CN205581333U - Machine carries weather station device suitable for unmanned aerial vehicle - Google Patents
Machine carries weather station device suitable for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205581333U CN205581333U CN201620334946.6U CN201620334946U CN205581333U CN 205581333 U CN205581333 U CN 205581333U CN 201620334946 U CN201620334946 U CN 201620334946U CN 205581333 U CN205581333 U CN 205581333U
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- CN
- China
- Prior art keywords
- weather station
- unmanned aerial
- aerial vehicle
- airbome
- unmanned plane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Abstract
The utility model discloses a machine carries weather station device suitable for unmanned aerial vehicle, unmanned aerial vehicle are many rotors of cavity formula unmanned aerial vehicle, and the device includes weather station shell body, weather station base, power module, transmission module, control module, and the weather station shell body is fixed in unmanned aerial vehicle cavity position, and its inner wall both sides are equipped with the guide rail, gear rotating band carry -over bar in the transmission module slides on the guide rail, weather station base both ends respectively with rack fixed connection, upper and lower both sides are equipped with the meteorological monitoring sensor, control module returns the data of gathering to ground through wireless transmission module in real time. During the operation, unmanned aerial vehicle hovers, and the machine carries weather station device adjustment rack and stops the different positions on the guide rail, finally obtains the not meteorological parameter of co -altitude of unmanned aerial vehicle fuselage vertical space through the meteorological monitoring sensor. The utility model discloses the wind field that can reduce unmanned aerial vehicle flight formation has monitoring precision height, characteristics easy and simple to handle nimble to the influence that the weather station recorded data.
Description
Technical field
This utility model relates to weather monitoring research field, particularly to a kind of airborne gas being applicable to unmanned plane
As station arrangement.
Background technology
Meteorological have important impact for human lives and agricultural production, and weather station is monitoring meteorological condition
Main device, nowadays weather station mostly fixes on the ground, can only monitor some meteorologies of Near Ground
Data, it is impossible to monitor the meteorological data of high empty position.And though manned fixed wing airplane can gather aerological
Data, but have that cost is high, acquisition time is short, trajectory planning is difficult, gather data class sky few, severe
The shortcoming such as under gas crew's danger is higher.
In recent years, unmanned plane just gets growing concern for because of the advantage of its convenient and efficient.Unmanned plane is permissible
Carrying kinds of platform and carry out various different work, using unmanned plane to carry out weather monitoring is just becoming a research heat
Point.But in actual applications, being affected by unmanned plane self rotor wind field, monitoring result is the most not fully up to expectations.
For overcoming disadvantages mentioned above, design a kind of airbome weather station arrangement being applicable to unmanned plane and there is important application valency
Value.
Utility model content
The deficiency that this utility model exists to overcome currently available technology, it is provided that a kind of simple in construction, conjunction
Reason, can effectively monitor the airbome weather station arrangement being applicable to unmanned plane of Upper Air Weather Condition.
The purpose of this utility model is realized by following technical scheme: a kind of airborne gas being applicable to unmanned plane
As station arrangement, described unmanned plane is the many rotor wing unmanned aerial vehicles of hollow type, and described airbome weather station arrangement includes meteorology
Stand shell body, weather station pedestal, power plant module, transmission module, control module, described weather station shell body
Being fixed on unmanned plane hollow position, its inwall both sides are provided with guide rail；Described transmission module includes gear, tooth bar,
Gear is fixed on weather station shell body inwall and is connected with power plant module, and every guide rail is provided with a slide block,
Described tooth bar is fixed on slide block, and every toothed rack engages with gear respectively, rotarily drives tooth bar by gear
At described slide on rails；Described weather station base interior hollow, is used for placing control module, weather station base
Seat two ends are fixing with the tooth bar on two side rails respectively to be connected, and the both sides up and down of weather station pedestal are provided with meteorological prison
Survey sensor；Described control module includes data acquisition unit, processor and wireless transport module, data acquisition
Acquisition means is connected with weather monitoring sensor, and the data of collection are sent to processor, and then processor is by number
According to being returned to ground in real time by wireless transport module.This utility model, by arranging transmission module, can be adjusted
Each weather monitoring sensor and the distance of unmanned plane rotor on whole weather station pedestal, thus reduce unmanned plane and fly
The wind field that row is formed, for the impact of weather station data measured, has monitoring accuracy high, convenient and flexible operation
Feature.
Preferably, described power plant module is the steering wheel being arranged on weather station shell body outer wall, and steering wheel has some
Individual.
Preferably, the both sides up and down of described weather station pedestal are respectively provided with a shutter, weather monitoring sensor
Built-in wherein.Here weather monitoring sensor includes temperature, air humidity, air pressure, gas sensor etc., logical
Cross arrange shutter can play protection sensor effect.
Preferably, described tooth bar two ends are without flute profile.Therefore do not produce with gear and engage, sliding up and down
Time can form self-locking, anti-locking apparatus slips.
Preferably, pedestal two ends, described weather station are connected with tooth bar by two horizontal support rod members.
Further, described support rod member uses carbon fiber pipe.
Preferably, the both sides up and down of described weather station pedestal are additionally provided with several sensor die massing mounting brackets,
Support is provided with the position for installation of modular sensor.Thus according to different demands, different moulds can be installed
Massing sensor.
Further, the both sides up and down of described weather station pedestal are additionally provided with several overhanging stocks, with sensing
The mating holes of device Modularized mounting frame middle position coordinates, and is fixedly connected by pin；Described outer elongation
Masthead end is provided with three-dimensional air velocity transducer, wind transducer.
Preferably, the planform of described unmanned plane hollow be square, circular, oval in any one,
Hollow position bottom is provided with fixed mount, and described weather station housing is fixed on this fixed mount, and unmanned plane includes machine
Body, and several rotor motors, rotor and support arm, described rotor is installed in the rotating shaft of rotor motor,
Described rotor motor is installed on one end of support arm, and the other end of described support arm is fixed on fuselage；Described
Rotor motor is symmetrical along the diagonal of fuselage.The quantity of rotor motor, rotor and support arm in unmanned plane
Can according to practical situation need determine, such as 6 or 8 etc..
This utility model compared with prior art, has the advantage that and beneficial effect:
1, this utility model simple in construction, uses that unmanned plane scheduling is convenient, low cost, can with vertical survey,
Can tackle in time for burst monitoring task, not affected by topography and geomorphology, the timely wireless backhaul of measurement data,
There is the highest real-time.
2, this utility model separate men from machines, unmanned plane can be relatively hazardous, with serious pollution, poisonous and hazardous
Environment works, it is not necessary to the loss of crew, and can be easier to obtain the gas that other modes are difficult to obtain
Image data.
3, this utility model monitoring results platform carries flexibly, can carry different instruments according to different demands and set
Standby, and job platform has recuperability and reusing.
4, unmanned plane hovering during this utility model monitoring results, can effectively record unmanned aerial vehicle body vertical space
The meteorologic parameter of differing heights；Can also be effectively isolated, by the rising of device, the wind field that aircraft is formed simultaneously
For the impact of weather station data measured, there is monitoring accuracy high, the feature of convenient and flexible operation.
Accompanying drawing explanation
Fig. 1 is the structural representation that airbome weather station arrangement is in original state before operation.
Fig. 2 is work opportunity carrier gas as station arrangement extends the structural representation below unmanned plane.
Fig. 3 is work opportunity carrier gas as station arrangement extends the structural representation above unmanned plane.
The structural representation of airbome weather station arrangement described in the present embodiment when Fig. 4 is not include unmanned plane.
Detailed description of the invention
Below in conjunction with embodiment and accompanying drawing, this utility model is described in further detail, but this utility model
Embodiment be not limited to this.
A kind of airbome weather station arrangement being applicable to unmanned plane as shown in Figure 1 to Figure 3, described unmanned plane is
The many rotor wing unmanned aerial vehicles of hollow type, described airbome weather station arrangement includes weather station shell body 21, weather station pedestal
24, power plant module, transmission module, control module, shutter 25, sensor die massing mounting bracket 26,
Modular sensor 261, overhanging stock 27 and fixed mount.Weather station shell body 21 is installed on by fixed mount
Unmanned plane hollow part.Described weather station pedestal 24 is positioned in the middle part of airbome weather station arrangement, with weather station shell
Body 21 inwall is connected.Described shutter 25, sensor die massing mounting bracket 26 are mounted on weather station
The both sides up and down of pedestal 24, described overhanging stock 27 is positioned at weather station device upper and lower two ends outermost.Described
Control module includes data acquisition unit 231, processor 232 and wireless transport module, data acquisition unit
231 are connected with weather monitoring sensor, and the data of collection are sent to processor 232, then processor 232
Data are returned to ground in real time by wireless transport module.
The planform of described unmanned plane hollow can be square, circular, oval in any one.This
Utility model preferred square while hollow position bottom have fixed mount.Described unmanned plane includes 11,4, fuselage
12,4 rotors 13 of rotor motor and 4 support arms 14, described rotor 13 is installed on rotor motor 12
Rotating shaft, described rotor motor 12 is installed on one end of support arm 14, and the other end of described support arm 14 is fixed
In fuselage 11.Described rotor motor 12 is symmetrical along the diagonal of fuselage 11.Rotor motor in aircraft
12, the quantity of rotor 13 and support arm 14 can according to practical situation need determine, such as 6 or 8 etc..
Described airbome weather station shell body 21, shape is approximately " mouth " font, housing exterior walls is provided with dynamic
Power module, inwall both sides are provided with guide rail.Described power plant module is the rudder being arranged on weather station shell body outer wall
Machine 2211, steering wheel 2211 quantity is 4.This utility model can use remote control or the controlling party automatically controlled
Formula controls rotor motor 12 and the action of steering wheel 2211.
Transmission module includes tooth bar 2222 and gear 2221, and gear 2221 quantity is 4, is fixed on meteorology
Standing shell body inwall and being connected with power plant module, every guide rail is provided with a slide block, described tooth bar 2222 number
Amount is 2, is fixed on slide block, and respectively with two the gear engagements of every toothed rack, by the rotation of gear 2221
Turn band carry-over bar 2222 to slide on described guide rail 2223.Described guide rail 2223 track uses oil lubrication.Tooth
Bar 2222 two ends, without flute profile, do not produce with gear 2221 and engage, and can form self-locking, and anti-locking apparatus slips.
Described weather station pedestal 24 inner hollow, is used for placing control module, and weather station pedestal 24 two ends lead to
Cross two horizontal support rod members 241 to be connected with tooth bar, support rod member 241 and use the carbon that intensity is higher fine
Dimension pipe.The both sides up and down of weather station pedestal 24 are provided with shutter 25, sensor die massing mounting bracket 26.
Described shutter 25 is cylindrical, and quantity is 2, in weather station pedestal 24 layout symmetrical above and below, built-in
Temperature, air humidity, air pressure, gas sensor etc..Described sensor die massing mounting bracket 26, quantity is 2
Individual, it is provided with 8 installation sites, according to different demands, different modular sensors 261 can be installed and install,
Support middle position has mating holes to coordinate with overhanging stock 27 hole axle simultaneously.
Described overhanging stock 27 is cylindrical bar, and length can regulate according to demand, installs with sensor die massing and props up
The mating holes of frame 26 middle position coordinates, and is fixedly connected by pin 273, and overhanging stock 27 top is pacified
Equipped with three-dimensional air velocity transducer 271, wind transducer 272.
The using method of device described in the present embodiment, comprises the following steps:
Respective sensor is installed on airbome weather station arrangement by a, the actual measuring task of foundation, the outer elongation of regulation
Pole length；
B, initial time airbome weather station arrangement shrink in unmanned plane hollow part, treat that unmanned plane flies to operating area
After, it is ensured that aircraft is steady, hovering；
C, power plant module and transmission module are started working, and weather station pedestal moves to tooth bar pole downwards along guide rail
Limit for length's degree；
D, each sensor are started working, and data acquisition unit sends the meteorological data of collection to processor subsequently,
Information is returned to ground by wireless transport module by processor in real time；
E, weather station pedestal start slowly to be moved upward along guide rail, stop after moving a certain distance, and repeat step
Rapid d；
F, repetition step e, until weather station pedestal moves to the limiting length of top tooth bar along guide rail；
G, complete above-mentioned steps after, unmanned plane terminates hovering, and other flown to operating area meteorological gather positions
Put repetition step b to step f；
H, complete all meteorological data collection operations after, airbome weather station arrangement is regained unmanned plane hollow again
Position, unmanned plane makes a return voyage.
Above-described embodiment is this utility model preferably embodiment, but embodiment of the present utility model is not
Being restricted to the described embodiments, any of other is made without departing from spirit of the present utility model and principle are lower
Change, modify, substitute, combine, simplify, all should be the substitute mode of equivalence, be included in this practicality
Within novel protection domain.
Claims (9)
1. being applicable to an airbome weather station arrangement for unmanned plane, described unmanned plane is that the many rotors of hollow type are unmanned
Machine, it is characterised in that described airbome weather station arrangement includes weather station shell body, weather station pedestal, power
Module, transmission module, control module, described weather station shell body is fixed on unmanned plane hollow position, in it
Wall both sides are provided with guide rail；Described transmission module includes gear, tooth bar, and gear is fixed in weather station shell body
Wall and being connected with power plant module, every guide rail is provided with a slide block, and described tooth bar is fixed on slide block, often
Toothed rack engages with gear respectively, rotarily drives tooth bar at described slide on rails by gear；Described gas
As station base interior hollow, be used for placing control module, pedestal two ends, weather station respectively with on two side rails
Tooth bar is fixing to be connected, and the both sides up and down of weather station pedestal are provided with weather monitoring sensor；Described control module bag
Include data acquisition unit, processor and wireless transport module, data acquisition unit and weather monitoring sensor phase
Even, the data of collection being sent to processor, then data are returned in real time by processor by wireless transport module
Return to ground.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described weather station pedestal
Both sides up and down be respectively provided with a shutter, weather monitoring sensor is built-in wherein.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described tooth bar two ends without
Flute profile.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described weather station pedestal
Two ends are connected with tooth bar by two horizontal support rod members.
Airbome weather station arrangement the most according to claim 4, it is characterised in that described support rod member is adopted
Use carbon fiber pipe.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described weather station pedestal
Both sides up and down be additionally provided with several sensor die massing mounting brackets, support is provided with for installation of modular
The position of sensor.
Airbome weather station arrangement the most according to claim 6, it is characterised in that described weather station pedestal
Both sides up and down be additionally provided with several overhanging stocks, with coordinating of sensor die massing mounting bracket middle position
Hole coordinates, and is fixedly connected by pin；Described overhanging stock top is provided with three-dimensional air velocity transducer, wind
To sensor.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described unmanned plane hollow
Planform be square, circular, oval in any one, hollow position bottom is provided with fixed mount,
Described weather station housing is fixed on this fixed mount, and unmanned plane includes fuselage, and several rotor motors,
Rotor and support arm, described rotor is installed in the rotating shaft of rotor motor, and described rotor motor is installed on support
One end of arm, the other end of described support arm is fixed on fuselage；Described rotor motor is along the diagonal of fuselage
Symmetrical.
Airbome weather station arrangement the most according to claim 1, it is characterised in that described power plant module is
Being arranged on the steering wheel on weather station shell body outer wall, steering wheel has several.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620334946.6U CN205581333U (en) | 2016-04-19 | 2016-04-19 | Machine carries weather station device suitable for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620334946.6U CN205581333U (en) | 2016-04-19 | 2016-04-19 | Machine carries weather station device suitable for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205581333U true CN205581333U (en) | 2016-09-14 |
Family
ID=56863409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620334946.6U Withdrawn - After Issue CN205581333U (en) | 2016-04-19 | 2016-04-19 | Machine carries weather station device suitable for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205581333U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN106741885A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | Using the autogyro and its application method of martian atmosphere circulation random probing |
| CN108051346A (en) * | 2017-11-07 | 2018-05-18 | 中国计量大学 | A kind of PM2_5 and its precursor monitoring system based on unmanned plane |
| CN111352438A (en) * | 2020-03-11 | 2020-06-30 | 深圳市多翼创新科技有限公司 | Full-automatic control method, device and system for unmanned aerial vehicle |
| WO2021036443A1 (en) * | 2019-08-30 | 2021-03-04 | 北京航空航天大学 | Atmospheric parameter measuring device for air sounding |
-
2016
- 2016-04-19 CN CN201620334946.6U patent/CN205581333U/en not_active Withdrawn - After Issue
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN106741885A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | Using the autogyro and its application method of martian atmosphere circulation random probing |
| CN106741885B (en) * | 2016-11-23 | 2019-08-23 | 上海卫星工程研究所 | Utilize the autogyro and its application method of martian atmosphere circulation random probing |
| CN108051346A (en) * | 2017-11-07 | 2018-05-18 | 中国计量大学 | A kind of PM2_5 and its precursor monitoring system based on unmanned plane |
| WO2021036443A1 (en) * | 2019-08-30 | 2021-03-04 | 北京航空航天大学 | Atmospheric parameter measuring device for air sounding |
| CN111352438A (en) * | 2020-03-11 | 2020-06-30 | 深圳市多翼创新科技有限公司 | Full-automatic control method, device and system for unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160914 Effective date of abandoning: 20180413 |