CN221189090U - Unmanned aerial vehicle sprinkler with dismouting structure - Google Patents
Unmanned aerial vehicle sprinkler with dismouting structure Download PDFInfo
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- CN221189090U CN221189090U CN202323170919.9U CN202323170919U CN221189090U CN 221189090 U CN221189090 U CN 221189090U CN 202323170919 U CN202323170919 U CN 202323170919U CN 221189090 U CN221189090 U CN 221189090U
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- aerial vehicle
- unmanned aerial
- vehicle body
- liquid tank
- support
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- 239000007788 liquid Substances 0.000 claims abstract description 38
- 230000000670 limiting effect Effects 0.000 claims abstract description 25
- 238000005507 spraying Methods 0.000 claims abstract description 21
- 230000006835 compression Effects 0.000 claims abstract description 12
- 238000007906 compression Methods 0.000 claims abstract description 12
- 230000001360 synchronised effect Effects 0.000 claims abstract description 9
- 239000007921 spray Substances 0.000 claims abstract description 4
- 238000004891 communication Methods 0.000 claims description 8
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
- 230000006978 adaptation Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 238000001125 extrusion Methods 0.000 description 4
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003973 irrigation Methods 0.000 description 1
- 230000002262 irrigation Effects 0.000 description 1
- 230000009916 joint effect Effects 0.000 description 1
- 239000002420 orchard Substances 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 125000003003 spiro group Chemical group 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle spraying equipment, in particular to unmanned aerial vehicle spraying equipment with a disassembly and assembly structure, which comprises an unmanned aerial vehicle body, wherein four supporting bodies are fixedly installed at the bottom of the unmanned aerial vehicle body, four supporting rods are fixedly installed at the upper side of the unmanned aerial vehicle body, a mounting cylinder is fixedly installed on each supporting rod, a synchronous motor is installed at the inner side of each mounting cylinder, a blade is fixedly installed at the output end of each synchronous motor, two supports are symmetrically installed at the upper side of the unmanned aerial vehicle body, a liquid tank is installed above each support, a clamping assembly is arranged at the bottom of each liquid tank, a limiting assembly is arranged at the inner side of each support, and a spray head is installed at the bottom of each unmanned aerial vehicle body. The fixing mode of the liquid tank is a clamping mode, the assembly and the disassembly are convenient and quick, meanwhile, different action directions of the extension spring and the compression spring are utilized, a reliable double-protection effect is provided for the clamping fixing mode of the liquid tank, and the unstable slipping of the liquid tank in the operation process of the unmanned aerial vehicle is prevented.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle spraying equipment, in particular to unmanned aerial vehicle spraying equipment with a disassembly and assembly structure.
Background
Unmanned aircraft, i.e., unmanned aircraft, is unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either entirely or intermittently, by an on-board computer; at present, pesticide spraying, irrigation and other aspects of large farms or orchards gradually tend to be operated by unmanned aerial vehicle spraying equipment, and the unmanned aerial vehicle spraying equipment has the advantages of high possession efficiency, large operation radius and the like and is not influenced by terrain.
The utility model discloses agricultural unmanned aerial vehicle spraying equipment with reference to an issued patent number of CN216805835U, which comprises a disc shell, wherein a supporting frame is fixedly arranged on the outer surface of the disc shell, six groups of integrated motors which are annularly distributed are fixedly arranged on the supporting frame, and paddles are rotatably arranged at the top of the integrated motors.
The above patents have some technical drawbacks in use: the fixed mode of its water tank adopts extrusion spring extrusion arc piece, utilizes the mode of arc piece extrusion block bearing bar to fix the water tank, and arc extrusion piece does not possess the joint ability when upwards lifting the water tank, consequently can arouse the water tank slope when unmanned aerial vehicle turns when aerial work, and the water tank receives gravity to influence there is the risk of slippage from the bearing bar, and the axis direction of joint mode relative bearing bar does not have the joint effect, and the water tank still exists unstability slippage risk because of the air current influence in unmanned aerial vehicle flight.
Disclosure of utility model
The utility model aims to solve the defects in the prior art, and provides unmanned aerial vehicle spraying equipment with a disassembly and assembly structure.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
Unmanned aerial vehicle sprinkler with dismouting structure, including the unmanned aerial vehicle body, unmanned aerial vehicle body bottom fixed mounting has four support bodies, unmanned aerial vehicle body upside fixed mounting has four branches, fixed mounting has a mounting cylinder on the branch, synchronous motor is installed to the mounting cylinder inboard, synchronous motor output fixed mounting has the blade, two supports are installed to unmanned aerial vehicle body upside symmetry, the liquid tank is installed to the support top, liquid tank bottom is provided with the joint subassembly, the support inboard is provided with spacing subassembly, the shower nozzle is installed to unmanned aerial vehicle body bottom.
Preferably, the upper side of the liquid tank is provided with a liquid injection port, and the bottom of the liquid tank is provided with a downpipe.
Preferably, the unmanned aerial vehicle body upside corresponds downpipe department and installs the adapter tube, the spiro union has the nut on the adapter tube.
Preferably, the downpipe and the connecting pipe are provided with continuous male threads, and the inner side of the nut is provided with female threads matched with the male threads.
Preferably, unmanned aerial vehicle body internally mounted has a communication pipe, battery and control mainboard, the communication pipe is linked together with the nozzle with the extension pipe.
Preferably, the clamping assembly comprises fixing strips, a notch, extension springs, sliding plates and sliding blocks, the four fixing strips are symmetrically arranged at the bottom of the liquid tank respectively, the notch is formed in the inner side of the fixing strips, the extension springs are arranged on the inner side of the notch and are fixedly connected with the sliding blocks and the inner walls of the notch respectively, the sliding blocks are fixedly arranged on the two sides of the sliding plates, and the sliding plates are connected with the fixing strips in a sliding mode through the sliding blocks.
Preferably, the limiting component comprises a sliding groove, a sleeve box, a limiting block and a compression spring, wherein the sliding groove is formed in the support, the sliding groove is matched with the section of the sliding plate in size, the sleeve box is fixedly mounted on the upper side of the unmanned aerial vehicle body, the limiting block is slidably connected to the inner side of the sleeve box, and the compression spring is fixedly mounted between the bottom of the limiting block and the bottom of the inner side of the sleeve box.
Preferably, the handle is fixedly arranged on the outer side of the sliding plate, a limiting groove is formed in the sliding plate, and the limiting groove is matched with the limiting block.
According to the unmanned aerial vehicle spraying equipment with the dismounting structure, the nut is screwed on the outer side of the faucet tube, the downpipe at the bottom of the liquid tank can be upwards connected by rotating the nut, the external walls of the downpipe and the faucet tube are provided with the male threads matched with the female threads on the inner side of the nut, and when the nut is rotated between the downpipe and the faucet tube, the communication between the downpipe and the faucet tube can be completed.
According to the unmanned aerial vehicle spraying equipment with the dismounting structure, the handle is pulled outwards to drive the sliding plate to move outwards, at the moment, the sliding block slides in the notch at the inner side of the fixing strip to drive the extension spring to stretch, the liquid tank is aligned to be placed on the support, the handle is loosened, the sliding block can be driven to slide under the action of the retraction force of the extension spring to drive the sliding plate to move inwards, the sliding plate penetrates through the sliding groove on the support, the inner side end acts on the inclined section of the limiting block, at the moment, the handle is pushed by force, the limiting block gradually retracts to the inner side of the sleeve box under the action of the pressure of the inner side end of the sliding plate, the handle is pushed continuously, when the limiting groove on the sliding plate is located right above the limiting block, at the moment, the limiting block is inserted into the inner side of the limiting groove to form a limiting action on the sliding plate under the action of the elasticity of the compression spring, the clamping action between the sliding groove and the sliding plate provides a fixing action for the liquid tank, at the moment, the risk of the sliding plate from the sliding groove is prevented due to the fact that the elasticity of the extension spring is insufficient, the sliding groove is used for the clamping action of the sliding plate, the sliding box is prevented from being blocked by the different action directions of the extension spring and the sliding box, and the reliable action of the liquid tank is prevented from being unstable in the process of the unmanned aerial vehicle.
The utility model has reasonable design, through arranging the convex screw threads matched with the concave screw threads on the inner side of the nut on the outer walls of the downpipe and the bearing pipe, the connection mode is fixed and reliable when the nut is rotated between the downpipe and the bearing pipe, in addition, the clamping mode is adopted in the fixing mode of the liquid tank, the assembly and the disassembly are convenient and quick, and meanwhile, the clamping and fixing modes of the liquid tank are provided with reliable double guarantee functions by utilizing different action directions of the extension spring and the compression spring, so as to prevent the unstable and slipping of the liquid tank in the operation process of the unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle spraying device with a detachable structure according to the present utility model;
Fig. 2 is a schematic cross-sectional structure of an unmanned aerial vehicle spraying device with a detachable structure according to the present utility model;
Fig. 3 is a schematic diagram of a partially disassembled three-dimensional structure of an unmanned aerial vehicle spraying device with a disassembly and assembly structure;
Fig. 4 is a partially disassembled perspective view of an unmanned aerial vehicle spraying device with a disassembly and assembly structure according to a second embodiment of the present utility model;
FIG. 5 is an enlarged schematic view of portion A of FIG. 2;
fig. 6 is an enlarged schematic view of a portion B of fig. 2.
In the figure: 1. an unmanned aerial vehicle body; 2. a support body; 3. a support rod; 4. a mounting cylinder; 5. a synchronous motor; 6. a blade; 7. a support; 8. a socket pipe; 9. a liquid tank; 10. a liquid injection port; 11. a fixing strip; 12. a notch; 13. a tension spring; 14. a slide plate; 15. a slide block; 16. a handle; 17. a limit groove; 18. a chute; 19. a sleeve; 20. a limiting block; 21. a compression spring; 22. a downpipe; 23. a nut; 24. a communicating pipe; 25. a spray head; 26. a storage battery; 27. and controlling the main board.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Referring to fig. 1-6, an unmanned aerial vehicle spraying equipment with dismouting structure, including unmanned aerial vehicle body 1, unmanned aerial vehicle body 1 bottom fixed mounting has four support bodies 2, unmanned aerial vehicle body 1 upside fixed mounting has four branches 3, fixed mounting has a mounting cylinder 4 on the branch 3, synchronous motor 5 is installed to the mounting cylinder 4 inboard, synchronous motor 5 output fixed mounting has blade 6, two supports 7 are installed to unmanned aerial vehicle body 1 upside symmetry, liquid tank 9 is installed to support 7 top, liquid tank 9 bottom is provided with the joint subassembly, support 7 inboard is provided with spacing subassembly, shower nozzle 25 is installed to unmanned aerial vehicle body 1 bottom, annotate liquid mouth 10 is installed to liquid tank 9 upside, down pipe 22 is installed to liquid tank 9 bottom.
In this embodiment, the position of the upper side of the unmanned aerial vehicle body 1 corresponding to the downpipe 22 is provided with a joint pipe 8, the joint pipe 8 is screwed with a nut 23, the downpipe 22 and the joint pipe 8 are provided with continuous male threads, and the inner side of the nut 23 is provided with female threads matched with the male threads.
Through the structure, when the nut 23 is rotated between the downpipe 22 and the joint pipe 8, the connection between the downpipe 22 and the joint pipe 8 can be completed, and the connection mode adopts the threaded connection, so that the connection is firm and the disassembly is easy.
In this embodiment, the unmanned aerial vehicle body 1 internally installs a communication pipe 24, a storage battery 26 and a control main board 27, and the communication pipe 24 is communicated with the faucet pipe 8 and the spray head 25.
Through the above structure, the electrical components in the device provided with the battery 26 provide power supply, and the control main board 27 controls the electrical components to cooperate and receive the operation command sent from the ground.
In this embodiment, the joint subassembly includes fixed strip 11, notch 12, extension spring 13, slide 14 and slider 15, and slider 15 fixed mounting is in slide 14 both sides, and slide 14 passes through slider 15 and fixed strip 11 sliding connection, and notch 12 is seted up at fixed strip 11 inboard, and four fixed strips 11 are symmetry respectively and are installed in liquid tank 9 bottom, and extension spring 13 sets up at notch 12 inboard and extension spring 13 both ends respectively with slider 15 and notch 12 inner wall fixed connection.
Through the structure, the retractive force of the extension spring 13 acts on the sliding block 15, so that the sliding block 15 has a trend of sliding inwards, namely, the sliding plate 14 is driven to slide inwards, when the liquid tank 9 is placed on the support 7, the sliding plate 14 slides inwards and is clamped into a sliding groove on the support 7 under the action of the extension spring 13, and the fixing and clamping effect on the liquid tank 9 is completed.
In this embodiment, spacing subassembly includes spout 18, box 19, stopper 20 and compression spring 21, box 19 fixed mounting is in unmanned aerial vehicle body 1 upside, spout 18 is seted up on support 7 and spout 18 size and slide 14 cross-section size looks adaptation, compression spring 21 fixed mounting is between stopper 20 bottom and box 19 inboard bottom, stopper 20 sliding connection is inboard at box 19, slide 14 outside fixed mounting has handle 16, limit groove 17 has been seted up on the slide 14, limit groove 17 and stopper 20 assorted.
Through the structure, the limiting block 20 adopts the design of the inclined section, so that when the sliding plate 14 acts on the inclined section of the limiting block 20 when being inserted inwards, the limiting block 20 automatically retracts to the inner side of the sleeve box 19 under the action of force, and the limiting block 20 can conveniently clamp the limiting groove 17 on the sliding plate 14 in the next step.
In the utility model, when the liquid box is used, the handle 16 is pulled outwards to drive the slide plate 14 to move outwards, at the moment, the slide block 15 slides in the notch 12 at the inner side of the fixed strip 11 to drive the extension spring 13 to stretch, the liquid box 9 is aligned to be placed on the support 7, the handle 16 is loosened, the slide block 15 can be driven to slide under the action of the retraction force of the extension spring 13, and further the slide plate 14 is driven to move inwards, the slide plate 14 passes through the slide groove 18 on the support 7, the inner side end acts on the inclined section of the limit block 20, at the moment, the handle 16 is pushed by force, the limit block 20 gradually retracts to the inner side of the sleeve 19 under the action of pressure at the inner side end of the slide plate 14, the handle 16 is pushed continuously, at the moment, the limit block 20 is inserted into the inner side of the limit groove 17 under the action of the elasticity of the compression spring 21 to form a limit action on the slide plate 14, the clamping process is completed, at the moment, the clamping action between the slide groove 18 and the slide plate 14 provides a fixing action for the liquid box 9, the clamping action of the limit block 20 and the limit groove 17 on the slide plate 14 is prevented from being unstable due to the fact that the elasticity of the extension spring 13 is insufficient, and the sliding action of the slide plate 14 is not stable, and the liquid box 9 is not fixed by the two-way of the compression spring 9 is ensured, and the double operation mode is guaranteed.
While the fundamental and principal features of the utility model and advantages of the utility model have been shown and described, it will be apparent to those skilled in the art that the utility model is not limited to the details of the foregoing exemplary embodiments, but may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.
Claims (6)
1. Unmanned aerial vehicle sprinkler with dismouting structure, a serial communication port, including unmanned aerial vehicle body (1), unmanned aerial vehicle body (1) bottom fixed mounting has four support bodies (2), unmanned aerial vehicle body (1) upside fixed mounting has four branch (3), fixed mounting has mounting cylinder (4) on branch (3), synchronous motor (5) are installed to mounting cylinder (4) inboard, synchronous motor (5) output fixed mounting has blade (6), unmanned aerial vehicle body (1) upside symmetry installs two support (7), liquid tank (9) are installed to support (7) top, liquid tank (9) bottom is provided with joint subassembly, support (7) inboard is provided with spacing subassembly, unmanned aerial vehicle body (1) bottom is installed shower nozzle (25), joint subassembly includes fixed strip (11), notch (12), extension spring (13), slide (14) and slider (15), four fixed strip (11) symmetry are installed in liquid tank (9) bottom respectively, notch (12) are seted up in fixed strip (12) and extension spring (13) both ends are connected with the extension spring (13) respectively, the utility model discloses a sliding plate, including slider (15), slider (14) are through slider (15) and fixed strip (11) sliding connection, spacing subassembly includes spout (18), cover box (19), stopper (20) and compression spring (21), spout (18) are seted up on support (7) just spout (18) size and slider (14) cross-section size looks adaptation, cover box (19) fixed mounting is in unmanned aerial vehicle body (1) upside, stopper (20) sliding connection is inboard at cover box (19), compression spring (21) fixed mounting is between stopper (20) bottom and cover box (19) inboard bottom.
2. The unmanned aerial vehicle spraying device with the dismounting structure according to claim 1, wherein the liquid injection port (10) is arranged on the upper side of the liquid tank (9), and the downpipe (22) is arranged at the bottom of the liquid tank (9).
3. The unmanned aerial vehicle spraying device with the dismounting structure according to claim 1, wherein a joint pipe (8) is installed at a position, corresponding to a downpipe (22), of the upper side of the unmanned aerial vehicle body (1), and a nut (23) is screwed on the joint pipe (8).
4. A unmanned aerial vehicle spraying device with a detachable structure according to claim 3, wherein the downpipe (22) and the adapter pipe (8) are provided with continuous male threads, and the inner side of the nut (23) is provided with female threads matching the male threads.
5. The unmanned aerial vehicle spraying device with the dismounting structure according to claim 1, wherein the unmanned aerial vehicle body (1) is internally provided with a communication pipe (24), a storage battery (26) and a control main board (27), and the communication pipe (24) is communicated with the faucet pipe (8) and the spray head (25).
6. The unmanned aerial vehicle spraying device with the dismounting structure according to claim 1, wherein a handle (16) is fixedly arranged on the outer side of the sliding plate (14), a limiting groove (17) is formed in the sliding plate (14), and the limiting groove (17) is matched with the limiting block (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323170919.9U CN221189090U (en) | 2023-11-23 | 2023-11-23 | Unmanned aerial vehicle sprinkler with dismouting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323170919.9U CN221189090U (en) | 2023-11-23 | 2023-11-23 | Unmanned aerial vehicle sprinkler with dismouting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221189090U true CN221189090U (en) | 2024-06-21 |
Family
ID=91491629
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323170919.9U Active CN221189090U (en) | 2023-11-23 | 2023-11-23 | Unmanned aerial vehicle sprinkler with dismouting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221189090U (en) |
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2023
- 2023-11-23 CN CN202323170919.9U patent/CN221189090U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant |