CN105836131A - Novel range-extended chemical spraying unmanned aerial vehicle for refuse landfill - Google Patents

Novel range-extended chemical spraying unmanned aerial vehicle for refuse landfill Download PDF

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Publication number
CN105836131A
CN105836131A CN201510023588.7A CN201510023588A CN105836131A CN 105836131 A CN105836131 A CN 105836131A CN 201510023588 A CN201510023588 A CN 201510023588A CN 105836131 A CN105836131 A CN 105836131A
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China
Prior art keywords
gasoline engine
medicine
gear
motor
pipeline
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Pending
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CN201510023588.7A
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Chinese (zh)
Inventor
吴志海
王克文
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Shandong Essence Environmental Science And Technology Co Ltd
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Shandong Essence Environmental Science And Technology Co Ltd
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Priority to CN201510023588.7A priority Critical patent/CN105836131A/en
Publication of CN105836131A publication Critical patent/CN105836131A/en
Pending legal-status Critical Current

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Abstract

A novel range-extended chemical spraying unmanned aerial vehicle for a refuse landfill mainly comprises auxiliary propeller blades, motors, a chemical box, a receiver, a supporting table and connecting rods. The supporting table is connected with a plurality of supporting legs, and the chemical box is arranged on the supporting table. The connecting rods are arranged in the bent position of each supporting leg, the extended ends of the connecting rods are connected with the motors, and the auxiliary propeller blades are arranged on the motors. A pipeline extending from each connecting rod is connected with a sprayer. Each sprayer mainly comprises an adjustable motor, a pipeline, a sprayer shell, a rotating head and small holes. The supporting table is provided with a driving shaft gear which is connected with a gasoline engine rotating shaft through a synchronous belt, and the gasoline engine rotating shaft is driven by a gasoline engine. The lower side of the driving shaft gear is connected with a counter gear set, and an upper gear and a lower gear of the counter gear set are connected with main propeller blades a and main propeller blades b correspondingly. The novel range-extended chemical spraying unmanned aerial vehicle is high in cruising power, chemicals can be efficiently and rapidly sprayed, safety and environmental friendliness are achieved, and time and labor are saved.

Description

A kind of novel journey refuse landfill spray medicine unmanned plane
Technical field
The invention mainly relates to environmental protection machinery technical field, be specifically related to a kind of novel journey refuse landfill spray medicine unmanned plane.
Background technology
Along with growth in the living standard and population amount increase, municipal refuse generation amount is huge, rubbish generally uses the mode burned and fill to process, rubbish in refuse landfill is not easy to rot, harmful substance can gradually infiltrate, and travels in neighbouring or subsoil water by current, contaminated soil and water quality, growing pathogenic bacteria, the landfill gas that after garbage loading embeading, organic principle produces in aerobic and anaerobic degradation process contains methane, hydrogen sulfide, other stenches and toxic gas, carbon dioxide etc.;A large amount of rubbish manually cannot be carried out disinfection by bad environments, prevent from growing pathogenic bacteria, and labor intensity is high, wastes time and energy.
Through the one unmanned pesticide applicator of many rotors ultra-low volume that retrieval Authorization Notice No. is (CN203005749U), it includes the combination of frame in combination, undercarriage, flight control system, sprinkling system, accumulator, protective cover, propeller, remote controller combination, frame in combination includes principal arm vertical folding mechanism and support arm horizontal folding mechanism, the principal arm of this unmanned pesticide applicator of many rotors ultra-low volume is responsible for three motors, support arm and the weight support of sprinkler part, and the twisting opposing in flight course;Medicine-chest is fixed on frame in combination, and medicine-chest is offered tube for transfusion opening, is provided with tube for transfusion on opening, and the medicinal liquid in medicine-chest enters tube for transfusion through Electromagnetic Flow pumping and enters centrifugal fluted disc. Unmanned pesticide applicator during actually used, can run into problem: 1) accumulator provides power, dynamic with oil compared with, flying power is relatively low;2) principal arm of unmanned pesticide applicator is responsible for three motors, and motor is arranged over propeller, and several propellers provide lifting force, and the electric power of consumption is relatively big, affects the service life of accumulator;3) medicinal liquid in medicine-chest enters tube for transfusion through Electromagnetic Flow pumping, needs motor to provide power, and power consumption is relatively large, relatively costly.
Summary of the invention
For the problem existing for herbal sprinkling under adverse circumstances in prior art, the one novel journey refuse landfill spray medicine unmanned plane that the present invention provides, flying power is strong, it is possible to achieve the most quickly spraying of medicine, and safety and environmental protection is time saving and energy saving.
To achieve these goals, the technical solution used in the present invention is as follows:
A kind of novel journey refuse landfill spray medicine unmanned plane, mainly includes secondary helical-blade, motor, medicine-chest, receptor, support platform, connecting rod.
Described support platform connects some supporting legs, supporting leg is set to bending, for supporting whole fuselage, described medicine-chest is located at above support platform, become half-surrounded, it is provided with receptor below described medicine-chest, being provided with gyroscope inside receptor, be used for sensing and maintaining direction, the knee of described supporting leg is provided with connecting rod, the one end stretched out by connecting rod is connected motor, described motor is provided with secondary helical-blade, and accumulator provides power, secondary helical-blade to be respectively used to control rotation and the advance and retreat of fuselage for motor, power consumption is little, and cruising time extends.
nullStretch out a segment pipe connection in described connecting rod and have shower nozzle,Shower nozzle mainly includes adjustable motor、Pipeline、Nozzle housing、Swivel head、Aperture,Described adjustable motor is externally provided with nozzle housing,Nozzle housing is provided with pipeline,Described nozzle housing bottom is provided with base,Base center is provided with gear pump,Described adjustable motor connects gear pump,Described swivel head is connected on adjustable motor head axle head,Swivel head sidewall is provided with aperture,Shower nozzle is connected in medicine-chest by pipeline,Medicinal liquid flows to above gear pump through pipeline,Adjustable motor driven gear pump quick rotation,When pinion rotation,The volume in space of side of being out of gear is big from little change,Form vacuum,Draw liquid into,The volume in the space of gear engagement side is from diminishing greatly,And liquid is clamp-oned in pipeline,Liquid is thrown away by the aperture of swivel head under the effect of high speed centrifugation power,Atomizing effect is more preferable.
Preferably, described support platform is provided with driving shaft gear, connected by Timing Belt on described driving shaft gear and have gasoline engine rotating shaft, described gasoline engine rotating shaft is driven by gasoline engine, it it is the source of fuselage active force, increase the flying power of fuselage, described gasoline engine side is provided with electromotor, electromotor provides power for accumulator charging, connect below described driving shaft gear and have counter gear group, two gears up and down of counter gear group are connected to principal screw leaf a and principal screw leaf b, described principal screw leaf a is contrary with principal screw leaf b direction of rotation, just cancel the revolving force of fuselage, define the equalising torque of unmanned aerial vehicle body, fuselage can be risen and fallen under upper and lower thrust, DCB Specimen power is better than the power of single rotor simultaneously, save the energy.
Beneficial effects of the present invention shows: 1) owing to principal screw leaf uses upper and lower two panels to reversely rotate, form the equalising torque of horizontal direction, need not tail-rotor to balance the moment in unmanned plane horizontal direction, the liter force rate normal spiral leaf of two secondary close coupled type helical-blades is higher, this results in and more easily safeguards and higher flying power;2) use the most secondary helical-blade to control to retreat and turn to, there is not the impact of mutual commissure between each axle, easily operated during flight, fuselage is owing to being coaxial Double helix leaf, and contour dimension is little, it is easy to carry, the unmanned plane spray medicine of refuse landfill can be realized, save manpower;3) shower nozzle is connected in medicine-chest by pipeline, medicinal liquid flows to above gear pump through pipeline, adjustable motor driven gear pump quick rotation, medicinal liquid can dispel the heat to electric motor temperature reduction, slows down the fatigue of motor, motor driven gear pump, motor controls the folding of spray medicine, the rotational speed regulation spray value of motor and fogging degree, simple and convenient, highly reliable;4) described gasoline engine side is provided with electromotor, and electromotor provides power for accumulator charging, increases the output electric energy of accumulator, and auxiliary improves the flying power of unmanned plane.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
Fig. 2 is the side structural representation of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
Fig. 3 is the drive mechanism schematic diagram of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
Fig. 4 is the chemical spraying device structural representation of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
Fig. 5 is the shower nozzle perspective view of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
Fig. 6 is the shower nozzle internal gear pump configuration schematic diagram of a kind of novel journey refuse landfill of present invention spray medicine unmanned plane;
In figure: 1-pair helical-blade, 2-motor, 3-medicine-chest, 4-gasoline engine, 5-supporting leg, 6-principal screw leaf a, 7-principal screw leaf b, 8-shower nozzle, 801-adjustable motor, 802-pipeline, 803-nozzle housing, 804-swivel head, 805-aperture, 806-base, 807-gear pump, 9-gasoline engine rotating shaft, 10-driving shaft gear, 11-counter gear group, 12-connecting rod, 13-support platform, 14-receptor.
Detailed description of the invention
For the ease of it will be appreciated by those skilled in the art that 1-6 below in conjunction with the accompanying drawings, the present invention is further illustrated.
A kind of novel journey refuse landfill spray medicine unmanned plane, mainly includes secondary helical-blade 1, motor 2, medicine-chest 3, gasoline engine 4, principal screw leaf a6, principal screw leaf b7, counter gear group 11, supports platform 13, connecting rod 12;nullDescribed support platform 13 connects some supporting legs 5,Supporting leg 5 is set to bending,Described support platform 13 is provided with driving shaft gear 10,Connect below described driving shaft gear 10 and have counter gear group 11,Two gears up and down of counter gear group 11 are connected to principal screw leaf a6 and principal screw leaf b7,Connected by Timing Belt on described driving shaft gear 10 and have gasoline engine rotating shaft 9,Described gasoline engine rotating shaft 9 is driven by gasoline engine 4,Described gasoline engine side is provided with electromotor,Gasoline engine 4 side is located at by described medicine-chest 3,Become half-surrounded,It is provided with receptor 14 below described medicine-chest 3,It is provided with gyroscope in receptor 14,The knee of described supporting leg 5 is provided with connecting rod 12,The one end stretched out by connecting rod 12 is connected motor 2,Described motor 2 is provided with secondary helical-blade 1,Stretch out a segment pipe connection in described connecting rod 12 and have shower nozzle 8,Shower nozzle 8 mainly includes adjustable motor 801、Pipeline 802、Nozzle housing 803、Swivel head 804、Aperture 805,Described adjustable motor 801 is externally provided with nozzle housing 803,Described nozzle housing 803 bottom is provided with base 806,Base 806 center is provided with gear pump 807,Nozzle housing 803 is provided with pipeline 802,Described adjustable motor 801 axle head center connects gear pump 807,Described swivel head 804 is connected to adjustable motor 801 axle head head,Swivel head 804 sidewall is provided with aperture 805,Shower nozzle 8 is connected in medicine-chest by pipeline 802,Medicinal liquid flows to above gear pump 807 through pipeline 802,Adjustable motor 801 driven gear pump 807 quick rotation,When pinion rotation,The volume in space of side of being out of gear is big from little change,Form vacuum,Draw liquid into,The volume in the space of gear engagement side is from diminishing greatly,And liquid is clamp-oned in pipeline,Liquid is thrown away by the aperture 805 of swivel head 804 under the effect of high speed centrifugation power,Atomizing effect is more preferable.
nullWork process is as follows: as a example by 4 in Figure of description 1 secondary helical-blades,Two secondary helical-blades above name shower nozzle 8 are A and B,4 secondary helical-blades of ranking name are respectively A clockwise、B、C、D,During fuselage flight aloft,Adjustment direction is carried out by 4 secondary helical-blades,Adjacent two secondary helical-blades of secondary helical-blade turn on the contrary,When two rotating speeds of C Yu D of secondary helical-blade increase,Fuselage will be made to advance to the direction at shower nozzle 8 place,When A and B rotating speed increases,Fuselage can be made to advance to the side not having shower nozzle 8,When two secondary helical-blade A at diagonal angle increase with C rotating speed,Fuselage can be made to rotate,Thus reach the purpose turned to,Medicine-chest 3 is connected to shower nozzle 8 by pipeline 802,Adjustable motor 801 on shower nozzle 8 is rotated 804,Medicine is sprayed from aperture 805,Swivel head 804 high-speed rotation makes medicinal atomized effect more preferable.
Above content is only the structure example to the present invention and explanation; described specific embodiment is made various amendment or supplements or use similar mode to substitute by affiliated those skilled in the art; without departing from invention structure or surmount scope defined in the claims, protection scope of the present invention all should be belonged to.

Claims (2)

1. a novel journey refuse landfill spray medicine unmanned plane, mainly includes secondary helical-blade, motor, medicine-chest, receptor, support platform, connecting rod;It is characterized in that the connection of described support platform has some supporting legs, supporting leg is set to bending, described medicine-chest is located at above support platform, become half-surrounded, being provided with receptor below described medicine-chest, be provided with gyroscope inside receptor, the knee of described supporting leg is provided with connecting rod, the one end stretched out by connecting rod is connected has motor, described motor to be provided with secondary helical-blade;Stretch out a segment pipe connection in described connecting rod and have shower nozzle, shower nozzle mainly includes adjustable motor, pipeline, nozzle housing, swivel head, aperture, described adjustable motor is externally provided with nozzle housing, nozzle housing is provided with pipeline, and described nozzle housing bottom is provided with base, and base center is provided with gear pump, described adjustable motor connects gear pump, described swivel head is connected on adjustable motor head axle head, and swivel head sidewall is provided with aperture, and shower nozzle is connected in medicine-chest by pipeline.
One the most according to claim 1 novel journey refuse landfill spray medicine unmanned plane, it is characterized in that described support platform is provided with driving shaft gear, connected by Timing Belt on described driving shaft gear and have gasoline engine rotating shaft, described gasoline engine rotating shaft is driven by gasoline engine, described gasoline engine side is provided with electromotor, connecting below described driving shaft gear and have counter gear group, two gears up and down of counter gear group are connected to principal screw leaf a and principal screw leaf b.
CN201510023588.7A 2015-01-17 2015-01-17 Novel range-extended chemical spraying unmanned aerial vehicle for refuse landfill Pending CN105836131A (en)

Priority Applications (1)

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CN201510023588.7A CN105836131A (en) 2015-01-17 2015-01-17 Novel range-extended chemical spraying unmanned aerial vehicle for refuse landfill

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Application Number Priority Date Filing Date Title
CN201510023588.7A CN105836131A (en) 2015-01-17 2015-01-17 Novel range-extended chemical spraying unmanned aerial vehicle for refuse landfill

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114011862A (en) * 2021-11-17 2022-02-08 甘肃省农业科学院土壤肥料与节水农业研究所 A high-efficient medicine prosthetic devices for heavy metal soil administers
WO2023079900A1 (en) * 2021-11-08 2023-05-11 株式会社石川エナジーリサーチ Flight device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023079900A1 (en) * 2021-11-08 2023-05-11 株式会社石川エナジーリサーチ Flight device
CN114011862A (en) * 2021-11-17 2022-02-08 甘肃省农业科学院土壤肥料与节水农业研究所 A high-efficient medicine prosthetic devices for heavy metal soil administers

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Application publication date: 20160810

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