CN113665802B - Unmanned aerial vehicle data remote pushing system and method - Google Patents

Unmanned aerial vehicle data remote pushing system and method Download PDF

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Publication number
CN113665802B
CN113665802B CN202111018712.2A CN202111018712A CN113665802B CN 113665802 B CN113665802 B CN 113665802B CN 202111018712 A CN202111018712 A CN 202111018712A CN 113665802 B CN113665802 B CN 113665802B
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China
Prior art keywords
unmanned aerial
aerial vehicle
data
communication
disaster area
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CN202111018712.2A
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Chinese (zh)
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CN113665802A (en
Inventor
王伟任
谢锋
黎相成
仝来源
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Wanhang Star Technology Development Co ltd
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Wanhang Star Technology Development Co ltd
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Priority to CN202111018712.2A priority Critical patent/CN113665802B/en
Publication of CN113665802A publication Critical patent/CN113665802A/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/30Supply or distribution of electrical power
    • B64U50/34In-flight charging
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00Television systems
    • H04N7/18Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • H04N7/183Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
    • H04N7/185Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source from a mobile camera, e.g. for remote control
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/20UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Multimedia (AREA)
  • Signal Processing (AREA)
  • Electric Cable Installation (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle data remote pushing system and method; the unmanned aerial vehicle data remote pushing system comprises a communication base station, a camera shooting structure, a communication unmanned aerial vehicle and a power supply unmanned aerial vehicle, wherein the communication base station comprises a first wireless transceiver module, a second wireless transceiver module and a data grouping module, the first wireless transceiver module is used for receiving disaster situation picture data shot by the camera shooting structure and transmission data in the communication process of people in a disaster area, the disaster situation picture data and the transmission data are transmitted to the data grouping module, after being grouped by the data grouping module, the grouping disaster situation picture data and the transmission data are transmitted to the outside through the second wireless transceiver module, and therefore the demand of the people in the disaster area on the transmission of remote data outside the disaster area is met.

Description

Unmanned aerial vehicle data remote pushing system and method
Technical Field
The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle data remote pushing system and method.
Background
When disaster conditions occur, such as flood or earthquake, communication equipment in the disaster affected area is often damaged, so that people in the disaster affected area cannot establish communication with the outside,
in the prior art, emergency satellite communication is generally adopted to establish connection with the outside, but the communication is limited by the transmission capability of satellites, so that the data transmission requirement of a large number of people cannot be met.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle data remote pushing system and method, which are used for quickly establishing an output transmission channel when a disaster happens so as to meet the data use requirements of people in the disaster area.
In order to achieve the above purpose, the invention provides an unmanned aerial vehicle data remote pushing system, which comprises a communication base station, a camera shooting structure, a communication unmanned aerial vehicle and a power supply unmanned aerial vehicle, wherein the communication base station is arranged at the lower side of the communication unmanned aerial vehicle and is fixedly connected with the communication unmanned aerial vehicle, the camera shooting structure is arranged at the front end of the lower side of the communication unmanned aerial vehicle and is electrically connected with the communication base station, and the power supply unmanned aerial vehicle is connected with a lead of the communication unmanned aerial vehicle;
the communication base station comprises a first wireless transceiver module, a second wireless transceiver module and a data grouping module, wherein the first wireless transceiver module is configured to receive user uploading data and the camera shooting structure uploading data and transmit the data to the data grouping module, the data grouping module is configured to group the data in the first wireless transceiver module and transmit the grouped data to the second wireless transceiver module, and the second wireless transceiver module is configured to transmit the grouped data to the base station outside the disaster area.
The first wireless transceiver module is utilized to receive disaster situation picture data shot by the shooting structure and transmission data in the communication process of people in the disaster area, the disaster situation picture data and the transmission data are transmitted to the data grouping module, the data grouping module is used for grouping, and the grouped disaster situation picture data and the grouped transmission data are transmitted to the outside through the second wireless transceiver module, so that the requirement of people in the disaster area on the transmission of remote data outside the disaster area is met, and the disaster situation can be limited timely.
The communication unmanned aerial vehicle comprises a communication unmanned aerial vehicle shell, a plurality of horn, external connection piece and joint, a plurality of the horn pass through the external connection piece with the communication unmanned aerial vehicle shell is connected, the joint then set up in the downside of communication unmanned aerial vehicle shell, just the joint with power supply unmanned aerial vehicle electricity is connected, the communication unmanned aerial vehicle shell then set up in the upside of communication basic station.
The utility model discloses a communication unmanned aerial vehicle shell, thereby utilize a plurality of the horn makes communication unmanned aerial vehicle shell can keep unsettled, utilizes again connect with power supply unmanned aerial vehicle cooperation charges, thereby makes the long-term work of communication unmanned aerial vehicle can effectively prolong disaster area communication time, outer connecting piece then is used for with the horn with communication unmanned aerial vehicle shell's joint strength promotes.
Each horn comprises a flying wing, a connecting arm and a prompting lamp, wherein the flying wings are connected with the communication unmanned aerial vehicle shell through the connecting arms, the connecting arms are fixedly connected with the communication unmanned aerial vehicle shell, and the prompting lamps are arranged on the outer sides of the flying wings and are electrically connected with the communication base station.
Utilize the flight wing keeps communication unmanned aerial vehicle's unsettled, utilize again the linking arm with the horn cooperation makes the flight wing with communication unmanned aerial vehicle shell can keep being connected, the warning light is used for warning at night on the one hand, on the other hand then lets disaster area masses can in time observe communication unmanned aerial vehicle's position indicates that external support is going on, can effectively pacify disaster area masses ' emotion.
The flying wing comprises a driving motor, a fan wing piece and a fixing frame, wherein the fixing frame is arranged on the upper side of the connecting arm and fixedly connected with the connecting arm, the driving motor is arranged on the upper side of the fixing frame, and the output end of the driving motor is connected with the fan wing piece.
Utilize driving motor drives fan fin rotates, thereby makes the flight wing drives communication unmanned aerial vehicle keeps unsettled, the mount is then used for installing driving motor, simultaneously be convenient for with linking arm fixed connection.
The communication unmanned aerial vehicle shell is provided with a power supply battery, a containing cavity and a positioning head, wherein the power supply battery is arranged in the containing cavity, the power supply battery is electrically connected with the connector, the containing cavity is arranged on the inner side of the communication unmanned aerial vehicle shell, and the positioning head is arranged on the lower side of the communication unmanned aerial vehicle shell and is matched with the power supply unmanned aerial vehicle.
Utilize power supply battery comes as communication unmanned aerial vehicle's power supply utilizes the holding chamber is placed power supply battery utilizes the locating head cooperation power supply unmanned aerial vehicle, thereby be convenient for power supply unmanned aerial vehicle is charged communication unmanned aerial vehicle.
The connector is provided with a magnetic ring, a sealing film and an electric lead, wherein the magnetic ring is arranged at the lower side of the connector, the sealing film is matched with the connector, the sealing film is provided with a cross-shaped notch, and the electric lead is electrically connected with the power supply battery.
Utilize the magnetism ring promotes communication unmanned aerial vehicle with the stability of power supply unmanned aerial vehicle when transmitting electricity utilizes the sealed film avoids in the condition such as raining again the rainwater is soaked connect, reuse the electric wire with power supply unmanned aerial vehicle cooperation, and then accomplish to power supply battery's charge.
The invention also provides a using method of the unmanned aerial vehicle data remote pushing system, which comprises the following steps:
shooting disaster area pictures by using a shooting structure, and transmitting picture data to a first wireless receiving and transmitting module;
the first wireless receiving and transmitting module receives transmission data in the communication process of the disaster area people, mixes the picture data and the transmission data and then transmits the picture data and the transmission data to the data grouping module;
the data grouping module separates and groups the mixed transmission data and the picture data, and then respectively transmits the transmission data and the picture data to the second wireless receiving and transmitting module;
the second wireless transceiver module respectively transmits the transmission data to the base station outside the disaster area, and transmits the picture data to the outside to display the disaster situation in time.
According to the unmanned aerial vehicle data remote pushing system and method, the first wireless receiving and transmitting module is used for receiving disaster situation picture data shot by the shooting structure and transmission data in the communication process of people in a disaster area, the disaster situation picture data and the transmission data are transmitted to the data grouping module, the data grouping module is used for grouping, and the grouped disaster situation picture data and the grouping transmission data are transmitted to the outside through the second wireless receiving and transmitting module, so that the requirement of people in the disaster area on the transmission of remote data outside the disaster area is met.
Drawings
In order to more clearly illustrate the embodiments of the invention or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic diagram of an axial measurement structure of an unmanned aerial vehicle data remote pushing system.
Fig. 2 is a schematic diagram of an axis measurement structure of a communication unmanned aerial vehicle of the unmanned aerial vehicle data remote pushing system provided by the invention.
Fig. 3 is a schematic cross-sectional structural diagram of a communication unmanned aerial vehicle of the unmanned aerial vehicle data remote pushing system.
Fig. 4 is a schematic diagram of an axis measurement structure of a power supply unmanned aerial vehicle of the unmanned aerial vehicle data remote pushing system.
Fig. 5 is a schematic diagram of a cross-sectional structure of a power supply contact of the unmanned aerial vehicle data remote pushing system provided by the invention.
Fig. 6 is a schematic structural diagram of a connector of an unmanned aerial vehicle data remote pushing system.
Fig. 7 is a schematic diagram of a cross-sectional structure of a joint of an unmanned aerial vehicle data remote pushing system.
Fig. 8 is a schematic structural diagram of a communication base station of the unmanned aerial vehicle data remote pushing system provided by the invention.
Fig. 9 is a schematic step diagram of a method for using an unmanned aerial vehicle data remote pushing system provided by the invention.
1-communication base station, 2-camera structure, 3-communication unmanned aerial vehicle, 4-power supply unmanned aerial vehicle, 11-first wireless transceiver module, 12-second wireless transceiver module, 13-data packet module, 31-communication unmanned aerial vehicle shell, 32-horn, 33-outer connector, 34-connector, 311-power supply battery, 312-accommodation chamber, 313-positioning head, 321-flight wing, 322-connecting arm, 323-indicator light, 324-driving motor, 325-fan wing, 326-fixing frame, 341-magnetic ring, 342-sealing film, 343-electric wire, 41-positioning fitting head, 42-power supply fitting head, 43-power storage battery, 44-power supply unmanned aerial vehicle shell, 421-power supply contact, 422-electromagnetic sheet, 423-power supply wire, 424-water stop, 425-elastic sheet.
Detailed Description
Embodiments of the present invention are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout. The embodiments described below by referring to the drawings are illustrative and intended to explain the present invention and should not be construed as limiting the invention.
In the description of the present invention, it should be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate describing the present invention and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present invention. Furthermore, in the description of the present invention, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
Referring to fig. 1 to 8, the present invention provides an unmanned aerial vehicle data remote pushing system, which includes a communication base station 1, a camera shooting structure 2, a communication unmanned aerial vehicle 3 and a power supply unmanned aerial vehicle 4, wherein the communication base station 1 is arranged at the lower side of the communication unmanned aerial vehicle 3 and is fixedly connected with the communication unmanned aerial vehicle 3, the camera shooting structure 2 is arranged at the front end of the lower side of the communication unmanned aerial vehicle 3 and is electrically connected with the communication base station 1, and the power supply unmanned aerial vehicle 4 is connected with the communication unmanned aerial vehicle 3 through a wire;
the communication base station 1 includes a first wireless transceiver module 11, a second wireless transceiver module 12, and a data grouping module 13, where the first wireless transceiver module 11 is configured to receive user upload data and upload data from the camera structure 2, and transfer the data to the data grouping module 13, and the data grouping module 13 is configured to group data in the first wireless transceiver module 11 and transfer the grouped data to the second wireless transceiver module 12, and the second wireless transceiver module 12 is configured to transfer the grouped data to a base station outside the disaster area.
In this embodiment, the communication base station 1 is responsible for transmitting the picture data captured by the image capturing structure 2 and the transmission data of communication between the disaster area people and the outside, the communication unmanned aerial vehicle 3 is used for driving the communication base station 1 to stay in the air, so as to avoid the interference of the outside, the first wireless transceiver module 11 is used for collecting the mixed data, the data grouping module 13 is used for grouping the mixed data into the picture data and the transmission data, and the second wireless transceiver module 12 is used for transmitting the grouped data to the outside, so that the transmission efficiency of the data is effectively improved.
Further, the communication unmanned aerial vehicle 3 includes a communication unmanned aerial vehicle housing 31, a plurality of horn 32, an external connection member 33 and a joint 34, wherein a plurality of horn 32 is connected with the communication unmanned aerial vehicle housing 31 through the external connection member 33, the joint 34 is disposed at the lower side of the communication unmanned aerial vehicle housing 31, the joint 34 is electrically connected with the power supply unmanned aerial vehicle 4, and the communication unmanned aerial vehicle housing 31 is disposed at the upper side of the communication base station 1;
each of the aircraft arms 32 includes a flight wing 321, a connection arm 322 and a warning light 323, the flight wing 321 is connected with the communication unmanned aerial vehicle housing 31 through the connection arm 322, the connection arm 322 is fixedly connected with the communication unmanned aerial vehicle housing 31, and the warning light 323 is arranged on the outer side of the flight wing 321 and is electrically connected with the communication base station 1;
the flying wing 321 comprises a driving motor 324, a fan wing 325 and a fixing frame 326, wherein the fixing frame 326 is arranged on the upper side of the connecting arm 322 and is fixedly connected with the connecting arm 322, the driving motor 324 is arranged on the upper side of the fixing frame 326, and the output end of the driving motor 324 is connected with the fan wing 325;
the communication unmanned aerial vehicle shell 31 is provided with a power supply battery 311, a containing cavity 312 and a positioning head 313, the power supply battery 311 is arranged in the containing cavity 312, the power supply battery 311 is electrically connected with the connector 34, the containing cavity 312 is arranged on the inner side of the communication unmanned aerial vehicle shell 31, and the positioning head 313 is arranged on the lower side of the communication unmanned aerial vehicle shell 31 and is matched with the power supply unmanned aerial vehicle 4;
the connector 34 has a magnetic ring 341, a sealing film 342 and an electrical lead 343, the magnetic ring 341 is disposed on the lower side of the connector 34, the sealing film 342 is engaged with the connector 34, the sealing film 342 is provided with a cross-shaped notch, and the electrical lead 343 is electrically connected with the power supply battery 311.
In this embodiment, the communication unmanned aerial vehicle housing 31 is used to protect each component, the plurality of the arms 32 drive the communication unmanned aerial vehicle housing 31 to hover, the outer connector 33 is used to raise the connection strength between the communication unmanned aerial vehicle housing 31 and the plurality of the arms 32, the connector 34 is matched with the power supply unmanned aerial vehicle 4, so as to realize charging of the communication unmanned aerial vehicle 3, that is, prolong the working time of the communication unmanned aerial vehicle 3, the flying wing 321 is used to provide flying power, the connecting arm 322 is used to make the flying wing 321 drive the communication unmanned aerial vehicle 3 to hover, the indicator lamp 323 prevents other aircrafts from touching the communication unmanned aerial vehicle 3 at night, and on the other hand, by means of lamplight, the people in disaster area are prompted, the people in disaster area can be effectively calmed by external rescue on the road, the driving motor 324 is used for driving the fan fin 325 to rotate, thereby giving the communication unmanned aerial vehicle 3 rises power, the fixing frame 326 then cooperates with the fan fin 325, thereby making the fan fin 325 can be fixed on the connecting arm 322, the power supply battery 311 then is used as the power supply of the communication unmanned aerial vehicle 3, the holding cavity 312 is used for placing the power supply battery 311, the positioning head 313 then cooperates with the power supply unmanned aerial vehicle 4, thereby effectively improving the connection strength of the communication unmanned aerial vehicle 3 and the power supply unmanned aerial vehicle 4, the magnetic ring 341 is used for cooperating with the power supply unmanned aerial vehicle 4, thereby improving the connection strength, the sealing film 342 is provided with a cross-shaped notch so as to prevent rainwater from immersing the joint 34 when raining, thereby influencing the subsequent charging, and the electric wire 343 then cooperates with the power supply battery 311, thereby completing the charging work.
Further, the power supply unmanned aerial vehicle 4 includes a positioning fitting head 41, a power supply fitting head 42, a power storage battery 43 and a power supply unmanned aerial vehicle housing 44, the power storage battery 43 is disposed on the inner side of the power supply unmanned aerial vehicle housing 44 and is electrically connected with the power supply fitting head 42, and the positioning fitting head 41 is disposed on the upper side of the power supply unmanned aerial vehicle 4 and is matched with the positioning head 313;
the power supply mating head 42 includes a power supply contact 421, an electromagnetic sheet 422, and a power supply wire 423, where the power supply wire 423 connects the power supply contact 421 and the power storage battery 43, the electromagnetic sheet 422 is disposed outside the power supply contact 421, and the electromagnetic sheet 422 is mated with the magnetic ring 341;
the power supply contact 421 has a water-stop plate 424 and an elastic piece 425, the water-stop plate 424 is disposed on the upper side of the power supply contact 421 and is rotatably connected with the power supply contact 421, and the elastic piece 425 connects the power supply contact 421 and the water-stop plate 424.
In this embodiment, the positioning matching head 41 is configured to match the positioning head 313, so as to improve connection accuracy of the communication unmanned aerial vehicle 3 and the power supply unmanned aerial vehicle 4 during charging, the electric storage battery 43 is configured to charge the communication unmanned aerial vehicle 3, the power supply unmanned aerial vehicle housing 44 is configured to protect each component, the power supply matching head 42 is configured to match the connector 34, so as to complete transmission of electric power, the power supply contact 421 is configured to match the connector 34, so as to complete transmission of electric power, the electromagnetic sheet 422 is configured to match the magnetic ring 341, when the communication unmanned aerial vehicle 3 is in butt joint with the power supply unmanned aerial vehicle 4 during charging, the electromagnetic sheet 422 is started, so that the electromagnetic sheet 422 is adsorbed with the magnetic ring 341, thereby improving connection strength of the communication unmanned aerial vehicle 3 and the power supply unmanned aerial vehicle 4, the power supply wire 423 is configured to protect each component, the water stop plate 424 is configured to match the elastic sheet 425, so that rainwater is prevented from immersing into the power supply contact 421 when the charging unmanned aerial vehicle is not charged, and when the water stop plate 421 is charged, the water stop plate 424 can rotate after charging.
Referring to fig. 9, the invention further provides a method for using the unmanned aerial vehicle data remote pushing system, which comprises the following steps:
s101: shooting disaster area pictures by using the shooting structure 2, and transmitting picture data to the first wireless transceiver module 11;
s102: the first wireless transceiver module 11 receives the transmission data in the communication process of the disaster area people, mixes the picture data and the transmission data and then transmits the picture data and the transmission data to the data grouping module 13;
s103: the data grouping module 13 separates and groups the mixed transmission data and picture data, and then respectively transmits the transmission data and the picture data to the second wireless transceiver module 12;
s104: the second wireless transceiver module 12 transmits the transmission data to the base station outside the disaster area, and transmits the picture data to the outside to display the disaster situation in time.
The above disclosure is only a preferred embodiment of the present invention, and it should be understood that the scope of the invention is not limited thereto, and those skilled in the art will appreciate that all or part of the procedures described above can be performed according to the equivalent changes of the claims, and still fall within the scope of the present invention.

Claims (7)

1. The unmanned aerial vehicle data remote pushing system is characterized in that the unmanned aerial vehicle data remote pushing system comprises:
communication unmanned plane;
the communication base station is arranged at the lower side of the communication unmanned aerial vehicle and is fixedly connected with the communication unmanned aerial vehicle so as to be suspended along with the communication unmanned aerial vehicle;
the camera shooting structure is arranged at the front end of the lower side of the communication unmanned aerial vehicle, is electrically connected with the communication base station and is used for shooting disaster area pictures to obtain picture data;
the power supply unmanned aerial vehicle is in butt joint with the communication unmanned aerial vehicle during charging, and charges the communication unmanned aerial vehicle through a wire;
wherein the communication base station includes:
the first wireless transceiver module is configured to receive mixed data comprising transmission data of communication between disaster area people and the outside and picture data obtained by shooting the shooting structure in the disaster area, and transmit the mixed data comprising the transmission data of communication between disaster area people and the outside and the picture data obtained by shooting the shooting structure in the disaster area to the data grouping module;
the data grouping module is configured to separate and group the transmission data which is transmitted by the first wireless receiving and transmitting module and contains communication between the disaster area people and the outside and the mixed data of the picture data which is obtained by shooting the disaster area by the shooting structure, and transmit the transmission data which is transmitted by the disaster area people and the outside and the picture data which is obtained by shooting the disaster area by the shooting structure to the second wireless receiving and transmitting module respectively;
the second wireless transceiver module is configured to transmit the transmission data of communication between the disaster area people and the outside after grouping to the base station outside the disaster area, and to transmit the picture data shot by the shooting structure after grouping to the outside so as to display the disaster condition of the disaster area in time.
2. The unmanned aerial vehicle data remote pushing system of claim 1, wherein,
the communication unmanned aerial vehicle includes communication unmanned aerial vehicle shell, a plurality of horn, external connection spare and connects, and is a plurality of the horn passes through external connection spare with communication unmanned aerial vehicle shell is connected, connect then set up in communication unmanned aerial vehicle shell's downside, just connect with power supply unmanned aerial vehicle electric connection, communication unmanned aerial vehicle shell then set up in communication base station's upside.
3. A remote data push system for unmanned aerial vehicles as claimed in claim 2,
every the horn all includes flight wing, linking arm and warning light, the flight wing pass through the linking arm with communication unmanned aerial vehicle shell is connected, the linking arm then with communication unmanned aerial vehicle shell fixed connection, the warning light set up in the outside of flight wing, and with communication basic station electric connection.
4. A remote data push system for unmanned aerial vehicles as claimed in claim 3,
the flying wing comprises a driving motor, a fan wing piece and a fixing frame, wherein the fixing frame is arranged on the upper side of the connecting arm and fixedly connected with the connecting arm, the driving motor is arranged on the upper side of the fixing frame, and the output end of the driving motor is connected with the fan wing piece.
5. The unmanned aerial vehicle data remote pushing system of claim 4, wherein,
the communication unmanned aerial vehicle shell has power supply battery, holding chamber and locating head, power supply battery set up in the holding intracavity, just power supply battery with connect electric connection, the holding chamber then set up in the inboard of communication unmanned aerial vehicle shell, the locating head set up in the downside of communication unmanned aerial vehicle shell, and with the cooperation of power supply unmanned aerial vehicle.
6. The unmanned aerial vehicle data remote pushing system of claim 5, wherein,
the connector is provided with a magnetic ring, a sealing film and an electric lead, wherein the magnetic ring is arranged at the lower side of the connector, the sealing film is matched with the connector, the sealing film is provided with a cross-shaped notch, and the electric lead is electrically connected with the power supply battery.
7. The method of using the unmanned aerial vehicle data remote push system of claim 6, comprising the steps of:
shooting disaster area pictures by using a shooting structure, and transmitting picture data to a first wireless receiving and transmitting module;
the first wireless receiving and transmitting module receives transmission data in the communication process of the disaster area people, mixes the picture data and the transmission data and then transmits the picture data and the transmission data to the data grouping module;
the data grouping module separates and groups the mixed transmission data and the picture data, and then respectively transmits the transmission data and the picture data to the second wireless receiving and transmitting module;
the second wireless transceiver module respectively transmits the transmission data to the base station outside the disaster area, and transmits the picture data to the outside to display the disaster situation in time.
CN202111018712.2A 2021-09-01 2021-09-01 Unmanned aerial vehicle data remote pushing system and method Active CN113665802B (en)

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1381155A (en) * 2000-05-30 2002-11-20 松下电器产业株式会社 Radio communication system and communication terminal apparatus used therein
CN205336281U (en) * 2015-12-31 2016-06-22 中国国土资源航空物探遥感中心 Aerial relay , data link system and emergent monitoring system
CN106921429A (en) * 2015-12-25 2017-07-04 顺丰科技有限公司 A kind of method and device of data double-way forwarding
WO2018152849A1 (en) * 2017-02-27 2018-08-30 深圳市大疆创新科技有限公司 Control method, remote monitoring device, base station, server and steaming media server
CN108521852A (en) * 2017-11-30 2018-09-11 深圳市大疆创新科技有限公司 UAV system and communication means
CN109921512A (en) * 2019-04-15 2019-06-21 湖南科技大学 A kind of UAV Communication base station system and usage
CN110069072A (en) * 2018-08-16 2019-07-30 北京电联宇科技股份有限公司 A kind of precise positioning overlength continuation of the journey unmanned plane inspection disaster prevention system
CN210469317U (en) * 2019-11-20 2020-05-05 黄锦山 Unmanned aerial vehicle platform of relaying communication deployment usefulness

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111065164B (en) * 2018-10-16 2023-09-12 荣耀终端有限公司 User equipment, method and device in base station for wireless communication

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1381155A (en) * 2000-05-30 2002-11-20 松下电器产业株式会社 Radio communication system and communication terminal apparatus used therein
CN106921429A (en) * 2015-12-25 2017-07-04 顺丰科技有限公司 A kind of method and device of data double-way forwarding
CN205336281U (en) * 2015-12-31 2016-06-22 中国国土资源航空物探遥感中心 Aerial relay , data link system and emergent monitoring system
WO2018152849A1 (en) * 2017-02-27 2018-08-30 深圳市大疆创新科技有限公司 Control method, remote monitoring device, base station, server and steaming media server
CN108700889A (en) * 2017-02-27 2018-10-23 深圳市大疆创新科技有限公司 Control method, remote supervisory and control(ling) equipment, base station, server and streaming media server
CN108521852A (en) * 2017-11-30 2018-09-11 深圳市大疆创新科技有限公司 UAV system and communication means
CN110069072A (en) * 2018-08-16 2019-07-30 北京电联宇科技股份有限公司 A kind of precise positioning overlength continuation of the journey unmanned plane inspection disaster prevention system
CN109921512A (en) * 2019-04-15 2019-06-21 湖南科技大学 A kind of UAV Communication base station system and usage
CN210469317U (en) * 2019-11-20 2020-05-05 黄锦山 Unmanned aerial vehicle platform of relaying communication deployment usefulness

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