CN107284670A - A kind of Intelligent unattended machine for being used to pour with shock-absorbing function - Google Patents
A kind of Intelligent unattended machine for being used to pour with shock-absorbing function Download PDFInfo
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- CN107284670A CN107284670A CN201710415585.7A CN201710415585A CN107284670A CN 107284670 A CN107284670 A CN 107284670A CN 201710415585 A CN201710415585 A CN 201710415585A CN 107284670 A CN107284670 A CN 107284670A
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- Prior art keywords
- buffer
- shock
- module
- absorbing function
- control module
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- 239000000872 buffer Substances 0.000 claims abstract description 102
- 230000007246 mechanism Effects 0.000 claims abstract description 52
- 238000002347 injection Methods 0.000 claims abstract description 12
- 239000007924 injection Substances 0.000 claims abstract description 12
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 13
- 230000003028 elevating effect Effects 0.000 claims description 12
- 238000004891 communication Methods 0.000 claims description 7
- 230000003139 buffering effect Effects 0.000 claims description 5
- 238000000465 moulding Methods 0.000 claims 1
- 230000006870 function Effects 0.000 description 18
- 238000000034 method Methods 0.000 description 8
- 239000003990 capacitor Substances 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 238000013016 damping Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000001914 filtration Methods 0.000 description 4
- 238000012544 monitoring process Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000009194 climbing Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 230000010415 tropism Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 239000006173 Good's buffer Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 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
- 239000000203 mixture Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Classifications
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- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G25/00—Watering gardens, fields, sports grounds or the like
- A01G25/09—Watering arrangements making use of movable installations on wheels or the like
-
- 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
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Pest Control & Pesticides (AREA)
- Water Supply & Treatment (AREA)
- Environmental Sciences (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of Intelligent unattended machine for being used to pour with shock-absorbing function, including body, generating mechanism, aviation mechanism, Zhong Kong mechanisms, pour the gentle punch mechanism of mechanism, buffer gear includes buffer ferrule, first Buffer Unit and the second Buffer Unit, second Buffer Unit includes fixed sleeving, connecting tube, airway tube and two the second buffer cells, second buffer cell includes housing, air guide storehouse and two air injection units, air injection unit includes jet pipe, breather pipe, hold-down support and cover plate, working power module includes working power circuit, this has in the Intelligent unattended machine for being used to pour of shock-absorbing function, pass through buffer gear, the reliable and secure land of unmanned plane can be realized, moreover, pass through working power circuit, reliable filter function can be realized, improve the reliability of output voltage, also reduce cost, improve the practical value of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of Intelligent unattended machine for being used to pour with shock-absorbing function.
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, it is for carrying out agriculture pouring, but, it is necessary to enter line frequency during pouring to have part
Numerous land, but be due to that unmanned plane lacks good buffer structure, thus easily cause the component of the inside of unmanned plane because
It is damaged for vibration, reduces the reliability of unmanned plane；Moreover, in the inside of unmanned plane, working power circuit, by
In lacking good filtering function, the job insecurity of unmanned plane is allowed for, the reliability of unmanned plane is reduced.
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 that there is shock-absorbing function there is provided one kind
Be used for pour Intelligent unattended machine.
The technical solution adopted for the present invention to solve the technical problems is：A kind of intelligence for being used to pour with shock-absorbing function
Can unmanned plane, including body, be arranged on above body generating mechanism, be arranged on the aviation mechanism of body both sides, be arranged on machine
Zhong Kong mechanisms, the pouring mechanism being arranged on below body and the buffer gear being arranged on below body on body, the generator
Structure, aviation mechanism and pouring mechanism are electrically connected with Zhong Kong mechanisms；
Wherein, generating mechanism, for converting solar energy into electric energy, improves the endurance of unmanned plane；Aviation mechanism,
For realizing the reliable flight of unmanned plane；Zhong Kong mechanisms, for carrying out reliable intelligentized control method to unmanned plane, improve nobody
The reliability of machine；Mechanism is poured, for being poured to specified region, the reliability of unmanned plane is improved；Buffer gear, is used
To realize the reliable land of unmanned plane.
The buffer gear includes buffer ferrule, the first Buffer Unit and the second Buffer Unit, and the buffer ferrule is vertical
The lower section of body is arranged on, the lower end of the buffer ferrule is provided with opening, and first Buffer Unit is arranged on buffer ferrule
Lower section, second Buffer Unit is arranged on buffer ferrule, and the inside of first Buffer Unit and buffer ferrule is provided with sky
Gas storehouse, second Buffer Unit is connected with air bin；
Second Buffer Unit includes being set in the fixed sleeving of buffer ferrule periphery, connecting tube, airway tube and two
Second buffer cell, the airway tube is arranged on the inside of fixed sleeving and connected by connecting tube with air bin, two second
Buffer cell is separately positioned on the two ends of fixed sleeving and connected with airway tube；
Second buffer cell includes housing, air guide storehouse and two air injection units, and the air guide storehouse is arranged on housing
Inside, the air guide storehouse is connected with airway tube, and the air guide storehouse is connected with air injection unit；
The air injection unit includes jet pipe, breather pipe, hold-down support and cover plate, and the air guiding layer passes through breather pipe and jet pipe
Connection, the hold-down support is arranged on the side of the connectivity part of jet pipe and breather pipe, and the cover plate is arranged on jet pipe and breather pipe
Connectivity part and be hinged with hold-down support；
Wherein, the first Buffer Unit will be oppressed the air bin inside buffer ferrule during lifting.With
The air inside air bin will enter the inside of airway tube by connecting tube afterwards, and subsequent air enters air guide from airway tube
In storehouse, the cover plate for being now placed in lower section will be blown open, be sprayed in the jet pipe that subsequent air will be from below, to the drop of unmanned plane
Fall and form damping action, subsequent unmanned plane can rise again, the cover plate for being subsequently positioned at lower section is covered, and cover plate above will
It is opened, air will enter from the jet pipe of top, the rise to unmanned plane forms damping action, so as to reduce nobody
Frequent vibrations of the machine in descent, 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 pouring control 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 signal receiver is additionally provided with the body；
The working power module includes working power circuit, and the working power circuit includes the first triode, second
Triode, the first electric capacity, the second electric capacity and resistance, the colelctor electrode of first triode and the colelctor electrode of the second triode connect
Connect, the colelctor electrode of first triode is connected by first resistor with the base stage of the second triode, second triode
Base stage by the first capacity earth, the emitter stage of first triode by the second capacity earth, second triode
Emitter stage is connected with the base stage of the first triode.
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；Control module is poured, for realizing the module of pouring, herein, by being controlled to gondola water faucet, is realized to referring to
Fixed region is poured；Motor control module, the module worked for controlled motor, herein, by entering to the first motor
Row control, realizes the flight of unmanned plane, by controlling the work of the second motor, realizes all tropisms control to gondola water faucet, carries
The high scope poured；Wireless communication module, for realizing the module of wireless telecommunications, herein, by with external communication terminal
Long distance wireless data transfer is carried out, realizes and remote monitoring is carried out to the information of unmanned plane, realize the intellectuality of unmanned plane；Language
Sound reminding module, for carrying out the module of voice message, herein, by being controlled to loudspeaker, so as to correlation
Alarm play；Display control module, for realizing the module of display control, herein, by being carried out to display interface
Control, can in real time be shown to the job information of unmanned plane, improve the practicality of unmanned plane；Key control module, is used
To carry out the module by key control, herein, it is acquired by the manipulation information to control button, so as to unmanned plane
Carry out implementing scene manipulation, improve the operability of unmanned plane；State indicator module, for realizing the module of state instruction,
Herein, by the bright dark control to status indicator lamp, the working condition of unmanned plane can in real time be shown, improves it
Practicality；Working power module, for providing the module of stabilized supply voltage, herein, for each inside unmanned plane
Module provides stable operating voltage, improves the reliability of unmanned plane.
Wherein, the circuit is electronic filter, and the effect of the first electric capacity is filtering.The same multiple tube of actually the first electric capacity
(being made up of the first triode and the second triode) constitutes an electronic filter.The advantage of so connection is to use less electric capacity
Device can reach preferable filter effect.Because connecing a small capacitor on the second transistor base equivalent to the transmitting at it
It is its several times large capacitor that pole, which connects one, so as to not only realize reliable filter function, while also reducing cost, is improved
The practical value of unmanned plane.
Specifically, first Buffer Unit includes buffer bar, spring, elevating lever and buffer stopper, the one of the buffer bar
End is positioned at the inside of buffer ferrule, and the other end of the buffer bar is provided with groove, the top of the elevating lever by spring with it is recessed
The top connection of groove, the buffer stopper is arranged on the bottom of elevating lever.
Wherein, when unmanned plane land, it will be supported first by buffer stopper, then by elevating lever in buffering
The inside grooves movement of bar, row buffering is entered by spring, it is achieved thereby that the primary to unmanned plane is buffered.
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, the first 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, and the aviation mechanism includes support bar, the first motor and some blades, and the support bar is arranged on
The side of body, first motor is arranged on the top of support bar, and first motor is connected with each blade, and described the
One motor is electrically connected with motor control module.
Specifically, the second motor is by controlling the rotation of gondola water faucet, realize that to need the region poured to carry out lower section reliable
Pour, the pouring mechanism includes gondola water faucet and the second motor, second motor is arranged on the inside of body and is driven with gondola water faucet
Connection, second motor is electrically connected with motor control module.
Specifically, being additionally provided with display interface on the body, the display interface is electrically connected with display control module.
Specifically, being additionally provided with status indicator lamp on the body, the status indicator lamp is electrically connected with state indicator module.
Specifically, being additionally provided with loudspeaker on the body, the loudspeaker is electrically connected with voice cue module.
Specifically, being additionally provided with control button on the body, the control button is electrically connected with key control module.
Specifically, the inside of the body is additionally provided with battery, the battery is electrically connected with working power module.
The beneficial effects of the invention are as follows should pass through buffer with the Intelligent unattended machine for being used to pour of shock-absorbing function
Structure, can realize the reliable and secure land of unmanned plane, moreover, by working power circuit, can realize reliable filtering work(
Can, the reliability of output voltage is improved, cost is also reduced, the practical value of unmanned plane is improved.
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 for being used to pour with shock-absorbing function of the present invention；
Fig. 2 is the structural representation of the buffer gear of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention
Figure；
Fig. 3 is that the structure of the second Buffer Unit of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention is shown
It is intended to；
Fig. 4 is the structural representation of the air injection unit of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention
Figure；
Fig. 5 is the structural representation of the Zhong Kong mechanisms of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention
Figure；
Fig. 6 is the systematic schematic diagram of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention；
Fig. 7 is that the circuit of the working power circuit of the Intelligent unattended machine for being used to pour with shock-absorbing function of the present invention is former
Reason figure；
In figure：1. body, 2. Zhong Kong mechanisms, 3. generating mechanisms, 4. aviation mechanisms, 5. signal receivers, 6. pour mechanism,
7. buffer gear, 8. buffer ferrules, 9. second Buffer Units, 10. buffer bars, 11. buffer stoppers, 12. elevating levers, 13. springs,
14. fixed sleeving, 15. connecting tubes, 16. airway tubes, 17. second buffer cells, 18. housings, 19. air guide storehouses, 20. jet pipes, 21.
Breather pipe, 22. hold-down supports, 23. cover plates, 24. panels, 25. display interfaces, 26. control buttons, 27. status indicator lamps, 28.
Loudspeaker, 29. central control modules, 30. pour control module, 31. motor control modules, 32. wireless communication modules, 33. languages
Sound reminding module, 34. display control modules, 35. key control modules, 36. state indicator modules, 37. working power modules,
38. battery, 39. first motors, 40. gondola water faucets, 41. second motors, the triodes of VT1. first, the triodes of VT2. second, C1.
One electric capacity, the electric capacity of C2. second, R1. resistance.
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 shown in Fig. 1-Fig. 7, a kind of Intelligent unattended machine for being used to pour with shock-absorbing function, including body 1, be arranged on
The generating mechanism 3 of the top of body 1, the aviation mechanism 4 for being arranged on the both sides of body 1, the Zhong Kong mechanisms 2 being arranged on body 1, setting
Pouring mechanism 6 and the buffer gear 7 being arranged on below body 1, the generating mechanism 3, the and of aviation mechanism 4 below body 1
Mechanism 6 is poured to electrically connect with Zhong Kong mechanisms 2；
Wherein, generating mechanism 3, for converting solar energy into electric energy, improves the endurance of unmanned plane；Aviation mechanism
4, for realizing the reliable flight of unmanned plane；Zhong Kong mechanisms 2, for carrying out reliable intelligentized control method to unmanned plane, are improved
The reliability of unmanned plane；Mechanism 6 is poured, for being poured to specified region, the reliability of unmanned plane is improved；Buffer
Structure 7, for realizing the reliable land of unmanned plane.
The buffer gear 7 includes buffer ferrule 8, the first Buffer Unit and the second Buffer Unit 9, the buffer ferrule 8
The lower section of body 1 is vertically provided at, the lower end of the buffer ferrule 8 is provided with opening, and first Buffer Unit is arranged on buffering
The lower section of sleeve pipe 8, second Buffer Unit 9 is arranged on buffer ferrule 8, first Buffer Unit and buffer ferrule 8
Inside is provided with air bin, and second Buffer Unit 9 is connected with air bin；
Second Buffer Unit 9 includes fixed sleeving 14, connecting tube 15, the airway tube for being set in the periphery of buffer ferrule 8
16 and two the second buffer cells 17, the airway tube 16 is arranged on the inside of fixed sleeving 14 and by connecting tube 15 and air
Storehouse is connected, and two the second buffer cells 17 are separately positioned on the two ends of fixed sleeving 14 and connected with airway tube 16；
Second buffer cell 17 includes housing 18, air guide storehouse 19 and two air injection units, and the air guide storehouse 19 is set
In the inside of housing 18, the air guide storehouse 19 is connected with airway tube 16, and the air guide storehouse 19 is connected with air injection unit；
The air injection unit includes jet pipe 20, breather pipe 21, hold-down support 22 and cover plate 23, and the air guiding layer passes through ventilation
Pipe 21 is connected with jet pipe 20, and the hold-down support 22 is arranged on the side of the connectivity part of jet pipe 20 and breather pipe 21, the cover plate
23 are arranged on the connectivity part of jet pipe 20 and breather pipe 21 and are hinged with hold-down support 22；
Wherein, the first Buffer Unit will be oppressed the air bin inside buffer ferrule 8 during lifting.
Air inside subsequent air bin will enter the inside of airway tube 16 by connecting tube 15, and subsequent air enters from airway tube 16
Enter into air guide storehouse 19, the cover plate 23 for being now placed in lower section will be blown open, sprayed in the jet pipe 20 that subsequent air will be from below
Go out, the landing to unmanned plane forms damping action, and subsequent unmanned plane can rise again, the cover plate 23 for being subsequently positioned at lower section is covered,
Cover plate 23 above will be opened, and air will enter from the jet pipe 20 of top, and the rise to unmanned plane is formd
Damping action, so as to reduce frequent vibrations of the unmanned plane in descent, improves the reliability of unmanned plane.
The Zhong Kong mechanisms 2 include panel 24 and middle control component, and the middle control component is arranged on the inside of panel 24, described
Middle control component includes central control module 29, the pouring control module 30 being connected with central control module 29, motor control module
31st, wireless communication module 32, voice cue module 33, display control module 34, key control module 35, state indicator module 36
With working power module 37, the central control module 29 is to be additionally provided with signal receiver 5 on PLC, the body 1；
The working power module 37 include working power circuit, the working power circuit include the first triode VT1,
Second triode VT2, the first electric capacity C1, the second electric capacity C2 and resistance R1, the colelctor electrode and the two or three of the first triode VT1
Pole pipe VT2 colelctor electrode connection, the colelctor electrode of the first triode VT1 passes through first resistor R1's and the second triode VT2
Base stage is connected, and the base stage of the second triode VT2 is grounded by the first electric capacity C1, the emitter stage of the first triode VT1
It is grounded by the second electric capacity C2, the emitter stage of the second triode VT2 is connected with the first triode VT1 base stage.
Wherein, central control module 29, for carrying out the module of intelligentized control method to unmanned plane, herein, center control
Module 29 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；Control module 30 is poured, it is herein, real by being controlled to gondola water faucet 40 for realizing the module of pouring
Show and specified region has been poured；Motor control module 31, the module worked for controlled motor, herein, by right
First motor 39 is controlled, and realizes the flight of unmanned plane, by controlling the work of the second motor 41, is realized to gondola water faucet 40
All tropisms control, improve the scope of pouring；Wireless communication module 32, for realizing the module of wireless telecommunications, herein, leads to
Cross and carry out long distance wireless data transfer with external communication terminal, realize and remote monitoring is carried out to the information of unmanned plane, realize
The intellectuality of unmanned plane；Voice cue module 33, for carrying out the module of voice message, herein, by entering to loudspeaker 28
Row control, so as to be played to related alarm；Display control module 34, for realizing the module of display control,
Here, by being controlled to display interface 25, the job information of unmanned plane can in real time be shown, improves unmanned plane
Practicality；Key control module 35, for carrying out the module by key control, herein, passes through the manipulation to control button 26
Information is acquired, and so as to carry out implementing scene manipulation to unmanned plane, improves the operability of unmanned plane；State instruction
Module 36, herein, can be to nobody by the bright dark control to status indicator lamp 27 for realizing the module of state instruction
The working condition of machine is shown in real time, improves its practicality；Working power module 37, 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, the circuit is electronic filter, and the first electric capacity C1 effect is filtering.Actually the first electric capacity C1 is with compound
Manage (being made up of the first triode VT1 and the second triode VT2) and constitute an electronic filter.The advantage of so connection be use compared with
Small capacitor can reach preferable filter effect.Because it is suitable to connect a small capacitor in the second triode VT2 base stages
It is its several times large capacitor to connect one in the emitter stage at it, so that reliable filter function is not only realized, while also dropping
Low cost, improves the practical value of unmanned plane.
Specifically, first Buffer Unit includes buffer bar 10, spring 13, elevating lever 12 and buffer stopper 11, it is described slow
One end of jumper bar 10 is located at the inside of buffer ferrule 8, and the other end of the buffer bar 10 is provided with groove, the top of the elevating lever 12
End is connected by spring 13 with the top of groove, and the buffer stopper 11 is arranged on the bottom of elevating lever 12.
Wherein, when unmanned plane land, it will be supported first by buffer stopper 11, then exist by elevating lever 12
The inside grooves movement of buffer bar 10, row buffering is entered by spring 13, it is achieved thereby that the primary to unmanned plane is buffered.
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 29.
Specifically, the first motor 39 can be realized by controlling the rotation of each blade and produce power of climbing to body 1, so that
Unmanned plane can be controlled to be flown, the aviation mechanism 4 includes support bar, the first motor 39 and some blades, the support
Bar is arranged on the side of body 1, and first motor 39 is arranged on the top of support bar, and first motor 39 is passed with each blade
Dynamic connection, first motor 39 is electrically connected with motor control module 31.
Specifically, the second motor 41 is by controlling the rotation of gondola water faucet 40, realizing needs the region poured to carry out lower section
Reliable to pour, the pouring mechanism 6 includes the motor 41 of gondola water faucet 40 and second, and second motor 41 is arranged on the inside of body 1
And be connected with gondola water faucet 40, second motor 41 is electrically connected with motor control module 31.
Specifically, being additionally provided with display interface 25 on the body 1, the display interface 25 is electrically connected with display control module 34
Connect.
Specifically, status indicator lamp 27 is additionally provided with the body 1, the status indicator lamp 27 and state indicator module 36
Electrical connection.
Specifically, being additionally provided with loudspeaker 28 on the body 1, the loudspeaker 28 is electrically connected with voice cue module 33.
Specifically, being additionally provided with control button 26 on the body 1, the control button 26 is electrically connected with key control module 35
Connect.
Specifically, the inside of the body 1 is additionally provided with battery 38, the battery 38 is electrically connected with working power module 37
Connect.
Compared with prior art, should have in the Intelligent unattended machine for being used to pour of shock-absorbing function, by buffer gear 7,
The reliable and secure land of unmanned plane can be realized, moreover, by working power circuit, reliable filter function can be realized,
The reliability of output voltage is improved, cost is also reduced, the practical value of unmanned plane is improved.
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 for being used to pour with shock-absorbing function, it is characterised in that including body, be arranged on body
Side generating mechanism, be arranged on the aviation mechanism of body both sides, be arranged on body Zhong Kong mechanisms, be arranged on below body
Pour mechanism and the buffer gear that is arranged on below body, the generating mechanism, aviation mechanism and pour mechanism with middle control machine
Structure is electrically connected；
The buffer gear includes buffer ferrule, the first Buffer Unit and the second Buffer Unit, and the buffer ferrule is vertically arranged
In the lower section of body, the lower end of the buffer ferrule is provided with opening, and first Buffer Unit is arranged on the lower section of buffer ferrule,
Second Buffer Unit is arranged on buffer ferrule, and the inside of first Buffer Unit and buffer ferrule is provided with air bin,
Second Buffer Unit is connected with air bin；
Second Buffer Unit includes being set in the fixed sleeving of buffer ferrule periphery, connecting tube, airway tube and two second
Buffer cell, the airway tube is arranged on the inside of fixed sleeving and connected by connecting tube with air bin, two second bufferings
Unit is separately positioned on the two ends of fixed sleeving and connected with airway tube；
Second buffer cell includes housing, air guide storehouse and two air injection units, and the air guide storehouse is arranged on the inside of housing,
The air guide storehouse is connected with airway tube, and the air guide storehouse is connected with air injection unit；
The air injection unit includes jet pipe, breather pipe, hold-down support and cover plate, and the air guiding layer is connected by breather pipe and jet pipe
Logical, the hold-down support is arranged on the side of the connectivity part of jet pipe and breather pipe, and the cover plate is arranged on jet pipe and breather pipe
Connectivity part and it is hinged with hold-down support；
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 pouring control 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 to be additionally provided with signal receiver on PLC, the body；
The working power module includes working power circuit, and the working power circuit includes the first triode, the two or three pole
Pipe, the first electric capacity, the second electric capacity and resistance, the colelctor electrode of first triode are connected with the colelctor electrode of the second triode, institute
The colelctor electrode for stating the first triode is connected by first resistor with the base stage of the second triode, and the base stage of second triode is led to
The first capacity earth is crossed, the emitter stage of first triode passes through the second capacity earth, the emitter stage of second triode
It is connected with the base stage of the first triode.
2. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that described first
Buffer Unit includes buffer bar, spring, elevating lever and buffer stopper, and one end of the buffer bar is located at the inside of buffer ferrule, institute
The other end for stating buffer bar is provided with groove, and the top of the elevating lever is connected by the top of spring and groove, the buffer stopper
It is arranged on the bottom of elevating lever.
3. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the generating
Mechanism includes solar panel, and the solar panel is electrically connected with central control module.
4. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the flight
Mechanism includes support bar, the first motor and some blades, and the support bar is arranged on the side of body, and first motor is set
On the top of support bar, first motor is connected with each blade, and first motor is electrically connected with motor control module.
5. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the pouring
Mechanism includes gondola water faucet and the second motor, and second motor is arranged on the inside of body and is connected with gondola water faucet, and described second
Motor is electrically connected with motor control module.
6. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the body
On be additionally provided with display interface, the display interface is electrically connected with display control module.
7. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the body
On be additionally provided with status indicator lamp, the status indicator lamp is electrically connected with state indicator module.
8. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the body
On be additionally provided with loudspeaker, the loudspeaker is electrically connected with voice cue module.
9. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the body
On be additionally provided with control button, the control button is electrically connected with key control module.
10. it is used for the Intelligent unattended machine of pouring with shock-absorbing function as claimed in claim 1, it is characterised in that the machine
The inside of body is additionally provided with battery, and the battery is electrically connected with working power module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710415585.7A CN107284670A (en) | 2017-06-05 | 2017-06-05 | A kind of Intelligent unattended machine for being used to pour with shock-absorbing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710415585.7A CN107284670A (en) | 2017-06-05 | 2017-06-05 | A kind of Intelligent unattended machine for being used to pour with shock-absorbing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107284670A true CN107284670A (en) | 2017-10-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710415585.7A Pending CN107284670A (en) | 2017-06-05 | 2017-06-05 | A kind of Intelligent unattended machine for being used to pour with shock-absorbing function |
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| CN (1) | CN107284670A (en) |
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| JP5890569B1 (en) * | 2015-08-12 | 2016-03-22 | ヒロボー株式会社 | Multi-rotor type helicopter and method of spraying medicine using the same |
| CN105836115A (en) * | 2016-04-12 | 2016-08-10 | 张萍 | Safe and reliable intelligent unmanned aerial vehicle based on internet of things |
| CN106043701A (en) * | 2016-06-15 | 2016-10-26 | 张萍 | Novel agricultural irrigation unmanned aerial vehicle based on Internet of Things |
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Application publication date: 20171024 |
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