CN205150244U - Unmanned aerial vehicle is scattered to intelligence - Google Patents
Unmanned aerial vehicle is scattered to intelligence Download PDFInfo
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- CN205150244U CN205150244U CN201520888165.7U CN201520888165U CN205150244U CN 205150244 U CN205150244 U CN 205150244U CN 201520888165 U CN201520888165 U CN 201520888165U CN 205150244 U CN205150244 U CN 205150244U
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Abstract
The utility model discloses an unmanned aerial vehicle is scattered to intelligence, this unmanned aerial vehicle include lift portion, unmanned aerial vehicle organism, and lift portion is for pulling unmanned aerial vehicle's parafoil through controing to restrict, the afterbody of unmanned aerial vehicle organism is provided with power device, still is provided with intelligence on the unmanned aerial vehicle organism and sows flight control system, and intelligence is sowed flight control system and is included the orientation steering wheel respectively and set up in the machine year flight control system of unmanned aerial vehicle organism head, and the middle part of unmanned aerial vehicle organism still is provided with sprinkler, and sprinkler is including setting up in the liquid case at unmanned aerial vehicle organism middle part, and spray lance and booster pump are fixed in the unmanned aerial vehicle underpart, and the booster pump will be treated the flushing liquor through the liquid pipe and follow liquid bottom of the case portion and pump, and carry be fixed with the spray lance of shower nozzle, still be provided with electrical power unit on the unmanned aerial vehicle body, it provides the power for unmanned aerial vehicle work. According to the utility model discloses the unmanned aerial vehicle is scattered to intelligence who realizes has the bearing force height, and the activity duration is long, work efficiency is high, operation and maintenance advantage such as with low costs.
Description
Technical field
The utility model belongs to agricultural aviation plant protection field, more specifically, relates to a kind of intelligence and sows unmanned plane.
Background technology
According to statistics; the equipment for plant protection that China uses at present is based on manual and minicomputer power driven mist blower; wherein manual dispenser medical instruments, power knapsack medical instruments account for 93.07% and 5.53% of domestic equipment for plant protection recoverable amount respectively; tractor mounted equipment for plant protection accounts for 0.57%; the labour that plant protection operation drops into is many, labour intensity large, and dispenser personnel poisoning happens occasionally.Current domestic pesticide dosage is increasing, and operating cost is high, and waste is serious, and utilization of resources rate is low, and crop yield and difficult quality are protected, and brings that serious water and soil resources pollute, the ecosystem is unbalance, degradation problem under quality of agricultural product simultaneously.
And for solving the above problems, the more of current appearance is that conventional agricultural aviation sows unmanned plane, wherein the principal mode of unmanned plane has depopulated helicopter and many rotor wing unmanned aerial vehicles, but mostly exist drugloading rate little, intelligence cannot be realized sow, and its operation, use and maintenance are complicated, the problem that empirical risk is larger.Wherein depopulated helicopter complex structure, need along with crop allocation in operation process and highly constantly flight attitude adjusted, and in the processes such as the lifting of helicopter, flight, rotation, have the coupled problem of lift and thrust to need to solve, increase the complexity of helicopter physical construction and control algorithm on the one hand, also improve the complexity of its remote operating on the other hand, therefore need to carry out professional training to no-manned machine distant control person.And on the other hand many rotor wing unmanned aerial vehicles are as plant protection operation platform, its load-carrying is little relative to helicopter many, and major cause have employed multiple small size rotor, and due to power supply can not be excessive, its continuous operation time is shorter.Therefore need in many rotor wing unmanned aerial vehicles operation process repeatedly return dosing and change battery, inefficiency, also result in the waste of the energy.Its problem also with other such as in addition: 1 drugloading rate is less, and be about 10 ~ 20kg, take-off weight within 35kg, operating efficiency is relatively low; 2 cannot accurately control to sow height, sow circuit and sow the key parameters such as dose, also cannot judge whether the problems such as replay or broadcast leakage; 3 complicated operations, difficult in maintenance, easily damage, application risk is larger.
Utility model content
For above defect or the Improvement requirement of prior art, the utility model provides a kind of intelligence and sows unmanned plane, and what complete intellectuality and automation thus sows function.
For achieving the above object, according to an aspect of the present utility model, provide a kind of intelligence and sow unmanned plane, it is characterized in that, this unmanned plane comprises lift portion, unmanned plane body, and described lift portion is the parafoil by control wire traction unmanned plane; The afterbody of described unmanned plane body is provided with engine installation, and described engine installation is driving engine and the screw propeller with described engine output shaft transmission; Described unmanned plane body is also provided with intelligence and sows flight control system, described intelligence sows the airborne flight control system that flight control system comprises direction steering wheel respectively and is arranged at described unmanned plane body head, described direction steering wheel is installed on the symmetrical both sides of described unmanned plane body respectively for coordinating with described lift portion the heading controlling described unmanned plane, and described airborne flight control system controls for the flight realizing described unmanned plane that communicates with ground control unit; The middle part of described unmanned plane body is also provided with sprinkler, described sprinkler comprises liquid case, spray boom and boost pump are fixed on described unmanned plane underpart, and liquid to be sprayed is pumped by liquid pipe by described boost pump bottom described liquid case, is fixed with the spray boom of shower nozzle described in being transported to; Described unmanned body is also provided with mains connection set, and it provides power supply for described unmanned plane work.
Further, described ground station control device is face equipment, it comprises source switch, battery electric quantity indicator panel, engine control button, mode selector switch, flight control handle, sow switch, flight path arranges read-out, described source switch is for opening the general supply of ground station, described battery electric quantity is used to refer to the electricity of described mains connection set, described engine control button is used for starting and killing engine, described mode selector switch is for switching remote control distributor and autonomous navigation flight, described flight control handle is used for heading and the landing of remotely pilotless machine, described switch of sowing sows function for unmanned plane during flying to opening after sowing region, described flight path arranges read-out for sowing region described in arranging and automatically generating vector.
Further, described liquid case is divided into nine rectangular areas be interconnected by nine grids dividing plate.
In general, the above technical scheme conceived by the utility model compared with prior art, can obtain following beneficial effect:
(1) intelligence realized according to the utility model sows unmanned plane, it adopts soft wing unmanned plane as the platform of unmanned plane, parafoil provides lift as wing, the power that driving engine provides the advance of unmanned plane, rise, to circle in the air etc., improve the load-carrying capacity of unmanned plane by means of large-area parafoil, make it carry dose and reach more than 100kg;
(2) left and right directions servos control soft wing unmanned plane parafoil both sides rear wing is adopted, to turn about unmanned plane body bilateral symmetry arranged direction steering wheel provides unmanned plane required actuating force, and direction steering wheel is by operation, the low-speed characteristic of parafoil ensure that intelligence sows the low-speed motion of unmanned plane in farmland simultaneously;
(3) the soft wing unmanned plane of the utility model only needs when flying to control left and right directions steering wheel and throttle size, and airworthiness stablizes not easily stall, and possesses and independently fly control ability, its structure and control principle simple, reduce input and maintenance cost, easy to maintenance, simple to operate easy to learn;
(4) the utility model has distributed the placement location that intelligence sows the various equipment in unmanned plane rationally, and the enforcement of this position can carry the spray tank of large volume, thus carry out long continuous operation, save the time needing to return dosing because liquid is not enough, improve Global Operation efficiency;
(5) in addition, the intelligence realized according to the utility model sows unmanned plane, due to power plant and parafoil with the use of, therefore require low to take-off venue, intelligence is sowed unmanned plane band and is carried take off distance and only need 50 ~ 80 meters, and this also just reduces to a great extent and takes off difficulty and relax limiting condition, substantially reduces the distance of takeoff point to operating area, reduce operation wait time, improve operating efficiency;
(6) intelligence realized according to the utility model is sowed unmanned plane unit and is sprayed about 150 mu ~ 400 mu/sortie, production time only needs 15 ~ 25 minutes, each frame intelligence sows unmanned plane every day can operation 3000 ~ 4000 mu, and the efficiency of artificial dispenser is every day 8 ~ 10 mu, intelligence sows the labour intensity that unmanned plane pesticide application technology had both reduced operating personnel, significantly improves operating efficiency simultaneously.
Accompanying drawing explanation
Fig. 1 is the overall schematic that the intelligence realized according to the utility model sows unmanned plane airflight state;
Fig. 2 is that the intelligence realized according to the utility model sows unmanned plane housing construction schematic diagram;
Fig. 3 is that the intelligence realized according to the utility model sows unmanned aerial vehicle station control inerface schematic diagram;
Fig. 4 be the intelligence realized according to the utility model sow unmanned plane sow path planning schematic diagram;
Fig. 5 is the structural representation of large solvent medicine-chest casing of the nine grids liquid lattice plate realized according to the utility model.
In all of the figs, identical Reference numeral is used for representing identical element or structure, wherein:
1-parafoil 2-control wire 3-straphanger 4-screw propeller 5-body, the 6-spray boom 7-alighting gear 8-driving engine 9-fuel tank 10-boost pump 11-medicine-chest 12-direction steering wheel 13-airborne flight control system 14-storage battery 15-source switch 16-electricity display 17-engine control button 18-mode switch button 19-control handle 20-that flies sows switch 21-flight path and arranges read-out 22-and sow vegetation area 23-vector
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.In addition, if below in described each embodiment of the utility model involved technical characteristic do not form conflict each other and just can mutually combine.
The utility model relates to a kind of intelligence and sows unmanned plane, this unmanned plane mainly comprises parafoil part and unmanned plane body part, wherein the Main Function of parafoil provides lift to unmanned plane body part and as flying platform, and unmanned plane during flying body part being taken off for providing, landing, being adjusted unmanned plane and sow the height of agricultural chemicals and provide Power output.
Wherein parafoil mainly comprise parafoil umbrella body and for the control wire that draws parafoil and unmanned plane and straphanger, parafoil is connected with body by straphanger as wing, for unmanned plane provides lift, wherein control wire is by configuring setting with the direction adjusting mechanism on unmanned plane, thus the course of adjustment unmanned plane and flight attitude.
In addition, wherein unmanned plane comprises body body, and body body is primarily of such as lower part composition:
Engine installation: the output shaft of driving engine is directly connected with screw propeller, wherein screw propeller is arranged at the afterbody of unmanned plane, the flying power of rising is provided, the Power output that the fuel reburning utilizing fuel tank to provide is driving engine, advance soft wing unmanned plane to advance, also control the flying height of soft wing unmanned plane by power size;
Alighting gear: the alighting gear being arranged at body body bottom portion, this alighting gear can be set to slide-type alighting gear, for soft wing unmanned plane take off and landing provide land support;
Airborne flight control system: airborne flight control system is installed in body body and realizes communicating with the control setup on ground, realize remote pilot, wherein airborne flight control system calculates flight track and the flying height of unmanned plane according to airborne sensors such as the GPS arranged in it, magnetic compass and Pitot meters, guarantee that soft wing unmanned plane is in predetermined work route, and except can, by the remote control of ground control unit, also carrying out carrying out sowing of intelligence according to the path of planning according to the program preset; Its main position is arranged on the head of body body;
Carry out with airborne flight control system the ground control system that communicates: ground control system is a handheld device, this equipment comprises source switch, battery electric quantity instruction frame, engine control button, mode selector switch, flight control handle respectively according to the part that equipment face is arranged, sows switch, flight path arranges read-out.Source switch is for opening the general supply of ground station.Battery electric quantity instruction is used for guaranteeing whether battery has enough electricity.Engine control button is used for starting and killing engine, and regulates throttle size.Mode selector switch is for switching remote control distributor and autonomous navigation flight.Flight control handle is used for heading and the landing of remotely pilotless machine.Sow switch and sow function for unmanned plane during flying to opening after sowing region.Flight path arranges read-out and also automatically generates vector for arranging the plant protection region needing to sow;
Sprinkler: special pesticide spraying system comprises medicine-chest, spray boom, the boost pump of large volume.Large volume medicine-chest comprises the medicine-chest casing and nine grids liquid dividing plate that volume is 100L.Be vertically fixed on large volume medicine-chest inwall at the bottom of nine grids liquid dividing plate and large volume medicine-chest case, large volume medicine-chest is divided into nine rectangular areas be interconnected, to prevent, liquid fluctuation is excessive causes the unbalance of unmanned plane.Large volume medicine-chest casing is used for holding spray medicine operation liquid used, medicine-chest, spray boom and boost pump are fixed on body body lower part, liquid is pumped by drug liquid tube by boost pump bottom large volume medicine-chest, spray boom is transported to by drug liquid tube with certain pressure, spray boom is fixed with shower nozzle, and medical liquid atomizing sprays by shower nozzle.After it arrives the region of sowing, relevant region of sowing is sowed;
Mains connection set: wherein for above-mentioned engine installation, airborne flight control system, sprinkler provide power supply to export.
Embodiment one
Unmanned plane comprises parafoil 1, control wire 2, straphanger 3, screw propeller 4, driving engine 8, body 5, spray boom 6 and alighting gear 7.Described parafoil 1 is connected with body 5 by straphanger 3 as wing, for soft wing unmanned plane provides lift.Screw propeller 4 is arranged on driving engine 8, and driving engine 8 is fixed on soft wing unmanned plane body 5 rear portion, and the Power output that the fuel reburning utilizing fuel tank 9 to provide is driving engine 8 advances soft wing unmanned plane to advance, and controls the flying height of soft wing unmanned plane by power size.Alighting gear 7 is slide-type alighting gear, for soft wing unmanned plane take off and landing provide land support.
Intelligence is sowed flight control system and is comprised the airborne flight control system 13 that direction steering wheel 12 communicates with earth station system.Direction steering wheel 12 has two covers, and side is not installed on the symmetrical both sides of body 5, is controlled the heading of parafoil 1 by control wire 2.Airborne flight control system 13 calculates flight track and the flying height of unmanned plane by airborne sensors such as the GPS on unmanned plane, magnetic compass and Pitot meters.Mains connection set concrete form is storage battery 14, is fixed on body 5 head, for airborne flight control system 13 and direction steering wheel 12 provide power supply.Earth station system comprises source switch 15, battery electric quantity instruction 16, engine control button 17, mode selector switch 18, flight control handle 19, sows switch 20, flight path arranges read-out 21.Source switch 15 is for opening the general supply of ground station.Battery electric quantity 16 instruction is used for guaranteeing whether battery has enough electricity.Engine control button 17 for starting and killing engine, and regulates throttle size.Mode selector switch 18 is for switching remote control distributor and autonomous navigation flight.Flight control handle 19 is for the heading of remotely pilotless machine and landing.Sow switch 20 and sow function for unmanned plane during flying to opening after sowing region.Flight path arranges read-out 21 and sows vegetation area 22 for arranging and automatically generate vector 23.
Special pesticide spraying system comprises large volume medicine-chest 11, spray boom 6, boost pump 10.Large volume medicine-chest 11 comprises the medicine-chest casing and nine grids liquid dividing plate that volume is 100L.Be vertically fixed on large volume medicine-chest inwall at the bottom of nine grids liquid dividing plate and large volume medicine-chest case, large volume medicine-chest is divided into nine rectangular areas be interconnected, to prevent, liquid fluctuation is excessive causes the unbalance of unmanned plane.Large volume medicine-chest casing 11 is used for holding spray medicine operation liquid used.Medicine-chest 11, spray boom 6 and boost pump 10 are fixed on underpart, and boost pump 10 is transported to spray boom 6 with certain pressure by drug liquid tube after being pumped bottom large volume medicine-chest 11 by liquid by drug liquid tube.Spray boom 6 is fixed with shower nozzle, and medical liquid atomizing can spray by shower nozzle.
The utility model intelligence sows the operational method of unmanned plane, comprises the steps:
(1) intelligence is sowed after unmanned plane is transported to operating area, arrange in read-out 21 to arrange at the flight path of earth station system and sow vegetation area 22, namely vegetation area 22 full screen display will sowed arranges read-out 21 to flight path, earth station system calculates spraying vector 23 according to sowing vegetation area 22, method of calculating is draw vector 23 parallel to each other according to the width of shower nozzle width 12 meters, vegetation area 22 will be sowed cover completely, and vector 23 will be uploaded to airborne flight control system 13;
(2) transport trolley accelerates traction, and with engine control button 17 start the engine 8, control throttle and strengthen screw propeller 4 rotating speed, unmanned plane steadily flies away from transport trolley.Keep throttle size, unmanned plane is stabilized in sow the proper height in overhead near vegetation area 22;
(3) pull the mode selector switch 18 on earth station system, flight is switched to autonomous flight by remote control distributor;
(4) intelligence is sowed unmanned plane and is flown into after sowing vegetation area 22, airborne flight control system 13 judges whether unmanned plane coordinate position enters vector 23, if enter vector 23, then airborne flight control system 13 sends instruction to the switch steering wheel of boost pump 10, switch steering wheel is opened and can be implemented the operation of spray medicine, unmanned plane flies along the vector 23 planned in advance, until unmanned plane completes whole spray medicine operation of sowing vegetation area 22;
(5) after sowing vegetation area 22 dispenser operation and completing, automatically close boost pump 10, stop spray medicine, unmanned plane automatically flies to drop zone and implements Autonomous landing or remote control landing, transports operating area after landing with transport trolley.
Those skilled in the art will readily understand; the foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (3)
1. intelligence sows a unmanned plane, it is characterized in that, this unmanned plane comprises lift portion, unmanned plane body (5), and described lift portion is the parafoil by control wire traction unmanned plane; The afterbody of described unmanned plane body (5) is provided with engine installation, and described engine installation is driving engine and the screw propeller with described engine output shaft transmission; Described unmanned plane body (5) is also provided with intelligence and sows flight control system, described intelligence sows the airborne flight control system (13) that flight control system comprises direction steering wheel (12) respectively and is arranged at described unmanned plane body (5) head, the symmetrical both sides that described direction steering wheel (12) is installed on described unmanned plane body (5) are respectively used for coordinating with described lift portion the heading controlling described unmanned plane, and described airborne flight control system (13) controls for the flight realizing described unmanned plane that communicates with ground station control device; The middle part of described unmanned plane body (5) is also provided with sprinkler, described sprinkler comprises liquid case, spray boom and boost pump are fixed on described unmanned plane body (5) bottom, liquid to be sprayed is pumped by liquid pipe by described boost pump bottom described liquid case, is fixed with the spray boom of shower nozzle described in being transported to; Described unmanned body (5) is also provided with mains connection set, and it provides power supply for described unmanned plane work.
2. intelligence as claimed in claim 1 sows unmanned plane, it is characterized in that, described ground station control device is face equipment, it comprises source switch (15), battery electric quantity indicator panel (16), engine control button (17), mode selector switch (18), flight control handle (19), sow switch (20), flight path arranges read-out (21), described source switch (15) is for opening the general supply of ground station, described battery electric quantity (16) is used to refer to the electricity of described mains connection set, described engine control button (17) is for starting and killing engine, described mode selector switch (18) is for switching remote control distributor and autonomous navigation flight, described flight control handle (19) is for the heading of remotely pilotless machine and landing, described switch (20) of sowing is opened for unmanned plane during flying afterwards sow function to being sowed region (22), described flight path arranges read-out (21) for sowing region (22) described in arranging and automatically generating vector (23).
3. intelligence as claimed in claim 1 or 2 sows unmanned plane, and it is characterized in that, described liquid case is divided into nine rectangular areas be interconnected by nine grids dividing plate.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043715A (en) * | 2016-05-27 | 2016-10-26 | 襄阳宏伟航空器有限责任公司 | In-flight auto-ignition control method of engine of unmanned aerial vehicle |
| WO2019063942A1 (en) * | 2017-09-27 | 2019-04-04 | Drone Air Fly | Dispersion aircraft |
| CN113226024A (en) * | 2019-01-16 | 2021-08-06 | 株式会社尼罗沃克 | Unmanned aerial vehicle system, unmanned aerial vehicle, moving body, partition member, control method for unmanned aerial vehicle system, and unmanned aerial vehicle system control program |
| CN116477053A (en) * | 2023-06-19 | 2023-07-25 | 西安富沃德光电科技有限公司 | Unmanned aerial vehicle airborne spraying device |
-
2015
- 2015-11-09 CN CN201520888165.7U patent/CN205150244U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043715A (en) * | 2016-05-27 | 2016-10-26 | 襄阳宏伟航空器有限责任公司 | In-flight auto-ignition control method of engine of unmanned aerial vehicle |
| CN106043715B (en) * | 2016-05-27 | 2018-03-27 | 襄阳宏伟航空器有限责任公司 | A kind of aerial method for controlling automatic ignition of unmanned vehicle engine |
| WO2019063942A1 (en) * | 2017-09-27 | 2019-04-04 | Drone Air Fly | Dispersion aircraft |
| CN113226024A (en) * | 2019-01-16 | 2021-08-06 | 株式会社尼罗沃克 | Unmanned aerial vehicle system, unmanned aerial vehicle, moving body, partition member, control method for unmanned aerial vehicle system, and unmanned aerial vehicle system control program |
| US12001225B2 (en) | 2019-01-16 | 2024-06-04 | Nileworks Inc. | Drone system, drone, movable body, demarcating member, control method for drone system, and drone system control program |
| CN116477053A (en) * | 2023-06-19 | 2023-07-25 | 西安富沃德光电科技有限公司 | Unmanned aerial vehicle airborne spraying device |
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