CN107258490B - Can collect circular motion flight watering ware that formula is used for trees - Google Patents
Can collect circular motion flight watering ware that formula is used for trees Download PDFInfo
- Publication number
- CN107258490B CN107258490B CN201710540623.1A CN201710540623A CN107258490B CN 107258490 B CN107258490 B CN 107258490B CN 201710540623 A CN201710540623 A CN 201710540623A CN 107258490 B CN107258490 B CN 107258490B
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- water
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 82
- 238000009434 installation Methods 0.000 claims abstract 3
- 239000000523 sample Substances 0.000 claims description 28
- 239000007921 spray Substances 0.000 claims description 9
- 230000008878 coupling Effects 0.000 abstract description 2
- 238000010168 coupling process Methods 0.000 abstract description 2
- 238000005859 coupling reaction Methods 0.000 abstract description 2
- 230000001413 cellular effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000003973 irrigation Methods 0.000 description 2
- 230000002262 irrigation Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G25/00—Watering gardens, fields, sports grounds or the like
- A01G25/09—Watering arrangements making use of movable installations on wheels or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Water Supply & Treatment (AREA)
- Environmental Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Aviation & Aerospace Engineering (AREA)
- Guiding Agricultural Machines (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model provides a can collect circular motion flight watering ware that is used for trees, belong to the agricultural equipment field, by the aircraft organism, the counter weight, rotor and water supply installation constitute, the aircraft organism is by the base, prop the leg, the horizontal pole, first wire, cellular type motor, ultrasonic transducer, the ultrasonic wave body of visiting, the spreader, the control box, the top cap, the second wire, the thick pipe, the shower nozzle, a water pump, the upstand, the lantern ring, the third wire, main control board and GPS module constitute, the counter weight comprises counter weight body and counter weight hook, the rotor comprises pivot and blade, water supply installation is by the box, the apron, micro motor, the thin water pipe, the board axle, the water drum, big motor, the bucket axle, the motor shaft, shaft coupling and water inlet are constituteed, the useful part is: the work of the micro motor controls the opening and closing of the cover plate, so that the aircraft body is stored and hidden; the ultrasonic sensor can control the aircraft to realize directional circular motion.
Description
Technical Field
The invention relates to a collectable circular motion flight watering device for trees, in particular to a retractable circular motion flight watering device for trees, which realizes circular telecontrol by controlling the distance through a sensor and realizes the functions of positioning and displacement through a GPS module so as to realize the storage and the concealment of the flight watering device, and belongs to the field of agricultural equipment.
Background
Nowadays, the use of aircrafts is quite common and can be seen in all walks of life, and in daily life, the aircrafts are used for watering, particularly for flood irrigation, however, most aircrafts used for flood irrigation are large in size, and if the size of the aircrafts is reduced to enable the aircrafts to be used for watering in a small range under a common condition, the cost consumption of a watering process can be greatly reduced, and the watering precision and efficiency can also be improved.
Disclosure of Invention
In order to overcome the defects, the invention provides a retractable circular motion flying watering device for trees.
The invention is realized by the following technical scheme: a retractable circular motion flying watering device for trees comprises an aircraft body, a counterweight, a rotor and a water supply device, wherein the aircraft body consists of a base, support legs, a cross rod, a first lead, a hole type motor, an ultrasonic probe body, a cross rod, a control box, a top cover, a second lead, a thick pipe, a spray head, a water pump, a vertical column, a lantern ring, a third lead, a main control board and a GPS module, the support legs are installed on the base, the control box is fixed above the support legs, the cross rod is fixed on the outer side of the control box, the hole type motor is installed on the cross rod, the cross rod is installed on the front side of the control box, the ultrasonic probe body is fixed on the front end of the cross rod, the vertical column is fixed on the bottom of the front side of the control box, the lantern ring is installed on the lower portion of the vertical column, a thick pipe is fixed at the rear end of the control box, a spray head is installed at the tail end of the thick pipe, a water pump is installed in the middle of the thick pipe, a main control board is fixed in the control box and connected with a first wire, a second wire and a third wire, the first wire is connected with the main control board and a hole type motor, the second wire is connected with the main control board and the water pump, the third wire is connected with the main control board and an ultrasonic probe, a GPS module is installed above the main control board, and a top cover is fixed at the upper part of the control box; the counterweight is composed of a counterweight body and a counterweight hook, the counterweight body is fixed below the counterweight hook, and the counterweight hook is arranged in the sleeve ring; the rotary wing consists of a rotary shaft and blades, the blades are fixed on the outer surface of the rotary shaft, and the rotary shaft is arranged on the hole type motor; the water supply device comprises a box body, a cover plate, a micro motor, a thin water pipe, a plate shaft, a water barrel, a large motor, a barrel shaft, a motor shaft, a coupler and a water inlet, wherein the micro motor is installed at the upper edge of the box body, the plate shaft is connected with the two ends of the micro motor, the cover plate is fixed on the plate shaft, the water barrel and the large motor are installed inside the box body, the barrel shaft is fixed at one end of the water barrel, the motor shaft is fixed at one end of the large motor, the motor shaft and the barrel shaft are connected together through the coupler, the water barrel is fixed with the water inlet, one end of the thin water pipe is connected with a water pump and penetrates into the thick pipe, and one end of the thin water pipe is inserted into the water barrel.
Furthermore, the number of the bases is two, the number of the supporting legs is four and the supporting legs are symmetrically distributed, the number of the cross rods, the hole type motors and the first wires is six and the first wires are evenly distributed for 360 degrees, the number of the second wires, the cross columns, the ultrasonic probes and the ultrasonic probes is two, and the two second wires, the cross columns, the ultrasonic probes and the ultrasonic probes are symmetrically distributed about a middle axis plane of the aircraft body.
Furthermore, the thick pipe consists of two sections, the two sections form an included angle of 135 degrees, and a through hole is processed on the water pump.
Further, the counterweight hook is U-shaped and is in interference fit with the lantern ring.
Further, the box be the cuboid structure, the quantity of motor shaft and flat axle be two and symmetric distribution, the quantity of apron be four and symmetric distribution, thin water pipe coil around a water drum surface.
The invention has the advantages that: the work of the micro motor controls the opening and closing of the cover plate, so that the aircraft body is stored and hidden; the ultrasonic sensor can control the aircraft to realize directional circular motion.
Drawings
Fig. 1 is a schematic axial view of the whole of the present invention, fig. 2 is a schematic axial view of the whole of the aircraft body of the present invention with a top cover, fig. 3 is a top plan view of the aircraft body of the present invention without a top cover, fig. 4 is a partially enlarged view of the present invention at a, fig. 5 is a schematic axial view of the counterweight of the present invention, fig. 6 is a schematic axial view of the rotor of the present invention, fig. 7 is a schematic axial view of the water supply device of the present invention, and fig. 8 is a top plan view of the water supply device of the present invention.
In the figure, 1, an aircraft airframe; 2. balancing weight; 3. a rotor; 4. a water supply device; 101. a base; 102. supporting legs; 103. a cross bar; 104. a first conductive line; 105. a bore motor; 106. an ultrasonic probe; 107. an ultrasonic probe; 108. a cross post; 109. a control box; 110 a top cover; 111. a second conductive line; 112. a thick pipe; 113. a spray head; 114. a water pump; 115. a vertical post; 116. a collar; 117. a third conductive line; 118. a main control board; 119. a GPS module; 201. a counterweight body; 202. a counterweight hook; 301. rotating the shaft; 302. a blade; 401. a box body; 402. a cover plate; 403. a micro motor; 404. a thin water pipe; 405. a plate shaft; 406. a water cylinder; 407. a large motor; 408. a barrel shaft; 409. a motor shaft; 410. a coupling; 411. a water inlet.
Detailed Description
A retractable circular motion flying watering device for trees comprises an aircraft body 1, a counterweight 2, a rotor 3 and a water supply device 4, wherein the aircraft body 1 comprises a base 101, a supporting leg 102, a cross rod 103, a first lead 104, a hole type motor 105, an ultrasonic probe 106, an ultrasonic probe 107, a cross column 108, a control box 109, a top cover 110, a second lead 111, a thick pipe 112, a spray head 113, a water pump 114, a vertical column 115, a lantern ring 116, a third lead 117, a main control board 118 and a GPS module 119, the supporting leg 102 is arranged on the base 101, the control box 109 is fixed above the supporting leg 102, the cross rod 103 is fixed on the outer side of the control box 109, the hole type motor 105 is arranged on the cross rod 103, the cross column 108 is arranged on the front side of the control box 109, the ultrasonic probe 107 is fixed on the front end of the cross column 108, the ultrasonic probe 106 is arranged on the front end of the ultrasonic probe 107, the vertical column 115 is fixed on the bottom of the front side, a lantern ring 116 is arranged at the lower part of the vertical column 115, a thick pipe 112 is fixed at the rear end of the control box 109, a spray head 113 is arranged at the tail end of the thick pipe 112, a water pump 114 is arranged in the middle of the thick pipe 112, a main control board 118 is fixed in the control box 109, the main control board 118 is connected with a first lead 104, a second lead 111 and a third lead 117, the first lead 104 is connected with the main control board 118 and the hole type motor 105, the second lead 111 is connected with the main control board 118 and the water pump 114, the third lead 117 is connected with the main control board 118 and the ultrasonic probe 107, a GPS module 119 is arranged above the main control board 118, and a top cover 110 is fixed at the upper; the counterweight 2 consists of a counterweight body 201 and a counterweight hook 202, the counterweight body 201 is fixed below the counterweight hook 202, and the counterweight hook 202 is installed in the lantern ring 116; the rotor 3 is composed of a rotary shaft 301 and blades 302, the blades 302 are fixed on the outer surface of the rotary shaft 301, and the rotary shaft 301 is installed on the hole type motor 105; the water supply device 4 comprises a box body 401, a cover plate 402, a micro motor 403, a thin water pipe 404, a plate shaft 405, a water cylinder 406, a large motor 407, a cylinder shaft 408, a motor shaft 409, a coupler 410 and a water inlet 411, wherein the micro motor 403 is arranged on the upper edge of the box body 401, the plate shaft 405 is connected with two ends of the micro motor 403, the cover plate 402 is fixed on the plate shaft 405, the water cylinder 406 and the large motor 407 are arranged in the box body 401, the cylinder shaft 408 is fixed at one end of the water cylinder 406, the motor shaft 409 is fixed at one end of the large motor 407, the motor shaft 409 and the cylinder shaft 408 are connected together through the coupler 410, the water inlet 411 is fixed on the water cylinder 406, one end of the thin water pipe 404 is connected with the water pump 114 and extends into the thick pipe 112, one end is inserted into the water cylinder 406, the number of the bases 101 is two, the number of the support legs 102 is four and is symmetrically distributed, the number of, the number of the second conducting wires 111, the transverse columns 108, the ultrasonic probes 106 and the ultrasonic probes 107 is two, the conducting wires are symmetrically distributed about a middle shaft plane of the aircraft body 1, the thick pipe 112 is composed of two sections, an included angle of 135 degrees is formed between the two sections, a through hole is processed in the water pump 114, the counterweight hook 202 is in a U shape, the counterweight hook is in interference fit with the lantern ring 116, the box body 401 is of a cuboid structure, the number of the motor shafts 409 and the plate shafts 405 is two and symmetrically distributed, the number of the cover plates 402 is four and symmetrically distributed, and the thin water pipes 404 are wound on the outer surface of the water barrel 406.
When the device works, the whole body composed of the aircraft body 1, the counterweight 2 and the rotor wings 3 is collected in the water supply device 4, the cover plate 402 is in a closed state, when a worker remotely controls the main control board 118 and sends a watering signal to the main control board, the micro motor 403 simultaneously receives a signal to rotate the board shaft 405 so as to open the cover plate 402, after 10 seconds, the main control board 118 sends a signal to the large motor 407 through a wireless signal so that the large motor 407 positively rotates the water cylinder 406 through the motor shaft 409, the coupler 410 and the cylinder shaft 408, so that the part of the thin water pipe 404 wound on the water cylinder 406 is shortened, meanwhile, the main control board 118 sends a signal to the hole motor 105 through the first lead 104 so that the hole motor 105 drives the rotor wings 3 to positively rotate so as to vertically move the aircraft body 1 upwards, when the GPS module 119 detects that the set highest height is reached, the rotating speeds of the six rotor wings 3 are the same at the moment, 5 seconds later, the main control board 118 sends a signal to the water pump 114 through the second lead 111, the water pump 114 starts to work, water in the water cylinder 406 passes through the thin water pipe 404, the water pump 114, the thick pipe 112 and the spray head 113 and is aligned with leaves and flowers to spray the water, the purpose of watering is achieved, in the watering process, the distance between the aircraft body 1 and the trees is controlled in real time through the third lead 117 by the cooperative work of the ultrasonic probe 106 and the ultrasonic probe 107, so that the circular motion of the aircraft body 1 is achieved, after the watering task is completed, the main control board 118 sends a signal to the hole type motor 105 through the first lead 104 to enable the hole type motor 105 to drive the rotor 3 to rotate reversely to enable the aircraft body 1 to move vertically downwards, meanwhile, the main control board 118 sends a signal to the large motor 407 through the motor shaft 409, the coupler 410 and the cylinder shaft 408 to enable the water cylinder 406 to rotate reversely, so that the thin water pipe 404 wound on the water cylinder, after the GPS module 119 detects that the set minimum height is reached along with the reduction of the height, the six rotors 3 stop rotating, and after 5 seconds, the micro motor 403 works to rotate the plate shaft 405 so as to close the cover plate 402, thereby completing the whole watering process.
It will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in the embodiments described above without departing from the principles and spirit of the invention, the scope of which is defined by the appended claims.
Claims (2)
1. The utility model provides a can collect formula circular motion flight watering ware that is used for trees, comprises aircraft organism, counter weight, rotor and water supply installation, its characterized in that: the aircraft body consists of a base, supporting legs, a cross rod, a first lead, a hole type motor, an ultrasonic probe body, a cross column, a control box, a top cover, a second lead, a thick pipe, a spray head, a water pump, a vertical column, a lantern ring, a third lead, a main control board and a GPS module, wherein the supporting legs are installed on the base, the control box is fixed above the supporting legs, the cross rod is fixed on the outer side of the control box, the hole type motor is installed on the cross rod, the cross column is installed on the front side of the control box, the ultrasonic probe body is fixed on the front end of the cross column, the ultrasonic probe body is installed on the front end of the ultrasonic probe body, the vertical column is fixed on the bottom of the front side of the control box, the lantern ring is installed on the lower portion of the vertical column, the thick pipe is fixed on the rear end of the control box, the spray head is installed at the tail end of the thick pipe, a main control board is fixed in the control box and is connected with a first wire, a second wire and a third wire, the first wire is connected with the main control board and the hole type motor, the second wire is connected with the main control board and the water pump, the second wire is connected with the main control board and the ultrasonic probe, a GPS module is arranged above the main control board, and a top cover is fixed at the upper part of the control box; the counterweight is composed of a counterweight body and a counterweight hook, the counterweight body is fixed below the counterweight hook, and the counterweight hook is arranged in the sleeve ring; the rotary wing consists of a rotary shaft and blades, the blades are fixed on the outer surface of the rotary shaft, and the rotary shaft is arranged on the hole type motor; the water supply device comprises a box body, a cover plate, a micro motor, a thin water pipe, a plate shaft, a water barrel, a large motor, a barrel shaft, a motor shaft, a coupler and a water inlet, wherein the micro motor is installed on the upper edge of the box body, the plate shaft is connected with two ends of the micro motor, the cover plate is fixed on the plate shaft, the water barrel and the large motor are installed inside the box body, the barrel shaft is fixed at one end of the water barrel, the motor shaft is fixed at one end of the large motor, the motor shaft and the barrel shaft are connected together through the coupler, the water inlet is fixed on the water barrel, one end of the thin water pipe is connected with a water pump and extends into the thick pipe, and the other end of the thin water pipe is inserted into the water barrel;
the number of the bases is two, the number of the supporting legs is four and the supporting legs are symmetrically distributed, the number of the cross rods, the number of the hole type motors and the number of the first wires are six and the first wires are evenly distributed in 360 degrees, the number of the second wires, the cross columns, the number of the ultrasonic probes and the number of the ultrasonic probes are two, and the two second wires, the cross columns, the two ultrasonic probes and the two ultrasonic probes are symmetrically distributed about a middle axis plane of an aircraft body;
the thick pipe consists of two sections, the two sections form an included angle of 135 degrees, and a through hole is processed on the water pump; the counterweight hook is in a U-shaped shape and is in interference fit with the lantern ring.
2. A stowable, circular motion, flight sprinkler for trees, as claimed in claim 1, wherein: the box be the cuboid structure, the figure of motor shaft and flat axle be two and symmetric distribution, the figure of apron be four and symmetric distribution, thin water pipe coil around a water drum surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710540623.1A CN107258490B (en) | 2017-07-05 | 2017-07-05 | Can collect circular motion flight watering ware that formula is used for trees |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710540623.1A CN107258490B (en) | 2017-07-05 | 2017-07-05 | Can collect circular motion flight watering ware that formula is used for trees |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107258490A CN107258490A (en) | 2017-10-20 |
| CN107258490B true CN107258490B (en) | 2021-02-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710540623.1A Expired - Fee Related CN107258490B (en) | 2017-07-05 | 2017-07-05 | Can collect circular motion flight watering ware that formula is used for trees |
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| Country | Link |
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| CN105966610A (en) * | 2016-06-29 | 2016-09-28 | 南京信息工程大学 | Centre-of-gravity shift and yaw single-rotor helicopter |
| CN205952303U (en) * | 2016-08-03 | 2017-02-15 | 安阳全丰航空植保科技股份有限公司 | Oil moves many rotors plant protection unmanned aerial vehicle flight posture adjustment and changes device |
| CN206136728U (en) * | 2016-10-13 | 2017-05-03 | 无锡飞天侠科技有限公司 | Aircraft for branch and leaf is pruned in forestry |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN203199180U (en) * | 2013-03-04 | 2013-09-18 | 于国防 | Four-propeller airship with wired energy supply infusion for pesticide spraying and fertilization of crops |
| CN103754368A (en) * | 2014-01-25 | 2014-04-30 | 华南农业大学 | Air-ground combined agricultural spraying device and application thereof |
| CN104743119B (en) * | 2015-03-04 | 2017-10-31 | 珠海羽人飞行器有限公司 | A kind of agricultural aviation device |
| CN205589501U (en) * | 2016-05-12 | 2016-09-21 | 江西兴航智控航空工业有限公司 | Novel automatically, keep away and hinder unmanned aerial vehicle that sprays insecticide |
| CN105966598A (en) * | 2016-05-17 | 2016-09-28 | 王勇 | Agricultural plant protection aircraft |
| CN205971886U (en) * | 2016-08-23 | 2017-02-22 | 成都翼高九天科技有限公司 | Unmanned aerial vehicle retrieves structure |
| CN106081147B (en) * | 2016-08-23 | 2019-03-26 | 成都翼高九天科技有限公司 | Recyclable device in a kind of small drone room |
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2017
- 2017-07-05 CN CN201710540623.1A patent/CN107258490B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204210732U (en) * | 2014-11-05 | 2015-03-18 | 国网辽宁省电力有限公司检修分公司 | A kind of four rotor wing unmanned aerial vehicles for removing the flammable foreign matter in high-altitude |
| CN105966610A (en) * | 2016-06-29 | 2016-09-28 | 南京信息工程大学 | Centre-of-gravity shift and yaw single-rotor helicopter |
| CN205952303U (en) * | 2016-08-03 | 2017-02-15 | 安阳全丰航空植保科技股份有限公司 | Oil moves many rotors plant protection unmanned aerial vehicle flight posture adjustment and changes device |
| CN206136728U (en) * | 2016-10-13 | 2017-05-03 | 无锡飞天侠科技有限公司 | Aircraft for branch and leaf is pruned in forestry |
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| Publication number | Publication date |
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| CN107258490A (en) | 2017-10-20 |
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| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Jia Jian Inventor after: Zhang Yan Inventor after: Yao Junbing Inventor after: Zhou Jinlin Inventor before: Zhou Jinlin |
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Effective date of registration: 20210201 Address after: No.195, Hedong East Street, Yanhu District, Yuncheng City, Shanxi Province 044000 Applicant after: Jia Jian Applicant after: Zhang Yan Applicant after: Yao Junbing Address before: 250101 School of mechanical and electrical engineering, Shandong Jianzhu University, No.1000, Fengming Road, Lingang Development Zone, Licheng District, Jinan City, Shandong Province Applicant before: Zhou Jinlin |
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Granted publication date: 20210226 |