CN208915444U - Meteorological detection unmanned plane - Google Patents
Meteorological detection unmanned plane Download PDFInfo
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- CN208915444U CN208915444U CN201821622475.4U CN201821622475U CN208915444U CN 208915444 U CN208915444 U CN 208915444U CN 201821622475 U CN201821622475 U CN 201821622475U CN 208915444 U CN208915444 U CN 208915444U
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- unmanned plane
- gondola
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- detection
- weather station
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Abstract
This application discloses a kind of meteorological detection unmanned planes, including unmanned plane, detection gondola and weather station, unmanned plane includes rack, weather station is fixed on the top of rack, frame lower has two carry bars, gondola bracket is fixed on carry bar, detection gondola is fixed on the horizontal mounting portion of gondola bracket by the first bolt.Two gondola brackets of the application are fixedly connected with shell by the first screw, this structure connection is reliable, the application is mounted on gondola is detected in the rack of unmanned plane, this form is for existing mode, it is very easy to use, detection gondola can be moved quickly by corresponding space by unmanned plane and detected.Detection gondola by the way that frame lower is arranged in can monitor Atmospheric components, and the weather station by being arranged on the rack portion can detect air data, and the meteorological detection unmanned plane of the application is realized vdiverse in function.
Description
Technical field
The utility model relates to detecting devices, and in particular to meteorological detection unmanned plane.
Background technique
It in the prior art, is usually all that will test equipment by balloon to take height in order to detect high aerial air parameter
In the air.This formal operations are difficult, and use is more inconvenient.
Utility model content
The utility model proposes a kind of meteorological detection unmanned plane in view of the above-mentioned problems, overcome deficiency.
The technical solution that the utility model is taken is as follows:
A kind of meteorological detection unmanned plane, including unmanned plane, detection gondola and weather station, the unmanned plane include rack,
The weather station is fixed on the top of rack, and the frame lower has two carry bars, and meteorological detection unmanned plane further includes the
One screw and two spaced gondola brackets, the gondola bracket are U-shaped structure, and gondola bracket includes horizontal mounting portion
And the bending part positioned at horizontal mounting portion both ends, two bending parts of gondola bracket are fixed with two carry bars respectively, described
Detect gondola include shell, the housing upper surface have threaded hole, first screw pass through horizontal mounting portion after with shell
Threaded hole connection, will detection gondola be fixed on gondola bracket, the biography for monitoring Atmospheric components is installed in the shell
Sensor.
Two gondola brackets are fixedly connected with shell by the first screw, and this structure connection is reliable, and the application will detect
Gondola is mounted in the rack of unmanned plane, and this form is very easy to use for existing mode, passes through unmanned plane
Detection gondola corresponding space can be moved quickly into detect.Detection gondola by the way that frame lower is arranged in can supervise
Atmospheric components are surveyed, the weather station by being arranged on the rack portion can detect air data, the meteorological detection unmanned plane of the application
That realizes is vdiverse in function.
In the utility model wherein an embodiment, the weather station further includes the test section for the side of being mounted on the base, inspection
Survey portion has multiple ventilation openings, is equipped with humidity sensor and baroceptor inside test section.
In the utility model wherein an embodiment, the test section bottom is equipped with blower, and the blower is located at humidity
The lower section of sensor and baroceptor, blower is for making outside air by entering test section after lowest level ventilation opening, logical
After crossing humidity sensor and baroceptor, it is discharged from other ventilation openings.
The humidity information that air can be detected by humidity sensor can detect air pressure letter by baroceptor
Breath.
In the utility model wherein an embodiment, wind speed wind direction sensor is installed above test section.Wind speed and direction
Sensor can measure the wind speed and direction information of air.
In the utility model wherein an embodiment, the sensor be carbon monoxide transducer, SO 2 sensor,
Any one or more of nitrogen dioxide sensor, ozone sensor, PM2.5 sensor or PM10 sensor.
In the utility model wherein an embodiment, one end of the bending part and the cooperation of carry bar has mounting hole, peace
Filling hole has opening, and opening both ends have extension, the mounting hole housing on corresponding carry bar, two bending parts it
Between be connected with the second screw, second screw makes mounting hole clamp carry bar for drawing close two extensions mutually.
This structure of bending part and carry bar can make extension sliding on carry bar so that unclamping the second bolt
It is dynamic, the position of detection gondola can be adjusted, so as to adjust position of centre of gravity of the detection gondola relative to unmanned plane, adjusting is arrived
Behind position, it can be fixed on carry bar by locking the second screw.
In the utility model wherein an embodiment, under horizontality, center of gravity, the center of gravity of weather station of the detection gondola
And the line of drone center of unmanned aerial vehicle is vertical line.
The beneficial effects of the utility model are: two gondola brackets are fixedly connected with shell by the first screw, this knot
Structure connection is reliable, and the application is mounted on gondola is detected in the rack of unmanned plane, this form for existing mode,
It is very easy to use, detection gondola can be moved quickly by corresponding space by unmanned plane and detected.Existed by setting
The detection gondola of frame lower can monitor Atmospheric components, and the weather station by being arranged on the rack portion can detect air number
According to the meteorological detection unmanned plane of the application is realized vdiverse in function.
Detailed description of the invention:
Fig. 1 is the structural schematic diagram of the utility model meteorological detection unmanned plane；
Fig. 2 is the schematic diagram after meteorological station base and frame top local cutting；
Fig. 3 is the schematic diagram detected after gondola and frame lower local cutting；
Fig. 4 is the partial schematic diagram after lower casing cutting；
Fig. 5 is the cross-sectional view of weather station；
Fig. 6 is the schematic diagram of pedestal and test section.
Each appended drawing reference in figure are as follows:
1, unmanned plane；2, rotor；3, support frame；4, weather station；5, gondola is detected；6, gondola bracket；7, rack；8, bottom
Seat；9, test section；10, adapter；11, wind speed wind direction sensor；12, unmanned plane shell；13, first through hole；14, second is logical
Hole；15, screw rod；16, nut；17, installation space；18, shell；19, upper casing；20, lower casing；21, plane is avoided；22, air inlet；
23, air outlet；24, carry bar；25, horizontal mounting portion；26, bending part；27, threaded hole；28, the first screw；29, mounting hole；
30, extension；31, the second screw；32, annular groove；33, breath light；34, fastener；35, undergauge section；36, blower；37, it protects
Blinds.
Specific embodiment:
Below with reference to each attached drawing, the utility model is described in detail.
As shown in Figure 1, a kind of meteorological detection unmanned plane, including unmanned plane 1 and the weather station being mounted on unmanned plane 14
With detection gondola 5, when practice, can only installation weather station 4 or only installation detection gondola 5, determine as needed.Nothing
Man-machine 1 includes rack 7 and multiple rotors 2, and 7 lower part of rack is also set up there are two support frame 3, and detection gondola 5 is arranged at two
Between support frame 3, detection gondola 5 is connect by two gondola brackets 6 with rack 7.
As shown in Fig. 2, 7 upper surface of rack is fixed with unmanned plane shell 12 in the present embodiment, the unmanned plane shell 12 has
There are multiple first through hole 13, the weather station 4 includes pedestal 8, and the pedestal 8 has second be aligned with corresponding first through hole 13
Through-hole 14, meteorological detection unmanned plane further include screw rod 15 and nut 16, and the pedestal 8 leans with unmanned plane shell 12, described
Nut 16 is arranged inside rack 7, after screw rod 15 sequentially passes through the second through-hole 14 and first through hole 13, with corresponding 16 spiral shell of nut
Line connection.
The application is for the structure at the top of existing unmanned plane, by increasing the length of screw rod 15, so that the pedestal of weather station 4
8 share screw rod 15 with unmanned plane shell 12, are finally reached while do not change or destroy unmanned plane structure, and reached fixed gas
As the purpose at station 4.The meteorological detection unmanned plane of the application, weather station 4 is reliably fixed on unmanned plane 1, and weather station 4 can be with
It flies with unmanned plane 1, detects the parameter of air.
As seen in figs, in the utility model wherein an embodiment, the weather station 4 further includes being mounted on pedestal 8
The test section 9 of top, test section 9 have multiple ventilation openings (being not shown in the figure, the flowing of wind can be seen by Fig. 6), test section 9
Inside is equipped with humidity sensor and baroceptor.
As shown in fig. 6,9 bottom of test section is equipped with blower 36, described in the utility model wherein an embodiment
Blower 36 is located at the lower section of humidity sensor and baroceptor, and blower 36 is for passing through outside air after lowest level ventilation opening
Into test section 9, after through humidity sensor and baroceptor, it is discharged from other ventilation openings.Pass through humidity sensor energy
The humidity information for detecting air can detect pressure information by baroceptor.
As shown in fig. 6, being equipped with protection blinds 37 at the ventilation opening in the utility model wherein an embodiment.It is logical
Crossing setting protection blinds 37 can effectively prevent chance water etc. to enter inside test section 9.
Shown in saying such as Fig. 2, in the utility model wherein an embodiment, there is installation space 17, institute inside the pedestal 8
Installation space 17 is stated for installing the control circuit (omit and be not drawn into figure) of weather station 4.
As shown in figures 2 and 5, in this present embodiment, the weather station 4 further include the test section 9 for being mounted on 8 top of pedestal,
The wind speed wind direction sensor 11 for being mounted on the adapter 10 on 9 top of test section, being mounted on 10 top of adapter, the wind speed and direction
Sensor 11 is located at the top of rotor 2.
When 1 flight of unmanned plane, rotor 2 is rotated, and the disturbance layer an of wind field, the weather station 4 of the application are had at the top of rotor 2
Make the height of wind speed wind direction sensor 11 be located at the top of rotor 2 by the way that adapter 10 is arranged, is more than disturbance layer, such rotor
2 would not have an impact the measurement of wind speed wind direction sensor 11.The application is led to by the way that weather station 4 to be mounted on unmanned plane 1
Crossing unmanned plane drives weather station 4 to move in the air, this operation format safe ready.
Wind speed wind direction sensor 11 can measure the wind speed and direction information of air, the wind speed wind direction sensor 11 of the application
Using the characteristic of ultrasonic sensor, in conjunction with its feature small in size, by ultrasonic wind speed sensor integration to weather station 4,
To reach the miniaturization of weather station 4, the purpose to simplify the structure.Due to not having mechanical component, it is not present " machinery inertial ", wind
Fast wind transducer 11 can capture instantaneous wind speed variation, can not only measure conventional wind speed (mean wind speed), can also measure any
Wind speed component on direction can especially measure the dither ingredient in wind speed.
In the utility model wherein an embodiment, the adapter 10 is easy broken piece, for breaking when unmanned plane 1 falls machine
It splits, protects wind speed wind direction sensor 11.The ultrasonic sensor lossless using one kind of wind speed wind direction sensor 11, it is more valuable,
Under preventing unmanned plane from turning on one's side or the broken situation of blade, sensor is broken, knot can reduce by the adapter 10 for being arranged easily broken
Structure intensity reaches under special circumstances, and adapter 10 is broken first, to be used to protect wind speed wind direction sensor 11.
As shown in figure 5, the adapter 10 has undergauge section 35 in the utility model wherein an embodiment.Undergauge section
Intensity is low at 35, and the wind speed wind direction sensor 11 when falling machine when weather station 4 is impacted, and adapter 10 can be from undergauge section 35
Fracture is to effective protection wind speed wind direction sensor 11.In the utility model wherein an embodiment, the material of the adapter 10
Matter is plastics.
As shown in figure 5, in the utility model wherein an embodiment, the lower end of the adapter 10 by fastener 34 with
Test section 9 connects, and the upper end of the adapter 10 is connect by fastener 34 with wind speed wind direction sensor 11.
As shown in figs. 1 and 3,7 lower part of rack has two carry bars 24, and meteorological detection unmanned plane further includes the first screw 28
And two spaced gondola brackets 6, the gondola bracket 6 are U-shaped structure, gondola bracket 6 includes horizontal mounting portion 25
And the bending part 26 positioned at 25 both ends of horizontal mounting portion, two bending parts 26 of gondola bracket 6 respectively with two carry bars 24
Fixed, the detection gondola 5 includes shell 18 (shell 18 includes upper casing 19 and lower casing 20), and 18 upper surface of shell has spiral shell
Pit 27, first screw 28 are connect after passing through horizontal mounting portion 25 with the threaded hole 27 of shell 18, and detection gondola 5 is fixed
On gondola bracket 6, the sensor (omit and be not drawn into figure) for monitoring Atmospheric components is installed in the shell 18.
Two gondola brackets 6 are fixedly connected with shell 18 by the first screw 28, and this structure connection is reliable, and the application will
Detection gondola 5 is mounted in the rack 7 of unmanned plane 1, and this form is very easy to use for existing mode, is led to
Corresponding space can be moved quickly into detection gondola 5 and detect by crossing unmanned plane 1.
When practice, the sensor in shell 18 can be carbon monoxide transducer, SO 2 sensor, titanium dioxide
Any one or more of nitrogen sensor, ozone sensor, PM2.5 sensor or PM10 sensor.
As shown in figure 3, being equipped with two bent support frames 3 in the rack 7, the shell 18 is oblate knot
Structure, detection gondola 5 and 3 respective side of support frame have evacuation plane 21.Evacuation plane 21 can effectively prevent detection gondola 5 and branch
Interfere between support 3.
As shown in figure 3, in the utility model wherein an embodiment, one end of the bending part 26 and the cooperation of carry bar 24
With mounting hole 29, mounting hole 29 has opening (not marking in figure), and opening both ends have extension 30, the mounting hole 29
Housing is connected with the second screw 31, second screw 31 is for making on corresponding carry bar 24 between two bending parts 26
Two extensions 30 are mutually drawn close, and mounting hole 29 is made to clamp carry bar 24.This structure of bending part 26 and carry bar 24, makes
The second bolt, which must be unclamped, can be such that extension 30 slides on carry bar 24, can adjust the position of detection gondola 5, thus
Position of centre of gravity of the adjustable detection gondola 5 relative to unmanned plane 1, after adjusting in place, by locking the second screw 31
It is fixed on carry bar 24.
As shown in Figures 3 and 4,18 lower part of shell has an air inlet 22, and the top of shell 18 has an air outlet 23, in shell 18
It is also equipped with forced ventilation device (being not drawn into figure, forced ventilation device can be exhaust fan 36), for keeping extraneous gas logical
It crosses air inlet 22 to enter in shell 18, and is discharged from air outlet 23；The lower surface of the shell 18 is equipped with breath light 33.
As shown in figure 4, the lower surface of shell 18 has annular groove 32, described in the utility model wherein an embodiment
Breath light 33 is annular, is inlaid in annular groove 32.
It can achieve the purpose that rapid survey by the way that forced ventilation device is arranged；Shell 18 draws up under using and send mode, with
Wind field flow direction is parallel after unmanned plane starting, while guaranteeing measurement accuracy, also avoids interfering with each other for wind field；Pass through
Breath light 33 is installed in 18 lower part of shell, after unmanned plane starting, breath light 33 is opened therewith, and operator is facilitated to capture rapidly
Unmanned plane is also set to have the guarantee of night flying while improving safety to the position of high-altitude flight unmanned plane.
In order to guarantee the gravity balance of entire meteorological detection unmanned plane, it is preferred that under horizontality, the detection gondola 5
Center of gravity, the center of gravity of weather station 4 and drone center of unmanned aerial vehicle on a vertical line.
The above is only the preferred embodiment of the present invention, not thereby limits the patent protection of the utility model
Range, it is all with equivalent structure transformation made by the utility model specification and accompanying drawing content, directly or indirectly it is used in it
His relevant technical field similarly includes within the protection scope of the present utility model.
Claims (7)
1. a kind of meteorological detection unmanned plane, which is characterized in that including unmanned plane, detection gondola and weather station, the unmanned plane
Including rack, the weather station is fixed on the top of rack, and the frame lower has two carry bars, meteorological detection unmanned plane
It further include the first screw and two spaced gondola brackets, the gondola bracket is U-shaped structure, and gondola bracket includes water
Flat mounting portion and bending part positioned at horizontal mounting portion both ends, two bending parts of gondola bracket are solid with two carry bars respectively
Fixed, the detection gondola includes shell, after there is the housing upper surface threaded hole, first screw to pass through horizontal mounting portion
Connect with the threaded hole of shell, will detection gondola be fixed on gondola bracket, be equipped in the shell for monitor atmosphere at
The sensor divided.
2. meteorological detection unmanned plane as described in claim 1, which is characterized in that the weather station further includes being mounted on the base
The test section in portion, test section have multiple ventilation openings, are equipped with humidity sensor and baroceptor inside test section.
3. meteorological detection unmanned plane as claimed in claim 2, which is characterized in that the test section bottom is equipped with blower, institute
The lower section that blower is located at humidity sensor and baroceptor is stated, blower is for keeping outside air laggard by lowest level ventilation opening
Enter test section, after through humidity sensor and baroceptor, is discharged from other ventilation openings.
4. meteorological detection unmanned plane as claimed in claim 2, which is characterized in that be equipped with wind speed and direction biography above test section
Sensor.
5. meteorological detection unmanned plane as described in claim 1, which is characterized in that the sensor be carbon monoxide transducer,
SO 2 sensor, nitrogen dioxide sensor, ozone sensor, PM2.5 sensor or PM10 sensor any one or
It is a variety of.
6. meteorological detection unmanned plane as described in claim 1, which is characterized in that one end of the bending part and the cooperation of carry bar
With mounting hole, mounting hole has opening, and opening both ends have extension, and the mounting hole housing is in corresponding carry bar
On, the second screw is connected between two bending parts, second screw makes to install for drawing close two extensions mutually
Hole clamps carry bar.
7. meteorological detection unmanned plane as described in claim 1, which is characterized in that under horizontality, the weight of the detection gondola
The line of the heart, the center of gravity of weather station and drone center of unmanned aerial vehicle is vertical line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821622475.4U CN208915444U (en) | 2018-09-30 | 2018-09-30 | Meteorological detection unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821622475.4U CN208915444U (en) | 2018-09-30 | 2018-09-30 | Meteorological detection unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208915444U true CN208915444U (en) | 2019-05-31 |
Family
ID=66708278
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821622475.4U Active CN208915444U (en) | 2018-09-30 | 2018-09-30 | Meteorological detection unmanned plane |
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| CN (1) | CN208915444U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654538A (en) * | 2019-08-30 | 2020-01-07 | 南京精微迅智能科技有限公司 | Weather detection unmanned aerial vehicle |
| CN113830435A (en) * | 2021-10-19 | 2021-12-24 | 山东交通学院 | Transport container suitable for unmanned aerial vehicle and use method thereof |
-
2018
- 2018-09-30 CN CN201821622475.4U patent/CN208915444U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654538A (en) * | 2019-08-30 | 2020-01-07 | 南京精微迅智能科技有限公司 | Weather detection unmanned aerial vehicle |
| CN110654538B (en) * | 2019-08-30 | 2021-02-12 | 南京精微迅智能科技有限公司 | Weather detection unmanned aerial vehicle |
| CN113830435A (en) * | 2021-10-19 | 2021-12-24 | 山东交通学院 | Transport container suitable for unmanned aerial vehicle and use method thereof |
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