CN107187587A - A kind of Intelligent unattended machine taken photo by plane for video display - Google Patents
A kind of Intelligent unattended machine taken photo by plane for video display Download PDFInfo
- Publication number
- CN107187587A CN107187587A CN201710314593.2A CN201710314593A CN107187587A CN 107187587 A CN107187587 A CN 107187587A CN 201710314593 A CN201710314593 A CN 201710314593A CN 107187587 A CN107187587 A CN 107187587A
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- China
- Prior art keywords
- plane
- module
- video display
- unmanned plane
- intelligent unattended
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- 230000007246 mechanism Effects 0.000 claims abstract description 81
- 238000001816 cooling Methods 0.000 claims abstract description 13
- 239000003381 stabilizer Substances 0.000 claims description 21
- 238000004891 communication Methods 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 6
- 238000000465 moulding Methods 0.000 claims 1
- 238000010248 power generation Methods 0.000 claims 1
- 230000000087 stabilizing effect Effects 0.000 abstract description 5
- 238000002955 isolation Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 8
- 230000003139 buffering effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 230000009194 climbing Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Studio Devices (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of Intelligent unattended machine taken photo by plane for video display, including body, Zhong Kong mechanisms, generating mechanism, aviation mechanism, camera and land mechanism, land mechanism includes housing, roller, buffer bar, buffer spring, cooling mechanism and guiding mechanism, cooling mechanism includes the rotation collar and radiating subassembly, radiating subassembly includes fix bar and some blades, working power module includes working power circuit, guiding mechanism includes gag lever post and directive wheel, this is used in the Intelligent unattended machine that video display are taken photo by plane, can be when unmanned plane land by land mechanism, internal heat is quickly handled, so as to improve the practicality of unmanned plane；Moreover, in working power circuit, the voltage stabilizing isolation of reference voltage can be realized, so as to improve the reliability of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of Intelligent unattended machine taken photo by plane for video display.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+sector application is that unmanned plane has really just been needed；At present taking photo by plane, agricultural, plant protection, miniature auto heterodyne, express delivery
Transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, system
The application in romance etc. field is made, the purposes of unmanned plane in itself has greatly been expanded, developed country also answers in actively extension industry
With with developing unmanned air vehicle technique.
In existing unmanned plane, there is what is taken photo by plane for video display, but, it is necessary to enter to unmanned plane during taking photo by plane
Capable frequently land, thus can gather substantial amounts of heat in the land mechanism of unmanned plane, if handled not in time, Jiu Huiying
The performance of the device of the inside of unmanned plane is rung, the reliability of unmanned plane is reduced；Moreover, in the internal circuit of unmanned plane
In, all lack stable reference voltage, so as to reduce the stability and reliability of unmanned plane operation.
The content of the invention
The technical problem to be solved in the present invention is：In order to overcome the deficiencies in the prior art to be taken photo by plane there is provided one kind for video display
Intelligent unattended machine.
The technical solution adopted for the present invention to solve the technical problems is：A kind of Intelligent unattended machine taken photo by plane for video display,
Including body, Zhong Kong mechanisms, generating mechanism, aviation mechanism, camera and land mechanism, the Zhong Kong mechanisms are arranged on body
On, the generating mechanism is arranged on the top of body, and the aviation mechanism is arranged on the both sides of body, and the camera is arranged on
The lower section of body, the land mechanism is arranged on the both sides of camera and positioned at the lower section of body；
Wherein, Zhong Kong mechanisms, for carrying out intelligentized control method to all parts in unmanned plane；Generating mechanism, for reality
Present line generates electricity, so as to improve the endurance of unmanned plane；Aviation mechanism, realizes the reliable flight of unmanned plane；Land machine
Structure, carries out bumper and absorbing shock when for unmanned plane land, improves the reliability of unmanned plane.
The land mechanism includes housing, roller, buffer bar, buffer spring, cooling mechanism and guiding mechanism, the housing
The lower section of body is vertically provided at, the roller of the housing is arranged on the bottom of buffer bar, and the upper semisection of the buffer bar is located at
The inside of housing and connected by the top of buffer spring and the inside of housing, the cooling mechanism is connected with buffer bar,
The guiding mechanism is connected with cooling mechanism；
The cooling mechanism includes the rotation collar and some radiating subassemblies, and the rotary sleeve ring set is located at the outer of buffer bar
Week, the inwall of the rotation collar is provided with internal thread, and the periphery of the buffer bar is provided with external screw thread, the internal thread and external screw thread
Matching, the radiating subassembly is uniformly arranged on the upper and lower ends of the rotation collar, and the radiating subassembly includes fix bar and some oars
Leaf, one end of the fix bar is arranged on the rotation collar, and the other end of the fix bar is connected with each blade, the fix bar
It is vertically arranged；
Wherein, housing is arranged on the lower section of body, when roller touches ground, and the upper semisection of buffer bar will be
The inside of housing is moved up, and subsequent buffer bar will enter row buffering by buffer spring, meanwhile, external screw thread and rotation on buffer bar
Internal thread on the collar is matched, and realizes the rotation of the rotation collar, so that the rotation to control each fix bar, then each blade
Also it can therewith rotate, the heat of enclosure interior will quickly be handled, so as to improve the reliability of unmanned plane.
The Zhong Kong mechanisms include panel and middle control component, and the middle control component is arranged on the inside of panel, the middle control
Component includes central control module, the image capture module being connected with central control module, motor control module, wireless telecommunications mould
Block, voice cue module, display control module, key control module, state indicator module and working power module, the center
Control module is PLC, and the camera is electrically connected with image capture module；
The working power module includes working power circuit, and the working power circuit includes operational amplifier, first
Resistance, second resistance, 3rd resistor, the 4th resistance, adjustable resistance, voltage-stabiliser tube, the first electric capacity and the second electric capacity, the computing are put
The external 5V DC voltage power supplies of power end of big device, the earth terminal ground connection of the operational amplifier, the operational amplifier it is anti-
The output end connection of phase input and operational amplifier, the in-phase input end of the operational amplifier passes through the 4th resistance, second
The external 5V DC voltage power supplies of series circuit of resistance and first resistor composition, the negative electrode of the voltage-stabiliser tube respectively with first resistor
With second resistance connection, the plus earth of the voltage-stabiliser tube, the reference edge of the voltage-stabiliser tube and the adjustable end of adjustable resistance are connected,
The voltage-stabiliser tube is in parallel with adjustable resistance, and one end of the 3rd resistor and the negative electrode of voltage-stabiliser tube are connected, the 3rd resistor
The one end for the series circuit that the other end is constituted with the first electric capacity and the second capacitance connection, first electric capacity and the second electric capacity respectively
Ground connection, the other end of the series circuit of the first electric capacity and the second electric capacity composition connects with second resistance and the 4th resistance respectively
Connect.
Wherein, central control module, for carrying out the module of intelligentized control method to unmanned plane, herein, center control mould
Block is PLC, also can be single-chip microcomputer, realizes and carries out intelligentized control method to the modules in unmanned plane, improves unmanned plane
Intellectuality；Image capture module, for carrying out the module of IMAQ, herein, by being controlled to camera, so that
Video display can be carried out to take photo by plane, the practicality of unmanned plane is improved；Motor control module, for carrying out the module of motor control,
Here, by being controlled to motor, the reliable flight of unmanned plane is realized；Wireless communication module, it is wireless for realizing
The module of communication, herein, by carrying out long distance wireless data transfer with external communication terminal, realizes the information to unmanned plane
Remote monitoring is carried out, the intellectuality of unmanned plane is realized；Voice cue module, for carrying out the module of voice message, herein,
By being controlled to loudspeaker, so as to be played to related alarm；Display control module, for realizing display control
The module of system, herein, by being controlled to display interface, can in real time be shown to the job information of unmanned plane, be carried
The high practicality of unmanned plane；Key control module, for carrying out the module by key control, herein, by control button
Manipulation information be acquired, so as to unmanned plane carry out implement scene manipulation, improve the operability of unmanned plane；Shape
State indicating module, herein, can be to nothing by the bright dark control to status indicator lamp for realizing the module of state instruction
Man-machine working condition is shown in real time, improves its practicality；Working power module, for providing stabilized supply voltage
Module, herein, for providing stable operating voltage to the modules inside unmanned plane, improves the reliable of unmanned plane
Property.
Wherein, in working power circuit, first pass around voltage-stabiliser tube and voltage stabilizing, subsequent operational amplifier are carried out to input voltage
In-phase input end input voltage is acquired, then followed by operational amplifier, realize to reference voltage every
From output, so as to improve the reliability and stability of working power circuit, the reliability of unmanned plane is improved.
Specifically, rotation the collar rotate during, directive wheel will guide groove inner rotation, while pass through limit
Position bar will be spacing to directive wheel, so as to realize rotation the collar Positive rotational, the guiding mechanism include gag lever post and
Directive wheel, the periphery of the rotation collar is provided with the guide groove matched with directive wheel, and the directive wheel is located at the inside of guide groove,
The gag lever post is connected with directive wheel.
Specifically, motor can be realized by controlling the rotation of each blade and produce power of climbing to body, so as to
Control unmanned plane is flown, if the aviation mechanism includes support bar, motor and dry run blade, the support bar is set
Put in the side of body, the motor is arranged on the top of support bar, the motor is driven with each flight blade to be connected
Connect, the motor is electrically connected with motor control module, the motor is electrically connected with motor control module.
Specifically, convert solar energy into electric energy by solar panel, realize unmanned plane follow-on mission away from
From the generating mechanism includes solar panel, and the solar panel is electrically connected with central control module.
Specifically, during in order to the operation irregularity of unmanned plane, carry out being additionally provided with loudspeaker on alarm, the panel,
The loudspeaker is electrically connected with voice cue module.
Specifically, in order to which the job information to unmanned plane is shown in real time, display interface, institute are additionally provided with the panel
Display interface is stated to electrically connect with display control module.
Specifically, unmanned plane is carried out for the ease of staff to be additionally provided with control button on implementation manipulation, the panel,
The control button is electrically connected with key control module.
Specifically, to the working condition of unmanned plane also set on Real Time Observation, the panel for the ease of staff
Stateful indicator lamp, the status indicator lamp is electrically connected with state indicator module.
Specifically, the inside of the panel is additionally provided with battery, the battery is electrically connected with working power module.
Specifically, can be received by signal transceiver to long-range remote signal, so as to realize work people
Member carries out being additionally provided with signal transceiver on long-range manipulation, the body to unmanned plane.
The beneficial effects of the invention are as follows this is used in the Intelligent unattended machine that video display are taken photo by plane, can be in nothing by land mechanism
When man-machine land, internal heat is quickly handled, so as to improve the practicality of unmanned plane；Moreover, exist
In working power circuit, the voltage stabilizing isolation of reference voltage can be realized, so as to improve the reliability of unmanned plane.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation of the Intelligent unattended machine taken photo by plane for video display of the present invention；
Fig. 2 is the structural representation of the land mechanism for being used for the Intelligent unattended machine that video display are taken photo by plane of the present invention；
Fig. 3 is the structural representation of the Zhong Kong mechanisms for being used for the Intelligent unattended machine that video display are taken photo by plane of the present invention；
Fig. 4 is the systematic schematic diagram of the Intelligent unattended machine taken photo by plane for video display of the present invention；
Fig. 5 is the circuit theory diagrams of the working power circuit for being used for the Intelligent unattended machine that video display are taken photo by plane of the present invention；
In figure：1. body, 2. Zhong Kong mechanisms, 3. generating mechanisms, 4. aviation mechanisms, 5. signal transceivers, 6. cameras, 7.
Land mechanism, 8. housings, 9. rollers, 10. buffer bars, the 11. rotation collars, 12. buffer springs, 13. gag lever posts, 14. directive wheels,
15. fix bar, 16. blades, 17. panels, 18. display interfaces, 19. control buttons, 20. status indicator lamps, 21. loudspeakers, 22.
Central control module, 23. image capture modules, 24. motor control modules, 25. wireless communication modules, 26. voice cue modules,
27. display control module, 28. key control modules, 29. state indicator modules, 30. working power modules, 31. batteries, 32.
Motor, U1. operational amplifiers, R1. first resistors, R2. second resistances, R3. 3rd resistors, the resistance of R4. the 4th, RP1. can
Adjust resistance, VD1. voltage-stabiliser tubes, the electric capacity of C1. first, the electric capacity of C2. second.
Embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These accompanying drawings are simplified schematic diagram, only with
Illustration illustrates the basic structure of the present invention, therefore it only shows the composition relevant with the present invention.
As Figure 1-Figure 5, a kind of Intelligent unattended machine taken photo by plane for video display, including body 1, Zhong Kong mechanisms 2, generator
Structure 3, aviation mechanism 4, camera 6 and land mechanism 7, the Zhong Kong mechanisms 2 are arranged on body 1, and the generating mechanism 3 is set
In the top of body 1, the aviation mechanism 4 is arranged on the both sides of body 1, and the camera 6 is arranged on the lower section of body 1, institute
State land mechanism 7 and be arranged on the both sides of camera 6 and positioned at the lower section of body 1；
Wherein, Zhong Kong mechanisms 2, for carrying out intelligentized control method to all parts in unmanned plane；Generating mechanism 3, is used for
Online generating is realized, so as to improve the endurance of unmanned plane；Aviation mechanism 4, realizes the reliable flight of unmanned plane；Land
Mechanism 7, carries out bumper and absorbing shock when for unmanned plane land, improves the reliability of unmanned plane.
The land mechanism 7 includes housing 8, roller 9, buffer bar 10, buffer spring 12, cooling mechanism and guiding mechanism,
The housing 8 is vertically provided at the lower section of body 1, and the roller 9 of the housing 8 is arranged on the bottom of buffer bar 10, the buffering
The upper semisection of bar 10 is located at the inside of housing 8 and is connected by buffer spring 12 with the top of the inside of housing 8, the radiating machine
Structure is connected with buffer bar 10, and the guiding mechanism is connected with cooling mechanism；
The cooling mechanism includes the rotation collar 11 and some radiating subassemblies, and the rotation collar 11 is set in buffer bar 10
Periphery, the inwall of the rotation collar 11 is provided with internal thread, and the periphery of the buffer bar 10 is provided with external screw thread, the internal thread
Matched with external screw thread, the radiating subassembly is uniformly arranged on the upper and lower ends of the rotation collar 11, the radiating subassembly includes fixing
Bar 15 and some blades 16, one end of the fix bar 15 are arranged on the rotation collar 11, the other end of the fix bar 15 with
Each blade 16 is connected, and the fix bar 15 is vertically arranged；
Wherein, housing 8 is arranged on the lower section of body 1, when roller 9 touches ground, the upper semisection of buffer bar 10
It will be moved up in the inside of housing 8, subsequent buffer bar 10 will enter row buffering by buffer spring 12, meanwhile, on buffer bar 10
External screw thread with rotation the collar 11 on internal thread match, realize rotate the collar 11 rotation so that each solid to control
The rotation of fixed pole 15, then each blade 16 can also rotate therewith, the heat inside housing 8 will quickly be handled, from
And improve the reliability of unmanned plane.
The Zhong Kong mechanisms 2 include panel 17 and middle control component, and the middle control component is arranged on the inside of panel 17, described
Image capture module 23, motor control module that middle control component includes central control module 22, is connected with central control module 22
24th, wireless communication module 25, voice cue module 26, display control module 27, key control module 28, state indicator module 29
With working power module 30, the central control module 22 is PLC, and the camera 6 is electrically connected with image capture module 23；
The working power module 30 include working power circuit, the working power circuit include operational amplifier U1,
First resistor R1, second resistance R2,3rd resistor R3, the 4th resistance R4, adjustable resistance RP1, voltage-stabiliser tube VD1, the first electric capacity C1
With the second electric capacity C2, the operational amplifier U1 external 5V DC voltage power supplies of power end, the operational amplifier U1's connects
Ground terminal is grounded, and the inverting input of the operational amplifier U1 is connected with operational amplifier U1 output end, the operation amplifier
The external 5V direct currents of series circuit that device U1 in-phase input end is made up of the 4th resistance R4, second resistance R2 and first resistor R1
Voltage source, the negative electrode of the voltage-stabiliser tube VD1 is connected with first resistor R1 and second resistance R2 respectively, the voltage-stabiliser tube VD1's
Plus earth, the reference edge of the voltage-stabiliser tube VD1 is connected with adjustable resistance RP1 adjustable end, the voltage-stabiliser tube VD1 and adjustable electric
Hinder RP1 in parallel, one end of the 3rd resistor R3 is connected with voltage-stabiliser tube VD1 negative electrode, the other end point of the 3rd resistor R3
It is not connected with the first electric capacity C1 and the second electric capacity C2, one end of the series circuit of the first electric capacity C1 and the second electric capacity C2 compositions
The other end of the series circuit of ground connection, the first electric capacity C1 and the second electric capacity C2 compositions is electric with second resistance R2 and the 4th respectively
Hinder R4 connections.
Wherein, central control module 22, for carrying out the module of intelligentized control method to unmanned plane, herein, center control
Module 22 is PLC, also can be single-chip microcomputer, realizes and carries out intelligentized control method to the modules in unmanned plane, improves nothing
Man-machine intellectuality；Image capture module 23, for carrying out the module of IMAQ, herein, by being controlled to camera 6
System, thus allows for video display and takes photo by plane, improve the practicality of unmanned plane；Motor control module 24, for carrying out motor control
Module, herein, by being controlled to motor 32, realize the reliable flight of unmanned plane；Wireless communication module 25,
For realizing the module of wireless telecommunications, herein, by carrying out long distance wireless data transfer with external communication terminal, realize pair
The information of unmanned plane carries out remote monitoring, realizes the intellectuality of unmanned plane；Voice cue module 26, for carrying out voice message
Module, herein, by being controlled to loudspeaker 21, so as to be played to related alarm；Display control mould
Block 27, herein, can be to the work of unmanned plane by being controlled to display interface 18 for realizing the module of display control
Make information to be shown in real time, improve the practicality of unmanned plane；Key control module 28, for carrying out the mould by key control
Block, herein, is acquired by the manipulation information to control button 19, so as to carry out implementing scene behaviour to unmanned plane
Control, improves the operability of unmanned plane；State indicator module 29, for realizing the module of state instruction, herein, by right
The bright dark control of status indicator lamp 20, can in real time be shown to the working condition of unmanned plane, improve its practicality；Work
Power module 30, for providing the module of stabilized supply voltage, herein, for providing steady to the modules inside unmanned plane
Fixed operating voltage, improves the reliability of unmanned plane.
Wherein, in working power circuit, first pass around voltage-stabiliser tube VD1 and voltage stabilizing is carried out to input voltage, subsequent computing is put
Big device U1 in-phase input end is acquired to input voltage, then is followed by operational amplifier U1, is realized to benchmark
The isolation and amplifier of voltage, so as to improve the reliability and stability of working power circuit, improves the reliable of unmanned plane
Property.
Specifically, rotation the collar 11 rotate during, directive wheel 14 will guide groove inner rotation, simultaneously lead to
Crossing gag lever post 13 will be spacing to directive wheel 14, so as to realize the Positive rotational of the rotation collar 11, the guiding mechanism bag
Gag lever post 13 and directive wheel 14 are included, the periphery of the rotation collar 11 is provided with the guide groove matched with directive wheel 14, the guiding
Wheel 14 is located at the inside of guide groove, and the gag lever post 13 is connected with directive wheel 14.
Specifically, motor 32 can be realized by controlling the rotation of each blade 16 and produce power of climbing to body 1, from
And unmanned plane can be controlled to be flown, if the aviation mechanism 4 includes support bar, motor 32 and dry run blade 16,
The support bar is arranged on the side of body 1, and the motor 32 is arranged on the top of support bar, the motor 32 with
Each flight blade 16 is connected, and the motor 32 is electrically connected with motor control module 24, the motor 32 and electricity
Machine control module 24 is electrically connected.
Specifically, convert solar energy into electric energy by solar panel, realize unmanned plane follow-on mission away from
From the generating mechanism 3 includes solar panel, and the solar panel is electrically connected with central control module 22.
Specifically, during in order to the operation irregularity of unmanned plane, carrying out being additionally provided with loudspeaker on alarm, the panel 17
21, the loudspeaker 21 is electrically connected with voice cue module 26.
Specifically, in order to which the job information to unmanned plane is shown in real time, display interface is additionally provided with the panel 17
18, the display interface 18 is electrically connected with display control module 27.
Specifically, carry out implementation manipulation to unmanned plane for the ease of staff, be additionally provided with the panel 17 control by
Key 19, the control button 19 is electrically connected with key control module 28.
Specifically, being carried out for the ease of staff to the working condition of unmanned plane on Real Time Observation, the panel 17 also
Provided with status indicator lamp 20, the status indicator lamp 20 is electrically connected with state indicator module 29.
Specifically, the inside of the panel 17 is additionally provided with battery 31, the battery 31 and the electricity of working power module 30
Connection.
Specifically, can be received by signal transceiver 5 to long-range remote signal, so as to realize work people
Member carries out being additionally provided with signal transceiver 5 on long-range manipulation, the body 1 to unmanned plane.
Compared with prior art, this is used in the Intelligent unattended machine that video display are taken photo by plane, can be in unmanned plane by land mechanism 7
When land, internal heat is quickly handled, so as to improve the practicality of unmanned plane；Moreover, in work
In power circuit, the voltage stabilizing isolation of reference voltage can be realized, so as to improve the reliability of unmanned plane.
Using the above-mentioned desirable embodiment according to the present invention as enlightenment, by above-mentioned description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property scope is not limited to the content on specification, it is necessary to its technical scope is determined according to right.
Claims (10)
1. a kind of Intelligent unattended machine taken photo by plane for video display, it is characterised in that including body, Zhong Kong mechanisms, generating mechanism, flight
Mechanism, camera and land mechanism, the Zhong Kong mechanisms are arranged on body, and the generating mechanism is arranged on the top of body,
The aviation mechanism is arranged on the both sides of body, and the camera is arranged on the lower section of body, and the land mechanism, which is arranged on, to be taken the photograph
Both sides as head and the lower section positioned at body；
The land mechanism includes housing, roller, buffer bar, buffer spring, cooling mechanism and guiding mechanism, and the housing is vertical
The lower section of body is arranged on, the roller of the housing is arranged on the bottom of buffer bar, and the upper semisection of the buffer bar is located at housing
Inside and connected by the top of buffer spring and the inside of housing, the cooling mechanism is connected with buffer bar, described
Guiding mechanism is connected with cooling mechanism；
The cooling mechanism includes the rotation collar and some radiating subassemblies, and the rotary sleeve ring set is located at the periphery of buffer bar, institute
The inwall for stating the rotation collar is provided with internal thread, and the periphery of the buffer bar is provided with external screw thread, and the internal thread is matched with external screw thread,
The radiating subassembly is uniformly arranged on the upper and lower ends of the rotation collar, and the radiating subassembly includes fix bar and some blades, institute
The one end for stating fix bar is arranged on the rotation collar, and the other end of the fix bar is connected with each blade, and the fix bar is vertical
Set；
The Zhong Kong mechanisms include panel and middle control component, and the middle control component is arranged on the inside of panel, the middle control component
The image capture module that is connected including central control module, with central control module, motor control module, wireless communication module,
Voice cue module, display control module, key control module, state indicator module and working power module, the center control
Molding block is PLC, and the camera is electrically connected with image capture module；
The working power module include working power circuit, the working power circuit include operational amplifier, first resistor,
Second resistance, 3rd resistor, the 4th resistance, adjustable resistance, voltage-stabiliser tube, the first electric capacity and the second electric capacity, the operational amplifier
The external 5V DC voltage power supplies of power end, the operational amplifier earth terminal ground connection, the operational amplifier it is anti-phase defeated
Enter end to be connected with the output end of operational amplifier, the in-phase input end of the operational amplifier passes through the 4th resistance, second resistance
The external 5V DC voltage power supplies of series circuit constituted with first resistor, the negative electrode of the voltage-stabiliser tube respectively with first resistor and the
Two resistance are connected, the plus earth of the voltage-stabiliser tube, and the reference edge of the voltage-stabiliser tube and the adjustable end of adjustable resistance are connected, described
Voltage-stabiliser tube is in parallel with adjustable resistance, and the negative electrode of one end of the 3rd resistor and voltage-stabiliser tube is connected, the 3rd resistor it is another
One termination of the series circuit that end is constituted with the first electric capacity and the second capacitance connection, first electric capacity and the second electric capacity respectively
Ground, the other end of the series circuit of the first electric capacity and the second electric capacity composition is connected with second resistance and the 4th resistance respectively.
2. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that the guiding mechanism includes limit
Position bar and directive wheel, the periphery of the rotation collar are provided with the guide groove matched with directive wheel, and the directive wheel is located at guide groove
Inside, the gag lever post is connected with directive wheel.
3. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that the aviation mechanism includes branch
If strut, motor and dry run blade, the support bar are arranged on the side of body, the motor is arranged on support
The top of bar, the motor is connected with each flight blade, and the motor is electrically connected with motor control module, institute
Motor is stated to electrically connect with motor control module.
4. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that the generating mechanism is included too
Positive energy power generation plate, the solar panel is electrically connected with central control module.
5. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that be additionally provided with and raise on the panel
Sound device, the loudspeaker is electrically connected with voice cue module.
6. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that be additionally provided with the panel aobvious
Show interface, the display interface is electrically connected with display control module.
7. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that control is additionally provided with the panel
Button processed, the control button is electrically connected with key control module.
8. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that be additionally provided with shape on the panel
State indicator lamp, the status indicator lamp is electrically connected with state indicator module.
9. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that the inside of the panel is also set
There is battery, the battery is electrically connected with working power module.
10. the Intelligent unattended machine taken photo by plane as claimed in claim 1 for video display, it is characterised in that be additionally provided with the body
Signal transceiver.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201710314593.2A CN107187587B (en) | 2017-05-06 | 2017-05-06 | A intelligent unmanned aerial vehicle for film and television aerial photography |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710314593.2A CN107187587B (en) | 2017-05-06 | 2017-05-06 | A intelligent unmanned aerial vehicle for film and television aerial photography |
Publications (2)
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| CN107187587A true CN107187587A (en) | 2017-09-22 |
| CN107187587B CN107187587B (en) | 2019-12-17 |
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| CN201710314593.2A Active CN107187587B (en) | 2017-05-06 | 2017-05-06 | A intelligent unmanned aerial vehicle for film and television aerial photography |
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| CN108248878A (en) * | 2018-01-22 | 2018-07-06 | 深圳达芬奇创新科技有限公司 | A kind of unmanned plane Master Control Center device mechanically automatically controlled |
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| CN108773478A (en) * | 2018-04-20 | 2018-11-09 | 河南机电职业学院 | A kind of industry park aerial device |
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| CN108839794A (en) * | 2018-06-01 | 2018-11-20 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of perfect heat-dissipating |
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Effective date of registration: 20191111 Address after: 327118 Zhejiang Hengdian film and Television Industry Experimental Zone, Dongyang City, Jinhua City, Zhejiang Province c7-005-b Applicant after: Guangxia Media Co., Ltd Address before: 518000 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A Applicant before: Shenzhen lightlink Guangtong Technology Co. Ltd |
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