 height, the mounting base 9 is provided with air velocity transducer 11, wind transducer 13, air velocity transducer
11 are provided with vane 10, and wind transducer 13 is provided with weathercock 12, information gathering chip 14, information are additionally provided with mounting base 9
The input of acquisition chip 14 is connected with air velocity transducer 11, wind transducer 13, the outfan of information gathering chip 14 and
Radio communication device 7 is connected.
The top of the unmanned plane body 1 is additionally provided with solar energy photovoltaic panel 5, electrical storage device 6, solar energy photovoltaic panel 5 and storage
The input of electric installation 6 is connected, the outfan and radio communication device 7 of electrical storage device 6, air velocity transducer 11, wind direction sensing
Device 13, information gathering chip 14 are connected.
The course of work of this example：
The setting of decoupling rod 3 can play good cushioning effect, and when preventing unmanned plane body 1 from landing, ground shock power is damaged
The harmful electronic devices and components that it is carried.
The setting of mounting base 9, both to the setting of air velocity transducer 11, wind transducer 13 and information gathering chip 14
There is provided enough spaces, the impact that the rotation of rotor 2 is caused to vane 10, weathercock 12 can be weakened again, improve monitoring numerical value
Reliability.
When using, presumptive area is entered into using cruise system control unmanned plane body 1, air velocity transducer 11, wind direction is passed
Sensor 13 can real-time monitoring wind speed and direction, and by these information transmissions to information gathering chip 14, information gathering chip 14 leads to
Cross radio communication device 7 and pass to ground monitoring end.
The setting of solar energy photovoltaic panel 5, electrical storage device 6, can provide power source for monitoring system, with environmental protection,
The effect of reducing energy consumption.
One embodiment of the present utility model has been described in detail above, but the content is only of the present utility model
Preferred embodiment, it is impossible to be considered as limiting practical range of the present utility model.It is all to be made according to this utility model application range
Impartial change with improve etc., all should still belong within patent covering scope of the present utility model.
Claims (2)
1. a kind of pilotless aircraft airborne remote sensing wind force monitoring device, it is characterised in that：Including unmanned plane body, rotor, decoupling rod,
Undercarriage, radio communication device, support, mounting base, vane, air velocity transducer, weathercock, wind transducer, information gathering core
Piece；
Four edges on the unmanned plane body top are provided with rotor, and the undercarriage is arranged on unmanned plane sheet by decoupling rod
The bottom of body；
The middle position on the unmanned plane body top is provided with support, and the top of the support is provided with mounting base, the installation
The height of base plate is higher than the height of rotor, and the mounting base is provided with air velocity transducer, wind transducer, the wind speed sensing
Device is provided with vane, and the wind transducer is provided with weathercock, and information gathering chip is additionally provided with mounting base, and described information is adopted
The input of collection chip is connected with air velocity transducer, wind transducer, the outfan and channel radio of described information acquisition chip
T unit is connected.
2. a kind of pilotless aircraft airborne remote sensing wind force monitoring device according to claim 1, it is characterised in that：It is described nobody
The top of machine body is additionally provided with the input phase of solar energy photovoltaic panel, electrical storage device, the solar energy photovoltaic panel and electrical storage device
Connection, the outfan and radio communication device of the electrical storage device, air velocity transducer, wind transducer, information gathering chip phase
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620595836.5U CN206114693U (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle carries remote sensing wind-force monitoring devices |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620595836.5U CN206114693U (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle carries remote sensing wind-force monitoring devices |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206114693U true CN206114693U (en) | 2017-04-19 |
Family
ID=58509550
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620595836.5U Active CN206114693U (en) | 2016-06-14 | 2016-06-14 | Unmanned aerial vehicle carries remote sensing wind-force monitoring devices |
Country Status (1)
| Country | Link |
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| CN (1) | CN206114693U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107215464A (en) * | 2017-06-27 | 2017-09-29 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with long battery life |
| CN108490215A (en) * | 2018-04-19 | 2018-09-04 | 广东华南农业航空工程研究院有限公司 | A kind of flight wind direction monitoring device of unmanned plane, monitoring system and monitoring method |
| WO2018205379A1 (en) * | 2017-05-08 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Tarmac |
-
2016
- 2016-06-14 CN CN201620595836.5U patent/CN206114693U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018205379A1 (en) * | 2017-05-08 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Tarmac |
| CN107215464A (en) * | 2017-06-27 | 2017-09-29 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with long battery life |
| CN107215464B (en) * | 2017-06-27 | 2018-10-02 | 吉林省翼启飞科技有限公司 | A kind of intelligent unmanned plane with long battery life |
| CN108490215A (en) * | 2018-04-19 | 2018-09-04 | 广东华南农业航空工程研究院有限公司 | A kind of flight wind direction monitoring device of unmanned plane, monitoring system and monitoring method |
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