CN210347968U - Flight equipment for meteorological monitoring - Google Patents

Flight equipment for meteorological monitoring Download PDF

Info

Publication number
CN210347968U
CN210347968U CN201920208655.6U CN201920208655U CN210347968U CN 210347968 U CN210347968 U CN 210347968U CN 201920208655 U CN201920208655 U CN 201920208655U CN 210347968 U CN210347968 U CN 210347968U
Authority
CN
China
Prior art keywords
sensor
unmanned aerial
monitoring
aerial vehicle
central shaft
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.)
Expired - Fee Related
Application number
CN201920208655.6U
Other languages
Chinese (zh)
Inventor
岳景东
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201920208655.6U priority Critical patent/CN210347968U/en
Application granted granted Critical
Publication of CN210347968U publication Critical patent/CN210347968U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The utility model relates to a flight device for meteorological monitoring, which comprises more than two groups of unmanned aerial vehicles and a ground monitoring device for controlling the unmanned aerial vehicles; each unmanned aerial vehicle comprises an unmanned aerial vehicle body, landing frames and more than two groups of wings, wherein even number of nacelle are arranged on the wings, and the even number of nacelle are symmetrically arranged on the wings at two sides of the unmanned aerial vehicle body; the nacelle comprises a containing part and a sealing cover which are connected, the containing part is connected with the wings, a temperature and humidity sensor and an air pressure sensor are arranged in the containing part, and a rain and snow sensor, a wind measuring sensor and more than two groups of visual sensors are arranged on the outer wall of the containing part; the nacelle is a rotatable spherical structure; the lowest end of the pod is positioned above the lowest end of the landing frame; each sensor is in wireless connection with the ground monitoring device. The utility model discloses can real-time multiple spot continuous monitoring weather, monitoring range is big, and the monitoring process can flexible regulation and control, and is difficult for receiving the environmental condition influence, does benefit to in time high-efficient grasp relevant regional meteorological information.

Description

Flight equipment for meteorological monitoring
Technical Field
The utility model relates to a meteorological monitoring technical field especially relates to a flight equipment for meteorological monitoring.
Background
Weather and environment have great influence on production and life of people, in general, weather monitoring is mainly carried out by monitoring points set by a weather department, and the accuracy of weather forecast information is different because weather forecast is an average estimated value of a certain area and the number and the addresses of the monitoring points are different; each monitoring point carries out fixed point monitoring through fixed equipment basically, and monitoring range is limited, and need set up multiunit monitoring facilities to need the periodic maintenance, consume a large amount of manpower and materials.
In the prior art, utility model ZL201721690093.0 discloses a portable environmental weather monitoring device, which comprises a movable box body, a first support rod, a second support rod and a control box are fixed on the top of the movable box body, a support plate is fixed on the top of the first support rod, an anemoscope is fixed on the top of the support plate, a support block is fixed on the top of the second support rod, a humidity sensor and a temperature sensor are installed on the top of the support block, a storage battery, a controller and a wireless communication module electrically connected with the controller are fixed in the control box, the storage battery is respectively connected with the anemoscope and the humidity sensor, the temperature sensor, the controller and the wireless communication module are electrically connected, the controller is electrically connected with the humidity sensor, the temperature sensor and the anemoscope, the outer walls of the left side and the right side of the movable box body are respectively fixed with a fixed block, the bottom of the fixed block is connected with a horizontal plate through a telescopic vertical leg, and the front end and the rear end of the bottom of the horizontal plate are respectively fixed with a movable wheel; the utility model discloses a make monitoring facilities not limited to fixed the application to a certain extent, can also remove on ground and use, the monitoring range increases to some extent, nevertheless needs manpower field control to remove, and is more difficult suitable for to the abominable condition of ground environment.
Therefore, it is urgently needed to research and develop better meteorological monitoring equipment, increase the monitoring range, improve the accuracy of meteorological monitoring, and effectively save the cost of manpower and material resources.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a flight equipment for meteorological monitoring to the problem that prior art exists, based on current unmanned aerial vehicle equipment carries out the improved design, easy operation, it is convenient to remove, realizes real-time meteorological monitoring on a large scale, fully improves meteorological monitoring information's the degree of accuracy.
The utility model provides a technical scheme of problem is: a flight device for meteorological monitoring comprises more than two groups of unmanned aerial vehicles and a ground monitoring device for controlling the unmanned aerial vehicles; each unmanned aerial vehicle comprises an unmanned aerial vehicle body, landing frames and more than two groups of wings, wherein the wings are provided with pods, the number of the pods is even, and the even number of the pods are symmetrically arranged on the wings on two sides of the unmanned aerial vehicle body; the pod comprises a containing part and a sealing cover which are connected, the containing part is connected with the wings of the unmanned aerial vehicle, a temperature and humidity sensor and an air pressure sensor are arranged in the containing part, and a rain and snow sensor, a wind measuring sensor and more than two groups of visual sensors are arranged on the outer wall of the containing part; the nacelle is of a rotatable spherical structure; the lowest end of the pod is positioned above the lowest end of the landing frame; the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the visual sensors are all in wireless connection with the ground monitoring device.
Further, a flight device for meteorological monitoring in, visual sensor more than two sets of includes visible light visual sensor and infrared visual sensor, visible light visual sensor and infrared visual sensor's quantity is the same, visible light visual sensor and infrared visual sensor set up at interval each other.
Further, be arranged in the aircraft for meteorological monitoring, be equipped with the ventilation window more than two on the lateral wall of the holding portion of nacelle, each be equipped with the blade that can overturn on the ventilation window.
Further, a flight equipment for meteorological monitoring in still be equipped with vertical center pin and horizontal center pin in the hanging cabin wear to be equipped with parallel first supporting part and second supporting part on the vertical center pin, first supporting part is located the well upper portion of vertical center pin, the second supporting part is located the tip of vertical center pin, temperature and humidity sensor and baroceptor set up on the first supporting part, rain and snow sensor and anemometry sensor set up on the second supporting part, visual sensor all is located the tip of horizontal center pin.
Preferably, in the flying apparatus for meteorological monitoring of the present invention, a plurality of first mounting grooves are disposed on the first supporting portion, each of the first mounting grooves is annularly distributed around the longitudinal central axis, and the temperature sensor and the air pressure sensor are symmetrically disposed on the first mounting groove; the second supporting part is provided with a plurality of second mounting grooves, the second mounting grooves surround the longitudinal central shaft and are distributed annularly, and the rain and snow sensor and the wind measuring sensor are symmetrically arranged on the second mounting grooves.
Preferably, in the flying device for meteorological monitoring of the utility model, the number of the vision sensors is even, and the vision sensors are symmetrically arranged at two ends of the transverse central shaft; at least half of the even number of visual sensors are infrared visual sensors.
Further, a flight equipment for meteorological monitoring in still be equipped with the communication device and the power supply unit that are connected on the unmanned aerial vehicle body, communication device with ground monitoring device wireless connection, temperature and humidity sensor, baroceptor, sleet sensor, anemometry sensor and visual sensor equally divide do not with communication device is connected.
Preferably, be used for meteorological monitoring's flight equipment in, communication device is based on beidou navigation positioning system's communication device.
Preferably, be in the flight equipment for meteorological monitoring in the utility model, power supply unit is super capacitor module, super capacitor module comprises the super capacitor who contains metal lithium more than two.
Further, be used for meteorological monitoring's flight equipment in each unmanned aerial vehicle moves simultaneously, horizontal distance between the adjacent unmanned aerial vehicle is 6m ~ 10m, vertical distance between the adjacent unmanned aerial vehicle is 30m ~ 500 m.
Compared with the prior art, the beneficial effects of the utility model are that: the structure innovation, can realize real-time multiple spot meteorological monitoring in succession, compare and show in current monitoring facilities and enlarge monitoring range, and can hover the monitoring as required fixed point, can carry out flexible real-time tracking regulation and control to the monitoring process, and be difficult for receiving external environment condition influence, do benefit to and solve the difficult problem of monitoring under the abominable hazardous environment, be convenient for relevant personnel in time master the meteorological information in target monitoring area high-efficiently, thereby arrange or the accident event handles and provide accurate meteorological information and guide for relevant operation, and then effectively avoid appearing the unnecessary loss, do benefit to the orderly operation of the relevant production life of guarantee.
Drawings
Fig. 1 is a schematic structural diagram (one) of a flight device for meteorological monitoring according to the present invention;
fig. 2 is a schematic structural diagram (two) of the flight device for meteorological monitoring of the present invention.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings and examples, but the present invention is not limited to the examples. In the following description of the preferred embodiments, for the purposes of promoting a thorough understanding of the invention by the public, specific details are set forth in order to provide a thorough understanding of the invention without the need for a skilled artisan to describe such details. In other instances, well-known elements, circuits, and methods of use have not been described in detail in order to avoid unnecessarily obscuring the spirit of the present invention.
As shown in fig. 1 and 2, the present invention relates to a flight device for meteorological monitoring, which includes more than two sets of unmanned aerial vehicles and a ground monitoring device for controlling the unmanned aerial vehicles; each unmanned aerial vehicle comprises an unmanned aerial vehicle body, landing frames and more than two groups of wings, wherein the wings are provided with pods, the number of the pods is even, and the even number of the pods are symmetrically arranged on the wings on two sides of the unmanned aerial vehicle body; the pod comprises a containing part and a sealing cover which are connected, the containing part is connected with the wings of the unmanned aerial vehicle, a temperature and humidity sensor and an air pressure sensor are arranged in the containing part, and a rain and snow sensor, a wind measuring sensor and more than two groups of visual sensors are arranged on the outer wall of the containing part; the nacelle is of a rotatable spherical structure; the lowest end of the pod is positioned above the lowest end of the landing frame; the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the visual sensors are all in wireless connection with the ground monitoring device.
In the above-mentioned embodiment, carry out meteorological monitoring simultaneously through setting up more than two sets of unmanned aerial vehicles, do benefit to the degree of accuracy that improves the monitoring, specifically unmanned aerial vehicle's quantity is arranged according to the region scope of target monitoring, preferably, starts monitoring time measuring, through each unmanned aerial vehicle of ground monitoring device control flies at the co-altitude not, realizes the meteorological information monitoring to the co-altitude department in same region, preferably each unmanned aerial vehicle moves simultaneously, and horizontal distance between the adjacent unmanned aerial vehicle is 6m ~ 10m, and vertical distance between the adjacent unmanned aerial vehicle is 30m ~ 500m, makes each unmanned person who participates in the monitoring tend to on same vertical line to make the meteorological information monitoring of same region co-altitude not go on in real time in step, and then improve monitoring information's the degree of accuracy.
In the above embodiment, the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the visual sensor are used for respectively monitoring the weather information of the temperature, the humidity, the air pressure, the rainfall and the snowfall and the wind direction and the wind speed in the flying area and acquiring the image of the monitoring environment; in order to enhance the meteorological monitoring effect and provide more visual and comprehensive information reference for ground personnel, the more than two groups of visual sensors preferably comprise visible light visual sensors and infrared visual sensors, the number of the visible light visual sensors is the same as that of the infrared visual sensors, and the visible light visual sensors and the infrared visual sensors are arranged at intervals; the system comprises a visible light vision sensor, an infrared vision sensor, a monitoring environment image acquisition module and a monitoring environment image acquisition module, wherein the visible light vision sensor is used for recording a monitoring environment image in the daytime and the infrared vision sensor is used for recording a monitoring environment scene image in the nighttime; preferably, the visible light sensor is an industrial CCD camera, and the infrared vision sensor is a short wave infrared camera, so as to facilitate the realization of more comprehensive monitoring.
In the embodiment, the number of the pods is preferably 2 or 4, the number of the pods is determined according to the environment of a monitored area, the monitoring information of each sensor in each pod is sent to the ground monitoring device in real time, the phenomenon that the meteorological monitoring is interrupted when a single pod breaks down is avoided, the monitoring can be kept to be continued through other pods, and the sample analysis is carried out on multiple groups of monitoring information, so that the monitoring accuracy is improved.
In the embodiment, the nacelle is of a rotatable spherical structure, so that the air resistance in flight is reduced, and the comprehensiveness of each sensor in monitoring meteorological information is improved; the lowest end of the pod is positioned above the lowest end of the landing frame, so that the sensor arranged in the pod and on the outer wall of the pod is prevented from being vibrated due to landing, and the pod, the sensor arranged in the accommodating part of the pod and other devices are effectively protected. Preferably, in order to ensure the monitoring accuracy, the internal and external air of the nacelle are the same, and the temperature and humidity detection and the air pressure detection inside the nacelle are accurate and efficient, more than two ventilation windows are arranged on the side wall of the containing part of the nacelle, and each ventilation window is provided with a blade capable of being turned; preferably, 2 to 4 ventilation windows are arranged above the temperature and humidity sensor and the air pressure sensor, and at least two ventilation windows are symmetrically arranged on two opposite sides of the accommodating part, so that the same internal and external air environments of the accommodating part are guaranteed; preferably, each ventilation window is closed by rotating the blade in rainy and snowy weather, so that the accommodating part and each device in the accommodating part can be protected; simultaneously, also do benefit to according to unmanned aerial vehicle's load and detection needs set up air sampling device and air contaminant detection device in the nacelle to when realizing meteorological information monitoring, realize the monitoring to air quality.
In some embodiments of the present invention, in order to ensure the stability of the pod during flight, preferably, a longitudinal central shaft and a transverse central shaft are further disposed in the pod, a first supporting portion and a second supporting portion, which are parallel to each other, are disposed on the longitudinal central shaft, the first supporting portion is located at the middle upper portion of the longitudinal central shaft, the second supporting portion is located at the end portion of the longitudinal central shaft, the temperature and humidity sensor and the air pressure sensor are disposed on the first supporting portion, the rain and snow sensor and the wind sensor are disposed on the second supporting portion, and the visual sensor is located at the end portion of the transverse central shaft; preferably, the second supporting part is positioned above the first supporting part, so that the rain and snow sensor and the wind measuring sensor are positioned at the top of the nacelle, the installation stability is guaranteed, and the stability and the accuracy of monitoring rain, snow and wind direction and wind speed are guaranteed; preferably, the cover of the pod is located at the bottom or side of the receptacle, preferably the cover is located at the side of the receptacle to facilitate pod servicing.
In the above embodiment, in order to enhance the monitoring stability, a plurality of first mounting grooves are respectively formed in the first supporting portion, each first mounting groove is annularly distributed around the longitudinal central axis, and the temperature sensor and the air pressure sensor are symmetrically arranged on the first mounting grooves; a plurality of second mounting grooves are formed in the second supporting portion, the second mounting grooves are distributed annularly around the longitudinal central shaft, and the rain and snow sensor and the wind measuring sensor are symmetrically arranged on the second mounting grooves; the number of the vision sensors is preferably even, and the vision sensors are symmetrically arranged at two ends of the transverse central shaft, so that the installation stability of each meteorological monitoring sensor and the stability of the nacelle in the flight process are effectively guaranteed, and the nacelle cannot swing due to unbalance. Preferably, at least half of the even number of visual sensors are infrared visual sensors, so that the visible light visual sensors and the infrared visual sensors which are arranged at intervals can record and track images of a monitored environment day and night, and weather monitoring information is more comprehensive and accurate.
The utility model discloses a in other embodiments, on the basis that ordinary unmanned aerial vehicle set up the signal command receiver who carries out flight control, for guarantee unmanned aerial vehicle's steady operation and meteorological monitoring's effective control and meteorological information's real-time conveying still be equipped with the communication device and the power supply unit that are connected on the unmanned aerial vehicle body, communication device with ground monitoring device wireless connection, temperature and humidity sensor, baroceptor, sleet sensor, anemometry sensor and visual sensor equally divide do not with communication device is connected. The communication device is set based on a positioning navigation system and is used for positioning and communication; specifically, the communication device is used for positioning the flight of the unmanned aerial vehicle and sending positioning information to the ground monitoring device in real time; the communication device is also used for receiving detection information transmitted by the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor and the wind measuring sensor and power supply information of the power supply device and transmitting the received detection information and power supply information to the ground monitoring device; the communication device is also used for receiving the instruction sent by the ground monitoring device and transmitting the received instruction sent by the ground monitoring device to a corresponding device, namely one or more of the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the power supply device. The power supply unit is used for supplying power to the unmanned aerial vehicle body and each sensor and communication device to guarantee the holistic steady operation power consumption of flight equipment, and give power supply unit's electric quantity information real-time transmission communication device, communication device gives the information transmission of receiving ground monitoring device, so that the flight time and the time of returning voyage of effective control unmanned aerial vehicle.
In the above embodiment, to ensure real-time and stable communication and positioning, the communication device is preferably a communication device based on a GPS or a beidou navigation positioning system, and preferably, the communication device is a communication device based on a beidou navigation positioning system, so as to more effectively monitor weather information in a dangerous and severe environment; in order to ensure the stable operation of the shuttle and monitoring of the flight equipment and relatively reduce the load of the unmanned aerial vehicle, the power supply device is preferably a super-capacitor module, and the super-capacitor module is preferably composed of more than two super-capacitors containing metal lithium.
In the above embodiment, the unmanned aerial vehicle can be any unmanned aerial vehicle, and the load of the pod, the sensors and the related devices is preferably selected as a standard, and the endurance time of the target monitoring area can be met; the ground monitoring device can be set according to the number of the unmanned aerial vehicles and the range of a target monitoring area, such as the setting based on the existing flight controller alone or the combination with a computer, a mobile communication terminal such as a mobile phone and the like, preferably a combination device of a flight controller, a remote computer and a mobile phone mobile terminal which are mutually in wireless communication connection, wherein the flight controller or the remote computer controls the flight distance, the height and the time of the unmanned aerial vehicle, the remote computer controls the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the power supply device, the remote computer and the mobile phone mobile terminal receive meteorological monitoring information, the remote computer stores, analyzes and displays the meteorological monitoring information, and the mobile phone mobile terminal receives and checks the analysis and processing result of the meteorological information, therefore, related workers can flexibly arrange, control and monitor, weather information can be mastered efficiently, and working efficiency is greatly improved.
In the application of the embodiment the utility model is used for during meteorological monitoring's flight equipment, by relevant managers according to the environment and the concrete operating mode in target place, through each unmanned aerial vehicle of ground monitoring device adjustment and control moves or monitoring meteorological information that hovers. Specifically, under the control of the ground monitoring device, all unmanned aerial vehicles participating in meteorological monitoring are started, starting detection instructions are transmitted to all meteorological sensors through a communication device, meteorological monitoring is carried out on a target monitoring area from different heights, and all unmanned aerial vehicles carry pods to pass through the target monitoring area through respective wings in the flight process; in the containing part of the pod, a temperature and humidity sensor detects temperature and humidity and transmits detected temperature and humidity information to a communication device, and an air pressure sensor detects air pressure and transmits detected air pressure information to the communication device; on the outer wall of the containing part of the nacelle, a rain and snow sensor detects rain and snow conditions of rainfall and snowfall and transmits detected rain and snow information to a communication device, and a wind measuring sensor detects wind direction and wind speed and transmits detected wind speed and wind direction information to the communication device; the communication device receives detection information transmitted by the temperature and humidity sensors, the air pressure sensor, the rain and snow sensor and the wind measuring sensor and transmits the received detection information to the ground monitoring device; in the monitoring process, the sensors for monitoring multiple groups of meteorological data are simultaneously monitored by the aid of the plurality of the nacelle, multiple groups of monitoring information are provided, and accuracy of the obtained meteorological information is fully improved. Through the utility model discloses an above-mentioned application realizes real-time multiple spot meteorological monitoring in succession, also can trail the regulation and control in real time to the monitoring process, can solve the monitoring difficulty problem under the abominable hazardous environment, makes relevant personnel in time master the meteorological information of paying attention to the ground high-efficiently to do benefit to and improve the efficiency that relevant operation arranged or accident event handled by a wide margin.
The present invention is not limited to the above-described embodiments, and any obvious modifications or alterations to the above-described embodiments may be made by those skilled in the art without departing from the spirit of the present invention and the scope of the appended claims.

Claims (6)

1. A flight device for meteorological monitoring, characterized in that: the system comprises more than two groups of unmanned aerial vehicles and a ground monitoring device for controlling the unmanned aerial vehicles; each unmanned aerial vehicle comprises an unmanned aerial vehicle body, landing frames and more than two groups of wings, wherein the wings are provided with pods, the number of the pods is even, and the even number of the pods are symmetrically arranged on the wings on two sides of the unmanned aerial vehicle body; the pod comprises a containing part and a sealing cover which are connected, the containing part is connected with the wings of the unmanned aerial vehicle, a temperature and humidity sensor and an air pressure sensor are arranged in the containing part, and a rain and snow sensor, a wind measuring sensor and more than two groups of visual sensors are arranged on the outer wall of the containing part; the nacelle is of a rotatable spherical structure; the lowest end of the pod is positioned above the lowest end of the landing frame; the temperature and humidity sensor, the air pressure sensor, the rain and snow sensor, the wind measuring sensor and the visual sensors are all in wireless connection with the ground monitoring device.
2. The flying apparatus for meteorological monitoring of claim 1, wherein: the visual sensors more than two sets of include visible light visual sensor and infrared visual sensor, visible light visual sensor and infrared visual sensor's quantity is the same, visible light visual sensor and infrared visual sensor set up at interval each other.
3. The flying apparatus for meteorological monitoring of claim 1, wherein: the hanging cabin is internally provided with a longitudinal central shaft and a transverse central shaft, a first supporting part and a second supporting part which are parallel are arranged on the longitudinal central shaft in a penetrating mode, the first supporting part is located on the middle upper portion of the longitudinal central shaft, the second supporting part is located at the end portion of the longitudinal central shaft, a temperature and humidity sensor and a pressure sensor are arranged on the first supporting part, a rain and snow sensor and a wind measuring sensor are arranged on the second supporting part, and a vision sensor is located at the end portion of the transverse central shaft.
4. The flying apparatus for meteorological monitoring of claim 3, wherein: a plurality of first mounting grooves are formed in the first supporting portion, the first mounting grooves are distributed annularly around the longitudinal central shaft, and the temperature and humidity sensor and the air pressure sensor are symmetrically arranged on the first mounting grooves;
the second supporting part is provided with a plurality of second mounting grooves, the second mounting grooves surround the longitudinal central shaft and are distributed annularly, and the rain and snow sensor and the wind measuring sensor are symmetrically arranged on the second mounting grooves.
5. The flying apparatus for meteorological monitoring of claim 3, wherein: the number of the visual sensors is even, and the visual sensors are symmetrically arranged at two ends of the transverse central shaft; at least half of the even number of visual sensors are infrared visual sensors.
6. Flight apparatus for meteorological monitoring according to any one of claims 1 to 5, characterized in that: when the unmanned aerial vehicles operate simultaneously, the horizontal distance between adjacent unmanned aerial vehicles is 6-10 m, and the vertical distance between adjacent unmanned aerial vehicles is 30-500 m.
CN201920208655.6U 2019-02-19 2019-02-19 Flight equipment for meteorological monitoring Expired - Fee Related CN210347968U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920208655.6U CN210347968U (en) 2019-02-19 2019-02-19 Flight equipment for meteorological monitoring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920208655.6U CN210347968U (en) 2019-02-19 2019-02-19 Flight equipment for meteorological monitoring

Publications (1)

Publication Number Publication Date
CN210347968U true CN210347968U (en) 2020-04-17

Family

ID=70173379

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920208655.6U Expired - Fee Related CN210347968U (en) 2019-02-19 2019-02-19 Flight equipment for meteorological monitoring

Country Status (1)

Country Link
CN (1) CN210347968U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112130230A (en) * 2020-09-18 2020-12-25 华能澜沧江水电股份有限公司 Three-dimensional monitoring method for local climate effect of high mountain canyon reservoir

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112130230A (en) * 2020-09-18 2020-12-25 华能澜沧江水电股份有限公司 Three-dimensional monitoring method for local climate effect of high mountain canyon reservoir
CN112130230B (en) * 2020-09-18 2022-08-30 华能澜沧江水电股份有限公司 Three-dimensional monitoring method for local climate effect of high mountain canyon reservoir

Similar Documents

Publication Publication Date Title
CN103612756B (en) The multi-rotor aerocraft of electric power line inspection and based on its system
CN106886225B (en) Multifunctional unmanned aerial vehicle intelligent landing station system
CN105067484A (en) Unmanned plane based live-line test apparatus for hydrophobicity of composite insulator of power transmission line
CN204808049U (en) Communication system with unmanned aerial vehicle
CN109061707A (en) Nuclear pollution region nuclear radiation monitoring system and method based on unmanned plane
CN102856827B (en) Omnibearing ground-space isomeric substation polling system
CN204822097U (en) Anti -jamming unmanned aerial vehicle system
CN208367220U (en) Nuclear pollution region nuclear radiation monitoring system based on unmanned plane
CN101807080A (en) Robot airship control system for overhead line inspection and control method thereof
CN204895881U (en) Unmanned aerial vehicle system with thermal imaging system
CN102201170A (en) Highway full-section in-time prompt system
CN111766895A (en) Unmanned aerial vehicle inspection system and method for photovoltaic power station
CN203381787U (en) Electric multi-shaft unmanned aerial vehicle for checking electric transmission line
CN104683759B (en) Inner wall of stack corrosion condition wireless video monitoring apparatus and method for based on aircraft
CN103345255A (en) Quad-rotor aerial photography positioning unmanned aerial vehicle
CN204944984U (en) Based on the hydrophobicity of composite insulator of power transmission line live testing device of unmanned plane
CN205203413U (en) Unmanned aerial vehicle with keep away obstacle function by oneself
CN203405734U (en) Quad-rotor aerial photography positioning unmanned aerial vehicle
CN210347968U (en) Flight equipment for meteorological monitoring
CN204846371U (en) Can keep away unmanned aerial vehicle system of barrier
CN103414851B (en) Region floating monitoring system is determined during long boat
CN205594453U (en) Patrol system of robot
CN105480417A (en) Intelligent unmanned aerial vehicle
CN107196790A (en) A kind of intelligent grid online detection instrument
CN205384515U (en) Forest fires monitoring and intelligent recognition system based on unmanned aerial vehicle platform

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20200417

Termination date: 20220219

CF01 Termination of patent right due to non-payment of annual fee