CN207502750U - A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform - Google Patents
A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform Download PDFInfo
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- CN207502750U CN207502750U CN201721650896.3U CN201721650896U CN207502750U CN 207502750 U CN207502750 U CN 207502750U CN 201721650896 U CN201721650896 U CN 201721650896U CN 207502750 U CN207502750 U CN 207502750U
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- radome fairing
- meteorologic parameter
- connecting rod
- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform, including flying body, upper radome fairing, lower radome fairing, the flying body quadrangle is provided with supporting rod, motor is provided on supporting rod, propeller is provided on motor, propeller periphery is provided with air guide ring, lithium battery is provided on air guide ring, undercarriage is provided with outside air guide ring, flash lamp is provided on undercarriage, undercarriage is arranged with beam, and connecting rod is provided among flying body, flight controller is provided with by connecting rod.The air-flow generated when instrument and unmanned plane during flying that the utility model is acquired meteorologic parameter using upper radome fairing and lower radome fairing separates, avoid interference of the air-flow to gathered data, channel is opened up at center by the smooth discharge of high-altitude condensate simultaneously, avoid the instrument short circuit that meteorologic parameter acquires, its is easy to operate, it can realize the quick obtaining of the typical meteorologicals element such as temperature, humidity, pressure, greatly improve the accuracy of region meteorologic parameter gathered data.
Description
Technical field
The utility model is related to meteorological fields, and in particular to a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform.
Background technology
With the development of the technologies such as meteorologic survey sensor, unmanned plane manufacture, flight control and data processing, unmanned plane gas
It is gradually ripe simultaneously to move towards to apply as Detection Techniques obtain significant progress.This big region, long-time, continuous meteorological detection side
Method is visited in Spacecraft Launch and return, important weapon experiment, battlefield meteorologic survey, bad weather watch, cyclone low coverage environment
Surveying has unique effect and advantage in the applications such as monitoring.
But in the prior art, the instrument generally directly by meteorologic parameter acquisition is mounted on unmanned plane, causes unmanned plane
Interference of the air-flow generated during flight to gathered data reduces the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains.
Utility model content
The purpose of this utility model is that solve the above-mentioned problems and provides a kind of meteorology based on unmanned aerial vehicle platform
Parameter obtaining device.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform, including flying body, upper radome fairing, lower radome fairing, institute
It states flying body quadrangle and is provided with supporting rod, motor is provided on the supporting rod, propeller, institute are provided on the motor
It states propeller periphery and is provided with air guide ring, lithium battery is provided on the air guide ring, is provided with undercarriage outside the air guide ring, institute
It states and flash lamp is provided on undercarriage, the undercarriage is arranged with beam, and connecting rod, institute are provided among the flying body
It states and flight controller is provided with by connecting rod, cradle is provided with before the flight controller, is provided among the connecting rod
Sluice, the connecting rod top are provided with the upper radome fairing, reflecting strips, the upper rectification are provided with outside the upper radome fairing
Barometer is provided in cover, thermometer is provided with by the barometer, hygrometer, the connecting rod are provided with by the thermometer
Bottom is provided with the lower radome fairing, and wireless transceiver is provided in the lower radome fairing, is provided with by the wireless transceiver
Data-analyzing machine.
In above structure, start the flight controller, the flight controller starts the motor, the motor
The propeller rotation forces air-flow is driven to pass downwardly through the air guide ring and generates lift, the flying body rises, and air-flow passes through
The upper radome fairing and the lower cowling surface flowing, do not influence the upper radome fairing and the lower radome fairing inner air,
After the wireless transceiver receives meteorologic parameter acquisition instructions, the barometer, the thermometer and the hygrometer will acquire
Meteorologic parameter send the data-analyzing machine to, the data-analyzing machine will pass through the wireless receiving and dispatching after Data Analysis Services
Device is spread out of, and when rising up into high-altitude, temperature reduces, and when there is condensation water in radome fairing on described, condensation water is along the sluice
It flows into the lower radome fairing and excludes.
In order to further improve the accuracy that meteorologic parameter based on unmanned aerial vehicle platform obtains, the upper radome fairing and described
Lower radome fairing is spherical in semicircle, and the upper radome fairing and the lower radome fairing are threadedly coupled respectively with the connecting rod use.
In order to further improve the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains, the connecting rod passes through described
Flying body, the connecting rod are connect with the flying body using hidden discount.
In order to further improve the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains, the supporting rod is welded on institute
It states on flying body, the motor is bolted with the supporting rod use, and the motor uses flat key with the propeller
Connection.
In order to further improve the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains, the lithium battery is led with described
Vane use snaps connection, and the air guide ring is in circular ring shape.
In order to further improve the accuracy that meteorologic parameter based on unmanned aerial vehicle platform obtains, the flash lamp and described subtract
Shake pad is respectively adhered on the undercarriage, and the reflecting strips are pasted onto the upper cowling surface.
In order to further improve the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains, the data-analyzing machine difference
It is electrically connected with the wireless transceiver, the thermometer, the barometer and the hygrometer use.
Advantageous effect is:The instrument and nothing that the utility model is acquired meteorologic parameter using upper radome fairing and lower radome fairing
The air-flow generated during man-machine flight separates, and avoids interference of the air-flow to gathered data, while open up channel by high-altitude at center
The smooth discharge of condensate, the instrument short circuit that meteorologic parameter is avoided to acquire, improves what the meteorologic parameter based on unmanned aerial vehicle platform obtained
Accuracy.
Description of the drawings
Fig. 1 is a kind of structure diagram of meteorologic parameter acquisition device based on unmanned aerial vehicle platform described in the utility model;
Fig. 2 is a kind of sluice signal of meteorologic parameter acquisition device based on unmanned aerial vehicle platform described in the utility model
Figure;
Fig. 3 is that a kind of upper radome fairing of meteorologic parameter acquisition device based on unmanned aerial vehicle platform described in the utility model is overlooked
Figure.
The reference numerals are as follows:
1st, flying body;2nd, motor;3rd, propeller;4th, undercarriage;5th, flash lamp;6th, beam;7th, lower radome fairing;8th, even
Extension bar;9th, air guide ring;10th, lithium battery;11st, flight controller;12nd, upper radome fairing;13rd, reflecting strips;14th, sluice;15th, it supports
Bar;16th, barometer;17th, wireless transceiver;18th, data-analyzing machine;19th, thermometer;20th, hygrometer;21st, cradle.
Specific embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings:
As shown in Figure 1-Figure 3, a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform, including flying body 1, upper rectification
Cover 12, lower radome fairing 7,1 four jiaos of flying body are provided with supporting rod 15, support motor 2, motor 2 is provided on supporting rod 15,
Driving propeller 3 rotates, and propeller 3 is provided on motor 2, and air-flow is pushed to pass downwardly through air guide ring 9 and promotes flying body 1, spiral shell
3 periphery of rotation paddle is provided with air guide ring 9, and dredging flow passes through, and lithium battery 10 is provided on air guide ring 9, stores electric power needed for flight,
Undercarriage 4 is provided with outside air guide ring 9, facilitates 1 landing of flying body, flash lamp 5 is provided on undercarriage 4, warns unmanned plane gabarit,
People are reminded note that undercarriage 4 is arranged with beam 6, vibrations during 1 landing of flying body is reduced, is provided among flying body 1
Connecting rod 8, radome fairing 12 and lower radome fairing 7 in connection are provided with flight controller 11 by connecting rod 8, control unmanned plane during flying,
Cradle 21 is provided with before flight controller 11, convenient for charging in the case where not dismantling lithium battery 10, is set among connecting rod 8
There are sluice 14, the channel that high-altitude condensation water flows through, 8 top of connecting rod is provided with radome fairing 12, reduces air-flow to measurement
Interference, upper radome fairing 12 are provided with reflecting strips 13 outside, remind people note that being provided with barometer 16 in upper radome fairing 12, acquire
Meteorological pneumatic parameter is provided with thermometer 19 by barometer 16, acquires meteorological temperature parameter, hygrometer is provided with by thermometer 19
20, meteorological humidity parameter is acquired, 8 bottom of connecting rod is provided with lower radome fairing 7, prevents air-flow from interfering upper rectification by sluice 14
Inside cover 12, it is provided with wireless transceiver 17 in lower radome fairing 7, transceiving data is provided with data analysis by wireless transceiver 17
Device 18 analyzes and processes the meteorologic parameter of acquisition.
In above structure, start flight controller 11, flight controller 11 starts motor 2, and motor 2 drives propeller
3 rotation forces air-flows pass downwardly through air guide ring 9 and generate lift, and flying body 1 rises, and air-flow passes through upper radome fairing 12 and lower radome fairing
7 surface flows, do not influence radome fairing 12 and lower 7 inner air of radome fairing, and wireless transceiver 17 receives meteorologic parameter acquisition and refers to
After order, barometer 16, thermometer 19 and hygrometer 20 send the meteorologic parameter of acquisition to data-analyzing machine 18, data-analyzing machine
18 will be spread out of after Data Analysis Services by wireless transceiver 17, and when rising up into high-altitude, temperature reduces, and occurs in upper radome fairing 12
During condensation water, condensation water flows into lower radome fairing 7 along sluice 14 and excludes.
In order to further improve the accuracy that the meteorologic parameter based on unmanned aerial vehicle platform obtains, upper radome fairing 12 and lower rectification
Cover 7 is spherical in semicircle, ensures that airflow smooth passes through, upper radome fairing 12 and lower radome fairing 7 are connected respectively with connecting rod 8 using screw thread
It connects, is easily installed, connecting rod 8 passes through flying body 1, ensures to connect up and down, connecting rod 8 is connect with flying body 1 using hidden discount, is reduced
Influence to outer gas stream, supporting rod 15 is welded on flying body 1, durable, and motor 2 is connected with supporting rod 15 using bolt
It connects, replacement easy to disassemble, motor 2 is connect with propeller 3 using flat key, effectively transmits rotary force, lithium battery 10 and air guide ring 9
Using snapping connection, easy to disassemble, air guide ring 9 is in circular ring shape, protects propeller 3, flash lamp 5 and beam 6 are respectively adhered on
On undercarriage 4, firm not easy to fall off, reflecting strips 13 are pasted onto 12 surface of radome fairing, it is not easy to it comes off, data-analyzing machine 18
It is electrically connected respectively with wireless transceiver 17, thermometer 19, barometer 16 and 20 use of hygrometer, convenient for data transmission.
The basic principle, main feature and advantage of the utility model has been shown and described above.The technical staff of the industry
It should be appreciated that the present utility model is not limited to the above embodiments, the above embodiments and description only describe this
The principle of utility model, on the premise of not departing from the spirit and scope of the utility model, the utility model also has various change
And improvement, these various changes and improvements fall within the scope of the claimed invention.The utility model requires protection scope
It is defined by appending claims and equivalents.
Claims (7)
1. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform, it is characterised in that:Including flying body (1), upper radome fairing
(12), lower radome fairing (7), flying body (1) quadrangle are provided with supporting rod (15), are provided on the supporting rod (15) electronic
Machine (2) is provided with propeller (3) on the motor (2), and propeller (3) periphery is provided with air guide ring (9), described to lead
Lithium battery (10) is provided on vane (9), undercarriage (4) is provided with outside the air guide ring (9), is set on the undercarriage (4)
There is flash lamp (5), the undercarriage (4) is arranged with beam (6), connecting rod (8) is provided among the flying body (1),
Flight controller (11) is provided with by the connecting rod (8), cradle (21) is provided with before the flight controller (11), it is described
Sluice (14) is provided among connecting rod (8), is provided with the upper radome fairing (12) at the top of the connecting rod (8), it is described on
Reflecting strips (13) are provided with outside radome fairing (12), barometer (16), the barometer are provided in the upper radome fairing (12)
(16) it is other to be provided with thermometer (19), hygrometer (20), connecting rod (8) the bottom setting are provided with by the thermometer (19)
There is the lower radome fairing (7), wireless transceiver (17) is provided in the lower radome fairing (7), the wireless transceiver (17) is other
It is provided with data-analyzing machine (18).
2. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Upper radome fairing (12) and the lower radome fairing (7) are in semicircle spherical shape, and the upper radome fairing (12) and the lower radome fairing (7) are respectively
It is threadedly coupled with the connecting rod (8) use.
3. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Connecting rod (8) is connect across the flying body (1), the connecting rod (8) with the flying body (1) using hidden discount.
4. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Supporting rod (15) is welded on the flying body (1), and the motor (2) is bolted with the supporting rod (15) use, institute
Motor (2) is stated to connect using flat key with the propeller (3).
5. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Lithium battery (10) is snapped connection with the air guide ring (9) use, and the air guide ring (9) is in circular ring shape.
6. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Flash lamp (5) and the beam (6) are respectively adhered on the undercarriage (4), and the reflecting strips (13) are pasted onto on described
Radome fairing (12) surface.
7. a kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform according to claim 1, it is characterised in that:It is described
Data-analyzing machine (18) respectively with the wireless transceiver (17), the thermometer (19), the barometer (16) and described wet
Degree meter (20) uses electrical connection.
Priority Applications (1)
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CN201721650896.3U CN207502750U (en) | 2017-12-01 | 2017-12-01 | A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform |
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CN201721650896.3U CN207502750U (en) | 2017-12-01 | 2017-12-01 | A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform |
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CN207502750U true CN207502750U (en) | 2018-06-15 |
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CN201721650896.3U Expired - Fee Related CN207502750U (en) | 2017-12-01 | 2017-12-01 | A kind of meteorologic parameter acquisition device based on unmanned aerial vehicle platform |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110673228A (en) * | 2019-08-30 | 2020-01-10 | 北京航空航天大学 | Formula of throwing sonde under imitative dandelion structure |
CN111498134A (en) * | 2020-04-29 | 2020-08-07 | 贵州电网有限责任公司 | Self-adaptive unmanned aerial vehicle take-off and landing platform |
-
2017
- 2017-12-01 CN CN201721650896.3U patent/CN207502750U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110673228A (en) * | 2019-08-30 | 2020-01-10 | 北京航空航天大学 | Formula of throwing sonde under imitative dandelion structure |
CN111498134A (en) * | 2020-04-29 | 2020-08-07 | 贵州电网有限责任公司 | Self-adaptive unmanned aerial vehicle take-off and landing platform |
CN111498134B (en) * | 2020-04-29 | 2023-09-01 | 贵州电网有限责任公司 | Self-adaptive unmanned aerial vehicle take-off and landing platform |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180615 Termination date: 20181201 |
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CF01 | Termination of patent right due to non-payment of annual fee |