CN103241377A - Soft-wing unmanned aerocraft with automatic fog dispersal function - Google Patents
Soft-wing unmanned aerocraft with automatic fog dispersal function Download PDFInfo
- Publication number
- CN103241377A CN103241377A CN2013102012901A CN201310201290A CN103241377A CN 103241377 A CN103241377 A CN 103241377A CN 2013102012901 A CN2013102012901 A CN 2013102012901A CN 201310201290 A CN201310201290 A CN 201310201290A CN 103241377 A CN103241377 A CN 103241377A
- Authority
- CN
- China
- Prior art keywords
- fog dispersal
- equipment
- wing unmanned
- cabin body
- unmanned vehicle
- 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.)
- Granted
Links
- 230000008859 change Effects 0.000 claims abstract description 4
- 238000001514 detection method Methods 0.000 claims abstract description 4
- 239000003795 chemical substances by application Substances 0.000 claims description 32
- IBSREHMXUMOFBB-JFUDTMANSA-N 5u8924t11h Chemical compound O1[C@@H](C)[C@H](O)[C@@H](OC)C[C@@H]1O[C@@H]1[C@@H](OC)C[C@H](O[C@@H]2C(=C/C[C@@H]3C[C@@H](C[C@@]4(O3)C=C[C@H](C)[C@@H](C(C)C)O4)OC(=O)[C@@H]3C=C(C)[C@@H](O)[C@H]4OC\C([C@@]34O)=C/C=C/[C@@H]2C)/C)O[C@H]1C.C1=C[C@H](C)[C@@H]([C@@H](C)CC)O[C@]11O[C@H](C\C=C(C)\[C@@H](O[C@@H]2O[C@@H](C)[C@H](O[C@@H]3O[C@@H](C)[C@H](O)[C@@H](OC)C3)[C@@H](OC)C2)[C@@H](C)\C=C\C=C/2[C@]3([C@H](C(=O)O4)C=C(C)[C@@H](O)[C@H]3OC\2)O)C[C@H]4C1 IBSREHMXUMOFBB-JFUDTMANSA-N 0.000 claims description 19
- 238000004080 punching Methods 0.000 claims description 16
- 238000012544 monitoring process Methods 0.000 claims description 14
- 238000004891 communication Methods 0.000 claims description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 claims description 6
- 238000010899 nucleation Methods 0.000 claims description 5
- 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 4
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 4
- 229910021612 Silver iodide Inorganic materials 0.000 claims description 4
- 235000011089 carbon dioxide Nutrition 0.000 claims description 4
- 239000007788 liquid Substances 0.000 claims description 4
- 229940045105 silver iodide Drugs 0.000 claims description 4
- 241000287127 Passeridae Species 0.000 claims description 3
- XSQUKJJJFZCRTK-UHFFFAOYSA-N Urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 claims description 3
- 239000004202 carbamide Substances 0.000 claims description 3
- 230000003993 interaction Effects 0.000 claims description 3
- 229910052757 nitrogen Inorganic materials 0.000 claims description 3
- 239000002245 particle Substances 0.000 claims description 3
- 239000000843 powder Substances 0.000 claims description 3
- 150000003839 salts Chemical class 0.000 claims description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims 2
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 239000003054 catalyst Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 238000007639 printing Methods 0.000 description 7
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 5
- 229910052731 fluorine Inorganic materials 0.000 description 5
- 239000011737 fluorine Substances 0.000 description 5
- 239000013078 crystal Substances 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000009331 sowing Methods 0.000 description 4
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 239000003595 mist Substances 0.000 description 3
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 150000002430 hydrocarbons Chemical group 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- WQZGKKKJIJFFOK-GASJEMHNSA-N Glucose Natural products OC[C@H]1OC(O)[C@H](O)[C@@H](O)[C@@H]1O WQZGKKKJIJFFOK-GASJEMHNSA-N 0.000 description 1
- 239000004721 Polyphenylene oxide Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 239000003945 anionic surfactant Substances 0.000 description 1
- 210000000481 breast Anatomy 0.000 description 1
- 239000003093 cationic surfactant Substances 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 239000003431 cross linking reagent Substances 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000013530 defoamer Substances 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000008103 glucose Substances 0.000 description 1
- 229930182478 glucoside Natural products 0.000 description 1
- 150000008131 glucosides Chemical class 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 1
- 230000002209 hydrophobic effect Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000004816 latex Substances 0.000 description 1
- 229920000126 latex Polymers 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002736 nonionic surfactant Substances 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 229920000570 polyether Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 230000002940 repellent Effects 0.000 description 1
- 239000005871 repellent Substances 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- CCEKAJIANROZEO-UHFFFAOYSA-N sulfluramid Chemical group CCNS(=O)(=O)C(F)(F)C(F)(F)C(F)(F)C(F)(F)C(F)(F)C(F)(F)C(F)(F)C(F)(F)F CCEKAJIANROZEO-UHFFFAOYSA-N 0.000 description 1
- BDHFUVZGWQCTTF-UHFFFAOYSA-M sulfonate Chemical compound [O-]S(=O)=O BDHFUVZGWQCTTF-UHFFFAOYSA-M 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
Images
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention provides a soft-wing unmanned aerocraft with an automatic fog dispersal function. The soft-wing unmanned aerocraft comprises a flexible stamping parawing, a structure cabin body, a power system, fog dispersal equipment and a control system, wherein the fog dispersal equipment comprises internal fog dispersal equipment and external fog dispersal equipment for simultaneously or respectively scattering an antifogging agent; the internal fog dispersal equipment is arranged in the structure cabin body, and the external fog dispersal equipment is arranged outside the structure cabin body; the internal fog dispersal equipment is composed of a scattering and throwing cabin, a flashboard, a steering engine and a throwing port; the external fog dispersal equipment is composed of fixing frames, scattering and throwing cylinders and exciting electrodes; and the fog dispersal equipment also comprises detection equipment. The soft-wing unmanned aerocraft provided by the invention has the beneficial effects that the operation is safe and reliable, the control is easy, and the carrying capacity is large; the distance range of flying fog dispersal can reach 200 kilometers through remote control and autonomous navigation; the cost is cheap, and the operation is simple and practicable; and the application range is wide, and the soft-wing unmanned aerocraft is suitable for situations needing local fog dispersal, such as improvements on highway traffic environments, dispelling of thick fog of an airport, and change of microclimate of a disaster relief region.
Description
Technical field
The present invention relates to the unmanned vehicle field, particularly, relate to a kind of gentle wing unmanned vehicle with automatic fog dispersal function.
Background technology
Unmanned plane and unmanned vehicle are driverless operation, but the difference of essence is arranged, and unmanned plane is fixed wing, and military use such as be used for high altitude surveillance mostly and attack on a surface target is less as civilian.
In order to adapt to many-sided demand, people study and have made various unmanned vehicles.The patent of invention ZL93202125.5(Granted publication CN2204774Y of research institute of parachutist of the Chinese People's Liberation Army) the flexible punching press parafoil of a kind of active flight is disclosed, the flexible punching press parafoil of this active flight is used for demonstration flight, advertising, frontier defense patrol and amusement flight, in addition, at Chinese utility model patent ZL201220565967.0(Granted publication CN202879795U) in, the use remote controlled powered flexible punching press parafoil of knowing clearly, it can be from ground be pulled by vehicle takes off, also can be from aerial input, can be used for exploration and investigation ground situation, carry out aerial atmospheric contamination sampling and volcano monitoring etc.Have advantages such as in light weight, that cost is low, the stock is convenient.
In the aircraft field, people attempt unmanned vehicle is used for arrtificial fog dissipation, and so-called arrtificial fog dissipation refers to eliminate the interior droplet of regional area to improve the method for visbility with the mode of artificial affecting.Particularly, be to use certain device, catalyst such as silver iodide, dry ice, liquid propane are sowed in the mist, produce a large amount of ice crystals, steam in the fog-zone is sublimated at numerous ice crystals, impels over cooling water droplet evaporation, and namely the ice crystal moisture of capturing former droplet is constantly grown up, drop to ground after ice crystal is grown up, thereby burn-off is lost.
At present, sow the catalyst fog dispersal and mainly contain following several mode:
First kind is aircraft seeding: utilizing transport plane or aviette to carry that the fog dispersal medicament carries out sowing on the mist or in the mist is present main fog dispersal means.Advantage is to carry out quick, large-area fog dispersal operation.But the aircraft fog dispersal has many deficiencies.At first aircraft is bigger in the risk of foggy weather landing and operation, the safety of entail dangers to aircraft and chaufeur; When carrying out aircraft seeding, course line permission and ground control etc. are very complicated; Aircraft flight and sow is highly higherly sowed poor accuracy, in addition, and aircraft utilization cost height.
Second kind is that unmanned plane is sowed: at present, existing relevant research institute carries out unmanned plane (containing fixed-wing unmanned plane and rotor wing unmanned aerial vehicle) and sows.Unmanned plane carries out terrestrial operation by operating personal, so relatively safe.But the unmanned plane capacity weight lower (general capacity weight 10～15kg), the amount of carrying of flight operation is little, the fog dispersal area is little, and unmanned plane takes off and the relative complex of landing, and cost is higher.
The third is that sow on ground: this method need arrange a plurality of catalyst and broadcast sowing a little on ground, count Mi Gaodu on ground and discharge catalyst, but this mode can be subjected to wind direction and wind speed influence.And a plurality of catalyst are set in the fog-zone, and to broadcast sowing the man power and material of a consumption huge.Particularly on express highway, the roadside just needs to settle an instrument of sowing catalyst every nearby on the way, and cost is very high.
Summary of the invention
Technical matters to be solved by this invention, fill up the blank that exists in the prior art exactly, provide a kind of safe and reliable, easy manipulation, with low cost, load carrying ability is big, can make flying distance reach the gentle wing unmanned vehicle of 200 kms by remote control and autonomous navigation, as automatic fog dispersal flight job platform.Particularly, the invention provides a kind of gentle wing unmanned vehicle with automatic fog dispersal function.
The present invention reaches the foregoing invention purpose by the following technical programs.
A kind of gentle wing unmanned vehicle with automatic fog dispersal function is characterized in that, comprising: flexible punching press parafoil, structure cabin body, power system, fog dispersal equipment and control system; Flexible punching press parafoil provides lift to system;
The bottom of flexible punching press parafoil is by umbrella rope connection structure cabin body; Body inside, structure cabin is equipped with control system and built-in fog dispersal equipment, and afterbody is installed power system;
Structure cabin body mainly comprises cabin body framework, mount pad and skid formula alighting gear, mount pad is fixed on cabin body base of frame and stretches out to both sides, external fog dispersal equipment is installed respectively on it, and skid formula alighting gear is installed in body framework bottom, cabin, is used for the buffering of taking off, land of system;
Power system is used for the required power that flies is provided, and mainly comprises driving engine and screw propeller;
Fog dispersal equipment comprises built-in fog dispersal equipment and external fog dispersal equipment, is used for the while or sows antifogging agent separately, and built-in fog dispersal equipment is installed in body inside, structure cabin, and external fog dispersal equipment is installed in structure cabin external body;
Built-in fog dispersal equipment constitutes by throwing loose cabin, plate, steering wheel and dispensing port, throw the cabin of loosing and be installed in the body of structure cabin, the bottom has dispensing port at structure cabin body, and plate is installed in to throw and looses the bottom, cabin and cover dispensing port, steering wheel one end links to each other with plate, and the control of controlled system;
External fog dispersal equipment is made of fixed mount, throw to loose tube and exciting electrode, throws the tube that looses and is fixed on below the mount pad by fixed mount, and exciting electrode is installed together with throwing the tube that looses, and the control of controlled system;
Fog dispersal equipment also comprises the detection detecting devices, detects detecting devices and is provided with: weather radar, satellite receiving equipment, the sub-measuring system of PMS cloud particle, weather meter, GPS location and number biography system, double channels microwave radiometer;
Control system has Navigation Control and communication, monitoring function, comprises navigation elements, control unit, communication unit, video monitoring unit and surface control station;
Navigation elements is used for providing the aerial mission course line and sends steering command to control unit, mainly comprises airborne computer, navigation software, locating module and various sensor; Control unit is used for carrying out the steering command that navigation elements sends, and drives and handles actuating unit, and change of flight attitude and course line mainly comprise driver train and supply module; Communication unit is used for carrying out data interaction between flying body and the surface control station, mainly comprises transmitting station and receiving wire; The video monitoring unit is used for passing to ground station under the video that the video prison bat equipment of installing on the flying body is captured and showing at telltale; Setting, the input of status data, sending with the monitoring of flight path with to the reception of flying body feedback data of flight directive that surface control station is used for finishing to flight path are handled, and mainly comprise hand-held remote control device and watch-dog.
In the gentle wing unmanned vehicle with automatic fog dispersal function of the present invention, fog dispersal equipment can also have airborne silver iodide producer, the liquid nitrogen producer, and equipment sowed by flame bullet producer, dry ice seeding device, salt powder, urea and HB-1 type antifogging agent is sowed equipment.
Gentle wing unmanned vehicle with automatic fog dispersal function of the present invention can adopt the ground launch, above-ground launcher comprises tractor truck, emission permanent seat, disconnecting gear and protective device, is used for having the gentle wing unmanned vehicle of automatic fog dispersal function from the ground launch.
The emission firm banking is located on the tractor truck; Armed gentle wing unmanned vehicle with automatic fog dispersal function places on the emission firm banking, and by belt tensioner with tighten up capstan winch and be connected; Protective device is located at the front end of emission base; Disconnecting gear is located at emission firm banking middle part, is positioned at unmanned plane to be launched below.
Gentle wing unmanned vehicle with automatic fog dispersal function of the present invention also can be by installing dropping gear emission aboard.
Gentle wing unmanned vehicle with automatic fog dispersal function of the present invention can also supportingly arrange the ground remote control system, it controls this flexibility punching press parafoil unmanned plane during flying behind predetermined altitude, fly to the coordinates of targets point according to contemplated route, finish at the task object point and to sow antifogging agent automatically after the task of fog dispersal, turn back to the spatial domain, destination according to projected route, and decision height information and landing site wind direction information, the mode that adopts sparrow to fall realizes pinpoint landing.
When needs dispersed fog, the wing unmanned vehicle flight that softens arrived the designated area, from external fog dispersal equipment input fog dispersal medium or from built-in fog dispersal equipment input fog dispersal medium or simultaneously from inside and outside input fog dispersal medium.
Compared with prior art, the present invention has following beneficial effect:
1. safe and reliable, easy manipulation, load carrying ability are big;
2. can make flight fog dispersal distance range reach 200 kms by remote control and autonomous navigation;
3. with low cost, simple;
4. range of use is wide, and every relating to need be in the situation of subrange fog dispersal, and the environment that for example improves highway communication, elimination airport thick fog improve disaster relief zone micrclimate etc., all can be suitable for.
Description of drawings
Fig. 1 is the overall appearance scheme drawing with gentle wing unmanned vehicle of automatic fog dispersal function of the present invention
Fig. 2 is the structural representation with gentle wing unmanned vehicle of automatic fog dispersal function of the present invention
Fig. 3 is the fog dispersal equipment structure chart with gentle wing unmanned vehicle of automatic fog dispersal function of the present invention
Fig. 4 is the control system figure with gentle wing unmanned vehicle of automatic fog dispersal function of the present invention
Fig. 5 is the connection diagram with gentle wing unmanned vehicle and ground traction feedway of automatic fog dispersal function of the present invention
Fig. 6 is the gentle wing unmanned vehicle system chart with automatic fog dispersal function of the present invention
Fig. 7 is the gentle wing unmanned vehicle ground with the automatic fog dispersal function of the present invention scheme drawing that takes off
Fig. 8 is the gentle wing unmanned vehicle air-drop emission scheme drawing with automatic fog dispersal function of the present invention
Among the figure: the flexible punching press parafoil of 1-, 2-structure cabin body, 3-power system, the 5-control system, 6-launches permanent seat, 7-tractor truck, 8-umbrella rope, 9-mount pad, 10-cabin body framework, 11-skid formula alighting gear, 12-driving engine, 13-screw propeller, the built-in fog dispersal equipment of 14-, the external fog dispersal equipment of 15-, 16-throws the cabin of loosing, the 17-plate, 18-steering wheel, 19-dispensing port, the 20-fixed mount, 21-throws the tube that looses, 22-exciting electrode, the 23-navigation elements, 24-control unit, 25-communication unit, 26-video monitoring unit, 27-surface control station, 28-disconnecting gear, the 29-protective device, the 30-belt tensioner, 31-tightens up capstan winch.
The specific embodiment
Further the present invention will be described by the following examples.
Fig. 1 is the schematic appearance of the gentle wing unmanned vehicle of the automatic fog dispersal function of having of present embodiment, and Fig. 2 is the structural representation of the gentle wing unmanned vehicle of the automatic fog dispersal function of having of present embodiment.Referring to Fig. 1 and Fig. 2, the gentle wing unmanned vehicle that present embodiment has automatic fog dispersal function comprises: flexible punching press parafoil 1, structure cabin body 2, power system 3, fog dispersal equipment and control system 5; Flexible punching press parafoil 1 provides lift to system.
The bottom of flexible punching press parafoil 1 is by umbrella rope 8 connection structure cabin bodies 2; Body 2 inside, structure cabin are equipped with control system 5 and built-in fog dispersal equipment 14, and afterbody is installed power system 3.
Structure cabin body 2 mainly comprises cabin body framework 10, mount pad 9 and skid formula alighting gear 11.Mount pad 9 is fixed on body framework 10 bottoms, cabin and stretches out to both sides, and external fog dispersal equipment 15 is installed respectively on it, and skid formula alighting gear 11 is installed in body framework 10 bottoms, cabin, is used for the buffering of taking off, land of system.
Fig. 3 is the fog dispersal equipment structure chart of the gentle wing unmanned vehicle of the automatic fog dispersal function of having of present embodiment, and as seen from Figure 3, fog dispersal equipment is the emphasis parts of present embodiment, and fog dispersal equipment comprises built-in fog dispersal equipment 14 and external fog dispersal equipment 15.As seen from Figure 3: built-in fog dispersal equipment 14 is installed in body 2 inside, structure cabin, and external fog dispersal equipment 15 is installed in body 2 outsides, structure cabin.
Built-in fog dispersal equipment 14 constitutes by throwing loose cabin 16, plate 17, steering wheel 18 and dispensing port 19, throwing the cabin 16 of loosing is installed in the structure cabin body 2, the bottom has dispensing port 19 at structure cabin body 2, plate 17 is installed in to throw and looses 16 bottoms, cabin and cover dispensing port 19, steering wheel 18 1 ends link to each other with plate 17, and 5 controls of controlled system.
The working process of built-in fog dispersal equipment 14 is as follows: control system 5 control steering wheels 18, steering wheel 18 pulling plates 17 are opened dispensing port 19, launch smoothly being placed in the antifogging agent of throwing in the cabin 16 of loosing in advance.
External fog dispersal equipment 15 is made of fixed mount 20, throw to loose tube 21 and exciting electrode 22, throws the tube 21 that looses and is fixed on below the mount pad 9 by fixed mount 20, and exciting electrode 22 is installed together with throwing the tube 21 that looses, 5 controls of controlled system.
The working process of external fog dispersal equipment 15 is as follows: control system 5 is controlled exciting electrodes 2, excites and throws the tube 21 that looses, and with placing the antifogging agent of throwing 21 li in diffusing tube to spill in advance, finishes fog dispersal.
Built-in fog dispersal equipment 14 and external fog dispersal equipment 15 can simultaneously or be sowed antifogging agent separately, fog dispersal equipment also comprises the detection detecting devices, detects detecting devices and is provided with: weather radar, satellite receiving equipment, the sub-measuring system of PMS cloud particle, weather meter, GPS location and number biography system, double channels microwave radiometer.
In the gentle wing unmanned vehicle of the automatic fog dispersal function of having of present embodiment, fog dispersal equipment can also have airborne silver iodide producer, the liquid nitrogen producer, and equipment sowed by flame bullet producer, dry ice seeding device, salt powder, urea and HB-1 type antifogging agent is sowed equipment.
Fig. 4 is the control system figure of the gentle wing unmanned vehicle of the automatic fog dispersal function of having of present embodiment, as seen from Figure 4, control system 5 has Navigation Control and communication, monitoring function, comprises navigation elements 23, control unit 24, communication unit 25, video monitoring unit 26 and surface control station 27.
Fig. 5 is the connection diagram of gentle wing unmanned vehicle and the ground traction feedway of the automatic fog dispersal function of having of present embodiment, referring to Fig. 5, above-ground launcher comprises tractor truck 7, emission permanent seat 6, disconnecting gear 28 and protective device 29, is used for having the gentle wing unmanned vehicle of automatic fog dispersal function from the ground launch.
Emission firm banking 6 is located on the tractor truck 7; Armed gentle wing unmanned vehicle with automatic fog dispersal function places on the emission firm banking 6, and by belt tensioner 30 with tighten up capstan winch 31 and be connected; Protective device 29 is located at the front end of emission base; Disconnecting gear 28 is located at emission firm banking 6 middle parts, is positioned at unmanned plane to be launched below.Concrete working process is at utility model patent ZL201220565967.0(Granted publication CN202879795U) in open, no longer describe in detail here.
Fig. 6 is the system chart that the present invention has the gentle wing unmanned vehicle of automatic fog dispersal function.
Fig. 7 is gentle wing unmanned vehicle ground with the automatic fog dispersal function scheme drawing that takes off, and concrete take-off process is at utility model patent ZL201220565967.0(Granted publication CN202879795U) in open, no longer describe in detail here.After the gentle wing unmanned vehicle that control has an automatic fog dispersal function rises to predetermined altitude, fly to the coordinates of targets point according to contemplated route, finish at the task object point and to sow antifogging agent automatically after the task of fog dispersal, turn back to the spatial domain, destination according to projected route again, and decision height information and landing site wind direction information, the mode that adopts sparrow to fall realizes pinpoint landing.
Fig. 8 is the gentle wing unmanned vehicle air-drop emission scheme drawing with automatic fog dispersal function of the present invention.Self-evident, those skilled in the art can implement the air-drop emission to the gentle wing unmanned vehicle with automatic fog dispersal function with reference to Fig. 8 and description of the present invention fully.
Adopt gentle wing unmanned vehicle to carry out fog dispersal operation, it is a kind of fog dispersal operation method of having no precedent, because gentle wing unmanned vehicle is wing with large tracts of land punching press parafoil, the aerodynamic drag that this parafoil produces is enough to avoid the gentle wing unmanned vehicle ground of can at full speed not landing to make equipment impaired, so in a sense, the safety of gentle wing unmanned vehicle is far above unmanned plane even be higher than some manned aircraft.
What present embodiment adopted has related parameter as follows:
Capacity weight: 〉=200kg;
Fuel weight: 〉=60kg;
Take-off weight :≤500kg;
Cruise duration: 〉=6h;
Cruising speed :≤50km/h;
Ceiling altitude height above sea level: 5000m;
Mode: remote manual control and autonomous navigation, the automatic navigation control pattern possesses external interface, can import the object point coordinate before using temporarily;
Remote manual control distance: 10km(add increase journey);
The mode of taking off: car launcher rope start;
Take off distance :≤150m;
Alighting gear: skid formula alighting gear;
Landing modes: remote manual control and independent landing;
The lift-launch interface and the control that possess fog dispersal equipment start interface;
The employed antifogging agent of present embodiment: antifogging agent is divided into the jet printing type antifogging agent and increases by two types of formula antifogging agents.The jet printing type antifogging agent has inorganic jet printing type antifogging agent, Polymer jet printing type antifogging agent and composite spraying formula antifogging agent again.Inorganic jet printing type antifogging agent is the compound that is mixed with by a certain percentage by the silica gel breast of SiO2 hydrate, A1203 hydrate latex, nonionic or anionic surfactant, crosslinking agent, catalyst and defoamer.Polymer jet printing type antifogging agent mainly is that polyether sulfonate and polymethylacrylic acid ethylene glycol glucose add a little auxiliary and solvent complex forms.Compound type jet printing type antifogging agent is mainly by the glucosides type non-ionic surface active agent compound formulated with general cationic surfactant.Increase formula antifogging agent can be divided into fluorine-containing, siliceous, phosphorous and the boracic antifogging agent.Fluorine increases the inhibiter that the formula antifogging agent refers to that the hydrogen atom on the hydrocarbon chain lipophilic group has been replaced by fluorine fully.In increasing the formula antifogging agent, fluorinated antifogging agent best results.Because C-F key that fluorine increases in the formula antifogging agent has good resistance to effect of heat, chemical inertness and hydrophobic and oil repellent dual nature, C-F key forms a directed peace alignment layer to reduce the surface tension of water on its surface, can make the faster of water droplet whereabouts, and reduced surperficial volatile quantity, made in the air steam drop to saturated vapor pressure.It is to be the class activating agent that lipophilic group and hydrophilic radical constitute with the silicone that silicon increases the formula antifogging agent.It has excellent heat stability and chemical inertness, and reduces capillary ability and be only second to fluorine and increase antifogging agent and increase the formula antifogging agent greater than hydrocarbon system.
The warm fog in runway zone can be eliminated or dilute to present embodiment by the reciprocal operation of many sorties in 30 minutes, improve visbility, and keep a period of time.
Claims (5)
1. the gentle wing unmanned vehicle with automatic fog dispersal function is characterized in that, comprising: flexible punching press parafoil (1), structure cabin body (2), power system (3), fog dispersal equipment and control system (5); Flexible punching press parafoil (1) provides lift to system;
The bottom of flexible punching press parafoil (1) is by umbrella rope (8) connection structure cabin body (2); Structure cabin body (2) inside is equipped with control system (5) and built-in fog dispersal equipment (14), and afterbody is installed power system (3);
Structure cabin body (2) mainly comprises cabin body framework (10), mount pad (9) and skid formula alighting gear (11), mount pad (9) is fixed on cabin body framework (10) bottom and stretches out to both sides, external fog dispersal equipment (15) is installed respectively on it, skid formula alighting gear (11) is installed in cabin body framework (10) bottom, is used for the buffering of taking off, land of system;
Power system (3) is used for the required power that flies is provided, and mainly comprises driving engine (12) and screw propeller (13);
Fog dispersal equipment comprises built-in fog dispersal equipment (14) and external fog dispersal equipment (15), be used for the while or sow antifogging agent separately, built-in fog dispersal equipment (14) is installed in structure cabin body (2) inside, and external fog dispersal equipment (15) is installed in structure cabin body (2) outside;
Built-in fog dispersal equipment (14) constitutes by throwing loose cabin (16), plate (17), steering wheel (18) and dispensing port (19), throwing the cabin (16) of loosing is installed in the structure cabin body (2), the bottom has dispensing port (19) at structure cabin body (2), plate (17) is installed in to throw and looses (16) bottom, cabin and cover dispensing port (19), steering wheel (18) one ends link to each other with plate (17), and controlled system (5) control;
External fog dispersal equipment (15) is loose tin (21) by fixed mount (20), throwing and exciting electrode (22) constitutes, the diffusing tube of throwing (21) is fixed on below the mount pad (9) by fixed mount (20), exciting electrode (22) is installed together with throwing the tube (21) that looses, and controlled system (5) control;
Fog dispersal equipment also comprises the detection detecting devices, detects detecting devices and is provided with: weather radar, satellite receiving equipment, the sub-measuring system of PMS cloud particle, weather meter, GPS location and number biography system, double channels microwave radiometer;
Control system (5) has Navigation Control and communication, monitoring function, comprises navigation elements (23), control unit (24), communication unit (25), video monitoring unit (26) and surface control station (27);
Navigation elements (23) is used for providing the aerial mission course line and sends steering command to control unit, mainly comprises airborne computer, navigation software, locating module and various sensor; Control unit (24) is used for carrying out the steering command that navigation elements sends, and drives and handles actuating unit, and change of flight attitude and course line mainly comprise driver train and supply module; Communication unit (25) is used for carrying out data interaction between flying body and the surface control station, mainly comprises transmitting station and receiving wire; Video monitoring unit (26) is used for passing to ground station under the video that the video prison bat equipment of installing on the flying body is captured and showing at telltale; Setting, the input of status data, sending with the monitoring of flight path with to the reception of flying body feedback data of flight directive that surface control station (27) is used for finishing to flight path are handled, and mainly comprise hand-held remote control device and watch-dog.
2. the gentle wing unmanned vehicle with automatic fog dispersal function according to claim 1 is characterized in that fog dispersal equipment also has airborne silver iodide producer, the liquid nitrogen producer, equipment sowed by flame bullet producer, dry ice seeding device, salt powder, urea and HB-1 type antifogging agent is sowed equipment.
3. the gentle wing unmanned vehicle with automatic fog dispersal function according to claim 1, it is characterized in that, above-ground launcher comprises tractor truck (7), emission permanent seat (6), disconnecting gear (28) and protective device (29), is used for having the gentle wing unmanned vehicle of automatic fog dispersal function from the ground launch;
Emission firm banking (6) is located on the tractor truck (7); Armed gentle wing unmanned vehicle with automatic fog dispersal function places in emission firm banking (6), and by belt tensioner (30) with tighten up capstan winch (31) and be connected; Protective device (29) is located at the front end of emission base; Disconnecting gear (28) is located at emission firm banking (6) middle part, is positioned at unmanned plane to be launched below.
4. the gentle wing unmanned vehicle with automatic fog dispersal function according to claim 1 is characterized in that, this unmanned vehicle is by installing dropping gear emission aboard.
5. according to each described gentle wing unmanned vehicle with automatic fog dispersal function of claim 1～4, it is characterized in that, be provided with the ground remote control system, it controls this flexibility punching press parafoil unmanned plane during flying behind predetermined altitude, fly to the coordinates of targets point according to contemplated route, finish at the task object point and sow antifogging agent automatically after the task of fog dispersal, turn back to the spatial domain, destination according to projected route, and decision height information and landing site wind direction information, the mode that adopts sparrow to fall realizes pinpoint landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310201290.1A CN103241377B (en) | 2013-05-27 | 2013-05-27 | There is the soft wing unmanned vehicle of automatic fog dispersal function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310201290.1A CN103241377B (en) | 2013-05-27 | 2013-05-27 | There is the soft wing unmanned vehicle of automatic fog dispersal function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103241377A true CN103241377A (en) | 2013-08-14 |
| CN103241377B CN103241377B (en) | 2015-08-12 |
Family
ID=48921310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310201290.1A Expired - Fee Related CN103241377B (en) | 2013-05-27 | 2013-05-27 | There is the soft wing unmanned vehicle of automatic fog dispersal function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103241377B (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104071342A (en) * | 2014-07-03 | 2014-10-01 | 国家电网公司 | Electrified foreign matter cleaning unmanned aerial vehicle protective cover |
| CN105366044A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Fog dispersal type unmanned aerial vehicle |
| CN105366055A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
| CN105383698A (en) * | 2015-12-15 | 2016-03-09 | 谷家菊 | Fog-dissipation unmanned aerial vehicle with flexible wings |
| CN105944474A (en) * | 2016-02-04 | 2016-09-21 | 叶伟武 | Fog dissipation and dust falling device |
| CN109310056A (en) * | 2016-01-29 | 2019-02-05 | Jg创业企业有限责任公司 | The aircraft and system changed for weather |
| US10669042B2 (en) | 2014-10-23 | 2020-06-02 | Wet | Unmanned aerial vehicle with lighting and cooling therefor |
| US10696395B2 (en) | 2015-12-28 | 2020-06-30 | Wet | Tethered unmanned aerial system |
| US10745126B2 (en) | 2015-12-28 | 2020-08-18 | Wet | Unmanned aerial system with transportable screen |
| CN112746592A (en) * | 2021-01-15 | 2021-05-04 | 郑尔历 | Method for eliminating large-range haze safely, quickly and at low cost |
| US11059601B2 (en) | 2015-12-28 | 2021-07-13 | Dezso Molnar | Water and lighting displays including unmanned aerial system |
| CN114471065A (en) * | 2022-01-18 | 2022-05-13 | 象谱信息产业有限公司 | Condensation nucleus method for fast defogging |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101195994A (en) * | 2007-12-13 | 2008-06-11 | 辛忻 | Airborne defogging equipment |
| WO2011004359A1 (en) * | 2009-07-06 | 2011-01-13 | Elbit Systems Ltd. | Powered parafoil cargo delivery device and method |
| TW201200680A (en) * | 2010-06-18 | 2012-01-01 | Jun-Shin Chang | Method for eliminating thick fog and volcanic ash to allow aircraft taking off and landing |
| CN202879795U (en) * | 2012-10-31 | 2013-04-17 | 襄阳宏伟航空器有限责任公司 | Multipurpose unmanned plane with flexible ram-type parawings |
| CN203294314U (en) * | 2013-05-27 | 2013-11-20 | 襄阳宏伟航空器有限责任公司 | Gentle wing unmanned aerial vehicle with automatic fog dissipation function |
-
2013
- 2013-05-27 CN CN201310201290.1A patent/CN103241377B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101195994A (en) * | 2007-12-13 | 2008-06-11 | 辛忻 | Airborne defogging equipment |
| WO2011004359A1 (en) * | 2009-07-06 | 2011-01-13 | Elbit Systems Ltd. | Powered parafoil cargo delivery device and method |
| TW201200680A (en) * | 2010-06-18 | 2012-01-01 | Jun-Shin Chang | Method for eliminating thick fog and volcanic ash to allow aircraft taking off and landing |
| CN202879795U (en) * | 2012-10-31 | 2013-04-17 | 襄阳宏伟航空器有限责任公司 | Multipurpose unmanned plane with flexible ram-type parawings |
| CN203294314U (en) * | 2013-05-27 | 2013-11-20 | 襄阳宏伟航空器有限责任公司 | Gentle wing unmanned aerial vehicle with automatic fog dissipation function |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104071342A (en) * | 2014-07-03 | 2014-10-01 | 国家电网公司 | Electrified foreign matter cleaning unmanned aerial vehicle protective cover |
| US10669042B2 (en) | 2014-10-23 | 2020-06-02 | Wet | Unmanned aerial vehicle with lighting and cooling therefor |
| CN105366044A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Fog dispersal type unmanned aerial vehicle |
| CN105366055A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
| CN105383698A (en) * | 2015-12-15 | 2016-03-09 | 谷家菊 | Fog-dissipation unmanned aerial vehicle with flexible wings |
| US10696395B2 (en) | 2015-12-28 | 2020-06-30 | Wet | Tethered unmanned aerial system |
| US10745126B2 (en) | 2015-12-28 | 2020-08-18 | Wet | Unmanned aerial system with transportable screen |
| US11059601B2 (en) | 2015-12-28 | 2021-07-13 | Dezso Molnar | Water and lighting displays including unmanned aerial system |
| CN109310056A (en) * | 2016-01-29 | 2019-02-05 | Jg创业企业有限责任公司 | The aircraft and system changed for weather |
| CN105944474A (en) * | 2016-02-04 | 2016-09-21 | 叶伟武 | Fog dissipation and dust falling device |
| CN112746592A (en) * | 2021-01-15 | 2021-05-04 | 郑尔历 | Method for eliminating large-range haze safely, quickly and at low cost |
| CN114471065A (en) * | 2022-01-18 | 2022-05-13 | 象谱信息产业有限公司 | Condensation nucleus method for fast defogging |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103241377B (en) | 2015-08-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103241377B (en) | There is the soft wing unmanned vehicle of automatic fog dispersal function | |
| CN203294314U (en) | Gentle wing unmanned aerial vehicle with automatic fog dissipation function | |
| US6868314B1 (en) | Unmanned aerial vehicle apparatus, system and method for retrieving data | |
| US8540183B2 (en) | Aerovehicle system including plurality of autogyro assemblies | |
| CN205390157U (en) | Drive bird unmanned aerial vehicle | |
| CN102910288B (en) | Multi-purpose flexible ram air parachute UAS | |
| US6220543B1 (en) | Safe and secure commercial air transportation | |
| US20060102798A1 (en) | Unmanned biplane for airborne reconnaissance and surveillance having staggered and gapped wings | |
| CN107539453A (en) | A kind of low-latitude flying operation unmanned plane and its control system and application | |
| US20220404272A1 (en) | Airborne remote sensing with sensor arrays | |
| RU2457531C1 (en) | Method of using unmanned aircraft and control apparatus | |
| US9308993B2 (en) | Aircraft payload apparatus and method | |
| CN205345355U (en) | Portable unmanned aerial vehicle transmitter | |
| CN106697292A (en) | Agricultural and forestal plant protection unmanned helicopter with large load capacity | |
| CN112902759A (en) | Anti-unmanned aerial vehicle system | |
| CN202879795U (en) | Multipurpose unmanned plane with flexible ram-type parawings | |
| CN202923888U (en) | Photovoltaic hawk-type unmanned scout for sea area governance | |
| CN108284954A (en) | A kind of unmanned increasing rain aircraft | |
| CN105292472A (en) | Multi-purpose flexible-wing unmanned aerial vehicle | |
| CN204021249U (en) | The soft wing unmanned plane of high-mobility, multipurpose, wheeled vehicle | |
| RU2005128131A (en) | METHOD AND COMPLEX OF MEANS FOR DETECTING AN EMERGENCY SITUATION AND ELIMINATING ITS CONSEQUENCES | |
| CN207242004U (en) | A kind of low-latitude flying operation unmanned plane | |
| Sasa et al. | Ongoing research on disaster monitoring UAV at JAXA’s Aviation Program Group | |
| Subramaniam et al. | Design of a fire-fighting unmanned air vehicle | |
| CN112630863A (en) | Unmanned modification artificial influence weather monitoring system and method based on man-machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| ASS | Succession or assignment of patent right |
Owner name: SUN YI Free format text: FORMER OWNER: XIANGYANG HONGWEI AIRCRAFT CO., LTD. Effective date: 20131112 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 441022 XIANGFAN, HUBEI PROVINCE TO: 430073 WUHAN, HUBEI PROVINCE |
|
| TA01 | Transfer of patent application right |
Effective date of registration: 20131112 Address after: 430073, East Lake Development Zone, Optics Valley square, world city, California Sunshine 1 building, 2 gate, 30 floor, Hubei, Wuhan Applicant after: Sun Yi Address before: 441022, No. 50, Qilihe Road, hi tech Zone, Xiangfan, Hubei, Xiangyang Applicant before: XIANGYANG HONGWEI AIRCRAFT Co.,Ltd. |
|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20160303 Granted publication date: 20150812 |
|
| RINS | Preservation of patent right or utility model and its discharge | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20170303 Granted publication date: 20150812 |
|
| PD01 | Discharge of preservation of patent | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190701 Address after: 430012 No. 2020 Jiefang Avenue, Jiangan District, Wuhan City, Hubei Province Patentee after: Wuhan Nansha Industry and Trade Co.,Ltd. Address before: 430073 Guanggu Square, Donghu Development Zone, Wuhan City, Hubei Province Patentee before: Sun Yi |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150812 Termination date: 20210527 |