CN207550485U - Unmanned plane and the environmental monitoring system based on the unmanned plane - Google Patents
Unmanned plane and the environmental monitoring system based on the unmanned plane Download PDFInfo
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- CN207550485U CN207550485U CN201721637279.XU CN201721637279U CN207550485U CN 207550485 U CN207550485 U CN 207550485U CN 201721637279 U CN201721637279 U CN 201721637279U CN 207550485 U CN207550485 U CN 207550485U
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- unmanned plane
- bottom plate
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Abstract
The utility model discloses a kind of unmanned plane and the environmental monitoring system based on the unmanned plane, the unmanned plane includes fuselage, air quality detecting device, flight controller, data transmission device and power supply are set on the fuselage, and the power supply is air quality detecting device, the power supply of flight controller, data transmission device；The fuselage includes support column, the top setting top plate of the support column, the bottom end setting bottom plate of the support column, fixed horn is symmetrical arranged at left and right sides of the support column, the fixed horn is fixed on support column or bottom plate, the both sides of the fixed horn are symmetrical arranged movable horn, and the activity horn, the fixed one end of horn far from bottom plate are respectively provided with motor, propeller set on the motor.The beneficial effects of the utility model are：Unmanned plane can be carried with folding convenient.
Description
Technical field
The utility model relates generally to environmental monitoring, specifically unmanned plane and the environmental monitoring system based on the unmanned plane
System.
Background technology
Existing environment monitor is mostly using one-point measurement, since the density of setting of environment detector is limited, there are the problem of
It can not accurately go to measure the air quality in specific region, with the raising of environmental consciousness, Environmental Protection in China department is to environment
Monitoring dynamics is also constantly being strengthened, and in order to which the efforts at environmental protection of enterprise are exercised supervision and instructed, needs to determine enterprise
Phase, irregular green audit, situation about can not only be prevented when checking by enterprise with various means, but also exist
It the problems such as monitoring real-time lag, limited space, precision be low and then occurs as soon as and unmanned plane is applied to environmental monitoring, in use
It there is also some problems：
1st, unmanned plane unfolded state is in irregular shape, and mechanical strength is less desirable, if protection is improper during carrying
The damage of unmanned plane especially horn part can be caused, but existing unmanned plane occupancy volume is larger and can not fold, and carries
When just need larger container, it is inconvenient.
2nd, existing environmental monitoring system earth station is fixed, once unmanned plane divides shape range to be detected beyond earth station
Distance, it is impossible at once by the data transmission obtained in the air to earth station.
Utility model content
To solve deficiency of the prior art, the utility model provides a kind of unmanned plane and the environment prison based on the unmanned plane
Examining system, unmanned plane can be carried with folding convenient, and earth station includes remote controler and data sink, and unmanned plane, which directly reaches, to be referred to
Determine region overhead and environmental monitoring is carried out to air, earth station can follow unmanned plane transfer to facilitate reception data, by acquisition
Sensing data and GPS coordinate pass earth station back by data transmission device, can determine whether data are exceeded in real time.
The utility model to achieve the above object, is achieved through the following technical solutions：
Unmanned plane, including fuselage, it is characterised in that：On the fuselage set air quality detecting device, flight controller,
Data transmission device and power supply, the power supply is air quality detecting device, the power supply of flight controller, data transmission device；
The fuselage includes support column, the top setting top plate of the support column, and the bottom end of the support column sets bottom plate,
Electron speed regulator is fixedly mounted between top plate, bottom plate, and supporting leg, the support column or so are symmetrical set on the bottom plate
Both sides are symmetrical arranged fixed horn, and the fixed horn is fixed on support column or bottom plate, the both sides of the fixed horn
Activity horn is symmetrical arranged, the activity horn, the fixed one end of horn far from bottom plate are respectively provided with motor, the motor and electronics
Governor is connected, the output terminal connection of electron speed regulator and flight controller, and propeller, the moving machine are set on the motor
The one end of arm far from motor is connect by first rotating shaft with bottom plate, and the activity horn is located relatively between motor and first rotating shaft
Screw hole A is set, setting locking nut A and arc chute corresponding with locking nut A quantity, position on the top plate, bottom plate
A。
Mounting base for installing supporting leg is set on the bottom plate, and the supporting leg is turned by the second shaft and mounting base
Dynamic connection, sets screw hole B on the supporting leg, in the mounting base installation locking nut B and with locking nut B quantity, position
Put corresponding arc chute B.
GPS sensor is also set up on the fuselage, GPS sensor is used to measure unmanned plane location information.
Data transmission device includes receiver, wireless data transmission module.
The wireless data transmission module is 433M wireless data transmission modules, and the receiver is R12DS receivers.
The air quality detecting device include PM sensors, Temperature Humidity Sensor and controller, the PM sensors,
The data transmission of acquisition to controller, the controller are connect by Temperature Humidity Sensor with data transmission device signal.
Galvanometer is further included, galvanometer one end is connected with power supply, and the other end is connected with flight controller.
The power supply is accumulator, and the bottom plate sets power supply hanger, the power supply hanger between being located relatively at mounting base
Including support plate, the both ends of the support plate are respectively provided with outer tube, are slided in the outer tube and are arranged interior bar, the bottom of the interior bar
End setting spring, the top of the interior bar are stretched out outer tube and are connect with bottom plate.
A kind of environmental monitoring system, including unmanned plane and moveable earth station, the earth station includes remote controler sum number
According to reception device, receiver is matched with remote controler, and display is set on the data sink.
Comparison and the prior art, the utility model advantageous effect are：
1st, the movable horn of the utility model unmanned plane can fold, and reduce the occupied space of unmanned plane, and fuselage interior
Most of space be hollow structure, the weight of unmanned plane can be reduced, the load of unmanned plane is effectively reduced, be effectively increased nothing
Man-machine duration performance.
2nd, the utility model supporting leg can also fold, and further reduce the occupied space of unmanned plane.
3rd, the utility model data transmission device includes receiver, wireless data transmission module, and receiver is matched with remote controler, and
Remote controler information is sent to flight controller, wireless data transmission module is read from flight controller, air quality detecting device
Acquisition information in direction, speed, position and sensor during unmanned plane during flying etc. is simultaneously transferred to earth station.
4th, the utility model bottom plate sets power supply hanger between being located relatively at two mounting bases, facilitates installation and replacement electric
Pond.
5th, the utility model earth station includes remote controler and data sink, and unmanned plane directly reaches specified region overhead
Environmental monitoring is carried out to air, earth station can follow unmanned plane transfer to facilitate reception data, by the sensing data of acquisition
Earth station is passed back by data transmission device with GPS coordinate, can determine whether data are exceeded in real time.
Description of the drawings
Attached drawing 1 is the structure diagram one of unmanned plane.
Attached drawing 2 is the structure diagram two of unmanned plane.
Attached drawing 3 is the vertical view of unmanned plane.
Attached drawing 4 is the structure diagram of bottom plate.
Attached drawing 5 is the folded state schematic diagram of unmanned plane.
Attached drawing 6 is the structure diagram of the utility model.
Label shown in attached drawing：1st, air quality detecting device；2nd, flight controller；21st, electron speed regulator；3rd, data pass
Defeated device；4th, power supply；5th, support column；6th, top plate；7th, bottom plate；8th, supporting leg；81st, mounting base；82nd, screw hole B；83rd, locking nut
B；84th, arc chute B；9th, fixed horn；90th, support plate；91st, outer tube；92nd, interior bar；93rd, spring；10th, movable horn；11、
Motor；12nd, screw hole A；13rd, locking nut A；14th, arc chute A；15th, GPS sensor；16th, galvanometer；17th, earth station.
Specific embodiment
With reference to the drawings and specific embodiments, the utility model is described in further detail.It should be understood that these embodiments are only used for
Illustrate the utility model rather than limitation the scope of the utility model.In addition, it should also be understood that, having read the utility model instruction
Content after, those skilled in the art can make various changes or modifications the utility model, and such equivalent forms are equally fallen
In range defined herein.
Unmanned plane including fuselage, sets air quality detecting device 1 on the fuselage, for the air to specifying region
Environmental monitoring is carried out, flight controller 2 controls the motor 11 of unmanned plane, and then controls the offline mode of unmanned plane.Number
According to transmitting device 3 and power supply 4, data transmission device 3 transmits for unmanned plane and earth station 17 into row information；The power supply 4 is
Air quality detecting device 1, flight controller 2, data transmission device 3 are powered.The fuselage includes support column 5, the support
The top setting top plate 6 of column 5, the bottom end setting bottom plate 7 of the support column 5, electron speed regulator 21 are fixedly mounted on top plate 6, bottom
Between plate 7, the quantity of electron speed regulator is identical with motor, and supporting leg 8, the support column 5 are symmetrical set on the bottom plate 7
The left and right sides is symmetrical arranged fixed horn 9, and the fixed horn 9 is fixed on support column 5 or bottom plate 7, the fixed machine
The both sides of arm 9 are symmetrical arranged movable horn 10, and the activity horn 10, the fixed one end of horn 9 far from bottom plate 7 are respectively provided with motor
11, the motor 11 is connected with electron speed regulator 21, and electron speed regulator 21 is connect with the output terminal of flight controller 2, the electricity
Propeller is set on machine 11, and the described activity one end of horn 10 far from motor 11 is connect by first rotating shaft with bottom plate 7, the work
Motivation arm 10 is located relatively at setting screw hole A12 between motor 11 and first rotating shaft, and locking nut is set on the top plate 6, bottom plate 7
A13 and arc chute A14 corresponding with locking nut A13 quantity, position, is preferably respectively provided at the both ends of arc chute A14
Baffle, the scope of activities of limitation activity horn 10.(as shown in Figure 3) is unfolded in movable horn 10 during use, it when not in use will be living
Motivation arm 10 folds (as shown in Figure 5), reduces the occupied space of unmanned plane, and most of space of fuselage interior is hollow knot
The new materials such as structure and use carbon fiber and aerolite, can reduce the weight of unmanned plane, effectively reduce unmanned plane
Load is effectively increased the duration performance of unmanned plane.
Preferably, the mounting base 81 for installing supporting leg 8 is set on the bottom plate 7, and the supporting leg 8 passes through second turn
Axis is rotatablely connected with mounting base 81, and screw hole B82 is set on the supporting leg 8, in the mounting base 81 installation locking nut B83 with
And arc chute B84 corresponding with locking nut B83 quantity, position, (as shown in Figure 2) is unfolded in supporting leg 8 during use, is not made
Supporting leg 8 is folded (as shown in Figure 1) by the used time, can further reduce the occupied space of unmanned plane.
Preferably, GPS sensor 15 is also set up on the fuselage, GPS sensor 15 is used to measure unmanned plane location information.
Preferably, data transmission device 3 includes receiver, wireless data transmission module, and receiver matches, and will be distant with remote controler
Control device information is sent to flight controller 2, and wireless data transmission module reads nothing from flight controller 2, air quality detecting device 1
Acquisition information in direction, speed, position and sensor during man-machine flight etc. is simultaneously transferred to earth station 17.
The wireless data transmission module is 433M wireless data transmission modules, and the receiver is R12DS receivers, is existing skill
Art is not described in detail herein.
The air quality detecting device 1 includes PM sensors, Temperature Humidity Sensor and controller, the PM sensings
By the data transmission of acquisition to controller, the PM sensors are preferably high-precision laser sensor for device, Temperature Humidity Sensor,
The controller is connect with 3 signal of data transmission device.Controller uses IAP15 microcontrollers, PM sensors, Temperature Humidity Sensor
The data transmission of acquisition is decoded to IAP15 microcontrollers, while GPS module is also by collected data transmission to IAP15
Microcontroller, IAP15 microcontrollers acquire the data mart modeling being collected into processing, IAP15 monolithics function accurately under relatively low power consumption
To the high accuracy data of 2 significant digits.
Galvanometer 16 is further included, 16 one end of galvanometer is connected with power supply 4, and the other end is connected with flight controller 2.
The power supply 4 is lithium battery, and the bottom plate 7 sets power supply hanger between being located relatively at two mounting bases 81, described
Power supply hanger includes support plate 90, and the both ends of the support plate 90 are respectively provided with outer tube 91, slide and be arranged in the outer tube 91
Interior bar 92, the bottom end setting spring 93 of the interior bar 92, the top of the interior bar 92 are stretched out outer tube 91 and are connect with bottom plate 7,
Facilitate installation and replacement battery.
A kind of environmental monitoring system, including unmanned plane and moveable earth station 17, the earth station 17 includes remote controler
And data sink, receiver are matched with remote controler, remote controler can control unmanned plane to carry out various actions, and the data connect
Display is set on receiving apparatus.IAP15 microcontrollers are by after the data mart modeling being collected into processing, by 433M wireless data sendings by data
It send to earth station 17, equally using IAP15 microcontrollers, IAP15 microcontrollers are mounted in housing for data sink, and connection is aobvious
It can be used after display screen, it is small, it is mobile flexible, 433M wireless data sendings are connected, the data received are decoded, are shown in aobvious
In display screen, display screen can be 12864 display screens.
Embodiment 1：
Unmanned plane including fuselage, sets air quality detecting device 1, Pixhawk flight controllers, number on the fuselage
According to transmitting device 3, power supply 4 and GPS sensor 15, GPS sensor 15 is used to measure unmanned plane location information.Data transmission device
3 include receiver, wireless data transmission module, and the wireless data transmission module is 433M wireless data transmission modules, and the receiver is R12DS
Receiver.The air quality detecting device 1 include PM sensors, Temperature Humidity Sensor and controller, the PM sensors,
The data transmission of acquisition to controller, the controller are connect by Temperature Humidity Sensor with 3 signal of data transmission device.The electricity
Source 4 is accumulator, and the power supply 4 is air quality detecting device 1, Pixhawk flight controllers, data transmission device 3 are powered,
Galvanometer 16 is further included, 16 one end of galvanometer is connected with power supply 4, and the other end is connected with Pixhawk flight controllers.The fuselage
Including support column 5, the top setting top plate 6 of the support column 5, the bottom end setting bottom plate 7 of the support column 5, electron speed regulator
21 are fixedly mounted between top plate 6, bottom plate 7, and the quantity of electron speed regulator is identical with motor, symmetrical on the bottom plate 7 to set
Supporting leg 8 is put, for installing the mounting base 81 of supporting leg 8, the supporting leg passes through the second shaft and peace for setting on the bottom plate 7
Dress seat 81 is rotatablely connected, and screw hole B82 is set on the supporting leg 8, in the mounting base 81 installation locking nut B83 and with lock
Tight nut B83 quantity, the corresponding arc chute B84 in position.Fixed horn 9, institute are symmetrical arranged at left and right sides of 5 column of support column
It states fixed horn 9 to be fixed on support column or bottom plate 7, the both sides of the fixed horn 9 are symmetrical arranged movable horn 10, institute
State movable horn 10, the fixed one end of horn far from bottom plate 7 is respectively provided with motor 11, the motor 11 and 21 phase of electron speed regulator
Even, electron speed regulator 21 is connect with the output terminal of Pixhawk flight controllers, and propeller, the work are set on the motor 11
The one end of motivation arm 10 far from motor 11 is connect by first rotating shaft with bottom plate 7, and the activity horn 10 is located relatively at motor 11
Screw hole A12 is set between first rotating shaft, on the top plate 6, bottom plate 7 setting locking nut A13 and with locking nut A13 numbers
Amount, the corresponding arc chute A14 in position.The bottom plate 7 sets power supply hanger between being located relatively at mounting base 81, and the power supply is hung
Frame includes support plate 90, and the both ends of the support plate 90 are respectively provided with outer tube 91, are slided in the outer tube 91 and be arranged interior bar 92,
The bottom end setting spring 93 of the interior bar 92, the top of the interior bar 92 are stretched out outer tube 91 and are connect with bottom plate 7.The present embodiment
Advantageous effect be：Unmanned plane can be carried with folding convenient.
Embodiment 2：
A kind of environmental monitoring system, including right unmanned plane described in embodiment 1 and moveable earth station 17, describedly
Face station 17 includes remote controler and data sink, and data transmission device 3 includes receiver, wireless data transmission module and network mould
Block, the network module can be gsm modules, can the information of sensor be sent to server in real time, permanently retain shelves
Case, as long as there is network to may have access to and download.Receiver is matched with remote controler, and display is set on the data sink.
Remote controler uses happy enlightening at9s remote controlers, is in terms of specific debugging：For this system altogether using 9 channels, 1-4 channels are respectively dynamic
Power, forward-reverse, left and right, rotation, 5 channels adjust offline mode, and respectively from steady pattern, GPS fixed point modes, land mould automatically
Formula, air pressure determine height mode, pitch of the laps pattern, the automatic simultaneously landing mode that makes a return voyage.The advantageous effect of the present embodiment is：Remote controler can be with
Unmanned plane is controlled to carry out various actions, display is set on the data sink.The data that IAP15 microcontrollers will be collected into
After working process, data are sent to earth station 17 by 433M wireless data sendings, data sink equally uses IAP15 monolithics
Machine connects 433M wireless data sendings, the data received is decoded, and IAP15 microcontrollers are mounted in housing and are equipped with switch,
Powered using battery (such as 5V-3000mah poly-lithium batteries), it is small, it is mobile flexible, open after power supply 4 automatically with nobody
Digital transmission module connects on machine, after receiving data and verification data accuracy, is displayed on the screen, and display screen is 12864 displays
Screen.
Claims (10)
1. unmanned plane, including fuselage, it is characterised in that：Air quality detecting device (1), flight controller are set on the fuselage
(2), electron speed regulator (21), data transmission device (3) and power supply (4), the power supply (4) for air quality detecting device (1),
Flight controller (2), data transmission device (3) power supply；
The fuselage includes support column (5), the top setting top plate (6) of the support column (5), the bottom end of the support column (5)
Bottom plate (7) is set, and electron speed regulator (21) is fixedly mounted between top plate (6), bottom plate (7), symmetrical on the bottom plate (7)
Supporting leg (8) is set, fixed horn (9) is symmetrical arranged at left and right sides of the support column (5), fixed horn (9) fixation is set
It puts on support column (5) or bottom plate (7), the both sides of the fixed horn (9) are symmetrical arranged movable horn (10), the moving machine
Arm (10), the fixed one end of horn (9) far from bottom plate (7) are respectively provided with motor (11), the motor (11) and electron speed regulator
(21) it is connected, electron speed regulator (21) is connect with the output terminal of flight controller (2), and propeller is set on the motor (11),
The described one end of activity horn (10) far from motor (11) is connect by first rotating shaft with bottom plate (7), the activity horn (10)
It is located relatively at motor (11) and screw hole A (12) is set between first rotating shaft, the top plate (6), bottom plate set locking nut on (7)
A (13) and arc chute A (14) corresponding with locking nut A (13) quantity, position.
2. unmanned plane according to claim 1, it is characterised in that：It sets that supporting leg (8) is installed on the bottom plate (7)
Mounting base (81), the supporting leg (8) is rotatablely connected by the second shaft and mounting base (81), set on the supporting leg (8)
Put screw hole B (82), installation locking nut B (83) and opposite with locking nut B (83) quantity, position on the mounting base (81)
Answer arc chute B (84).
3. unmanned plane according to claim 1, it is characterised in that：GPS sensor (15), GPS are also set up on the fuselage
Sensor (15) is for measuring unmanned plane location information.
4. unmanned plane according to claim 1, it is characterised in that：Data transmission device (3) includes receiver, wireless data sending
Module.
5. unmanned plane according to claim 4, it is characterised in that：The wireless data transmission module is 433M wireless data sending moulds
Block, the receiver are R12DS receivers.
6. according to the unmanned plane described in claim 1-5 any one, it is characterised in that：The air quality detecting device
(1) including PM sensors, Temperature Humidity Sensor and controller, the PM sensors, Temperature Humidity Sensor pass the data of acquisition
Defeated to arrive controller, the controller is connect with data transmission device (3) signal.
7. unmanned plane according to claim 1, it is characterised in that：Further include galvanometer (16), galvanometer (16) one end with
Power supply (4) is connected, and the other end is connected with flight controller (2).
8. unmanned plane according to claim 1, it is characterised in that：The power supply (4) be accumulator, bottom plate (7) phase
Power supply hanger is set to being located between two mounting bases (81), the power supply hanger includes support plate (90), the support plate
(90) both ends are respectively provided with outer tube (91), are slided in the outer tube (91) and are arranged interior bar (92), the bottom of the interior bar (92)
End setting spring (93), the top of the interior bar (92) are stretched out outer tube (91) and are connect with bottom plate (7).
9. a kind of environmental monitoring system, it is characterised in that：Including nobody described in 1,2,3,4,5,7,8 any one of claim
Machine and moveable earth station (17), the earth station (17) include remote controler and data sink, receiver and remote controler
It matches, display is set on the data sink.
10. a kind of environmental monitoring system, it is characterised in that：Including the unmanned plane described in claim 6 and moveable earth station
(17), the earth station (17) includes remote controler and data sink, and receiver is matched with remote controler, the data receiver dress
Put setting display.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721637279.XU CN207550485U (en) | 2017-11-29 | 2017-11-29 | Unmanned plane and the environmental monitoring system based on the unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721637279.XU CN207550485U (en) | 2017-11-29 | 2017-11-29 | Unmanned plane and the environmental monitoring system based on the unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN207550485U true CN207550485U (en) | 2018-06-29 |
Family
ID=62678109
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721637279.XU Active CN207550485U (en) | 2017-11-29 | 2017-11-29 | Unmanned plane and the environmental monitoring system based on the unmanned plane |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109187884A (en) * | 2018-10-08 | 2019-01-11 | 西北农林科技大学 | A kind of Atmospheric components of anti-disturbance based on unmanned plane monitor system |
| CN111003175A (en) * | 2019-10-11 | 2020-04-14 | 浙江华奕航空科技有限公司 | Air inlet processing method of atmospheric environment monitoring unmanned aerial vehicle |
| CN111749094A (en) * | 2020-07-12 | 2020-10-09 | 京山俊平机电科技有限公司 | Detection device for highway bridge maintenance and use method thereof |
| CN112946200A (en) * | 2021-02-23 | 2021-06-11 | 广州市景让信息科技有限公司 | Data monitoring equipment based on big data platform |
-
2017
- 2017-11-29 CN CN201721637279.XU patent/CN207550485U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109187884A (en) * | 2018-10-08 | 2019-01-11 | 西北农林科技大学 | A kind of Atmospheric components of anti-disturbance based on unmanned plane monitor system |
| CN111003175A (en) * | 2019-10-11 | 2020-04-14 | 浙江华奕航空科技有限公司 | Air inlet processing method of atmospheric environment monitoring unmanned aerial vehicle |
| CN111749094A (en) * | 2020-07-12 | 2020-10-09 | 京山俊平机电科技有限公司 | Detection device for highway bridge maintenance and use method thereof |
| CN112946200A (en) * | 2021-02-23 | 2021-06-11 | 广州市景让信息科技有限公司 | Data monitoring equipment based on big data platform |
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