CN108284954A - A kind of unmanned increasing rain aircraft - Google Patents
A kind of unmanned increasing rain aircraft Download PDFInfo
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- CN108284954A CN108284954A CN201711293274.4A CN201711293274A CN108284954A CN 108284954 A CN108284954 A CN 108284954A CN 201711293274 A CN201711293274 A CN 201711293274A CN 108284954 A CN108284954 A CN 108284954A
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- rain
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- 238000010899 nucleation Methods 0.000 claims abstract description 34
- 239000002245 particle Substances 0.000 claims abstract description 27
- 238000001514 detection method Methods 0.000 claims abstract description 18
- 238000001556 precipitation Methods 0.000 claims abstract description 10
- 238000003384 imaging method Methods 0.000 claims abstract description 9
- 239000000523 sample Substances 0.000 claims description 19
- 239000003795 chemical substances by application Substances 0.000 claims description 15
- 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 13
- 229910021612 Silver iodide Inorganic materials 0.000 claims description 13
- 229940045105 silver iodide Drugs 0.000 claims description 13
- 238000006555 catalytic reaction Methods 0.000 claims description 9
- 150000001875 compounds Chemical class 0.000 claims description 9
- 238000001228 spectrum Methods 0.000 claims description 7
- 210000001015 abdomen Anatomy 0.000 claims description 6
- 239000000443 aerosol Substances 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 238000000748 compression moulding Methods 0.000 claims description 3
- 238000009792 diffusion process Methods 0.000 claims description 3
- 239000003365 glass fiber Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 230000006911 nucleation Effects 0.000 claims description 3
- 238000013439 planning Methods 0.000 claims description 3
- 239000013612 plasmid Substances 0.000 claims description 3
- 238000009331 sowing Methods 0.000 claims description 3
- 238000003786 synthesis reaction Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 2
- 238000004458 analytical method Methods 0.000 abstract description 3
- 230000005540 biological transmission Effects 0.000 abstract description 3
- 238000005259 measurement Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000000116 mitigating effect Effects 0.000 description 2
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 239000005427 atmospheric aerosol Substances 0.000 description 1
- 230000037396 body weight Effects 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- WVXWEYJXFYCIDJ-UHFFFAOYSA-L disilver;diiodide Chemical compound [Ag+].[Ag+].[I-].[I-] WVXWEYJXFYCIDJ-UHFFFAOYSA-L 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035479 physiological effects, processes and functions Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000001931 thermography Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bomb doors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Investigating Or Analysing Materials By Optical Means (AREA)
Abstract
The present invention provides a kind of unmanned increasing rain aircrafts, the unmanned rain aircraft that increases is equipped with cloud particle detection system and cloud macroscopic imaging systems, detection image and data are real-time transmitted to ground control centre by Air-Ground data Transmission system, carry out atmospheric conditions analysis, realizes meteorological detection function.By analyzing unmanned increasing rain airplane sounding the data obtained and image, if cloud layer has artificial precipitation condition, instruction of increasing rain artificially can be sent out to the unmanned rain machine that increases, function of increasing rain artificially finally is realized by flame seeding device and flame bullet seeding device.
Description
Technical field
The present invention relates to unmanned Special Aircraft field, especially a kind of unmanned increasing rain aircraft.
Background technology
There are mainly two types of modes for country's artificial snowfall operation at present：Manned aircraft urges rain operation and ground shell, fire
Arrow urges rain operation.Manned aircraft is suitble to work continuously to stratiform precipitable water cloud system, by a variety of sowing apparatus that catalyst is straight
It connects and is sown into cloud.But manned increase rain artificially aircraft utilization and maintenance cost height, flight formality is cumbersome, easily by weather condition system
About.And unmanned plane be it is a kind of can remote control distributor can autonomous flight unmanned vehicle, production cost is only someone
5%~15% to drive an airplane, flight cost be only its 1%~5%.With economical and practical, operation is flexible, safe and reliable, load
Lotus diversification, performance the advantages such as are not limited by Human Physiology condition.
Invention content
The object of the present invention is to provide it is a kind of integrate the functions such as meteorological detection and artificial snowfall operation it is extraordinary nobody
Machine.
A kind of unmanned increasing rain aircraft, using no swept-back high mounted wing, wing planform uses RECTANGULAR WINGS, and aerofoil profile is using high
Lift laminar flow airfoil, nacelle formula fuselage, twin beams brace type empennage, separate unit push type piston engine, bikini undercarriage layout,
The unmanned rain aircraft that increases has autonomous landing and by task trajectory planning autonomous flight function, and during task Reprogrammable or
Remote driving, body uses carbon fiber and glass fiber compound material hot compression molding, unmanned to increase rain aircraft maximum take-off weight
Not less than 1100kg, 200~300km/h of max level speed, max-endurance is not less than 6h, and ceiling is not less than 6000m, should
Unmanned increasing rain machine is integrated with meteorological detection system and artificial rain operation sows system, and meteorological detection and artificial snowfall operation function is made to close
It is integrated.
Meteorological detection system includes fuselage head equipped with extension type synthesis meteorological measuring system probe；Left side fuselage stage casing fills
There are cloud particle spectrum probe (CDP) and back scattering cloud dimension physical characteristic probe (BCP)；Right side fuselage stage casing is equipped with particulate
Spectrometer (PCASP-100X+SPP200)；Middle fuselage top left side is equipped with cloud particle coupling probe (CIP)；At the top of middle fuselage
Right side is equipped with precipitation particles imaging probe (PIP)；Wide-angle cloud macroscopic view imager is housed at the top of nosing；At the top of aft body and
Abdomen respectively fills a uncooled infrared imager instrument.
The artificial rain operation system of sowing includes that respectively one flame seeding device of hanging and belly install a flame to left and right wing
Seeding device is played, under the premise of ensureing that flame item sows operation, flame seeding device uses pyramid type head, cylindrical type stage casing to shrink
Type tail cone, flame seeding device meet certain slenderness ratio, and the tangential securement head of flame seeding device protrudes the leading edge of a wing, flame seeding device
It is mainly used to carry out silver iodide or the catalysis of warm cloud flame agent is sowed, ignition generation is shocked by electricity largely by the compound flame agent of silver iodide
Silver iodide aerosol, generation surface is strong at ice activity, and the high thin clouds colloidal sol plasmid of nucleation rate, flame agent is oriented by unmanned plane toward cloud
In sow, by the eddy diffusion of aircraft, there is certain catalysis depth；Equivalent section is bored using inverted triangle among flame bullet seeding device
Shape section is designed, and the left and right sides can respectively load 100 pieces of flame bullets, equivalent section front and back belt radome fairing, can be installed and be sowed a little in radome fairing
Fire and control device, the smooth streamline of flame bullet seeding device monnolithic case.Flame bullet seeding device is mainly used to carry out silver-colored flame agent to sow, and passes through
The compound flame agent burning of silver iodide generates a large amount of silver iodide aerosols, and flame bullet vertical mounting surface emits obliquely, and transmitting has certain
Range, after being sowed into cloud, flame bullet burning fall, have certain catalysis depth.
The unmanned rain aircraft that increases is equipped with cloud particle detection system and cloud macroscopic imaging systems, and detection image and data are led to
It crosses Air-Ground data Transmission system and is real-time transmitted to ground control centre, carry out atmospheric conditions analysis, realize meteorological detection function.It is logical
It crosses and unmanned increasing rain airplane sounding the data obtained and image is analyzed, it, can be to nobody if cloud layer has artificial precipitation condition
Increase rain machine and send out instruction of increasing rain artificially, function of increasing rain artificially finally is realized by flame seeding device and flame bullet seeding device.
Description of the drawings
Fig. 1 left side views
Fig. 2 right side views
Fig. 3 front views
Fig. 4 rearviews
Fig. 5 vertical views
Fig. 6 upward views
Fig. 7 task devices schematic layout pattern one
Fig. 8 task devices schematic layout pattern two
Fig. 9 long endurance flame schematic layout patterns
Explanation is numbered in figure：101, comprehensive meteorological measuring system probe；102, back scattering cloud dimension physical characteristic probe；
103, cloud particle coupling probe；104, precipitation particles imaging probe；105, wide-angle cloud macroscopic view imager；106, uncooled IRFPA is infrared
Thermal imaging system；107, flame seeding device；108, flame bullet seeding device；109, particulate spectrometer
Specific implementation mode
According to the present invention, it is described it is unmanned increase rain aircraft using no swept-back high mounted wing (wing planform using RECTANGULAR WINGS,
Shape is succinct, simple for process, at low cost；Aerofoil profile uses high-lift laminar flow airfoil, and with lower cruise drag, climb lift resistance ratio
Greatly, maximum lift coefficient is high, stalling characteristics compare mitigation), nacelle formula fuselage, twin beams brace type empennage, separate unit push type piston
Engine, bikini undercarriage layout (being specifically shown in attached drawing 1~6), the unmanned plane have autonomous landing and by task trajectory plannings
Autonomous flight function, and Reprogrammable or remote driving during task.For mitigation body weight, mission payload is improved, and
And considering the requirement of built-in antenna equipment wave, body uses carbon fiber and glass fiber compound material hot compression molding.The nothing
People increases rain aircraft maximum take-off weight and is not less than 1100kg, 200~300km/h of max level speed, and max-endurance is small
In 6h, ceiling is not less than 6000m.
For the detection demand for meeting to air cloud particle, unmanned increase is configured with Cloud particle detection system on rain machine
With wide angle imaging system (being specifically shown in attached drawing 7~8)：
Fuselage head is mainly used for and cloud precipitation Microphysical equipped with extension type synthesis meteorological measuring system probe (ADP) 101
The measurement for the air temperature and pressure wet wind and airplane motion parameter that measurement data matches, detection content includes air speed, the angle of attack, sideslip
The GPS information of angle, air pressure and relative humidity and aircraft.
Physical characteristic probe (BCP) 102 is tieed up in left side fuselage stage casing equipped with cloud particle spectrum probe (CDP) and back scattering cloud,
CDP mainly measures the cloud particle of 2~50um, and BCP mainly surveys the cloud particle scale spectrum of 5~75um
Amount, calculates the data such as total number density, Liquid water content, median diameter, the effective diameter of this range cloud particle.
Right side fuselage stage casing is used for equipped with particulate spectrometer (PCASP-100X+SPP200) 109, PCASP-100X
Atmospheric aerosol particle diameter spectrum within the scope of a diameter of 0.1~3um is measured, and SPP200 is installed on PCASP-100X
It is mainly used to monitor sampling air flow and sheath gas.
Middle fuselage top left side is equipped with cloud particle coupling probe (CIP) 103, mainly measures the cloud particle of 15~930um
Son spectrum and its particle two dimensional image, including Liquid water content (0.01~3g/m of measurement range3), temperature, air pressure, relative humidity pass
Sensor.
Middle fuselage top right side is equipped with precipitation particles imaging probe (PIP) 104, and resolution ratio 100um can be measured big
The small atmospheric particles between 100~6200um are mainly used for the measurement of larger water particle concentration and size and image in cloud.It can
Measure size and shape, the two dimensional image for generating precipitation particles and the one-dimensional particle spectra of precipitation particles.
Wide-angle cloud macroscopic view imager 105 is housed at the top of nosing, the cloud profile in aircraft forward fixed range is carried out
Shooting realizes the imaging of cloud macroscopic view, there is stabilization function.
At the top of aft body and abdomen respectively fills a uncooled infrared imager instrument 106, above and below to carrier aircraft
Cloud layer, observe the distribution and variation of cloud layer.
To realize the purpose increased rain artificially, it is described it is unmanned increase equipment artificial rain operation on rain machine and sow system (be specifically shown in attached drawing 7
~8)：
Respectively one flame seeding device 107 of hanging, each seeding device can respectively carry 20 flame items to left and right wing, to meet
Different artificial rain operation demands, it is also optional to hang diameter and the smaller flame seeding device 107 (being specifically shown in attached drawing 9) of weight, each sow
Device can carry 10 flame items, alleviate mission payload, increase cruise duration.Flame seeding device is mainly used to carry out silver iodide or warm
The catalysis of cloud flame agent is sowed, and is generated a large amount of silver iodide aerosols by the compound flame agent electric shock ignition of silver iodide, is generated surface
Strong, the high thin clouds colloidal sol plasmid of nucleation rate at ice activity.Flame agent is oriented by unmanned plane sows into cloud, passes through the power of aircraft
Diffusion has certain catalysis depth.
Belly installs a flame bullet seeding device 108, front and back belt radome fairing, and the straight sections such as centre left and right sides can respectively load
100 pieces of flame bullets.It is mainly used to carry out silver-colored flame agent to sow, passes through the compound flame agent burning of silver iodide and generate a large amount of silver iodide aerosols.
Flame bullet vertical mounting surface emits obliquely, and transmitting has certain range, and after being sowed into cloud, the burning of flame bullet is fallen, and is had certain
Catalysis depth.
According to the present invention, the unmanned rain aircraft that increases is equipped with cloud particle detection system and cloud macroscopic imaging systems, and detection is schemed
Picture and data are real-time transmitted to ground control centre by Air-Ground data Transmission system, carry out atmospheric conditions analysis, realize meteorological
Detecting function.By analyzing unmanned increasing rain airplane sounding the data obtained and image, if cloud layer has artificial precipitation condition,
Can then instruction of increasing rain artificially be sent out to the unmanned rain machine that increases, work(of increasing rain artificially finally is realized by flame seeding device and flame bullet seeding device
Energy.
Claims (3)
1. a kind of unmanned increasing rain aircraft, using no swept-back high mounted wing, wing planform uses RECTANGULAR WINGS, aerofoil profile to use promotion
Power laminar flow airfoil, nacelle formula fuselage, twin beams brace type empennage, separate unit push type piston engine, bikini undercarriage layout, nothing
People increases rain aircraft and has autonomous landing and by task trajectory planning autonomous flight function, and the Reprogrammable or distant during task
Control drives, and body uses carbon fiber and glass fiber compound material hot compression molding, unmanned to increase rain aircraft maximum take-off weight not
Less than 1100kg, 200~300km/h of max level speed, max-endurance is not less than 6h, and ceiling is not less than 6000m, special
Sign is that unmanned increasing rain machine is integrated with meteorological detection system and artificial rain operation sows system, makes meteorological detection and artificial snowfall operation
Function is integrated.
2. a kind of unmanned increasing rain aircraft according to claim 1, it is characterised in that the meteorological detection system includes fuselage
Head is equipped with extension type synthesis meteorological measuring system probe；Left side fuselage stage casing is dissipated equipped with cloud particle spectrum probe (CDP) and backward
Penetrate cloud dimension physical characteristic probe (BCP)；Right side fuselage stage casing is equipped with particulate spectrometer (PCASP-100X+SPP200)；Machine
Body stage casing top left side is equipped with cloud particle coupling probe (CIP)；Middle fuselage top right side is equipped with precipitation particles imaging probe
(PIP)；Wide-angle cloud macroscopic view imager is housed at the top of nosing；At the top of aft body and abdomen respectively fills the infrared heat of uncooled IRFPA
Imager.
A kind of unmanned increase rain aircraft 3. according to claim 1, it is characterised in that the artificial rain operation system of sowing includes
Respectively one flame seeding device of hanging and belly install a flame bullet seeding device to left and right wing, and operation is sowed in guarantee flame item
Under the premise of, flame seeding device uses pyramid type head, and cylindrical type stage casing, shrinkage type tail cone, it is thin that flame seeding device meets a fixed length
Than the tangential securement head of flame seeding device protrudes the leading edge of a wing, and flame seeding device is mainly used to carry out silver iodide or warm cloud flame agent
Catalysis sow, a large amount of silver iodide aerosols are generated by the compound flame agent of silver iodide ignition of shocking by electricity, surface is generated and lives at ice
Strong, the high thin clouds colloidal sol plasmid of nucleation rate of property, flame agent are oriented by unmanned plane and are sowed into cloud, by the eddy diffusion of aircraft,
With certain catalysis depth；Equivalent section is designed using inverted triangle taper section among flame bullet seeding device, and the left and right sides can respectively fill
100 pieces of flame bullets are carried, equivalent section front and back belt radome fairing can be installed in radome fairing and sow igniting and control device, and flame bullet seeding device is whole
Body smooth-shaped streamline.Flame bullet seeding device is mainly used to carry out silver-colored flame agent to sow, and is generated by the compound flame agent burning of silver iodide big
Silver iodide aerosol is measured, flame bullet vertical mounting surface emits obliquely, and transmitting has certain range, after being sowed into cloud, flame bullet
Burning is fallen, and has certain catalysis depth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711293274.4A CN108284954A (en) | 2017-12-08 | 2017-12-08 | A kind of unmanned increasing rain aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711293274.4A CN108284954A (en) | 2017-12-08 | 2017-12-08 | A kind of unmanned increasing rain aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108284954A true CN108284954A (en) | 2018-07-17 |
Family
ID=62831883
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711293274.4A Pending CN108284954A (en) | 2017-12-08 | 2017-12-08 | A kind of unmanned increasing rain aircraft |
Country Status (1)
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| CN (1) | CN108284954A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110175793A (en) * | 2019-06-14 | 2019-08-27 | 吉林工程技术师范学院 | A kind of course line design method of increasing rain artificially based on ground demand analysis |
| CN111610793A (en) * | 2019-02-26 | 2020-09-01 | 北京京东尚科信息技术有限公司 | Artificial rainfall method and device |
| CN112793782A (en) * | 2021-01-14 | 2021-05-14 | 青海大学 | Rain and snow increasing method and system based on unmanned aerial vehicle |
| CN114384828A (en) * | 2020-10-16 | 2022-04-22 | 中航西飞民用飞机有限责任公司 | Airplane rain enhancement control system and control method |
| CN117898156A (en) * | 2024-03-07 | 2024-04-19 | 成都润联科技开发有限公司 | Artificial weather intervention system based on unmanned aerial vehicle |
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| CN117898156A (en) * | 2024-03-07 | 2024-04-19 | 成都润联科技开发有限公司 | Artificial weather intervention system based on unmanned aerial vehicle |
| CN117898156B (en) * | 2024-03-07 | 2024-05-31 | 成都润联科技开发有限公司 | Artificial weather intervention system based on unmanned aerial vehicle |
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