CN107667746B - Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform - Google Patents
Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform Download PDFInfo
- Publication number
- CN107667746B CN107667746B CN201610619602.4A CN201610619602A CN107667746B CN 107667746 B CN107667746 B CN 107667746B CN 201610619602 A CN201610619602 A CN 201610619602A CN 107667746 B CN107667746 B CN 107667746B
- Authority
- CN
- China
- Prior art keywords
- platform
- cable
- straight
- automatic
- cloud layer
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims abstract description 26
- 230000005611 electricity Effects 0.000 claims abstract description 29
- 238000012544 monitoring process Methods 0.000 claims abstract description 22
- 238000004891 communication Methods 0.000 claims abstract description 7
- 239000003795 chemical substances by application Substances 0.000 claims description 47
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 40
- 239000002245 particle Substances 0.000 claims description 39
- 150000003839 salts Chemical class 0.000 claims description 34
- 239000012267 brine Substances 0.000 claims description 27
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 claims description 27
- 239000007788 liquid Substances 0.000 claims description 20
- 229910052757 nitrogen Inorganic materials 0.000 claims description 20
- 239000007921 spray Substances 0.000 claims description 13
- 238000003860 storage Methods 0.000 claims description 11
- 239000003990 capacitor Substances 0.000 claims description 10
- 238000001704 evaporation Methods 0.000 claims description 10
- 230000008020 evaporation Effects 0.000 claims description 10
- 238000009423 ventilation Methods 0.000 claims description 10
- JKFYKCYQEWQPTM-UHFFFAOYSA-N 2-azaniumyl-2-(4-fluorophenyl)acetate Chemical compound OC(=O)C(N)C1=CC=C(F)C=C1 JKFYKCYQEWQPTM-UHFFFAOYSA-N 0.000 claims description 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 5
- 229910021612 Silver iodide Inorganic materials 0.000 claims description 5
- 235000011089 carbon dioxide Nutrition 0.000 claims description 5
- 238000010612 desalination reaction Methods 0.000 claims description 5
- 229940045105 silver iodide Drugs 0.000 claims description 5
- 238000001223 reverse osmosis Methods 0.000 claims description 4
- 230000008901 benefit Effects 0.000 abstract description 14
- 230000000694 effects Effects 0.000 abstract description 12
- WCUXLLCKKVVCTQ-UHFFFAOYSA-M Potassium chloride Chemical compound [Cl-].[K+] WCUXLLCKKVVCTQ-UHFFFAOYSA-M 0.000 description 59
- 239000001103 potassium chloride Substances 0.000 description 35
- 235000011164 potassium chloride Nutrition 0.000 description 35
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 34
- 238000005457 optimization Methods 0.000 description 16
- XSQUKJJJFZCRTK-UHFFFAOYSA-N Urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 description 12
- 239000004202 carbamide Substances 0.000 description 12
- 230000010165 autogamy Effects 0.000 description 8
- 238000005516 engineering process Methods 0.000 description 7
- 239000007787 solid Substances 0.000 description 5
- 241001347978 Major minor Species 0.000 description 4
- 229910002651 NO3 Inorganic materials 0.000 description 4
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 4
- QAOWNCQODCNURD-UHFFFAOYSA-L Sulfate Chemical compound [O-]S([O-])(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-L 0.000 description 4
- 230000009471 action Effects 0.000 description 4
- 239000007864 aqueous solution Substances 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 4
- 239000000428 dust Substances 0.000 description 4
- 210000001161 mammalian embryo Anatomy 0.000 description 4
- 230000013011 mating Effects 0.000 description 4
- 230000009347 mechanical transmission Effects 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 238000009331 sowing Methods 0.000 description 4
- 238000005728 strengthening Methods 0.000 description 4
- 239000000725 suspension Substances 0.000 description 4
- 241000255925 Diptera Species 0.000 description 3
- 238000001179 sorption measurement Methods 0.000 description 3
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- UXVMQQNJUSDDNG-UHFFFAOYSA-L Calcium chloride Chemical compound [Cl-].[Cl-].[Ca+2] UXVMQQNJUSDDNG-UHFFFAOYSA-L 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000001110 calcium chloride Substances 0.000 description 2
- 229910001628 calcium chloride Inorganic materials 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 239000003673 groundwater Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000013535 sea water Substances 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- 239000002351 wastewater Substances 0.000 description 2
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005660 chlorination reaction Methods 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 238000009738 saturating Methods 0.000 description 1
- 239000010865 sewage Substances 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000002352 surface water Substances 0.000 description 1
Classifications
-
- 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
- A01G15/00—Devices or methods for influencing weather conditions
Landscapes
- Life Sciences & Earth Sciences (AREA)
- Atmospheric Sciences (AREA)
- Environmental Sciences (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform are supported the present invention relates to a kind of smart grid, it is at high cost to solve the prior art, rainfall effect and problem of poor benefits, it is to be powered with cable with multiple electronic lifting rotors and electronic steady position rotor, platform bearer of going straight up to intelligent controller sends out the intelligent navigation rotor wing unmanned aerial vehicle for increasing rain agent, the cloud layer observation radar guide configured with platform configuration or ground goes straight up to platform lift-off height and rotor wing unmanned aerial vehicle flight path is guided to carry out precisely sending out operation to target cloud, intelligent controller connects ground monitoring control centre by wireless or wired and wireless spare communication modes, the smart grid supply station of low ebb Electricity Functional is saved to going straight up to platform and cloud layer observation radar and the power supply of ground monitoring control centre with having.It is at low cost, precision is high, rainfall effect and profitable advantage with can be applicable in thin layer and scattered cloud.
Description
Technical field
The present invention relates to a kind of rain making methods, and the essence for having cable to go straight up to platform is supported more particularly to a kind of smart grid
Quasi- high-efficiency artificial rainfall method and system.
Background technique
With global air temperature warming, ground temperature is necessarily also increased, land moisture evaporation intensity increases therewith, soil water storage
Ability can also die down therewith, the also inevitable corresponding aggravation of nature water shortage caused by air temperature warming.Meanwhile pushing away with urbanization process
Into crowd of flood tide under the conditions of life in the countryside is switched to need the great urban life of water by the life in the countryside mode for needing water electrode few
Mode, as went to the toilet originally in the people of life in the countryside do not need to wash by water, move to go to the toilet behind city if need using flushing toiler,
Can pass through after original life in the countryside discharge discharge of wastewater stratigraphic filtration recharge groundwater, move to the waste water being discharged behind city can only
River is arranged by city and is discharged into sea, after rainfall can seep recharge groundwater, migration by the way that exposed earth's surface is naturally lower in original village
The rainfall of urban community is because that can not blend down the river course for sewage discharge that cannot can only drain off floodwaters by city with regard to underground infiltration filtration, purification, precipitation
It is discharged into sea etc., keeps water shortage even more serious.It solves water shortage problem and there was only two roads, first is that increasing income, second is that throttling.Water-saving is one
A complicated, progressive system engineering, does not have remarkable result in short-term, the method for really being able to solve water shortage problem in time
Only increase income.Strange land water-transferring cost is high, water diversion volume is very limited, is far from satisfying needs;Sea water desalination is at high cost, economically
It is infeasible.It is not limited by surface water resources although worker increases drop, it is inexhaustible, it is inexhaustible.But rocket therein or big gun benefit
It is sowed with shell and increases rain agent, transmitting ammunition is at high cost, shell case generally requires to recycle, and increasing rain area is very limited, to cloud layer requirement
Height, rainfall agent utilization rate is low, rainfall effect is poor, far can not obtain popularity application;Aircraft seeding therein increases rain agent, though
So to cloud layer require it is low, rainfall effect is good, still because with high costs, only do not need meter cost few special circumstances
Under can use.
Northwest plateau in extremely arid desert and drought, day can also sail often rich in supersaturated vapor in the air
Cloud, especially some long-term arid areas, due to special Geography And Land Features and climate reasons, although often thering is cloud layer to float
It crosses, but is extremely difficult to rainfall occur.Because cloud layer area and thickness are small, can not be increased with the existing rocket gun for being applicable in big spissatus layer rain by
Poor in precision, rainfall effect is poor, can not use, existing aircraft send out increase rain due to single flight operating cost is too high,
Rainfall is very little, and cost-effectiveness is too poor, can not be applicable in.Therefore, be badly in need of it is a kind of thin layer and scattered cloud can be carried out it is low at
The rainfall new technology of this accurate efficiently artificial rain operation.
Summary of the invention
Present invention aims to overcome that the drawbacks described above of the prior art, provide it is a kind of can be applicable in thin layer and scattered cloud,
Smart grid at low cost, rainfall effect is good supports the accurate high-efficiency artificial rainfall method for having cable to go straight up to platform, the object of the invention
The system provided for realizing the method is be provided.
To achieve the above object, smart grid of the present invention supports the accurate high-efficiency artificial rainfall method for having cable to go straight up to platform to use
Cable power supply sends out increasing rain with multiple electronic lifting rotors and electronic steady position rotor, the platform bearer of going straight up to intelligent controller
Platform lift-off height is gone straight up in the intelligent navigation rotor wing unmanned aerial vehicle of agent, the cloud layer observation radar guide configured with platform configuration or ground
With guide rotor wing unmanned aerial vehicle flight path to carry out precisely sending out operation to target cloud, intelligent controller by wireless or wired and
Wireless spare communication modes connect ground monitoring control centre, with having the smart grid supply station of saving low ebb Electricity Functional to straight
Peaceful and cloud layer observation radar and the power supply of ground monitoring control centre.Platform configuration rises to above cloud layer going straight up to platform
It is lower to go straight up to platform depending on cloud layer observation radar or configuration and rise to upper view cloud layer observation radar below cloud layer, it is regarded in the configuration of ground
Cloud layer observation radar.Power supply mode with the smart grid supply station for saving low ebb Electricity Functional can significantly reduce power cost.
It goes straight up to platform liter and provides launching platform in outage to send out the intelligent navigation rotor wing unmanned aerial vehicle of increasing rain agent, unmanned plane can be significantly improved
Load, significant decrease send out cost, dramatically increase unmanned plane voyage, improve in amplitude and increase rain workload, significantly improve and increase rain warp
Ji benefit.Especially rotor wing unmanned aerial vehicle carries out sending out operation, can significantly increase and send out density and intensity, significantly improves cloud layer water
The rainfall efficiency of vapour, the cloud small for thin layer, area also can be by precisely sending out realization effective rainfall, this is any existing
There is increasing rain technology irrealizable.Therefore, thin layer and scattered cloud can be applicable in by having, at low cost, precision is high, rainfall effect
With profitable advantage.
As optimization, the platform of going straight up to is furnished with the super capacitor electric power storage standby electricity enabled automatically in cable power supply trouble
Source or the super capacitor electric power storage backup power source enabled automatically in cable power supply trouble and for reducing forced landing power consumption emergency
Parachute;With cloud layer observation radar go straight up to platform forced landing when, close synchronously cloud layer observation radar.The platform of going straight up to rises to
Above cloud layer, cloud layer is observed using its autogamy cloud layer observation radar from top to bottom, guides unmanned machine operation;Or it is described
It goes straight up to platform to rise to below cloud layer, cloud layer is observed using its autogamy cloud layer observation radar from bottom to top, guides nobody
Machine operation.
It is automatic as needed to disconnect the connection for going straight up to platform and cable of powering or automatic disconnect when forced landing as optimization
The connection on ground and power supply cable;After closing cloud layer observation radar, the global position system matched by intelligent controller guides forced landing
Path.
As optimization, the automatic coupler connection supply lines going straight up to platform base center and being controlled by intelligent controller
Cable, the automatic cable hoist engine or automatic spiral fashion retractable cable cable of the control of smart grid supply station configuration monitoring control centre
Machine;Intelligent navigation rotor wing unmanned aerial vehicle is furnished with cloud layer Image Acquisition identification device, according to cloud when intelligent navigation rotor wing unmanned aerial vehicle operation
The accurate navigation of tomographic image acquisition identification data progress increases rain agent and sends out.Automatic coupler includes before going straight up to platform base center configuration
The lock tongue end of the major-minor electric lock interlocked afterwards, main electric lock connects electricity directly or by mechanical transmission mechanism connection configuration is indented
Socket, cable upper end configure the mating with the electrical connector socket of connect plug, and secondary electric lock lock tongue suspension cable upper end is solid
The cable hanging ring matched, when needing to disconnect cable, the lock tongue and electrical connector socket of main electric lock are inside contracted, due to the limit of the electronic lock body of master
Position is detached from connect plug with electrical connector socket from inside contracting with electrical connector socket, after main electric lock completes above-mentioned movement, lock tongue
The electric switch for touching secondary electric lock starts secondary electric lock, makes the lock tongue internal lock of secondary electric lock, due to the limit of secondary electric lock body
Position, cable hanging ring cannot be moved together therewith, so that cable hanging ring be made to lose the support of secondary electric lock lock tongue, and be fallen off, thus
Realize automatically disengaging for cable.
As optimization, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are configured with cable electronic tensile
Meter, it is described go straight up to platform base center according to ground and aerial platform measure and release in real time length of cable and platform lift-off highly
Upper limit tension and lower limit tension that cable is born are calculated in real time, when the cable strain that cable electronic tensile measures is greater than the upper limit
Power and be less than lower limit tension when, go straight up to automatic cable hoist engine described in the real-time control of platform base center or automatic spiral fashion receipts
It puts cable machine and carries out unwrapping wire and take-up.The automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are packed in a water
The Pressure turntable of flat configuration, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine can be according to cables to aerial
The real-time adjust automatically direction of the angle of drawing, being in automatic cable hoist engine or automatic spiral fashion retractable cable cable machine always has
Conducive to the orientation of unwrapping wire and take-up.
As optimization, the rainfall agent includes silver iodide, dry ice, liquid nitrogen, salt or potassium chloride particle;Smart grid power supply
The liquid nitrogen device for making driven of standing fills liquid nitrogen to the rotor wing unmanned aerial vehicle for sowing liquid nitrogen rainfall agent;The driving of smart grid supply station
Reverse osmosis desalination device produces strong brine, and strong brine produces salt particle by spray evaporation device.Smart grid power supply
Station is also equipped with steam-electric power plant and wind power plant.Potassium chloride particle is that potassium chloride fortified aqueous is filled by spray evaporation
It sets and produces salt particle.Certain rainfall agent can also be other insoluble but can be water-moistened particle such as dust, can be
The rainfall agent of its adsorption steam generation drop embryo;Be also possible to other soluble-salt particles, as sulfate, nitrate,
Calcium chloride etc..
As optimization, it is described produce salt or potassium chloride particle be setting one middle and lower part have the reversed louvre type of multilayer from
The up-thin-low-thick perpendicular conical tube type high tower of right ventilation opening, sprays the strong brine or dense into tower using micro-nozzle at the top of high tower
Sylvite water, because of the salt or potassium chloride particle that moisture evaporates and is formed during tower bottom is collected and declined, the outer wall of high tower exists
The top and two sides of reversed louvre type natural ventilation port are configured with the rain shade for rain cover;The reversed blind window is can
The blind window for the reverse configuration for passing freely through natural wind, and salt or potassium chloride particle capable of being stopped to outflow.The strong brine or
Dense sylvite water can be blended into urea, strong brine by aqueous solution of urea or brackish water replacement or the strong brine or brackish water
Or the weight ratio of salt and urea preferred 90-99: 10-0.1 in dense sylvite water, more preferable 95-99: 5-1, more specifically 90 kilograms:
10 kilograms, 95 kilograms: 5 kilograms, 97 kilograms: 3 kilograms, 99 kilograms: 1 kilograms, 99.2 kilograms: 0.8 kilograms, 99.5 kilograms: 0.5 public affairs
Jin, 99.7 kilograms: 0.3 kilograms, 99.9 kilograms: 0.1 kilograms.
As optimization, square or circle go straight up to platform quadrangle and are respectively furnished with the equally distributed electricity of circumferential direction by horizontal semi-girder
Dynamic vertical pivot lifting rotor or spindle go straight up to platform both ends and respectively configure a symmetrical electronic vertical pivot liter by horizontal semi-girder
Power rotor, goes straight up to and configures undercarriage below platform, goes straight up to and configures at least one below platform for resisting the electronic of crosswind force
The steady position rotor of horizontal axis, go straight up to above platform by intelligent controller control automatic locking device configure more side by side send out increase rain agent
Intelligent navigation rotor wing unmanned aerial vehicle.The undercarriage is that square or circle go straight up to and be respectively fixedly mounted with a foundation below platform quadrangle with slow
The supporting leg of foot is rushed, is connected between each supporting leg by transversely strengthening bar.The undercarriage is that spindle is gone straight up to below platform two sides
It is each to be fixedly mounted with the undercarriage being parallel to each other downwards.It goes straight up to center below platform and is fixedly mounted with a line standpipe excessively downwards, cross line standpipe
Lower end is fixedly mounted with the automatic coupler of cable, and automatic coupler, which connects up, goes straight up to platform power line, connects power cable downwards, needs
Automatic coupler can disconnect power cable automatically when wanting, and keep power cable automatically born, to reduce platform load and make platform
It can not be restrained by cable, realize most energy-efficient emergency forced landing or downlink.It crosses periphery in the middle part of line standpipe and passes through two-way pressure turntable
It is fixedly mounted with the horizontal spindle bracket of the steady position rotor of electronic horizontal axis, one end of spindle bracket configures the steady position rotor of electronic horizontal axis, another
End is fixedly mounted with guiding empennage.Under the action of being oriented to empennage, rotate the steady position rotor of electronic horizontal axis windward always to overcome wind to flat
The displacement force that platform applies.It can certainly be: cross line standpipe middle part periphery by two-way pressure turntable and be directly fixedly mounted with electronic horizontal axis
Steady position rotor, goes straight up to platform configuration electronics anemoscope, and the periphery rotating part configuration of Pressure turntable is manipulated by the electronics anemoscope
Make the automatic control rotation drive device of the steady position rotor of electronic horizontal axis always windward.Automatic control rotation drive device is the periphery of Pressure turntable
Rotation portion is fixedly mounted with an outer gear ring upwards, crosses line standpipe or goes straight up to and is fixedly mounted with a stepping decelerating motor below platform, and stepping is slowed down electricity
The output shaft of machine is fixedly mounted with the driving gear engaged with outer gear ring.A pair of of position sensing is at least configured between outer gear ring and excessively line standpipe
Device, electronics anemoscope and position sensor pass through the positive and negative rotation amount and start and stop of intelligent device real-time control stepping decelerating motor, make electricity
The dynamic steady position rotor of horizontal axis is always windward.The platform edges of going straight up to of horizontal semi-girder base portion or horizontal semi-girder base portion are fixed with for stopping electricity
What dynamic vertical pivot lifting rotor generated blows to the arc wind board for going straight up to the beam wind of platform.
Electronic vertical pivot lifting rotor uses fixing axle, can significantly improve lift, and significantly simplify structure, itself matter
Amount, significantly improves payload.Square or circle, which go straight up to platform quadrangle and be respectively furnished with a circumferential direction by horizontal semi-girder, to be uniformly distributed
Electronic vertical pivot lifting rotor when, if a wherein electronic vertical pivot lifting rotor failure, can simultaneously close off symmetrical therewith
Another electronic vertical pivot lifting rotor, so that balance of wrestling, guarantees that platform does not rotate.So to guarantee mesa corners dynamic balance, institute
It all must be opposite with symmetrical electronic vertical pivot lifting rotor direction of rotation.
As optimization, the central control room gone straight up to center above platform and be formed with built-in intelligent controller, center control
The parachute automatic releasing device of intelligent controller control is configured above room by vertical supports;Square or circle go straight up to platform
Delta Region respectively configures an intelligent navigation by automatic locking device above platform between adjacent horizontal semi-girder and central control room
Rotor wing unmanned aerial vehicle, spindle are gone straight up to respectively to pass through above platform in the two sides of central control room and straight line where horizontal semi-girder and be locked automatically
Device configures one or more intelligent navigation rotor wing unmanned aerial vehicle;The cloud layer of ground or the rotation of vertical supports configuration level observes thunder
It reaches.After automatic locking device release, intelligent navigation rotor wing unmanned aerial vehicle is from horizontal semi-girder intermediate region along half that central control room is the center of circle
Radial line laterally flies away from platform, and carries out precisely sending out rainfall agent operation, operation to target cloud layer under the guide of cloud layer observation radar
After the completion, the airplane parking area of monitoring control centre is returned in the case where cloud layer observation radar or global position system guide.Vertical supports
Upper end configures the parachute automatic releasing device of intelligent controller control, and vertical supports periphery configures circumferential rotation by Pressure turntable
Rotatable radar antenna.Automatic locking device is gone straight up to configured with intelligently locking above platform, and the undercarriage of rotor wing unmanned aerial vehicle has and intelligence
The lock nose of energy ground lock lock tongue cooperation.
System for realizing the method for the invention includes cable power supply with multiple electronic lifting rotors and electronic steady
Position rotor sends out with intelligent controller, carrying and increases the intelligent navigation rotor wing unmanned aerial vehicle of rain agent and go straight up to platform, with platform configuration or
Ground configuration cloud layer observation radar guide go straight up to platform lift-off height and guide rotor wing unmanned aerial vehicle flight path to target cloud into
Row precisely sends out operation, and intelligent controller is connected in ground monitoring control by wireless or wired and wireless spare communication modes
The heart has and saves the smart grid supply station of low ebb Electricity Functional to going straight up in platform and cloud layer observation radar and ground monitoring control
Heart power supply.Platform configuration go straight up to platform rise to above cloud layer it is lower depending on cloud layer observation radar or configuration go straight up to platform rise
Upper view cloud layer observation radar below to cloud layer, ground configure and regard cloud layer observation radar.With the intelligence for saving low ebb Electricity Functional
The power supply mode of energy power grid supply station can significantly reduce power cost.Go straight up to platform liter outage be send out increase rain agent intelligence lead
The rotor wing unmanned aerial vehicle that navigates provides launching platform, can significantly improve unmanned plane load, and significant decrease sends out cost, dramatically increases unmanned plane
Voyage improves in amplitude and increases rain workload, significantly improves and increases rain economic benefit.Especially rotor wing unmanned aerial vehicle carries out sending out operation,
It can significantly increase and send out density and intensity, significantly improve the rainfall efficiency of cloud layer steam, the cloud small for thin layer, area
Coloured silk, also can be by precisely sending out realization effective rainfall, this is that any existing increasing rain technology is irrealizable.Therefore, having can fit
It is at low cost, precision is high, rainfall effect and profitable advantage with thin layer and scattered cloud.
As optimization, the platform of going straight up to is furnished with the super capacitor electric power storage standby electricity enabled automatically in cable power supply trouble
Source or the super capacitor electric power storage backup power source enabled automatically in cable power supply trouble and for reducing forced landing power consumption emergency
Parachute;With cloud layer observation radar go straight up to platform forced landing when, close synchronously cloud layer observation radar.The platform of going straight up to rises to
Above cloud layer, cloud layer is observed using its autogamy cloud layer observation radar from top to bottom, guides unmanned machine operation;Or it is described
It goes straight up to platform to rise to below cloud layer, cloud layer is observed using its autogamy cloud layer observation radar from bottom to top, guides nobody
Machine operation.
It is automatic as needed to disconnect the connection for going straight up to platform and cable of powering or automatic disconnect when forced landing as optimization
The connection on ground and power supply cable;After closing cloud layer observation radar, the global position system matched by intelligent controller guides forced landing
Path.
As optimization, the automatic coupler connection supply lines going straight up to platform base center and being controlled by intelligent controller
Cable, the automatic cable hoist engine or automatic spiral fashion retractable cable cable of the control of smart grid supply station configuration monitoring control centre
Machine;Intelligent navigation rotor wing unmanned aerial vehicle is furnished with cloud layer Image Acquisition identification device, according to cloud when intelligent navigation rotor wing unmanned aerial vehicle operation
The accurate navigation of tomographic image acquisition identification data progress increases rain agent and sends out.Automatic coupler includes before going straight up to platform base center configuration
The lock tongue end of the major-minor electric lock interlocked afterwards, main electric lock connects electricity directly or by mechanical transmission mechanism connection configuration is indented
Socket, cable upper end configure the mating with the electrical connector socket of connect plug, and secondary electric lock lock tongue suspension cable upper end is solid
The cable hanging ring matched, when needing to disconnect cable, the lock tongue and electrical connector socket of main electric lock are inside contracted, due to the limit of the electronic lock body of master
Position is detached from connect plug with electrical connector socket from inside contracting with electrical connector socket, after main electric lock completes above-mentioned movement, lock tongue
The electric switch for touching secondary electric lock starts secondary electric lock, makes the lock tongue internal lock of secondary electric lock, due to the limit of secondary electric lock body
Position, cable hanging ring cannot be moved together therewith, so that cable hanging ring be made to lose the support of secondary electric lock lock tongue, and be fallen off, thus
Realize automatically disengaging for cable.
As optimization, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are configured with cable electronic tensile
Meter, it is described go straight up to platform base center according to ground and aerial platform measure and release in real time length of cable and platform lift-off highly
Upper limit tension and lower limit tension that cable is born are calculated in real time, when the cable strain that cable electronic tensile measures is greater than the upper limit
Power and be less than lower limit tension when, go straight up to automatic cable hoist engine described in the real-time control of platform base center or automatic spiral fashion receipts
It puts cable machine and carries out unwrapping wire and take-up.The automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are packed in a water
The Pressure turntable of flat configuration, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine can be according to cables to aerial
The real-time adjust automatically direction of the angle of drawing, being in automatic cable hoist engine or automatic spiral fashion retractable cable cable machine always has
Conducive to the orientation of unwrapping wire and take-up.
As optimization, the rainfall agent includes silver iodide, dry ice, liquid nitrogen, salt or potassium chloride particle;Smart grid power supply
The liquid nitrogen device for making driven of standing fills liquid nitrogen to the rotor wing unmanned aerial vehicle for sowing liquid nitrogen rainfall agent;The driving of smart grid supply station
Reverse osmosis desalination device produces strong brine, and strong brine produces salt particle by spray evaporation device.Smart grid power supply
Station is also equipped with steam-electric power plant and wind power plant.Potassium chloride particle is that potassium chloride fortified aqueous is filled by spray evaporation
It sets and produces salt particle.Certain rainfall agent can also be other insoluble but can be water-moistened particle such as dust, can be
The rainfall agent of its adsorption steam generation drop embryo;Be also possible to other soluble-salt particles, as sulfate, nitrate,
Calcium chloride etc..
As optimization, it is described produce salt or potassium chloride particle be setting one middle and lower part have the reversed louvre type of multilayer from
The up-thin-low-thick perpendicular conical tube type high tower of right ventilation opening, sprays the strong brine or dense into tower using micro-nozzle at the top of high tower
Sylvite water, because of the salt or potassium chloride particle that moisture evaporates and is formed during tower bottom is collected and declined, the outer wall of high tower exists
The top and two sides of reversed louvre type natural ventilation port are configured with the rain shade for rain cover;The reversed blind window is can
The blind window for the reverse configuration for passing freely through natural wind, and salt or potassium chloride particle capable of being stopped to outflow.The strong brine or
Dense sylvite water can be blended into urea, strong brine by aqueous solution of urea or brackish water replacement or the strong brine or brackish water
Or the weight ratio of salt and urea preferred 90-99: 10-0.1 in dense sylvite water, more preferable 95-99: 5-1, more specifically 90 kilograms:
10 kilograms, 95 kilograms: 5 kilograms, 97 kilograms: 3 kilograms, 99 kilograms: 1 kilograms, 99.2 kilograms: 0.8 kilograms, 99.5 kilograms: 0.5 public affairs
Jin, 99.7 kilograms: 0.3 kilograms, 99.9 kilograms: 0.1 kilograms.
As optimization, square or circle go straight up to platform quadrangle and are respectively furnished with the equally distributed electricity of circumferential direction by horizontal semi-girder
Dynamic vertical pivot lifting rotor or spindle go straight up to platform both ends and respectively configure a symmetrical electronic vertical pivot liter by horizontal semi-girder
Power rotor, goes straight up to and configures undercarriage below platform, goes straight up to and configures at least one below platform for resisting the electronic of crosswind force
The steady position rotor of horizontal axis, go straight up to above platform by intelligent controller control automatic locking device configure more side by side send out increase rain agent
Intelligent navigation rotor wing unmanned aerial vehicle.The undercarriage is that square or circle go straight up to and be respectively fixedly mounted with a foundation below platform quadrangle with slow
The supporting leg of foot is rushed, is connected between each supporting leg by transversely strengthening bar.The undercarriage is that spindle is gone straight up to below platform two sides
It is each to be fixedly mounted with the undercarriage being parallel to each other downwards.It goes straight up to center below platform and is fixedly mounted with a line standpipe excessively downwards, cross line standpipe
Lower end is fixedly mounted with the automatic coupler of cable, and automatic coupler, which connects up, goes straight up to platform power line, connects power cable downwards, needs
Automatic coupler can disconnect power cable automatically when wanting, and keep power cable automatically born, to reduce platform load and make platform
It can not be restrained by cable, realize most energy-efficient emergency forced landing or downlink.It crosses periphery in the middle part of line standpipe and passes through two-way pressure turntable
It is fixedly mounted with the horizontal spindle bracket of the steady position rotor of electronic horizontal axis, one end of spindle bracket configures the steady position rotor of electronic horizontal axis, another
End is fixedly mounted with guiding empennage.Under the action of being oriented to empennage, rotate the steady position rotor of electronic horizontal axis windward always to overcome wind to flat
The displacement force that platform applies.It can certainly be: cross line standpipe middle part periphery by two-way pressure turntable and be directly fixedly mounted with electronic horizontal axis
Steady position rotor, goes straight up to platform configuration electronics anemoscope, and the periphery rotating part configuration of Pressure turntable is manipulated by the electronics anemoscope
Make the automatic control rotation drive device of the steady position rotor of electronic horizontal axis always windward.Automatic control rotation drive device is the periphery of Pressure turntable
Rotation portion is fixedly mounted with an outer gear ring upwards, crosses line standpipe or goes straight up to and is fixedly mounted with a stepping decelerating motor below platform, and stepping is slowed down electricity
The output shaft of machine is fixedly mounted with the driving gear engaged with outer gear ring.A pair of of position sensing is at least configured between outer gear ring and excessively line standpipe
Device, electronics anemoscope and position sensor pass through the positive and negative rotation amount and start and stop of intelligent device real-time control stepping decelerating motor, make electricity
The dynamic steady position rotor of horizontal axis is always windward.The platform edges of going straight up to of horizontal semi-girder base portion or horizontal semi-girder base portion are fixed with for stopping electricity
What dynamic vertical pivot lifting rotor generated blows to the arc wind board for going straight up to the beam wind of platform.
Electronic vertical pivot lifting rotor uses fixing axle, can significantly improve lift, and significantly simplify structure, itself matter
Amount, significantly improves payload.Square or circle, which go straight up to platform quadrangle and be respectively furnished with a circumferential direction by horizontal semi-girder, to be uniformly distributed
Electronic vertical pivot lifting rotor when, if a wherein electronic vertical pivot lifting rotor failure, can simultaneously close off symmetrical therewith
Another electronic vertical pivot lifting rotor, so that balance of wrestling, guarantees that platform does not rotate.So to guarantee mesa corners dynamic balance, institute
It all must be opposite with symmetrical electronic vertical pivot lifting rotor direction of rotation.
As optimization, the central control room gone straight up to center above platform and be formed with built-in intelligent controller, center control
The parachute automatic releasing device of intelligent controller control is configured above room by vertical supports;Square or circle go straight up to platform
Delta Region respectively configures an intelligent navigation by automatic locking device above platform between adjacent horizontal semi-girder and central control room
Rotor wing unmanned aerial vehicle, spindle are gone straight up to respectively to pass through above platform in the two sides of central control room and straight line where horizontal semi-girder and be locked automatically
Device configures one or more intelligent navigation rotor wing unmanned aerial vehicle;The cloud layer of ground or the rotation of vertical supports configuration level observes thunder
It reaches.After automatic locking device release, intelligent navigation rotor wing unmanned aerial vehicle is from horizontal semi-girder intermediate region along half that central control room is the center of circle
Radial line laterally flies away from platform, and carries out precisely sending out rainfall agent operation, operation to target cloud layer under the guide of cloud layer observation radar
After the completion, the airplane parking area of monitoring control centre is returned in the case where cloud layer observation radar or global position system guide.Vertical supports
Upper end configures the parachute automatic releasing device of intelligent controller control, and vertical supports periphery configures circumferential rotation by Pressure turntable
Rotatable radar antenna.Automatic locking device is gone straight up to configured with intelligently locking above platform, and the undercarriage of rotor wing unmanned aerial vehicle has and intelligence
The lock nose of energy ground lock lock tongue cooperation.
After above-mentioned technology, smart grid of the present invention support the accurate high-efficiency artificial rainfall method for thering is cable to go straight up to platform and
There is system the power supply mode for the smart grid supply station for saving low ebb Electricity Functional can significantly reduce power cost.Go straight up to platform liter
Launching platform is provided to send out the intelligent navigation rotor wing unmanned aerial vehicle of increasing rain agent in outage, unmanned plane load can be significantly improved, significantly
Reduction sends out cost, dramatically increases unmanned plane voyage, improves in amplitude and increases rain workload, significantly improves and increases rain economic benefit.It is special
It is not that rotor wing unmanned aerial vehicle carries out sending out operation, can significantly increases and send out density and intensity, significantly improve the rainfall of cloud layer steam
Efficiency, the cloud small for thin layer, area also can be by precisely sending out realization effective rainfall, this is any existing increasing rain skill
Art is irrealizable.Therefore, thin layer and scattered cloud can be applicable in by having, at low cost, precision is high, rainfall effect and profitable
The advantages of.
Specific embodiment
Smart grid of the present invention supports matching for the accurate high-efficiency artificial rainfall method cable for having cable to go straight up to platform power supply more
A electronic lifting rotor and electronic steady position rotor, the platform bearer of going straight up to intelligent controller send out the intelligent navigation rotation for increasing rain agent
Wing unmanned plane, the cloud layer observation radar guide configured with platform configuration or ground go straight up to platform lift-off height and guide rotor nobody
Machine flight path carries out target cloud precisely to send out operation, and intelligent controller passes through wireless or wired and wireless spare communication side
Formula connects ground monitoring control centre, saves the smart grid supply station of low ebb Electricity Functional to going straight up to platform and cloud layer is seen with having
Survey radar and the power supply of ground monitoring control centre.Platform configuration observes thunder going straight up to platform and rise to lower view cloud layer above cloud layer
It reaches or configures and go straight up to platform and rise to upper view cloud layer observation radar below cloud layer, regard cloud layer observation radar in the configuration of ground.
Power supply mode with the smart grid supply station for saving low ebb Electricity Functional can significantly reduce power cost.Platform liter is gone straight up in sky
It is a height of that the intelligent navigation rotor wing unmanned aerial vehicle offer launching platform for increasing rain agent is provided, unmanned plane load can be significantly improved, is significantly reduced
It sends out cost, dramatically increase unmanned plane voyage, improved in amplitude and increase rain workload, significantly improve and increase rain economic benefit.Especially
Rotor wing unmanned aerial vehicle carries out sending out operation, can significantly increase and send out density and intensity, significantly improves the rainfall efficiency of cloud layer steam,
The cloud small for thin layer, area, also can be by precisely sending out realization effective rainfall, this is that any existing increasing rain technology cannot
It realizes.Therefore, thin layer and scattered cloud can be applicable in by having, at low cost, precision is high, rainfall effect and profitable excellent
Point.
Specifically: the platform of going straight up to is furnished with the super capacitor electric power storage backup power source enabled automatically in cable power supply trouble
Or the super capacitor electric power storage backup power source that is enabled automatically in cable power supply trouble and should plunge for reducing forced landing power consumption
Fall umbrella;With cloud layer observation radar go straight up to platform forced landing when, close synchronously cloud layer observation radar.The platform of going straight up to rises to cloud
Layer top, is from top to bottom observed cloud layer using its autogamy cloud layer observation radar, guides unmanned machine operation;Or it is described straight
Peaceful rises to below cloud layer, is observed from bottom to top using its autogamy cloud layer observation radar to cloud layer, guides unmanned plane
Operation.
More specifically: when forced landing, disconnecting the connection or automatic disconnection for going straight up to platform and cable of powering automatically as needed
The connection on ground and power supply cable;After closing cloud layer observation radar, the global position system matched by intelligent controller guides forced landing
Path.
Specifically: the automatic coupler connection supply lines going straight up to platform base center and being controlled by intelligent controller
Cable, the automatic cable hoist engine or automatic spiral fashion retractable cable cable of the control of smart grid supply station configuration monitoring control centre
Machine;Intelligent navigation rotor wing unmanned aerial vehicle is furnished with cloud layer Image Acquisition identification device, according to cloud when intelligent navigation rotor wing unmanned aerial vehicle operation
The accurate navigation of tomographic image acquisition identification data progress increases rain agent and sends out.Automatic coupler includes before going straight up to platform base center configuration
The lock tongue end of the major-minor electric lock interlocked afterwards, main electric lock connects electricity directly or by mechanical transmission mechanism connection configuration is indented
Socket, cable upper end configure the mating with the electrical connector socket of connect plug, and secondary electric lock lock tongue suspension cable upper end is solid
The cable hanging ring matched, when needing to disconnect cable, the lock tongue and electrical connector socket of main electric lock are inside contracted, due to the limit of the electronic lock body of master
Position is detached from connect plug with electrical connector socket from inside contracting with electrical connector socket, after main electric lock completes above-mentioned movement, lock tongue
The electric switch for touching secondary electric lock starts secondary electric lock, makes the lock tongue internal lock of secondary electric lock, due to the limit of secondary electric lock body
Position, cable hanging ring cannot be moved together therewith, so that cable hanging ring be made to lose the support of secondary electric lock lock tongue, and be fallen off, thus
Realize automatically disengaging for cable.
More specifically: the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are configured with cable electronic tensile
Meter, it is described go straight up to platform base center according to ground and aerial platform measure and release in real time length of cable and platform lift-off highly
Upper limit tension and lower limit tension that cable is born are calculated in real time, when the cable strain that cable electronic tensile measures is greater than the upper limit
Power and be less than lower limit tension when, go straight up to automatic cable hoist engine described in the real-time control of platform base center or automatic spiral fashion receipts
It puts cable machine and carries out unwrapping wire and take-up.The automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are packed in a water
The Pressure turntable of flat configuration, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine can be according to cables to aerial
The real-time adjust automatically direction of the angle of drawing, being in automatic cable hoist engine or automatic spiral fashion retractable cable cable machine always has
Conducive to the orientation of unwrapping wire and take-up.
Specifically: the rainfall agent includes silver iodide, dry ice, liquid nitrogen, salt or potassium chloride particle;Smart grid supply station
The liquid nitrogen device for making of driving fills liquid nitrogen to the rotor wing unmanned aerial vehicle for sowing liquid nitrogen rainfall agent;Smart grid supply station drives anti-
Penetration sea water desalinization device produces strong brine, and strong brine produces salt particle by spray evaporation device.Smart grid supply station
It is also equipped with steam-electric power plant and wind power plant.Potassium chloride particle is that potassium chloride fortified aqueous passes through spray evaporation device
Produce salt particle.Certainly the rainfall agent can also be other insoluble but can be water-moistened particle such as dust, can be at it
The rainfall agent of adsorption steam generation drop embryo;It is also possible to other soluble-salt particles, such as sulfate, nitrate, chlorine
Change calcium etc..
More specifically: it is described produce salt or potassium chloride particle be setting one middle and lower part have the reversed louvre type of multilayer from
The up-thin-low-thick perpendicular conical tube type high tower of right ventilation opening, sprays the strong brine or dense into tower using micro-nozzle at the top of high tower
Sylvite water, because of the salt or potassium chloride particle that moisture evaporates and is formed during tower bottom is collected and declined, the outer wall of high tower exists
The top and two sides of reversed louvre type natural ventilation port are configured with the rain shade for rain cover;The reversed blind window is can
The blind window for the reverse configuration for passing freely through natural wind, and salt or potassium chloride particle capable of being stopped to outflow.The strong brine or
Dense sylvite water can be blended into urea, strong brine by aqueous solution of urea or brackish water replacement or the strong brine or brackish water
Or the weight ratio of salt and urea preferred 90-99: 10-0.1 in dense sylvite water, more preferable 95-99: 5-1, more specifically 90 kilograms:
10 kilograms, 95 kilograms: 5 kilograms, 97 kilograms: 3 kilograms, 99 kilograms: 1 kilograms, 99.2 kilograms: 0.8 kilograms, 99.5 kilograms: 0.5 public affairs
Jin, 99.7 kilograms: 0.3 kilograms, 99.9 kilograms: 0.1 kilograms.
Specifically: square or circle go straight up to platform quadrangle by horizontal semi-girder to be respectively furnished with a circumferential direction equally distributed electronic
Vertical pivot lifting rotor or spindle go straight up to platform both ends and respectively configure a symmetrical electronic vertical pivot lift by horizontal semi-girder
Rotor goes straight up to and configures undercarriage below platform, goes straight up to and configures at least one below platform for resisting the electronic cross of crosswind force
Axis steady position rotor, goes straight up to configure more by the automatic locking device that intelligent controller controls above platform and send out side by side and increases rain agent
Intelligent navigation rotor wing unmanned aerial vehicle.The undercarriage is that square or circle go straight up to and be respectively fixedly mounted with a foundation below platform quadrangle with buffering
The supporting leg of foot is connected between each supporting leg by transversely strengthening bar.The undercarriage is that spindle is gone straight up to below platform two sides respectively
It is fixedly mounted with the undercarriage being parallel to each other downwards.It goes straight up to center below platform and is fixedly mounted with a line standpipe excessively downwards, cross under line standpipe
End is fixedly mounted with the automatic coupler of cable, and automatic coupler, which connects up, goes straight up to platform power line, connects power cable downwards, needs
When automatic coupler can disconnect power cable automatically, keep power cable automatically born, platform load and enable platform to reduce
It is enough not restrained by cable, realize most energy-efficient emergency forced landing or downlink.It is solid by two-way pressure turntable to cross periphery in the middle part of line standpipe
The horizontal spindle bracket of the steady position rotor of electronic horizontal axis is filled, one end of spindle bracket configures the steady position rotor of electronic horizontal axis, the other end
It is fixedly mounted with guiding empennage.Under the action of being oriented to empennage, rotate the steady position rotor of electronic horizontal axis windward always to overcome wind to platform
The displacement force of application.Can certainly be: crossing in the middle part of line standpipe periphery, to be directly fixedly mounted with electronic horizontal axis steady by two-way pressure turntable
Position rotor, goes straight up to platform configuration electronics anemoscope, and the periphery rotating part configuration of Pressure turntable is made by electronics anemoscope manipulation
The automatic control rotation drive device of the electronic steady position rotor of horizontal axis always windward.Automatic control rotation drive device is that the outer of Pressure turntable is socialized
Portion is fixedly mounted with an outer gear ring upwards, crosses line standpipe or goes straight up to and is fixedly mounted with a stepping decelerating motor, stepping decelerating motor below platform
Output shaft be fixedly mounted with the driving gear engaged with outer gear ring.A pair of of position sensing is at least configured between outer gear ring and excessively line standpipe
Device, electronics anemoscope and position sensor pass through the positive and negative rotation amount and start and stop of intelligent device real-time control stepping decelerating motor, make electricity
The dynamic steady position rotor of horizontal axis is always windward.The platform edges of going straight up to of horizontal semi-girder base portion or horizontal semi-girder base portion are fixed with for stopping electricity
What dynamic vertical pivot lifting rotor generated blows to the arc wind board for going straight up to the beam wind of platform.
Electronic vertical pivot lifting rotor uses fixing axle, can significantly improve lift, and significantly simplify structure, itself matter
Amount, significantly improves payload.Square or circle, which go straight up to platform quadrangle and be respectively furnished with a circumferential direction by horizontal semi-girder, to be uniformly distributed
Electronic vertical pivot lifting rotor when, if a wherein electronic vertical pivot lifting rotor failure, can simultaneously close off symmetrical therewith
Another electronic vertical pivot lifting rotor, so that balance of wrestling, guarantees that platform does not rotate.So to guarantee mesa corners dynamic balance, institute
It all must be opposite with symmetrical electronic vertical pivot lifting rotor direction of rotation.
More specifically: the central control room gone straight up to center above platform and be formed with built-in intelligent controller, center control
The parachute automatic releasing device of intelligent controller control is configured above room by vertical supports;Square or circle go straight up to platform
Delta Region respectively configures an intelligent navigation by automatic locking device above platform between adjacent horizontal semi-girder and central control room
Rotor wing unmanned aerial vehicle, spindle are gone straight up to respectively to pass through above platform in the two sides of central control room and straight line where horizontal semi-girder and be locked automatically
Device configures one or more intelligent navigation rotor wing unmanned aerial vehicle;The cloud layer of ground or the rotation of vertical supports configuration level observes thunder
It reaches.After automatic locking device release, intelligent navigation rotor wing unmanned aerial vehicle is from horizontal semi-girder intermediate region along half that central control room is the center of circle
Radial line laterally flies away from platform, and carries out precisely sending out rainfall agent operation, operation to target cloud layer under the guide of cloud layer observation radar
After the completion, the airplane parking area of monitoring control centre is returned in the case where cloud layer observation radar or global position system guide.Vertical supports
Upper end configures the parachute automatic releasing device of intelligent controller control, and vertical supports periphery configures circumferential rotation by Pressure turntable
Rotatable radar antenna.Automatic locking device is gone straight up to configured with intelligently locking above platform, and the undercarriage of rotor wing unmanned aerial vehicle has and intelligence
The lock nose of energy ground lock lock tongue cooperation.
System for realizing the method for the invention includes cable power supply with multiple electronic lifting rotors and electronic steady
Position rotor sends out with intelligent controller, carrying and increases the intelligent navigation rotor wing unmanned aerial vehicle of rain agent and go straight up to platform, with platform configuration or
Ground configuration cloud layer observation radar guide go straight up to platform lift-off height and guide rotor wing unmanned aerial vehicle flight path to target cloud into
Row precisely sends out operation, and intelligent controller is connected in ground monitoring control by wireless or wired and wireless spare communication modes
The heart has and saves the smart grid supply station of low ebb Electricity Functional to going straight up in platform and cloud layer observation radar and ground monitoring control
Heart power supply.Platform configuration go straight up to platform rise to above cloud layer it is lower depending on cloud layer observation radar or configuration go straight up to platform rise
Upper view cloud layer observation radar below to cloud layer, ground configure and regard cloud layer observation radar.With the intelligence for saving low ebb Electricity Functional
The power supply mode of energy power grid supply station can significantly reduce power cost.Go straight up to platform liter outage be send out increase rain agent intelligence lead
The rotor wing unmanned aerial vehicle that navigates provides launching platform, can significantly improve unmanned plane load, and significant decrease sends out cost, dramatically increases unmanned plane
Voyage improves in amplitude and increases rain workload, significantly improves and increases rain economic benefit.Especially rotor wing unmanned aerial vehicle carries out sending out operation,
It can significantly increase and send out density and intensity, significantly improve the rainfall efficiency of cloud layer steam, the cloud small for thin layer, area
Coloured silk, also can be by precisely sending out realization effective rainfall, this is that any existing increasing rain technology is irrealizable.Therefore, having can fit
It is at low cost, precision is high, rainfall effect and profitable advantage with thin layer and scattered cloud.
It is specific: it is described go straight up to platform be furnished with the super capacitor electric power storage backup power source that is enabled automatically in cable power supply trouble or
The super capacitor electric power storage backup power source that person enables automatically in cable power supply trouble and the emergency landing for reducing forced landing power consumption
Umbrella;With cloud layer observation radar go straight up to platform forced landing when, close synchronously cloud layer observation radar.The platform of going straight up to rises to cloud layer
Top is from top to bottom observed cloud layer using its autogamy cloud layer observation radar, guides unmanned machine operation;Or it described goes straight up to
Platform rises to below cloud layer, is observed from bottom to top using its autogamy cloud layer observation radar to cloud layer, and unmanned plane is guided to make
Industry.
It is more specific: when forced landing, to disconnect the connection for going straight up to platform and cable of powering or automatic disconnection ground automatically as needed
The connection in face and power supply cable;After closing cloud layer observation radar, the global position system matched by intelligent controller guides forced landing road
Diameter.
It is specific: the automatic coupler connection power cable going straight up to platform base center and being controlled by intelligent controller,
The automatic cable hoist engine or automatic spiral fashion retractable cable cable machine of smart grid supply station configuration monitoring control centre control;Intelligence
The rotor wing unmanned aerial vehicle that can navigate is furnished with cloud layer Image Acquisition identification device, according to cloud layer image when intelligent navigation rotor wing unmanned aerial vehicle operation
The accurate navigation of acquisition identification data progress increases rain agent and sends out.Automatic coupler includes going straight up to platform base center configuration forward and backward linkage
Major-minor electric lock, the lock tongue end of main electric lock configures indented electrical connector socket directly or by mechanical transmission mechanism connection,
Cable upper end configures the mating with the electrical connector socket of connect plug, the line that secondary electric lock lock tongue suspension cable upper end is matched admittedly
Cable hanging ring, when needing to disconnect cable, the lock tongue and electrical connector socket of main electric lock are inside contracted, and due to the limit of the electronic lock body of master, are made
Connect plug cannot be inside contracted with electrical connector socket and is detached from electrical connector socket, and after main electric lock completes above-mentioned movement, lock tongue touches
The electric switch of secondary electric lock starts secondary electric lock, makes the lock tongue internal lock of secondary electric lock, due to the limit of secondary electric lock body, line
Cable hanging ring cannot move together therewith, so that cable hanging ring be made to lose the support of secondary electric lock lock tongue, and fall off, to realize line
Cable automatically disengages.
More specific: the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are configured with cable electronic tensile
Meter, it is described go straight up to platform base center according to ground and aerial platform measure and release in real time length of cable and platform lift-off highly
Upper limit tension and lower limit tension that cable is born are calculated in real time, when the cable strain that cable electronic tensile measures is greater than the upper limit
Power and be less than lower limit tension when, go straight up to automatic cable hoist engine described in the real-time control of platform base center or automatic spiral fashion receipts
It puts cable machine and carries out unwrapping wire and take-up.The automatic cable hoist engine or automatic spiral fashion retractable cable cable machine are packed in a water
The Pressure turntable of flat configuration, the automatic cable hoist engine or automatic spiral fashion retractable cable cable machine can be according to cables to aerial
The real-time adjust automatically direction of the angle of drawing, being in automatic cable hoist engine or automatic spiral fashion retractable cable cable machine always has
Conducive to the orientation of unwrapping wire and take-up.
Specific: the rainfall agent includes silver iodide, dry ice, liquid nitrogen, salt or potassium chloride particle;Smart grid supply station drives
Dynamic liquid nitrogen device for making fills liquid nitrogen to the rotor wing unmanned aerial vehicle for sowing liquid nitrogen rainfall agent;The reverse osmosis of smart grid supply station driving
Saturating desalination plant produces strong brine, and strong brine produces salt particle by spray evaporation device.Smart grid supply station is also
Equipped with steam-electric power plant and wind power plant.Potassium chloride particle is that potassium chloride fortified aqueous passes through spray evaporation device system
Feeding salt particle.Certainly the rainfall agent can also be other insoluble but can be water-moistened particle such as dust, can be in its table
Adsorb the rainfall agent that steam generates drop embryo in face;It is also possible to other soluble-salt particles, such as sulfate, nitrate, chlorination
Calcium etc..
It is more specific: described to produce salt or potassium chloride particle is that one middle and lower part of setting has the reversed louvre type of multilayer natural
The up-thin-low-thick perpendicular conical tube type high tower of ventilation opening sprays the strong brine or dense potassium into tower using micro-nozzle at the top of high tower
Salt water, because of the salt or potassium chloride particle that moisture evaporates and is formed during tower bottom is collected and declined, the outer wall of high tower is anti-
The rain shade for rain cover is configured with to the top of louvre type natural ventilation port and two sides;The reversed blind window is can to make
Natural wind passes freely through, and the blind window for the reverse configuration that salt or potassium chloride particle can be stopped to outflow.The strong brine is dense
Sylvite water can be replaced by aqueous solution of urea or brackish water or the strong brine or brackish water can be blended into urea, strong brine or
The weight ratio of salt and urea preferred 90-99: 10-0.1 in dense sylvite water, more preferable 95-99: 5-1, more specifically 90 kilograms: 10
Kilogram, 95 kilograms: 5 kilograms, 97 kilograms: 3 kilograms, 99 kilograms: 1 kilograms, 99.2 kilograms: 0.8 kilograms, 99.5 kilograms: 0.5 it is public
Jin, 99.7 kilograms: 0.3 kilograms, 99.9 kilograms: 0.1 kilograms.
Specific: square or circle go straight up to platform quadrangle by horizontal semi-girder to be respectively furnished with a circumferential direction equally distributed electronic perpendicular
Axis lifting rotor or spindle go straight up to platform both ends and respectively configure a symmetrical electronic vertical pivot lift rotation by horizontal semi-girder
The wing goes straight up to and configures undercarriage below platform, goes straight up to and configures at least one below platform for resisting the electronic horizontal axis of crosswind force
Steady position rotor goes straight up to and configures the more intelligence for sending out increasing rain agent side by side by the automatic locking device that intelligent controller controls above platform
Can navigate rotor wing unmanned aerial vehicle.The undercarriage is that square or circle go straight up to and be respectively fixedly mounted with a foundation below platform quadrangle with buffering foot
Supporting leg, be connected between each supporting leg by transversely strengthening bar.The undercarriage be spindle go straight up to below platform two sides respectively to
Under be fixedly mounted with the undercarriage being parallel to each other.It goes straight up to center below platform and is fixedly mounted with a line standpipe excessively downwards, cross line lower riser end
It is fixedly mounted with the automatic coupler of cable, automatic coupler, which connects up, goes straight up to platform power line, power cable is connected downwards, when needing
Automatic coupler can disconnect power cable automatically, keep power cable automatically born, to reduce platform load and enable platform
It is not restrained by cable, realizes most energy-efficient emergency forced landing or downlink.Periphery in the middle part of line standpipe is crossed to be fixedly mounted with by two-way pressure turntable
The horizontal spindle bracket of the electronic steady position rotor of horizontal axis, it is solid that one end of spindle bracket configures the steady position rotor of electronic horizontal axis, the other end
Dress guiding empennage.Under the action of being oriented to empennage, rotate the steady position rotor of electronic horizontal axis windward always to overcome wind to apply platform
The displacement force added.It can certainly be: cross line standpipe middle part periphery by two-way pressure turntable and be directly fixedly mounted with the steady position of electronic horizontal axis
Rotor, goes straight up to platform configuration electronics anemoscope, and the periphery rotating part configuration of Pressure turntable makes electricity by electronics anemoscope manipulation
The dynamic automatic control rotation drive device of the steady position rotor of horizontal axis always windward.Automatic control rotation drive device is the outer portion of socializing of Pressure turntable
It is fixedly mounted with an outer gear ring upwards, crosses line standpipe or go straight up to and be fixedly mounted with a stepping decelerating motor below platform, stepping decelerating motor
Output shaft is fixedly mounted with the driving gear engaged with outer gear ring.A pair of of position sensor is at least configured between outer gear ring and excessively line standpipe,
Electronics anemoscope and position sensor pass through the positive and negative rotation amount and start and stop of intelligent device real-time control stepping decelerating motor, make electronic cross
The steady position rotor of axis is always windward.The platform edges of going straight up to of horizontal semi-girder base portion or horizontal semi-girder base portion are fixed with for stopping electronic erect
What axis lifting rotor generated blows to the arc wind board for going straight up to the beam wind of platform.
Electronic vertical pivot lifting rotor uses fixing axle, can significantly improve lift, and significantly simplify structure, itself matter
Amount, significantly improves payload.Square or circle, which go straight up to platform quadrangle and be respectively furnished with a circumferential direction by horizontal semi-girder, to be uniformly distributed
Electronic vertical pivot lifting rotor when, if a wherein electronic vertical pivot lifting rotor failure, can simultaneously close off symmetrical therewith
Another electronic vertical pivot lifting rotor, so that balance of wrestling, guarantees that platform does not rotate.So to guarantee mesa corners dynamic balance, institute
It all must be opposite with symmetrical electronic vertical pivot lifting rotor direction of rotation.
It is more specific: the central control room gone straight up to center above platform and be formed with built-in intelligent controller, central control room
Top configures the parachute automatic releasing device of intelligent controller control by vertical supports;Square or circle go straight up to platform phase
Delta Region respectively configures an intelligent navigation by automatic locking device and revolves above platform between adjacent horizontal semi-girder and central control room
Wing unmanned plane, spindle, which is gone straight up to, respectively passes through automatic locking device in the two sides of straight line where central control room and horizontal semi-girder above platform
Configure one or more intelligent navigation rotor wing unmanned aerial vehicle;The cloud layer observation radar of ground or the rotation of vertical supports configuration level.
After automatic locking device release, intelligent navigation rotor wing unmanned aerial vehicle is the radius in the center of circle along central control room from horizontal semi-girder intermediate region
Platform is laterally flown away from, and target cloud layer is carried out under the guide of cloud layer observation radar precisely to send out rainfall agent operation, operation is completed
Afterwards, the airplane parking area of monitoring control centre is returned in the case where cloud layer observation radar or global position system guide.Vertical supports upper end
The parachute automatic releasing device of intelligent controller control is configured, vertical supports periphery configures the formula that rotates in a circumferential direction by Pressure turntable
Radar antenna.Automatic locking device is to go straight up to above platform configured with intelligently locking, the undercarriage of rotor wing unmanned aerial vehicle have with intelligently
Lock the lock nose of lock tongue cooperation.
After above-mentioned technology, smart grid of the present invention support the accurate high-efficiency artificial rainfall method for thering is cable to go straight up to platform and
There is system the power supply mode for the smart grid supply station for saving low ebb Electricity Functional can significantly reduce power cost.Go straight up to platform liter
Launching platform is provided to send out the intelligent navigation rotor wing unmanned aerial vehicle of increasing rain agent in outage, unmanned plane load can be significantly improved, significantly
Reduction sends out cost, dramatically increases unmanned plane voyage, improves in amplitude and increases rain workload, significantly improves and increases rain economic benefit.It is special
It is not that rotor wing unmanned aerial vehicle carries out sending out operation, can significantly increases and send out density and intensity, significantly improve the rainfall of cloud layer steam
Efficiency, the cloud small for thin layer, area also can be by precisely sending out realization effective rainfall, this is any existing increasing rain skill
Art is irrealizable.Therefore, thin layer and scattered cloud can be applicable in by having, at low cost, precision is high, rainfall effect and profitable
The advantages of.
Claims (10)
1. a kind of smart grid supports the accurate high-efficiency artificial rainfall method for having cable to go straight up to platform, it is characterised in that powered with cable
The platform bearer of going straight up to multiple electronic lifting rotors and electronic steady position rotor, with intelligent controller send out the intelligence for increasing rain agent
Navigate rotor wing unmanned aerial vehicle, goes straight up to platform lift-off height with the cloud layer observation radar guide for going straight up to platform configuration or ground configuration and refers to
Draw rotor wing unmanned aerial vehicle flight path target cloud is carried out precisely to send out operation, intelligent controller passes through wireless or wired and wireless
Spare communication modes connect ground monitoring control centre, with having the smart grid supply station for saving low ebb Electricity Functional flat to going straight up to
Platform and cloud layer observation radar and the power supply of ground monitoring control centre.
2. method according to claim 1, it is characterised in that the platform of going straight up to equipped with opening automatically in cable power supply trouble
Super capacitor electric power storage backup power source or the super capacitor electric power storage backup power source enabled automatically in cable power supply trouble and
For reducing the emergency parachute of forced landing power consumption;With cloud layer observation radar go straight up to platform forced landing when, close synchronously cloud layer observation
Radar.
3. method according to claim 2, it is characterised in that when forced landing, automatic disconnect goes straight up to platform and current supply cable as needed
The connection of line or the automatic connection for disconnecting ground and cable of powering;After closing cloud layer observation radar, matched by intelligent controller
Global position system guides forced landing path.
4. method according to claim 1, it is characterised in that the platform base center of going straight up to is controlled by intelligent controller
Automatic coupler connect power cable, smart grid supply station configuration monitoring control centre control automatic cable hoist engine or
The automatic spiral fashion retractable cable cable machine of person;Intelligent navigation rotor wing unmanned aerial vehicle is furnished with cloud layer Image Acquisition identification device, intelligent navigation rotation
Identify that data carry out precisely navigation and increase rain agent to send out according to cloud layer Image Acquisition when the unmanned machine operation of the wing.
5. method according to claim 4, it is characterised in that the automatic cable hoist engine or automatic spiral fashion retractable cable
Cable machine be configured with cable electronic tensile meter, it is described go straight up to platform base center according to ground and in the air go straight up to platform measure in real time and
It releases length of cable and goes straight up to platform lift-off height and calculate upper limit tension and lower limit tension that cable is born in real time, when cable electronics
When the cable strain that tensometer measures is greater than upper limit tension or is less than lower limit tension, go straight up to described in the real-time control of platform base center
Automatic cable hoist engine or automatic spiral fashion retractable cable cable machine carry out unwrapping wire or take-up.
6. method according to claim 1, it is characterised in that the increasing rain agent includes that silver iodide, dry ice, liquid nitrogen, salt are micro-
Grain;The liquid nitrogen device for making of smart grid supply station driving increases the rotor wing unmanned aerial vehicle filling liquid nitrogen of rain agent to liquid nitrogen is sowed;Intelligence
The reverse osmosis desalination device of power grid supply station driving produces strong brine, and it is micro- that strong brine by spray evaporation device produces salt
Grain.
7. method according to claim 6, it is characterised in that the salt particle of producing is that one middle and lower part of setting has multilayer
The up-thin-low-thick perpendicular conical tube type high tower of reversed louvre type natural ventilation port, is sprayed using micro-nozzle into tower at the top of high tower
The strong brine, because of the salt particle that moisture evaporates and is formed during tower bottom is collected and declined, the outer wall of high tower is reversed
The top and two sides of louvre type natural ventilation port are configured with the rain shade for rain cover;The reversed blind window is can to make certainly
The blind window for the reverse configuration that right wind passes freely through, and salt particle can be stopped to outflow.
8. method according to claim 1, it is characterised in that square or circle are gone straight up to platform quadrangle and respectively matched by horizontal semi-girder
There are the equally distributed electronic vertical pivot lifting rotor of a circumferential direction or spindle to go straight up to platform both ends and respectively configures one by horizontal semi-girder
The symmetrical electronic vertical pivot lifting rotor of platform, goes straight up to and configures undercarriage below platform, go straight up to and configure at least one below platform
The steady position rotor of electronic horizontal axis for resisting crosswind force goes straight up to the automatic locking device controlled above platform by intelligent controller
It configures more and sends out the intelligent navigation rotor wing unmanned aerial vehicle for increasing rain agent side by side.
9. method according to claim 8, it is characterised in that described to go straight up to center above platform and be formed with built-in intelligent controller
Central control room, configure the parachute that intelligent controller controls by vertical supports above central control room and discharge dress automatically
It sets;Square or the round Delta Region above platform of going straight up to gone straight up between the adjacent horizontal semi-girder of platform and central control room respectively pass through
Automatic locking device configures an intelligent navigation rotor wing unmanned aerial vehicle, and spindle is gone straight up to above platform in central control room and horizontal semi-girder institute
Respectively pass through automatic locking device in the two sides of straight line and configures one or more intelligent navigation rotor wing unmanned aerial vehicle;Ground or vertical supports
The cloud layer observation radar of configuration level rotation.
10. for realizing the system of claim 1 the method, it is characterised in that match multiple electronic lift including cable power supply
Rotor and electronic steady position rotor, send out the intelligent navigation rotor wing unmanned aerial vehicle for increasing rain agent with intelligent controller, carrying go straight up to platform,
Platform lift-off height is gone straight up to the cloud layer observation radar guide for going straight up to platform configuration or ground configuration and rotor wing unmanned aerial vehicle is guided to fly
Walking along the street diameter carries out target cloud precisely to send out operation, and intelligent controller is connected by wireless or wired and wireless spare communication modes
Ground plane monitors control centre, has and saves the smart grid supply station of low ebb Electricity Functional to going straight up to platform and cloud layer observation radar
And ground monitoring control centre power supply.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610619602.4A CN107667746B (en) | 2016-08-02 | 2016-08-02 | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610619602.4A CN107667746B (en) | 2016-08-02 | 2016-08-02 | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform |
Publications (2)
Publication Number | Publication Date |
---|---|
CN107667746A CN107667746A (en) | 2018-02-09 |
CN107667746B true CN107667746B (en) | 2019-07-26 |
Family
ID=61133780
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610619602.4A Active CN107667746B (en) | 2016-08-02 | 2016-08-02 | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107667746B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114631453B (en) * | 2022-02-23 | 2023-03-14 | 水利部牧区水利科学研究所 | Movable artificial rainfall simulation method based on unmanned aerial vehicle platform |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
CN101617616A (en) * | 2008-07-02 | 2010-01-06 | 赵健 | Device and system for expelling cloud and rain |
CN102935886B (en) * | 2012-11-05 | 2016-01-06 | 上海交通大学无锡研究院 | A kind of multistage mooring rotor lift-off plateform system |
US9612354B2 (en) * | 2014-02-06 | 2017-04-04 | Cgg Services Sas | Geophysical survey system using hybrid aircraft |
CN105292456A (en) * | 2015-11-24 | 2016-02-03 | 齐心 | Multi-rotor unmanned aerial vehicle |
-
2016
- 2016-08-02 CN CN201610619602.4A patent/CN107667746B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN107667746A (en) | 2018-02-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103895823B (en) | Snorkeling cumulative guide type wave-energy power generation platform | |
CN102686875B (en) | Wind generator with water float sail | |
US9777709B2 (en) | Translating foil system for harvesting kinetic energy from wind and flowing water | |
CN105569928A (en) | Single point mooring type deep sea floating type draught fan | |
CN101882894B (en) | Suspended solar power station | |
CN203756425U (en) | Submerged type offshore wave-energy power generation device | |
CN107867373A (en) | A kind of rotary photovoltaic tracking waterborne and vaporization prevention screen device and its method | |
CN107651130A (en) | The photovoltaic plant buoyant means waterborne of adjustable inclination and its application | |
CN109441727A (en) | Marine wave energy-wind energy integrated system and integrated electricity-generating method | |
CN106063437B (en) | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to machine tool | |
CN107667746B (en) | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform | |
CN206135789U (en) | Green house based on photovoltaic tracking system | |
CN106523250A (en) | Water-floating type hydroelectric generator | |
CN204989994U (en) | Showy assembled solar azimuth angle tracking means on water | |
CN209376367U (en) | A kind of energy-saving and environment-friendly treegarden irrigation device | |
CN107278732A (en) | The overhead potential energy ejecting rain making method and system of mountain shape are relied on based on intelligent grid | |
CN207937877U (en) | Floating type photovoltaic solar Bearings tracking system waterborne | |
CN110821744A (en) | Scalable floating trend can power generation facility | |
CN206686823U (en) | Energy-saving is from water-drawing type water supply installation | |
CN102359092B (en) | Suspended reservoir generating station | |
CN108343559A (en) | A kind of aerial formula wind generator system that floats for skyscraper public electricity-using | |
CN205567081U (en) | Pumping system is removed in complementary integration of wind light storage | |
CN210537949U (en) | Reel formula sprinkling irrigation machine for large tracts of land field irrigation | |
CN102705167A (en) | Lotus-shaped wind power generation device | |
CN106917721A (en) | Take turns to stream power centrifugation slide plate stream wheel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |