CN114013639B - Plant protection unmanned aerial vehicle based on 5G communication control - Google Patents
Plant protection unmanned aerial vehicle based on 5G communication control Download PDFInfo
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- CN114013639B CN114013639B CN202111548748.1A CN202111548748A CN114013639B CN 114013639 B CN114013639 B CN 114013639B CN 202111548748 A CN202111548748 A CN 202111548748A CN 114013639 B CN114013639 B CN 114013639B
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- aerial vehicle
- unmanned aerial
- box body
- plant protection
- communication control
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- 238000004891 communication Methods 0.000 title claims abstract description 20
- 239000003814 drug Substances 0.000 claims abstract description 22
- 238000005507 spraying Methods 0.000 claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 35
- 238000003756 stirring Methods 0.000 claims description 15
- 238000004146 energy storage Methods 0.000 claims description 12
- 238000005381 potential energy Methods 0.000 claims description 6
- 239000007921 spray Substances 0.000 claims description 6
- 239000012634 fragment Substances 0.000 claims description 5
- 230000000452 restraining effect Effects 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims 2
- 238000012423 maintenance Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000000875 corresponding effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- -1 seeds Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- 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
-
- 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
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
- B64D17/54—Opening, e.g. manual automatic
-
- 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
The application discloses a plant protection unmanned aerial vehicle based on 5G communication control. The device comprises a base, a transverse plate, a box body and a plurality of long arms fixedly arranged on the transverse plate, wherein each long arm is provided with rotatable flying pulp, and the transverse plate is also provided with a power mechanism for driving each flying pulp to rotate; the base is provided with a cylinder for containing the medicament and a spraying mechanism for extracting and spraying the medicament in the cylinder; the box body is internally provided with a disc installed through an elastic supporting mechanism, and the disc is internally provided with a parachute, and the parachute can be ejected to the outside of the box body through the elastic supporting mechanism to rescue the unmanned aerial vehicle. The beneficial effects are that: the falling speed of the unmanned aerial vehicle is slowed down, and the unmanned aerial vehicle is effectively rescue, so that the damage degree of the final unmanned aerial vehicle is reduced, and the subsequent maintenance cost is reduced.
Description
Technical Field
The application relates to an unmanned aerial vehicle, in particular to a plant protection unmanned aerial vehicle based on 5G communication control.
Background
The unmanned plane is usually composed of a flight platform (fixed wing, helicopter and multiaxis aircraft), a navigation flight control and a spraying mechanism, and various operations such as spraying medicament, seeds, powder and the like are realized through ground remote control or navigation flight control, wherein the unmanned plane needs to acquire instructions by acquiring signals in radio waves and complete corresponding actions.
At present, with the increasing maturity of 5G communication technology, compared with 4G communication technology, the performance goal of 5G communication is high data rate, reduce delay, save energy, reduce cost, improve system capacity and large-scale equipment connection, because the data transmission speed of 5G is fast, apply 5G on the plant protection unmanned aerial vehicle, can improve the sensitivity to unmanned aerial vehicle control greatly.
However, the existing plant protection unmanned aerial vehicle is not provided with a corresponding emergency protection measure, even if the control sensitivity is high due to the 5G communication technology, the unmanned aerial vehicle is difficult to control emergently and effectively due to insufficient power or special conditions, so that the unmanned aerial vehicle still can fall rapidly, and finally, the unmanned aerial vehicle is damaged to a great extent, and therefore, the cost of subsequent maintenance is increased.
Disclosure of Invention
The application aims to solve the technical problem of providing a plant protection unmanned aerial vehicle based on 5G communication control, which can rescue the unmanned aerial vehicle when the unmanned aerial vehicle falls rapidly due to insufficient power or special conditions, and reduce the damage degree of the final unmanned aerial vehicle.
In order to solve the technical problems, the plant protection unmanned aerial vehicle based on 5G communication control comprises a base, a transverse plate, a box body and a plurality of long arms fixedly arranged on the transverse plate, wherein each long arm is provided with rotatable flying pulp, and a power mechanism for driving each flying pulp to rotate is further arranged on the transverse plate; the base is provided with a cylinder for containing the medicament and a spraying mechanism for extracting and spraying the medicament in the cylinder; the box body is internally provided with a disc installed through an elastic supporting mechanism, and the disc is internally provided with a parachute, and the parachute can be ejected to the outside of the box body through the elastic supporting mechanism to rescue the unmanned aerial vehicle.
The utility model discloses a medicine box, including the base, the diaphragm is in the top of base, the diaphragm passes through four stand parallel mount the top of base, the box passes through two fixed settings of riser the top of diaphragm, spray mechanism includes the suction mechanism that sets up on the base and is connected and set up each with suction mechanism the sprinkler head of long arm bottom, the inside of drum is provided with the stirring piece of being connected with suction mechanism, through suction mechanism can with the medicine in the drum is taken out and is spouted through the sprinkler head that sets up long arm bottom, elasticity holds out the mechanism by installing the speed sensor control work of box bottom.
The suction mechanism comprises a water pump arranged on the upper part of the base and a second driving device arranged on the side part of the water pump, the output end of the second driving device is connected with a driving shaft of the water pump, a water inlet of the water pump is communicated with the cylinder through a guide pipe, and a water outlet of the water pump is connected with each spray head.
The inside of each stand is hollow structure, and two adjacent stand are through connecting pipe intercommunication, each stand respectively through a water piping connection sprinkler head, the delivery port of water pump with one of them stand passes through the pipe connection.
The stirring piece comprises a rotating shaft arranged in the cylinder and a plurality of stirring rods arranged on the outer circumference of the rotating shaft, wherein the upper end of the rotating shaft extends out to the top of the cylinder, and a bevel gear set is arranged between the upper end of the rotating shaft and the tail end of a driving shaft of the water pump.
The elastic supporting mechanism comprises an energy storage component arranged in the box body and an unlocking component arranged at the bottom of the box body, wherein elastic potential energy is reserved in the energy storage component when the parachute is positioned in the box body, and the unlocking component is used for restraining the elastic potential energy reserved in the energy storage component.
The energy storage component comprises a sliding structure arranged on the inner wall of the lower part of the box body and a supporting structure which is arranged on the sliding structure and connected with the disc; the sliding structure comprises two cross bars fixedly mounted on the inner wall of the lower portion of the box body, two sliding plates slidably arranged on the two cross bars, and two tension springs sleeved on the cross bars and connected between the two sliding plates.
The supporting structure comprises a cross bar arranged above the cross bar, a sliding groove formed in the bottom of the cross bar, two sliding blocks symmetrically and slidingly embedded in the sliding groove, and at least one group of scissors fork groups connected between the sliding blocks and the sliding plates, and the disc is fixed on the upper portion of the cross bar.
The unlocking component comprises two limiting strips positioned at the bottom of the box body, an electric telescopic rod arranged at the bottom of the box body and a connecting plate connected to the bottom ends of the two limiting strips, and the movable end of the electric telescopic rod is fixedly connected with the connecting plate;
the side edge of base still installs the polylith backup pad, the backup pad with be provided with first shell fragment between the bottom of base, the pulley is installed to the end of backup pad.
Compared with the prior art, the application has the beneficial effects that: when unmanned aerial vehicle appears falling fast because of the power is not enough or runs into special circumstances, the expansion end action of electric telescopic handle for spacing slat breaks away from with the slide, thereby the extension spring is kick-backed, make two slides be close to each other on the horizontal pole and slide, and drive two sliders and be close to each other at the bottom of whipstock through cutting fork group, then, just make the whipstock rise in the twinkling of an eye, pop out the parachute to the outside of box and open, slowed down unmanned aerial vehicle's falling speed, rescue effectively, thereby reduced final unmanned aerial vehicle and damaged the degree, reduced subsequent cost of maintenance.
Drawings
FIG. 1 is a schematic diagram of a plant protection unmanned aerial vehicle based on 5G communication control according to the present application;
FIG. 2 is a schematic top view of the case of the present application after being removed;
FIG. 3 is a schematic view of the bottom angle structure of the case of the present application after the case is removed;
FIG. 4 is a schematic view of the internal structure of the case in the present application in a top view;
FIG. 5 is a schematic view showing the internal structure of the case according to the present application;
fig. 6 is a schematic view of the internal structure of the cylinder according to the present application.
In the figure: 1-a base; 2-stand columns; 3-a cross plate; 4-vertical plates; 5-a box body; 6-long arms; 7-flying pulp; 8-a sprinkler; 9-supporting plates; 10-pulleys; 11-a first elastic piece; 12-a first drive; 13-a drive gear; 14-a driven gear; 15-a transmission belt; 16-cylinder; 17-a second drive; 18-a water pump; 19-bevel gear set; 20-rotating shaft; 21-stirring rod; 22-conduit; 23-connecting pipes; 24-turning cover; 25-a second spring plate; 26-parachute; 27-a disc; 28-a cross bar; 29-a slide plate; 30-a tension spring; 31-a bar; 32-a slider; 33-a scissors group; 34-limiting laths; 35-connecting plates; 36-an electric telescopic rod; 37-speed sensor.
Detailed Description
In the following description of the present application, the 5G communication control-based plant protection unmanned aerial vehicle will be further described in detail with reference to the accompanying drawings and the specific embodiments, it should be noted that, in the description of the present application, the directions or positional relationships indicated by the terms "inner", "outer", "upper", "lower", "front", "rear", etc. are positional relationships indicated based on the drawings, only for convenience of describing the present application and simplifying the description, and are not indicative or implying that the referred devices or elements must have a specific direction, be configured and operated in a specific direction, and therefore should not be construed as limiting the present application.
Referring to fig. 1 to 6, the plant protection unmanned aerial vehicle based on 5G communication control of the present embodiment includes a base 1, a transverse plate 3 fixedly installed above the base 1 and parallel to the base through four upright posts 2, and a box 5 fixedly installed above the transverse plate 3 through two upright plates 4, wherein the two upright plates 4 are respectively fixed at two sides of the transverse plate 3; four long arms 6 are fixedly mounted on the side of the transverse plate 3, one flying pulp 7 is rotatably arranged on the upper portion of each long arm 6, a power mechanism for rotating the four flying pulps 7 is mounted on the transverse plate 3, the power mechanism comprises a driving gear 13 rotatably mounted on the upper portion of the transverse plate 3, four driven gears 14 rotatably mounted on the upper portion of the transverse plate 3 and a first driving device 12 mounted on the bottom of the transverse plate 13, the driven gears 14 are meshed with the driving gear 13, the driven gears 14 are connected with rotating shafts of the flying pulps 7 through driving belts 15, and when the unmanned aerial vehicle is used, the first driving device 17 drives the flying pulps 7 to rotate through the driving gears 13, the driven gears 14 and the driving belts 15, so that ascending power is provided for the unmanned aerial vehicle, and a device (not shown in the drawing) for driving the unmanned aerial vehicle to generate horizontal displacement is also arranged in the unmanned aerial vehicle, and is connected with the ground through a 5G network and controlled by workers.
The bottom of the base 1 is provided with a cylinder 16 for containing the medicament to be sprayed, the upper part of the base 1 is provided with a spraying mechanism for extracting and spraying the medicament in the cylinder 16, the spraying mechanism comprises a suction mechanism arranged on the base 1 and spraying heads 8 connected with the suction mechanism and arranged at the bottom of each long arm 6, the inside of the cylinder 16 is provided with stirring pieces connected with the suction mechanism, the medicament in the cylinder 16 can be extracted through the suction mechanism and sprayed out through the spraying heads 8 arranged at the bottom of the long arms 6, wherein, as can be seen in fig. 3, the suction mechanism comprises a water pump 18 arranged at the upper part of the base 1, a second driving device 17 arranged at the side part of the water pump 18, the output end of the second driving device 17 is connected with the driving shaft of the water pump 18, the water inlet of the water pump 18 is communicated with the cylinder 16 through a conduit 22, the water outlet of the water pump 18 is connected with each spraying head 8 through four upright posts 2, specifically, the inside of each upright post 2 is hollow structure, two adjacent upright posts 2 are communicated through a connecting pipe 23, each upright post is connected with the water outlet 2 through a water pipe connecting head 8, and one upright post 2 is connected with a pipeline.
The disc 27 installed through the elastic supporting mechanism is arranged in the box body 5, the parachute 26 is arranged in the disc 27, the elastic supporting mechanism is controlled to work by the speed sensor 37 installed at the bottom of the box body 5, and therefore the parachute can be ejected to the outside of the box body through the elastic supporting mechanism to rescue the unmanned aerial vehicle.
Further, the elastic supporting mechanism comprises an energy storage component installed in the box 5 and an unlocking component installed at the bottom of the box 5, the energy storage component stores elastic potential energy when the parachute 26 is positioned in the box 5, the unlocking component is used for restraining the elastic potential energy stored by the energy storage component, and the energy storage component comprises a sliding structure arranged on the inner wall of the lower part of the box 5 and a supporting structure arranged on the sliding structure and connected with the disc 27 as shown in fig. 4 and 5; the sliding structure comprises two cross bars 28 fixedly arranged on the inner wall of the lower part of the box body 5, two sliding plates 29 arranged on the two cross bars 28 in a sliding manner and two tension springs 30 connected between the two sliding plates 29, specifically, the tension springs 30 are sleeved on the cross bars 28, and two ends of the tension springs are respectively connected with the two sliding plates 29; the structure of holding out includes setting up the bar 31 in horizontal pole 28 top, two sliders 32 of symmetry slip gomphosis in the spout of spout offered in the bottom of bar 31 and two sets of scissors group 33 of connection between slider 32 and slide 29, disc 27 fixes the upper portion at bar 31, wherein, scissors group 33 includes two equal and the bracing piece that is "X" shape setting of length, the intersection department of two bracing pieces passes through the shaft rotation to be connected, and the head end of two articulates with slide 29, the end articulates with slider 32, the unblock subassembly includes two limit slat 34 that are located box 5 bottom, install the electric telescopic handle 36 in the bottom of box 5 and connect the connecting plate 35 in the bottom of two limit slat 34, electric telescopic handle 36's expansion end and connecting plate 35 fixed connection, limit slat 34 and slide 29 butt, when unmanned aerial vehicle appears falling fast because of the power is insufficient or runs into special circumstances, speed sensor 37 then perceives the speed of its whereabouts, electric telescopic handle 36's expansion end makes limit slat 34 and slide 29 break away from, thereby the extension spring 30 makes two limit slat 30 and slide bar 29 slide out at the bottom of two sides 31 at the bottom of the box 31, make two sides at the speed of falling down to the box 31, make two pairs of the horizontal pole 26 slide mutually near each other, the speed of falling down at the box 31, the speed of the horizontal bar is opened, the outside is closed to the speed of the horizontal bar is opened, the top down at the speed of the top of the horizontal bar is opened, and the speed is opened.
Still further, the lateral edge of base 1 still rotate and install polylith backup pad 9, be provided with first shell fragment 11 between backup pad 9 and the bottom of base 1, it can be seen from the figure that one side of first shell fragment 11 is fixed with backup pad 9, the another side is fixed with base 1, pulley 10 is installed to the end of backup pad 9, when unmanned aerial vehicle whereabouts, backup pad 9 at first contacts with ground, pulley 10 rolls on ground, rotation of certain angle takes place for backup pad 9 to make first shell fragment 11 take place a degree of deformation, in this way, just played the cushioning effect to unmanned aerial vehicle's whereabouts, further promoted unmanned aerial vehicle's protection effect.
Still further, the stirring member includes a rotating shaft 20 rotatably installed in the cylinder 16, a plurality of stirring rods 21 uniformly circumferentially disposed on the outer surface of the rotating shaft 20, wherein the central axes of the rotating shaft 20 and the cylinder 16 are coincident, a bevel gear set 19 is installed between the upper end of the rotating shaft 20 and the end of the driving shaft, the bevel gear set 19 includes a first bevel gear fixed on the end of the driving shaft of the water pump 18 and a second bevel gear fixed on the top end of the rotating shaft 20, the first bevel gear is meshed with the second bevel gear, when in use, the second driving device 17 drives the water pump 18 to work, the water pump 18 sucks out the medicine in the cylinder 16 through a guide pipe 22, and the water outlet discharges the medicine to the spray head 8 for spraying, at the same time, the driving shaft of the water pump 18 drives the rotating shaft 20 through the bevel gear set 19 to rotate, and the stirring rods 21 mix and stir the medicine in the cylinder 16, so that the uniformity of the medicine is ensured, and the effect of plant protection is improved.
Still further, two flip covers 24 may be rotatably disposed on the upper portion of the case 5, a second elastic sheet 25 is disposed between the bottom of the two flip covers 24 and the side wall of the case 5, one side of the elastic sheet 25 is fixed to the side wall of the case 5, and the other side of the elastic sheet is fixed to the bottom of the flip cover 24, so that when the elastic supporting mechanism works, the disc 27 is driven to move vertically upwards to open the two flip covers 24, and the parachute 26 is supported.
In the concrete implementation of the application, the medicament to be sprayed is input into the cylinder 16, a worker controls the unmanned aerial vehicle to fly on the ground, the suction mechanism works to pump the medicament out of the cylinder 16 and spray the medicament downwards through the spray head 8, and at the same time, the suction mechanism also drives the stirring piece to work, the stirring piece mixes and stirs the medicament in the cylinder 16, the uniformity of medicament spraying is improved, and the operation effect of the unmanned aerial vehicle is improved.
In addition, the speed sensor 37 is an application of the prior art, and the present application is not described in detail with respect to its specific working principle;
in the unmanned aerial vehicle in-process of using, speed sensor 37 is used for monitoring unmanned aerial vehicle's speed of falling, when unmanned aerial vehicle appears falling fast because of the power is not enough or runs into special circumstances, speed sensor 37 then can send control signal for control module, and control module just controls elasticity and holds in the palm out mechanism work, pops out parachute 26 to the outside of box 5, rescue unmanned aerial vehicle, reduce final unmanned aerial vehicle damage degree, reduce subsequent cost of maintenance.
The first elastic sheet 11 and the second elastic sheet 25 are common elastic components, and can be replaced by torsion springs, so that the application is not limited in detail and can be selected according to actual requirements.
The present application is not limited to the above-mentioned embodiments, and any equivalent embodiments which can be changed or modified by the technical content disclosed above can be applied to other fields, but any simple modification, equivalent changes and modification made to the above-mentioned embodiments according to the technical substance of the present application without departing from the technical content of the present application still belong to the protection scope of the technical solution of the present application.
Claims (7)
1. The utility model provides a plant protection unmanned aerial vehicle based on 5G communication control, includes base (1), diaphragm (3), box (5) and many long arms (6) of fixed mounting on diaphragm (3), each be provided with on long arm (6) rotatable flight thick liquid (7), still install on diaphragm (3) be used for driving each flight thick liquid (7) pivoted power unit; the base (1) is provided with a cylinder (16) for containing the medicament and a spraying mechanism for extracting and spraying the medicament in the cylinder (16); the box body (5) is internally provided with a disc (27) which is installed through an elastic supporting mechanism, a parachute (26) is arranged in the disc (27), and the parachute can be ejected to the outside of the box body through the elastic supporting mechanism to rescue the unmanned aerial vehicle; the elastic supporting mechanism comprises an energy storage component arranged in the box body (5) and an unlocking component arranged at the bottom of the box body (5), wherein the energy storage component stores elastic potential energy when the parachute (26) is positioned in the box body (5), and the unlocking component is used for restraining the elastic potential energy stored by the energy storage component; the energy storage assembly comprises a sliding structure arranged on the inner wall of the lower part of the box body (5) and a supporting structure which is arranged on the sliding structure and is connected with the disc (27); the sliding structure comprises two cross bars (28) fixedly arranged on the inner wall of the lower part of the box body (5), two sliding plates (29) arranged on the two cross bars (28) in a sliding manner, and two tension springs (30) sleeved on the cross bars (28) and connected between the two sliding plates (29); the supporting structure comprises a cross bar (31) arranged above the cross bar (28), a chute formed in the bottom of the cross bar (31), two sliding blocks (32) symmetrically and slidingly embedded in the chute, and at least one group of scissors group (33) connected between the sliding blocks (32) and the sliding plates (29), wherein the disc (27) is fixed on the upper portion of the cross bar (31).
2. The 5G communication control-based plant protection drone of claim 1, wherein: the horizontal plate (3) is installed in parallel through four stand columns (2) the top of base (1), box (5) are in through the fixed top that sets up of two riser (4) diaphragm (3), spraying mechanism includes the suction mechanism that sets up on base (1) and is connected and set up in each with suction mechanism sprinkler head (8) of long arm (6) bottom, the inside of drum (16) is provided with the stirring piece of being connected with suction mechanism, through suction mechanism can be with medicament in drum (16) is taken out and is being in sprinkler head (8) blowout of long arm (6) bottom through setting up, elasticity holds out the mechanism by install speed sensor (37) control work in box (5) bottom.
3. The plant protection unmanned aerial vehicle based on 5G communication control according to claim 2, wherein: the suction mechanism comprises a water pump (18) arranged on the upper portion of the base (1), and a second driving device (17) arranged on the side portion of the water pump (18), wherein the output end of the second driving device (17) is connected with a driving shaft of the water pump (18), a water inlet of the water pump (18) is communicated with the cylinder (16) through a guide pipe (22), and a water outlet of the water pump (18) is connected with each spray head (8).
4. A plant protection unmanned aerial vehicle based on 5G communication control according to claim 3, wherein: the inside of each stand (2) is hollow structure, and two adjacent stands (2) are communicated through connecting pipe (23), each stand respectively through a water piping connection sprinkler head (8), the delivery port of water pump (18) with one of them stand (2) pass through the pipe connection.
5. The 5G communication control-based plant protection drone of claim 3 or 4, wherein: the stirring piece comprises a rotating shaft (20) arranged in the cylinder (16), and a plurality of stirring rods (21) arranged on the outer circumference of the rotating shaft (20), wherein the upper end of the rotating shaft (20) extends out to the top of the cylinder (16) and a bevel gear set (19) is arranged between the upper end of the rotating shaft and the tail end of a driving shaft of the water pump (18).
6. The 5G communication control-based plant protection drone of claim 5, wherein: the unlocking assembly comprises two limiting strips (34) arranged at the bottom of the box body (5), an electric telescopic rod (36) arranged at the bottom of the box body (5) and a connecting plate (35) connected to the bottom ends of the two limiting strips (34), and the movable end of the electric telescopic rod (36) is fixedly connected with the connecting plate (35).
7. The 5G communication control-based plant protection drone of claim 6, wherein: the side edge of base (1) still installs polylith backup pad (9), backup pad (9) with be provided with first shell fragment (11) between the bottom of base (1), pulley (10) are installed to the end of backup pad (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111548748.1A CN114013639B (en) | 2021-12-17 | 2021-12-17 | Plant protection unmanned aerial vehicle based on 5G communication control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111548748.1A CN114013639B (en) | 2021-12-17 | 2021-12-17 | Plant protection unmanned aerial vehicle based on 5G communication control |
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| Publication Number | Publication Date |
|---|---|
| CN114013639A CN114013639A (en) | 2022-02-08 |
| CN114013639B true CN114013639B (en) | 2023-10-17 |
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| CN202111548748.1A Active CN114013639B (en) | 2021-12-17 | 2021-12-17 | Plant protection unmanned aerial vehicle based on 5G communication control |
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| CN113120243A (en) * | 2021-04-14 | 2021-07-16 | 国网山东省电力公司淄博供电公司 | Passive mechanical general parachute of unmanned aerial vehicle |
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