CN109479592A - A kind of no pylon weather regulating system - Google Patents
A kind of no pylon weather regulating system Download PDFInfo
- Publication number
- CN109479592A CN109479592A CN201811532746.1A CN201811532746A CN109479592A CN 109479592 A CN109479592 A CN 109479592A CN 201811532746 A CN201811532746 A CN 201811532746A CN 109479592 A CN109479592 A CN 109479592A
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- power carrying
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- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000008054 signal transmission Effects 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 230000001360 synchronised effect Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 description 10
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- 229910052760 oxygen Inorganic materials 0.000 description 4
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- 230000017260 vegetative to reproductive phase transition of meristem Effects 0.000 description 2
- 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 description 1
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 229910021612 Silver iodide Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 235000011089 carbon dioxide Nutrition 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
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- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
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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)
- Elimination Of Static Electricity (AREA)
Abstract
本发明公开了一种无塔架天气调节系统，其包括飞行装置和电能携带装置；飞行装置上设置有天线；电能携带装置设置于飞行装置上，和/或电能携带装置固定或移动地设置于飞行装置之上或之下的独立区域；飞行装置天线与地面等电位或者绝缘，飞行装置与地面的距离为n米；天线与地面或者天线与电能携带装置之间具有mKV的压差。本发明的飞行装置天线与地面等电位或者与地面绝缘，天线与地面或者天线与电能携带装置之间具有mKV的压差，不需要设置塔架就能够实现天气的调节，节约了成本；该无塔架天气调节系统可移动作业，一个系统的可作用范围大，投入产出比高。
The invention discloses a towerless weather conditioning system, which comprises a flying device and a power carrying device; the flying device is provided with an antenna; the power carrying device is arranged on the flying device, and/or the power carrying device is fixedly or movably arranged in An independent area above or below the flying device; the antenna of the flying device is equipotential or insulated from the ground, and the distance between the flying device and the ground is n meters; there is a voltage difference of mKV between the antenna and the ground or between the antenna and the power carrying device. The antenna of the flying device of the present invention is equipotential with the ground or insulated from the ground, and there is a pressure difference of mKV between the antenna and the ground or between the antenna and the power carrying device, so that the weather can be adjusted without setting a tower, and the cost is saved; The tower weather adjustment system can be operated in a mobile way, and a system has a large scope of action and a high input-output ratio.
Description
Technical field
The present invention relates to weather regulation technology field, in particular to a kind of no pylon weather regulating system.
Background technique
Artificial rainmaking is the condition that artificial supplement forms precipitation, and water dust is promoted to condense or touch and increase into raindrop rapidly, is dropped
It falls to the ground.Currently used method is to select proper moment according to the physical characteristics of different cloud layers, with aircraft, rocket to cloud
In sow the catalyst such as dry ice, silver iodide, salt fines, make cloud layer precipitation or increase precipitation, with release or alleviate agricultural drought, increase
Add reservoir duty or water supply capacity, or increase water amount of power generating etc..
" a kind of device and method of regional joint catalysis rainfall snow " is disclosed in CN104737867B, which includes
Measurement and control system, high pressure generator, high-tension cable, emission electrode, high pressure pylon, insulation system, the quantity of high pressure pylon
To be multiple, for the altitude range of high pressure pylon in 70m to 100m, each high pressure pylon distance range is 200m to 500m.The device
Although can be realized Precipitation simulation snow, need that multiple high pressure pylons, occupied area is arranged in pre- rainfall snow range
Big and cost is high；High pressure pylon is once built up, and can only serve a corresponding panel region, and input-output ratio is not high.
Summary of the invention
The present invention is directed at least solve the technical problems existing in the prior art, a kind of no pylon is especially innovatively proposed
Weather regulating system.
In order to realize above-mentioned purpose of the invention, the present invention provides a kind of no pylon weather regulating systems comprising flies
Luggage is set and electric energy carrying device；Antenna is provided on the flight instruments；The electric energy carrying device is set to flight instruments
On and/or the electric energy carrying device isolated area fixing or be movably set on or below flight instruments；The flight dress
Setting is n meters at a distance from ground, and the n is positive number；The flight instruments antenna and ground equipotential insulate with ground, day
With the pressure difference of mKV between line and ground or antenna and electric energy carrying device, the m is positive number.
It is of the invention without pylon weather regulating system use flight instruments, flight instruments antenna and ground equipotential or with
Ground insulation does not need setting pylon energy with the pressure difference of mKV between antenna and ground or antenna and electric energy carrying device
The adjusting for enough realizing weather, has saved cost；Without pylon weather regulating system movable operation, system acts on model for this
Enclose big, input-output ratio height.
In the preferred embodiment of the present invention, it can be used such as one or a combination set of flowering structure:
Structure one: including flight instruments, laser beam emitting device, the laser beam emitting device are carried on the flight instruments
Emit laser to the ground and makes the air ionization of laser traffic areas；
Further include electric energy carrying device, the electric energy carrying device be set on flight instruments and/or flight instruments or
Under isolated area, the flight instruments be equipped with antenna；
Structure two: including flight instruments, being provided with laser receiver/laser beam emitting device on the flight instruments, also
Including being provided with laser beam emitting device/laser receiver ground installation, the laser beam emitting device is to laser receiver
Transmitting laser and the air ionization for making laser traffic areas, the flight instruments are equipped with antenna, the flight instruments and/or ground
Electric energy carrying device is set on the device of face, or electric energy carrying device is arranged in the isolated area on or below flight instruments.
Make air ionization by laser beam emitting device, realizes flight instruments antenna and ground or ground installation equipotential.
In another preferred embodiment of the invention, also there is photoelectric conversion on the laser receiver in structure two
Device, the photoelectric conversion device are received laser signal and are generated electricity using laser, and photoelectric conversion device stores electric power, Huo Zhechuan
It is defeated by electric energy carrying device, be perhaps transferred to the energy storage component of flight instruments or is transferred to the energy storage part of ground mobile device
Part.
Electric energy is converted laser light into, is improved resource utilization.
It further include sender unit in another preferred embodiment of the invention, the sender unit produces
Raw signal is sent out by the antenna of flight instruments.
No pylon realizes the transmission of signal, reduces signal and sends cost.
In another preferred embodiment of the invention, electric energy is set on flight instruments and/or ground installation and is carried
When device, it is provided with ground connection under or over flight instruments or is electrically insulated with the electric energy carrying device and earth-free gold
Belong to driving device, when driving device is located under electric energy carrying device, the driving device has compared to electric energy carrying device
There is upward driving tip；When driving device is located on electric energy carrying device, the electric energy carrying device is compared to driving
Device has driving tip equivalent upwards.
Electric energy carrying device makes surrounding air and haze charging particle, position be located at lower part high voltage direct current carrying portion or
A large amount of charged haze particles or the negative oxygen ion driving of surrounding are sent to high-altitude by driving device.Electric energy carrying device of the present invention with
Strong electrical field is formed between driving device, no matter high voltage direct current carries position setting in driving device lower part or driving device position
Surrounding air and haze charging particle will all be made by carrying subordinate portion positioned at high voltage direct current, and by a large amount of charged hazes of surrounding
High-altitude is sent in grain or negative oxygen ion driving, has very high pushing efficiency.
Additional aspect and advantage of the invention will be set forth in part in the description, and will partially become from the following description
Obviously, or practice through the invention is recognized.
Detailed description of the invention
Above-mentioned and/or additional aspect of the invention and advantage will become from the description of the embodiment in conjunction with the following figures
Obviously and it is readily appreciated that, in which:
Fig. 1 is the structural schematic diagram without pylon weather regulating system in a kind of preferred embodiment of the present invention；
Fig. 2 is the structural schematic diagram without pylon weather regulating system in another preferred embodiment of the invention.
Specific embodiment
The embodiment of the present invention is described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning to end
Same or similar label indicates same or similar element or element with the same or similar functions.Below with reference to attached
The embodiment of figure description is exemplary, and for explaining only the invention, and is not considered as limiting the invention.
In the description of the present invention, unless otherwise specified and limited, it should be noted that term " installation ", " connected ",
" connection " shall be understood in a broad sense, for example, it may be mechanical connection or electrical connection, the connection being also possible to inside two elements can
, can also indirectly connected through an intermediary, for the ordinary skill in the art to be to be connected directly, it can basis
Concrete condition understands the concrete meaning of above-mentioned term.
The present invention provides a kind of no pylon weather regulating systems, as shown in Figure 1 comprising flight instruments B and electric energy are taken
Band device A.Antenna is provided on flight instruments B, in the present embodiment, antenna can may be orientation for omnidirectional antenna
Antenna, preferably directional aerial.Its direction is adjustable, can towards on just, side or tiltedly on, be preferably directed towards right above.
Electric energy carrying device A is set on flight instruments B, is carried by flight instruments B and/or electric energy carrying device is fixed
Or movably it is set to the isolated area on or below flight instruments.The antenna of flight instruments B and ground G equipotential (can be with
Equipotential is realized by wired or wireless electric current transmission channel) or insulate, the flight instruments are n at a distance from ground
Rice, the n are positive number；With the pressure difference of mKV between antenna and ground or antenna and electric energy carrying device, the m is positive number.
In the present embodiment, electric energy carrying device A is preferably high pressure generator, is specifically as follows the voltage of high voltage power transmission
Or higher voltage, it is limited with the ceiling voltage that the mankind accomplish, electric energy carrying device A is connect with antenna, and antenna to releasing in the air
Electric discharge energy, makes charging particle, as shown in charged particle C in Fig. 1 and Fig. 2.
It in the present embodiment, specifically can be using such as one or a combination set of flowering structure:
Structure one: as shown in Figure 1, the structure includes flight instruments B, Laser emission dress is carried on the flight instruments B
D is set, the laser beam emitting device D emits laser to the ground and makes the air ionization of laser traffic areas；
It further include electric energy carrying device A, the electric energy carrying device A is set on flight instruments and/or flight instruments
Isolated area under or, the flight instruments are equipped with antenna；
Structure two: as shown in Fig. 2, include flight instruments B, be provided on the flight instruments B laser receiver F or
Laser beam emitting device D further includes being provided with the ground installation of laser beam emitting device D or laser receiver F, such as flight instruments
It is provided with laser receiver F on B, laser beam emitting device D is provided on ground installation；Or it is provided on flight instruments B sharp
Light emitting devices D is provided with laser receiver F on ground installation.The laser beam emitting device D is sent out to laser receiver F
It penetrates laser and makes the air ionization of laser traffic areas, the flight instruments are equipped with antenna, the flight instruments and/or ground
Electric energy carrying device A is set on device, or electric energy carrying device is arranged in the isolated area on or below flight instruments.
Multiple no pylon weather regulating systems can be set in a piece of regional scope, it specifically can be all using structure
One, it can also can also be used in mixed way all using structure two with structure one and structure two.
In the present embodiment, ground installation is ground mobile device.Specific flight instruments can be unmanned plane or gas
Ball, ground mobile device can be vehicle.Ground mobile device and flight instruments in the horizontal direction mobile synchronous, that is, guarantee
Ground mobile device and flight instruments relative position in the horizontal direction are constant, and preferably ground mobile device is located at flight instruments
Underface.
In the present embodiment, laser beam emitting device is any laser that can be realized air ionization, is specifically as follows
But it is not limited to x-ray laser or ultraviolet laser, when carrying out practically, settable operating area avoids or limit people
Member enters.
In structure two, also there is photoelectric conversion device on laser receiver, the photoelectric conversion device receives laser
Signal is simultaneously generated electricity using laser, for example, by using semiconductor photoproduction volt device, is absorbed laser signal and is converted to laser signal
Electric energy.Photoelectric conversion device stores electric power, is perhaps transferred to electric energy carrying device or is transferred to the energy storage part of flight instruments
Part, or it is transferred to the energy storage component of ground mobile device.
It in the present embodiment, further include sender unit (such as sending communication information), the sender unit
The signal of generation is sent out by the antenna of flight instruments, and the prior art can be used in the specific principle that sends.And/or including letter
Number reception device (such as receiving the control information of aircraft or the modulation intelligence of laser signal), the signal receiving device
The control command of flight instruments is received by the air or wireless transfer channel of ionization and controls flight instruments operation；Or it receives
The modulation intelligence of laser signal successively adjusts the operation of laser.Concrete signal sending device and signal receiving device can be set
It is placed on flight instruments, also can be set on ground.
In another embodiment, as shown in Fig. 2, laser signal modulator E or flying vehicles control are arranged on the ground
Device adjusts the operation of laser by sending modulated signal to signal receiving device.
In structure one, when laser beam emitting device emits laser and makes the air ionization of laser traffic areas, antenna passes through
The isolated area on or below flight instruments is arranged in the air and the earth equipotential of ionization, electric energy carrying device.
In structure two, when laser beam emitting device emits laser and makes the air ionization of laser traffic areas, the flight dress
It sets and ground installation equipotential.
It is of the invention without pylon weather regulating system use flight instruments, flight instruments antenna and ground equipotential or with
Ground insulation does not need setting pylon energy with the pressure difference of mKV between antenna and ground or antenna and electric energy carrying device
The adjusting for enough realizing weather, has saved cost；Without pylon weather regulating system movable operation, system acts on model for this
Enclose big, input-output ratio height.
When electric energy carrying device is arranged on flight instruments and/or ground installation, it is arranged under or over flight instruments
There is ground connection or be electrically insulated with the electric energy carrying device and earth-free metal driving device, when driving device is taken positioned at electric energy
When under band device, the driving device has upward driving tip compared to electric energy carrying device；When driving device is located at
When on electric energy carrying device, the electric energy carrying device has driving tip equivalent upwards compared to driving device.Electric energy
Carrying device makes surrounding air and haze charging particle, and position is located at the high voltage direct current carrying portion of lower part or driving device will be all
High-altitude is sent in a large amount of charged haze particles or the negative oxygen ion driving enclosed.Between electric energy carrying device of the present invention and driving device
Strong electrical field is formed, no matter high voltage direct current, which carries position, is located at high voltage direct current setting in driving device lower part or driving device position
Electricity, which carries subordinate portion, will all make surrounding air and haze charging particle, and by a large amount of charged haze particles of surrounding or negative oxygen from
High-altitude is sent in son driving, has very high pushing efficiency.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or spy described in conjunction with this embodiment or example
Point is included at least one embodiment or example of the invention.In the present specification, schematic expression of the above terms are not
Centainly refer to identical embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be any
One or more embodiment or examples in can be combined in any suitable manner.
Although an embodiment of the present invention has been shown and described, it will be understood by those skilled in the art that: not
A variety of change, modification, replacement and modification can be carried out to these embodiments in the case where being detached from the principle of the present invention and objective, this
The range of invention is defined by the claims and their equivalents.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811532746.1A CN109479592A (en) | 2018-12-14 | 2018-12-14 | A kind of no pylon weather regulating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811532746.1A CN109479592A (en) | 2018-12-14 | 2018-12-14 | A kind of no pylon weather regulating system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109479592A true CN109479592A (en) | 2019-03-19 |
Family
ID=65710362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811532746.1A Pending CN109479592A (en) | 2018-12-14 | 2018-12-14 | A kind of no pylon weather regulating system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109479592A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607018A (en) * | 2020-12-07 | 2021-04-06 | 华中科技大学 | Platform is scattered to electrified particle of no ground connection aircraft |
| CN116584266A (en) * | 2023-05-10 | 2023-08-15 | 广西壮族自治区农业科学院 | Unmanned aerial vehicle sugarcane electric shock equipment with high-voltage discharge function and application method thereof |
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|---|---|---|---|---|
| CN1434671A (en) * | 2002-01-24 | 2003-08-06 | 中国科学院物理研究所 | Laser lightning leading device |
| CN103326478A (en) * | 2013-06-27 | 2013-09-25 | 北京空间机电研究所 | Spatial solar energy wireless transmission method based on laser-induce plasma body |
| CN203775217U (en) * | 2014-01-21 | 2014-08-13 | 桂林航天光比特科技股份公司 | Aircraft laser energy supply communication system |
| CN104686264A (en) * | 2015-02-12 | 2015-06-10 | 华中科技大学 | Method and device for artificially falling rain and snow by sowing charges in air |
| CN104737867A (en) * | 2015-02-12 | 2015-07-01 | 华中科技大学 | Regional joint catalytic snow and rain falling device and method |
| CN105977621A (en) * | 2016-06-08 | 2016-09-28 | 武汉芯泰科技有限公司 | Air antenna preparation method and communication method |
| CN108539877A (en) * | 2017-12-22 | 2018-09-14 | 天津蓝天太阳科技有限公司 | A kind of Intelligent laser energy supplying system for long-range free space |
| CN209449358U (en) * | 2018-12-14 | 2019-10-01 | 黄朝一 | Towerless Weather Conditioning System |
-
2018
- 2018-12-14 CN CN201811532746.1A patent/CN109479592A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1434671A (en) * | 2002-01-24 | 2003-08-06 | 中国科学院物理研究所 | Laser lightning leading device |
| CN103326478A (en) * | 2013-06-27 | 2013-09-25 | 北京空间机电研究所 | Spatial solar energy wireless transmission method based on laser-induce plasma body |
| CN203775217U (en) * | 2014-01-21 | 2014-08-13 | 桂林航天光比特科技股份公司 | Aircraft laser energy supply communication system |
| CN104686264A (en) * | 2015-02-12 | 2015-06-10 | 华中科技大学 | Method and device for artificially falling rain and snow by sowing charges in air |
| CN104737867A (en) * | 2015-02-12 | 2015-07-01 | 华中科技大学 | Regional joint catalytic snow and rain falling device and method |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607018A (en) * | 2020-12-07 | 2021-04-06 | 华中科技大学 | Platform is scattered to electrified particle of no ground connection aircraft |
| CN116584266A (en) * | 2023-05-10 | 2023-08-15 | 广西壮族自治区农业科学院 | Unmanned aerial vehicle sugarcane electric shock equipment with high-voltage discharge function and application method thereof |
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Application publication date: 20190319 |