CN210653642U - Unmanned aerial vehicle for environmental monitoring - Google Patents

Unmanned aerial vehicle for environmental monitoring Download PDF

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Publication number
CN210653642U
CN210653642U CN201921690867.9U CN201921690867U CN210653642U CN 210653642 U CN210653642 U CN 210653642U CN 201921690867 U CN201921690867 U CN 201921690867U CN 210653642 U CN210653642 U CN 210653642U
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CN
China
Prior art keywords
aerial vehicle
unmanned aerial
environmental monitoring
fuselage
singlechip
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Active
Application number
CN201921690867.9U
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Chinese (zh)
Inventor
刘炜杰
张吴霜
贾素
戴燕峰
徐振华
徐春花
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangsu Zhongqi Environment Technology Co ltd
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Jiangsu Zhongqi Environment Technology Co ltd
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Priority to CN201921690867.9U priority Critical patent/CN210653642U/en
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Publication of CN210653642U publication Critical patent/CN210653642U/en
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Abstract

The utility model discloses an unmanned aerial vehicle for environmental monitoring, which comprises an unmanned aerial vehicle for environmental monitoring, wherein the unmanned aerial vehicle for environmental monitoring is provided with a machine body, a detection mechanism, a screw mounting groove, an anti-collision rubber ring, a machine foot, a telescopic sampling mechanism, an empty groove and a circuit board, the unmanned aerial vehicle for environment monitoring is in a round cake shape, the side edge of the unmanned aerial vehicle body for environment monitoring is thin, the middle of the unmanned aerial vehicle body for environment monitoring is thick, so that the unmanned aerial vehicle for environment monitoring is less windage when flying in the air, so that the unmanned aerial vehicle for environment monitoring can fly stably and rapidly in the air, a telescopic mining mechanism is arranged below a detection mechanism of the unmanned aerial vehicle for environment monitoring, the telescopic mining mechanism extends and retracts under the driving of a stepping motor, detect the air in the external world or the water in waters, this device reasonable in design, simple structure, the fuselage is small and exquisite, adopts the design of flying saucer formula, improves unmanned aerial vehicle's for environmental monitoring stability.

Description

Unmanned aerial vehicle for environmental monitoring
Technical Field
The utility model relates to an unmanned aerial vehicle technical field for environmental monitoring specifically is an unmanned aerial vehicle for environmental monitoring.
Background
In recent years, various pollution modes such as severe weather, haze and the like are intuitively presented to people, and great troubles are caused to the traveling and the body health of people.
With the development of social economy, the degree of industrial automation is improved, various mechanical equipment runs, and vehicles on roads are increased day by day, so that gasoline or coal is combusted at every moment, and a large amount of pollutants are discharged to the atmosphere. Therefore, in order to monitor the pollution condition in the air in real time, an environment monitoring unmanned aerial vehicle is generally adopted for pollution monitoring.
Disclosure of Invention
An object of the utility model is to provide a simple structure, the fuselage is small and exquisite, adopts the design of flying saucer formula, improves the unmanned aerial vehicle for environmental monitoring of unmanned aerial vehicle for environmental monitoring's stability to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle for environmental monitoring, includes unmanned aerial vehicle for environmental monitoring, be equipped with the fuselage on the unmanned aerial vehicle for environmental monitoring, the inside central authorities of fuselage are equipped with detection mechanism, detection mechanism's bottom central authorities are equipped with flexible sampling mechanism, detection mechanism's outside symmetry is equipped with the screw mounting groove, the outside edge of fuselage is equipped with the crashproof rubber circle, and the crashproof rubber circle passes through glue and pastes in the outside of fuselage, the bottom of fuselage is equipped with the undercarriage, and undercarriage and fuselage structure as an organic whole.
Preferably, the top of detection mechanism is equipped with the circuit board, be equipped with the singlechip on the circuit board, the top link of singlechip is equipped with the battery, and the left side link of singlechip is equipped with the stabiliser, the below link of singlechip is equipped with memory and wireless transceiver, another link of singlechip is equipped with the gyroscope, the GPS module, the driver, gyroscope, GPS module, driver are parallelly connected each other.
Preferably, a motor mounting bracket is arranged in the propeller mounting groove, and a micro motor is arranged in the middle of the motor mounting bracket.
Preferably, the telescopic sampling mechanism is provided with a telescopic rod, one end of the telescopic rod is provided with a stepping motor, the bottom end of the telescopic rod is provided with a hollow groove, the hollow groove transversely penetrates through the telescopic rod, and a PM2.5 sensor, a carbon dioxide sensor, a water body PH value sensor, an inhalable particle sensor and a temperature and humidity sensor are arranged inside the hollow groove.
Preferably, the fuselage adopts the design of flying saucer formula.
Compared with the prior art, the beneficial effects of the utility model are that:
this device reasonable in design, simple structure, the fuselage is small and exquisite, adopts the design of flying saucer formula, improves unmanned aerial vehicle's for environmental monitoring stability.
Drawings
Fig. 1 is a schematic structural view of the unmanned aerial vehicle for environmental monitoring of the present invention;
fig. 2 is a top view of the unmanned aerial vehicle for environmental monitoring of the present invention;
fig. 3 is a schematic diagram of the circuit board structure of the present invention.
In the figure: 1. an unmanned aerial vehicle for environmental monitoring; 2. a body; 3. a detection mechanism; 4. a propeller mounting groove; 5. an anti-collision rubber ring; 6. a machine leg; 7. a telescopic mining mechanism; 8. an empty groove; 9. a circuit board; 10. a storage battery; 11. a voltage regulator; 12. a single chip microcomputer; 13. a memory; 14. a wireless transceiver; 15. a gyroscope; 16. a GPS module; 17. a driver; 18. a micro motor; 19. a telescopic rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle for environmental monitoring, including unmanned aerial vehicle 1 for environmental monitoring, be equipped with fuselage 2 on unmanned aerial vehicle 1 for environmental monitoring, fuselage 2 adopts flying saucer formula design, the inside central authorities of fuselage 2 are equipped with detection mechanism 3, detection mechanism 3's top is equipped with circuit board 9, be equipped with singlechip 12 on the circuit board 9, singlechip 12's top link is equipped with battery 10, singlechip 12's left side link is equipped with stabiliser 11, singlechip 12's below link is equipped with memory 13 and wireless transceiver 14, another link of singlechip 12 is equipped with gyroscope 15, GPS module 16, driver 17, gyroscope 15, GPS module 16, driver 17 is parallelly connected each other.
Bottom central authorities of detection mechanism 3 are equipped with flexible sampling mechanism 7, be equipped with telescopic link 19 on the flexible sampling mechanism 7, the one end of telescopic link 19 is equipped with step motor, the bottom of telescopic link 19 is equipped with dead slot 8, dead slot 8 transversely runs through telescopic link 19, the inside of dead slot 8 is equipped with the PM2.5 sensor, the carbon dioxide sensor, water PH value sensor, the granule sensor can inhale, temperature and humidity sensor, the outside symmetry of detection mechanism 3 is equipped with screw mounting groove 4, the inside of screw mounting groove 4 is equipped with the motor installing support, the centre of motor installing support is equipped with micro motor 18.
The outside edge of fuselage 2 is equipped with crashproof rubber circle 5, and crashproof rubber circle 5 pastes in the outside of fuselage 2 through glue, protects for fuselage 2, and the bottom of fuselage 2 is equipped with undercarriage 6, and undercarriage 6 and fuselage 2 structure as an organic whole.
This device reasonable in design, simple structure, the fuselage is small and exquisite, adopts the design of flying saucer formula, improves unmanned aerial vehicle's for environmental monitoring stability.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (5)

1. The utility model provides an unmanned aerial vehicle for environmental monitoring, includes unmanned aerial vehicle (1) for environmental monitoring, its characterized in that: be equipped with fuselage (2) on unmanned aerial vehicle (1) for environmental monitoring, the inside central authorities of fuselage (2) are equipped with detection mechanism (3), the bottom central authorities of detection mechanism (3) are equipped with flexible sampling mechanism (7), the outside symmetry of detection mechanism (3) is equipped with screw mounting groove (4), the outside edge of fuselage (2) is equipped with crashproof rubber circle (5), and crashproof rubber circle (5) are pasted in the outside of fuselage (2) through glue, the bottom of fuselage (2) is equipped with machine foot (6), and machine foot (6) and fuselage (2) structure as an organic whole.
2. The unmanned aerial vehicle for environmental monitoring of claim 1, wherein: the top of detection mechanism (3) is equipped with circuit board (9), be equipped with singlechip (12) on circuit board (9), the top link of singlechip (12) is equipped with battery (10), and the left side link of singlechip (12) is equipped with stabiliser (11), the below link of singlechip (12) is equipped with memory (13) and wireless transceiver (14), another link of singlechip (12) is equipped with gyroscope (15), GPS module (16), driver (17), gyroscope (15), GPS module (16), driver (17) are parallelly connected each other.
3. The unmanned aerial vehicle for environmental monitoring of claim 1, wherein: and a motor mounting bracket is arranged in the propeller mounting groove (4), and a micro motor (18) is arranged in the middle of the motor mounting bracket.
4. The unmanned aerial vehicle for environmental monitoring of claim 1, wherein: the telescopic sampling mechanism (7) is provided with a telescopic rod (19), one end of the telescopic rod (19) is provided with a stepping motor, the bottom end of the telescopic rod (19) is provided with an empty groove (8), the empty groove (8) transversely penetrates through the telescopic rod (19), and the inside of the empty groove (8) is provided with a PM2.5 sensor, a carbon dioxide sensor, a water body PH value sensor, an inhalable particle sensor and a temperature and humidity sensor.
5. The unmanned aerial vehicle for environmental monitoring of claim 1, wherein: the machine body (2) is designed in a flying saucer type.
CN201921690867.9U 2019-10-11 2019-10-11 Unmanned aerial vehicle for environmental monitoring Active CN210653642U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921690867.9U CN210653642U (en) 2019-10-11 2019-10-11 Unmanned aerial vehicle for environmental monitoring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921690867.9U CN210653642U (en) 2019-10-11 2019-10-11 Unmanned aerial vehicle for environmental monitoring

Publications (1)

Publication Number Publication Date
CN210653642U true CN210653642U (en) 2020-06-02

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Application Number Title Priority Date Filing Date
CN201921690867.9U Active CN210653642U (en) 2019-10-11 2019-10-11 Unmanned aerial vehicle for environmental monitoring

Country Status (1)

Country Link
CN (1) CN210653642U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113720388A (en) * 2021-08-31 2021-11-30 扬州宇安电子科技有限公司 Miniature environmental monitoring positioning device based on many rotor unmanned aerial vehicle platforms

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113720388A (en) * 2021-08-31 2021-11-30 扬州宇安电子科技有限公司 Miniature environmental monitoring positioning device based on many rotor unmanned aerial vehicle platforms

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