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CN106809388A - A kind of wireless monitor aircraft - Google Patents

A kind of wireless monitor aircraft Download PDF

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Publication number
CN106809388A
CN106809388A CN201710116932.6A CN201710116932A CN106809388A CN 106809388 A CN106809388 A CN 106809388A CN 201710116932 A CN201710116932 A CN 201710116932A CN 106809388 A CN106809388 A CN 106809388A
Authority
CN
China
Prior art keywords
module
shell
output end
electrically connected
input
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.)
Pending
Application number
CN201710116932.6A
Other languages
Chinese (zh)
Inventor
张琛
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 CN201710116932.6A priority Critical patent/CN106809388A/en
Publication of CN106809388A publication Critical patent/CN106809388A/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00—Programme-control systems
    • G05B19/02—Programme-control systems electric
    • G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/05—Programmable logic controllers, e.g. simulating logic interconnections of signals according to ladder diagrams or function charts
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00—Television systems
    • H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
    • H04N7/185—Closed-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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/10—Plc systems
    • G05B2219/15—Plc structure of the system
    • G05B2219/15053—Microcontroller
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/12—Electric charging stations
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Multimedia (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The present invention relates to vehicle technology field,A kind of especially wireless monitor aircraft,Including shell and wireless charging panel,The bottom of the shell sets exhaust empennage,The top of the shell sets supervising device,The inner chamber of the shell is installed by control mainboard,Propulsion electric machine and rechargeable battery,Charging module is electrically connected with the rechargeable battery,The second coil is electrically connected with the charging module,WIFI devices are installed on the shell,The supervising device includes image capture module and audio collection module,The output end of described image acquisition module,The output end of audio collection module distinguishes the input of corresponding audio transmission module,The input of image transmission module is electrically connected with,The wireless monitor aircraft can implement remote control,Audio frequency and video is shared,The function of data transfer and GPS location,Wireless charging can be carried out simultaneously,Have the advantages that monitoring range is wide.

Description

A kind of wireless monitor aircraft
Technical field
The present invention relates to vehicle technology field, more particularly to a kind of wireless monitor aircraft.
Background technology
At present, common wireless monitor is mostly fixed, indoor near radio monitoring device, is suitable only for interior Wireless monitor, the function that outdoor can carry out the wireless monitor aircraft that activity monitoring positioning and long-distance video show is complete not enough It is kind, can not for example be charged in outdoor, monitoring scope is small, however it remains the drawbacks of more.
The content of the invention
Can not be monitored positioning and remotely regard in outdoor the invention aims to solve to exist in the prior art The shortcoming of frequency display, and a kind of wireless monitor aircraft for proposing.
To achieve these goals, present invention employs following technical scheme：
A kind of wireless monitor aircraft, including shell and wireless charging panel are designed, the bottom of the shell sets exhaust Empennage, the top of the shell sets supervising device, and control mainboard, propulsion electric machine are installed and the electricity that charges in the inner chamber of the shell Pond, is electrically connected with charging module on the rechargeable battery, the second coil is electrically connected with the charging module, pacifies on the shell Equipped with WIFI devices, the supervising device includes image capture module and audio collection module, described image acquisition module it is defeated Go out end, the output end of audio collection module distinguishes the input of corresponding audio transmission module, image transmission module it is defeated Enter end be electrically connected with, the output end of the audio transmission module, the output end of image transmission module with the input of control mainboard End signal is connected, and the output end of control mainboard input respectively with propulsion electric machine, the input of WIFI devices electrically connect Connect, the WIFI devices are connected with remote terminal two-way signaling；
The wireless charging panel includes power supply, and the output end of the power supply is electrically connected with the input of AC-DC module, The output end of the AC-DC module is electrically connected with the input of PLC, the output end and electronics of the PLC The input of switch is electrically connected with, the first coil of output end connection with the second coil mutual induction of the electronic switch, institute State and annular is provided with wireless charging panel parks position, the annular parks the wall being provided with position for parking the aircraft Body, GPS module is electrically connected with the control mainboard.
Preferably, the WIFI devices include WIFI receiver modules and WIFI sending modules.
Preferably, the first coil is arranged on wireless charging panel near the side of wall, and second coil is set In the intracavity bottom of shell, aircraft is parked on wall, and first coil keeps ten to two ten centimetres of spacing with the second coil.
Preferably, the shell 1 is gas filled outer jacket or plastics lightweight shell.
Preferably, the SIM for recognizing its identity is installed on the communication module.
A kind of wireless monitor aircraft proposed by the present invention, beneficial effect is：By setting WIFI devices so that people The function of shared remote control, audio frequency and video, data transfer and GPS location can be implemented to aircraft by WiFi devices, passed through Wireless charging platform is set, and when electric quantity of rechargeable battery is too low, controllable aircraft flies to wireless charging platform and charged, it is real The function of being charged to aircraft in outdoor is showed, when setting multiple wireless charging platforms, aircraft can fly to any one Charging platform is charged, and the Surveillance center that need not fly back, it is greatly improved the monitoring scope of the aircraft.
Brief description of the drawings
Fig. 1 is a kind of generalized section of wireless monitor aircraft proposed by the present invention；
Fig. 2 is a kind of wireless charging panel generalized section of wireless monitor aircraft proposed by the present invention；
Fig. 3 is a kind of theory diagram of wireless monitor aircraft proposed by the present invention.
In figure：1 shell, 2 supervising devices, 3 control mainboards, 4 propulsion electric machines, 5 exhaust empennages, 6WIFI devices, 7 charging electricity Pond, 8 wireless charging platforms, 9 annulars park position, 10 walls.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.
Reference picture 1-3, a kind of wireless monitor aircraft, including shell 1 and wireless charging panel 8, shell 1 are gas filled outer jacket Or plastics lightweight shell, the bottom of shell 1 sets exhaust empennage 5, the top setting supervising device 2 of shell 1, the inner chamber of shell 1 Control mainboard 3, propulsion electric machine 4 and rechargeable battery 7 are installed, charging module is electrically connected with rechargeable battery 7, on charging module electrically The second coil is connected, WIFI devices 6 is installed on shell 1, supervising device 2 includes image capture module and audio collection module, The output end of image capture module, the output end of audio collection module distinguish corresponding audio transmission module input, The input of image transmission module is electrically connected with, the output end of audio transmission module, the output end of image transmission module with control The input end signal connection of mainboard processed, the output end of control mainboard input respectively with propulsion electric machine 4, WIFI devices 6 it is defeated Enter end, the input of communication module is electrically connected with, WIFI devices 6 are connected with remote terminal two-way signaling, communication module and intelligence Mobile phone two-way signaling is connected, and the SIM for recognizing its identity is provided with communication module.
Wireless charging panel 8 includes power supply, and the output end of power supply is electrically connected with the input of AC-DC module, AC-DC moulds The output end of block is electrically connected with the input of PLC, and the output end of PLC is electrical with the input of electronic switch Connection, output end connection and the first coil of the second coil mutual induction of electronic switch, ring is provided with wireless charging panel 8 Shape parks position 9, and annular parks the wall 10 being provided with position 9 for parking the aircraft, and GPS moulds are electrically connected with control mainboard Block, WIFI devices 6 include WIFI receiver modules and WIFI sending modules, and first coil is arranged on wireless charging panel 8 near wall The side of body 10, the second coil is arranged on the intracavity bottom of shell 1, and aircraft is parked on wall 10, first coil and second Coil keeps ten to two ten centimetres of spacing.
Operation principle：Operationally, the collection of supervising device 2 video, audio signal simultaneously pass through the wireless monitor aircraft WIFI devices send to remote terminal the function of realizing monitoring, while be connected using communication module and smart mobile phone realization, when filling When electricity is too low in battery 7, GPS module is used for the navigation of aircraft, and remote terminal controls aircraft by WIFI signal Fly to annular and park position 9, PLC controls electronic switch that the magnetic for making first coil produce change is opened and closed with certain frequency , the second coil-induced change to magnetic field is filled so as to the induced-current for producing induced-current, generation to rechargeable battery 7 Electricity, GPS module is used for the navigation of aircraft, and monitoring is can proceed with after charging complete.
The above, the only present invention preferably specific embodiment, but protection scope of the present invention is not limited thereto, Any one skilled in the art the invention discloses technical scope in, technology according to the present invention scheme and its Inventive concept is subject to equivalent or change, should all be included within the scope of the present invention.

Claims (5)

1. a kind of wireless monitor aircraft, including shell (1) and wireless charging panel (8), the bottom of the shell (1) set row Gas empennage (5), top setting supervising device (2) of the shell (1), inner chamber installation control mainboard (3) of the shell (1), Propulsion electric machine (4) and rechargeable battery (7), are electrically connected with charging module, it is characterised in that described to fill on the rechargeable battery (7) The second coil is electrically connected with electric module, WIFI devices (6) are installed on the shell (1), the supervising device (2) includes figure As acquisition module and audio collection module, the output end of described image acquisition module, the output end of audio collection module respectively with The input of corresponding audio transmission module, the input of image transmission module be electrically connected with, the audio transmission module Output end, the output end of image transmission module are connected with the input end signal of control mainboard, the output end of the control mainboard Input respectively with propulsion electric machine (4), the input of WIFI devices (6), the input of communication module are electrically connected with, described WIFI devices (6) are connected with remote terminal two-way signaling, and the communication module is connected with smart mobile phone two-way signaling；
The wireless charging panel (8) includes power supply, and the output end of the power supply is electrically connected with the input of AC-DC module, The output end of the AC-DC module is electrically connected with the input of PLC, the output end and electronics of the PLC The input of switch is electrically connected with, the first coil of output end connection with the second coil mutual induction of the electronic switch, institute State and annular is provided with wireless charging panel (8) parks position (9), the annular is parked to be provided with position (9) and flown for parking this The wall (10) of row device, GPS module is electrically connected with the control mainboard.
2. a kind of wireless monitor aircraft according to claim 1, it is characterised in that the WIFI devices (6) include WIFI receiver modules and WIFI sending modules.
3. a kind of wireless monitor aircraft according to claim 1, it is characterised in that the first coil is arranged on wirelessly Charging panel (8) is arranged on the intracavity bottom of shell (1) near the side of wall (10), second coil, and aircraft is parked On wall (10), first coil keeps ten to two ten centimetres of spacing with the second coil.
4. a kind of wireless monitor aircraft according to claim 1, it is characterised in that the shell (1) is gas filled outer jacket Or plastics lightweight shell.
5. a kind of wireless monitor aircraft according to claim 1, it is characterised in that be provided with use on the communication module In the SIM for recognizing its identity.
CN201710116932.6A 2017-03-01 2017-03-01 A kind of wireless monitor aircraft Pending CN106809388A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710116932.6A CN106809388A (en) 2017-03-01 2017-03-01 A kind of wireless monitor aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710116932.6A CN106809388A (en) 2017-03-01 2017-03-01 A kind of wireless monitor aircraft

Publications (1)

Publication Number Publication Date
CN106809388A true CN106809388A (en) 2017-06-09

Family

ID=59114445

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710116932.6A Pending CN106809388A (en) 2017-03-01 2017-03-01 A kind of wireless monitor aircraft

Country Status (1)

Country Link
CN (1) CN106809388A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103645740A (en) * 2013-12-30 2014-03-19 中国科学院自动化研究所 Intelligent cruise robot based on wireless charging odd-shaft aircraft
CN104503349A (en) * 2014-12-10 2015-04-08 天津大学 Monitoring device based on unmanned aerial vehicle
CN104795861A (en) * 2015-04-09 2015-07-22 天津大学 Wireless charging system and method based on unmanned aerial vehicle
CN204623851U (en) * 2015-03-30 2015-09-09 五邑大学 Based on the electrical equipment online monitoring system of unmanned plane

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103645740A (en) * 2013-12-30 2014-03-19 中国科学院自动化研究所 Intelligent cruise robot based on wireless charging odd-shaft aircraft
CN104503349A (en) * 2014-12-10 2015-04-08 天津大学 Monitoring device based on unmanned aerial vehicle
CN204623851U (en) * 2015-03-30 2015-09-09 五邑大学 Based on the electrical equipment online monitoring system of unmanned plane
CN104795861A (en) * 2015-04-09 2015-07-22 天津大学 Wireless charging system and method based on unmanned aerial vehicle

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20170609

WD01 Invention patent application deemed withdrawn after publication