CN219532639U - Many atmospheric inspection unmanned aerial vehicle based on cluster formation - Google Patents
Many atmospheric inspection unmanned aerial vehicle based on cluster formation Download PDFInfo
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- CN219532639U CN219532639U CN202320223503.XU CN202320223503U CN219532639U CN 219532639 U CN219532639 U CN 219532639U CN 202320223503 U CN202320223503 U CN 202320223503U CN 219532639 U CN219532639 U CN 219532639U
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- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 24
- 238000001514 detection method Methods 0.000 claims abstract description 51
- 230000006978 adaptation Effects 0.000 claims description 9
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Abstract
The utility model discloses a cluster formation-based multi-atmosphere inspection unmanned aerial vehicle, which comprises a bottom plate and four unmanned aerial vehicle bodies arranged at the top of the bottom plate, wherein telescopic rods are arranged on the outer walls of the two ends and the outer walls of the two sides of the unmanned aerial vehicle bodies, motors are arranged on the outer walls of the tops of the telescopic rods, two paddles are fixedly arranged at one end of an output shaft of each motor, and a detection box is fixedly arranged on the outer wall of the bottom of the unmanned aerial vehicle body; according to the utility model, the fan is started, air is sucked into the detection box, the high-speed sucked air can impact the circular plate and compress the first spring, so that the circular plate is separated from the through groove, the air can enter the detection box, after a certain time is sucked, the fan is closed, the first spring is released, the circular plate is pushed to be meshed into the through groove again, the detection box can be sealed, at the moment, the detection is carried out through the atmosphere detector, a stable and undisturbed detection environment is formed in the detection box during detection, and the detection accuracy is improved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a cluster formation-based multi-atmosphere inspection unmanned aerial vehicle.
Background
Unmanned plane is simply unmanned plane, is the unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, or is operated independently by on-vehicle computer is complete or intermittent type, according to the application, can divide into for military use and civilian, for military use aspect, unmanned plane divide into reconnaissance aircraft and target aircraft, for civilian aspect, unmanned plane + trade application is the real just need of unmanned plane, along with technological development, unmanned plane can rise to higher and higher degree, consequently people also use unmanned plane to detect atmospheric quality.
Through retrieving, a unmanned aerial vehicle with atmospheric detection function of patent publication No. CN213502903U ", through the setting of electric heat piece, electric heat conducting plate, heating wire, after unmanned aerial vehicle risees to the high altitude, because the rising air temperature of altitude becomes low, low temperature has the influence to the testing result, the heating wire heats electric heat conducting plate this moment, the heat can be conducted to each electric heat piece from electric heat conducting plate, the electric heat piece radiates the heat to atmospheric component detecting sensor again, thereby improve atmospheric component detecting sensor's operating temperature, make atmospheric component detecting sensor begin to detect after reaching suitable temperature, unmanned aerial vehicle of current atmospheric detection function has been solved, because unmanned aerial vehicle is lower at high altitude atmospheric temperature when high altitude operation, cause the problem that testing result can produce the error easily.
The technical characteristics have the following defects: the atmosphere detection device of the device is directly exposed outside, the air flow is unstable in high altitude, the ambient temperature is low, various uncertain factors exist, the environment is detected, the detection instrument with high precision is easy to interfere or even damage, the obtained detection result is not practical, and therefore, the design of a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation is needed to solve the problems.
Disclosure of Invention
The utility model aims to provide a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation so as to solve the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation comprise a bottom plate and four unmanned aerial vehicle bodies arranged at the top of the bottom plate, wherein telescopic rods are arranged on the outer walls of the two ends and the outer walls of the two sides of the unmanned aerial vehicle bodies, motors are arranged on the outer walls of the tops of the telescopic rods, two paddles are fixedly arranged at one end of an output shaft of each motor, and a detection box is fixedly arranged on the outer wall of the bottom of the unmanned aerial vehicle body;
the detecting box comprises a detecting box body, wherein an air suction pipe is fixedly arranged on one side outer wall of the detecting box body, a fan is fixedly arranged on the circumferential inner wall of the air suction pipe, the air suction pipe is communicated with the detecting box body, a support is arranged on one side inner wall of the detecting box body, a first spring is fixedly arranged on one side inner wall of the support, a circular plate is arranged on one end outer wall of the first spring, a through groove is formed in one side inner wall of the detecting box body, the circular plate is matched with the through groove, an atmosphere detector is fixedly arranged on the top inner wall of the detecting box body, and a control mechanism for cluster formation is arranged on the top outer wall of the bottom plate.
Preferably, the control mechanism comprises a main controller, and the top outer walls of the four unmanned aerial vehicle bodies are provided with auxiliary controllers, and the main controller is matched with the auxiliary controllers.
Preferably, two sliding rods are fixedly arranged on the inner wall of one side of the circular plate, and the two sliding rods are both in sliding connection with the inner wall of one side of the bracket.
Preferably, a sealing ring is arranged on the circumferential outer wall of the circular plate, and the sealing ring is made of rubber.
Preferably, square grooves are formed in the outer walls of the two sides and the outer walls of the two ends of the unmanned aerial vehicle body, and the telescopic rod is matched with the square grooves.
Preferably, eight spacing holes are all opened to the top outer wall of unmanned aerial vehicle body, and two spacing grooves are all opened to the top outer wall of telescopic link, and the equal fixed mounting of top outer wall of unmanned aerial vehicle body has eight second springs, is provided with the connecting plate between the top outer wall of two second springs, and the bottom outer wall of connecting plate all is provided with two gag lever posts, gag lever post and spacing hole, spacing groove looks adaptation.
Preferably, the top outer wall of bottom plate is provided with eight fixed blocks, and rotates between the relative one end inner wall of two fixed blocks and install two-way threaded rod, and two baffles have all been cup jointed through the screw thread slip to two-way threaded rod's circumference outer wall, and four dovetail groove are opened to the top outer wall of bottom plate, and the bottom outer wall of baffle all is provided with the trapezoidal piece, trapezoidal piece and dovetail groove looks adaptation, and the bottom outer wall of unmanned aerial vehicle body all is provided with two landing legs, baffle and landing leg looks adaptation.
Compared with the prior art, the utility model has the beneficial effects that:
when the unmanned aerial vehicle is lifted to a proper height for atmospheric detection, the fan is started, air is sucked into the detection box, the high-speed sucked air can impact the circular plate and compress the first spring, the circular plate is further separated from the through groove, the air can enter the detection box, after the air is sucked for a certain time, the fan is closed, the first spring is released, the circular plate is pushed to be meshed into the through groove again, the detection box can be sealed, at the moment, the detection is carried out through the atmospheric detector, a stable and interference-free detection environment is formed in the detection box during detection, and the detection accuracy is improved;
in the utility model, when in use, the main controller and the auxiliary controller are arranged, so that four unmanned aerial vehicle bodies can fly in a cluster formation mode, the atmosphere of the same airspace can be detected at the same time to improve the detection accuracy or the large-area airspace can be detected in a distributed mode to improve the detection efficiency, and when in use, the tightness of the detection box can be further improved through the arranged sealing ring;
according to the utility model, after the unmanned aerial vehicle is used, the unmanned aerial vehicle body is placed between the two baffles, the two baffles are driven to be close to each other by rotating the bidirectional threaded rod, the two baffles can be fixed after sliding until the baffles are contacted with the supporting legs, the position of the unmanned aerial vehicle body is further fixed, and the stability of the baffles during sliding can be maintained through the arranged trapezoidal blocks.
Drawings
Fig. 1 is a schematic diagram of the overall structure of a plurality of atmosphere inspection robots based on cluster formation.
Fig. 2 is a schematic diagram of an air suction pipe structure of a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation.
Fig. 3 is a schematic structural diagram of a detection box of a plurality of atmospheric inspection unmanned aerial vehicles based on cluster formation.
Fig. 4 is a schematic diagram of a support structure of a plurality of atmospheric inspection robots based on cluster formation.
Fig. 5 is a schematic diagram of a leg structure of a plurality of atmospheric inspection robots based on cluster formation.
Fig. 6 is a schematic structural diagram of a telescopic rod of a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation.
Fig. 7 is a schematic structural diagram of a connection board of a plurality of atmosphere inspection robots based on cluster formation.
Fig. 8 is a schematic diagram of a base plate structure of a plurality of atmosphere inspection robots based on cluster formation.
Fig. 9 is a schematic diagram of a bidirectional threaded rod structure of a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation.
Fig. 10 is a schematic diagram of a baffle structure of a plurality of atmospheric inspection robots based on cluster formation.
In the figure: 1. a bottom plate; 2. an unmanned aerial vehicle body; 3. a main controller; 4. a telescopic rod; 5. a motor; 6. a paddle; 7. a detection box; 8. an air suction pipe; 9. a fan; 10. a bracket; 11. a through groove; 12. a first spring; 13. a circular plate; 14. a slide bar; 15. an atmospheric detector; 16. a seal ring; 17. a square groove; 18. a limiting hole; 19. a sub controller; 20. a support leg; 21. a limit groove; 22. a second spring; 23. a connecting plate; 24. a limit rod; 25. a fixed block; 26. a two-way threaded rod; 27. a baffle; 28. a trapezoid groove; 29. trapezoidal blocks.
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. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
Referring to fig. 1-10, in the embodiment of the utility model, a plurality of atmosphere inspection unmanned aerial vehicles based on cluster formation comprise a bottom plate 1 and four unmanned aerial vehicle bodies 2 arranged at the top of the bottom plate 1, telescopic rods 4 are arranged on the outer walls of two ends and the outer walls of two sides of the unmanned aerial vehicle bodies 2, motors 5 are arranged on the outer walls of the tops of the telescopic rods 4, two paddles 6 are fixedly arranged at one end of an output shaft of each motor 5, and a detection box 7 is fixedly arranged on the outer wall of the bottom of the unmanned aerial vehicle body 2;
the air suction pipe 8 is fixedly arranged on one side outer wall of the detection box 7, the fan 9 is fixedly arranged on the circumferential inner wall of the air suction pipe 8, the air suction pipe 8 is communicated with the detection box 7, the support 10 is arranged on one side inner wall of the detection box 7, the first spring 12 is fixedly arranged on one side inner wall of the support 10, the circular plate 13 is arranged on one end outer wall of the first spring 12, the through groove 11 is formed in one side inner wall of the detection box 7, the circular plate 13 is matched with the through groove 11, the atmosphere detector 15 is fixedly arranged on the top inner wall of the detection box 7, the control mechanism for cluster formation is arranged on the top outer wall of the bottom plate 1, when the atmosphere is detected, the unmanned aerial vehicle is lifted to a proper height, the fan 9 is started, air is sucked into the detection box 7, the air sucked at a high speed can impact the circular plate 13, the first spring 12 is compressed, the circular plate 13 is separated from the through groove 11, the air can enter the detection box 7, after a certain time of suction, the fan 9 is closed, the first spring 12 is released, the circular plate 13 is meshed into the through groove 11 again, the detection box 7 can be sealed, the atmosphere is detected, the atmosphere detector 15 is detected, the detection box 7 can be detected, the detection environment can be stably, and the detection environment can be stably detected, and the detection environment can be stably is improved.
Wherein, control mechanism includes master controller 3, and the top outer wall of four unmanned aerial vehicle bodies 2 is provided with auxiliary controller 19, and master controller 3 and auxiliary controller 19 looks adaptation when using, through master controller 3 and auxiliary controller 19 that set up, can make four unmanned aerial vehicle bodies 2 carry out cluster formation formula flight, can detect the atmosphere in same airspace simultaneously in order to improve detection accuracy or carry out the distributed detection in order to improve detection efficiency to large tracts of land airspace.
Wherein, two slide bars 14 are fixedly arranged on one side inner wall of the circular plate 13, and the two slide bars 14 are both in sliding connection with one side inner wall of the bracket 10, and when in use, the circular plate 13 can be kept stable during sliding by the arranged slide bars 14, so that the circular plate 13 is prevented from deviating from the through groove 11.
Wherein, the circumference outer wall of plectane 13 is provided with sealing washer 16, and sealing washer 16 is the rubber material, when using, through the sealing washer 16 that sets up, can further improve the leakproofness of detecting case 7.
Wherein, both sides outer wall and both ends outer wall of unmanned aerial vehicle body 2 all open square groove 17, and telescopic link 4 and square groove 17 looks adaptation, when accomodating unmanned aerial vehicle body 2, can slide into square groove 17 with four telescopic links 4 to reduce unmanned aerial vehicle body 2's volume, facilitate the use person accomodates.
Wherein, eight spacing holes 18 have all been opened to unmanned aerial vehicle body 2's top outer wall, and two spacing grooves 21 have all been opened to telescopic link 4's top outer wall, unmanned aerial vehicle body 2's top outer wall all fixed mounting has eight second springs 22, be provided with connecting plate 23 between two second springs 22's the top outer wall, connecting plate 23's bottom outer wall all is provided with two gag lever posts 24, gag lever post 24 and spacing hole 18, spacing groove 21 looks adaptation, when using, pulling connecting plate 23, tensile two second springs 22, drive gag lever post 24 and break away from spacing groove 21, can unblock telescopic link 4, slide telescopic link 4 in square groove 17 this moment, after sliding to the end, loosen connecting plate 23, two second springs 22 shrink, drive two gag lever posts 24 meshing into two spacing grooves 21, can lock its position after telescopic link 4 withdraws.
Example 2
Referring to fig. 9-10, as distinct from embodiment 1, eight fixing blocks 25 are disposed on the top outer wall of the base plate 1, a bidirectional threaded rod 26 is rotatably mounted between inner walls of opposite ends of the two fixing blocks 25, two baffle plates 27 are slidably sleeved on the circumferential outer walls of the bidirectional threaded rod 26 through threads, four trapezoid grooves 28 are formed on the top outer wall of the base plate 1, trapezoid blocks 29 are disposed on the bottom outer walls of the baffle plates 27, trapezoid blocks 29 are matched with trapezoid grooves 28, two supporting legs 20 are disposed on the bottom outer walls of the unmanned aerial vehicle body 2, the baffle plates 27 are matched with the supporting legs 20, after the unmanned aerial vehicle body 2 is placed between the two baffle plates 27, the bidirectional threaded rod 26 is rotated to drive the two baffle plates 27 to approach each other, the two supporting legs 20 can be fixed after the baffle plates 27 are slid to contact with the supporting legs 20, and then positions of the unmanned aerial vehicle body 2 are fixed, and stability of the unmanned aerial vehicle body 27 during sliding can be maintained through the disposed trapezoid blocks 29.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof.
Claims (7)
1. Many atmospheres inspection unmanned aerial vehicle based on cluster formation, including bottom plate (1) and four unmanned aerial vehicle bodies (2) of setting at bottom plate (1) top, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (2), wherein telescopic rods (4) are arranged on the outer walls of the two ends and the outer walls of the two sides of the unmanned aerial vehicle body, motors (5) are arranged on the outer walls of the tops of the telescopic rods (4), two paddles (6) are fixedly arranged at one end of an output shaft of each motor (5), and a detection box (7) is fixedly arranged on the outer wall of the bottom of the unmanned aerial vehicle body (2);
one side outer wall fixed mounting of detection case (7) has breathing pipe (8), the circumference inner wall fixed mounting of breathing pipe (8) has fan (9), breathing pipe (8) are linked together with detection case (7), one side inner wall of detection case (7) is provided with support (10), one side inner wall fixed mounting of support (10) has first spring (12), one end outer wall of first spring (12) is provided with plectane (13), open one side inner wall of detection case (7) has logical groove (11), plectane (13) and logical groove (11) looks adaptation, the top inner wall fixed mounting of detection case (7) has atmospheric detector (15), the top outer wall of bottom plate (1) is provided with the control mechanism who is used for the cluster formation.
2. The cluster-formation-based multiple atmosphere inspection drone of claim 1, wherein: the control mechanism comprises a main controller (3), and the top outer walls of the four unmanned aerial vehicle bodies (2) are provided with a secondary controller (19), and the main controller (3) is matched with the secondary controller (19).
3. The cluster-formation-based multiple atmosphere inspection drone of claim 2, wherein: two sliding rods (14) are fixedly arranged on the inner wall of one side of the circular plate (13), and the two sliding rods (14) are both in sliding connection with the inner wall of one side of the bracket (10).
4. A cluster-formation-based multiple atmosphere inspection drone as claimed in claim 3, wherein: a sealing ring (16) is arranged on the circumferential outer wall of the circular plate (13), and the sealing ring (16) is made of rubber.
5. The cluster-formation-based multiple atmosphere inspection drone of any one of claims 1-4, wherein: both sides outer wall and both ends outer wall of unmanned aerial vehicle body (2) all open have square groove (17), and telescopic link (4) and square groove (17) looks adaptation.
6. The cluster-formation-based multiple atmosphere inspection drone of claim 1, wherein: eight spacing holes (18) are all opened to the top outer wall of unmanned aerial vehicle body (2), and two spacing groove (21) are all opened to the top outer wall of telescopic link (4), and the equal fixed mounting in top outer wall of unmanned aerial vehicle body (2) has eight second springs (22), is provided with connecting plate (23) between the top outer wall of two second springs (22), and the bottom outer wall of connecting plate (23) all is provided with two gag lever posts (24), gag lever post (24) and spacing hole (18), spacing groove (21) looks adaptation.
7. The cluster-formation-based multiple atmosphere inspection drone of claim 1, wherein: eight fixed blocks (25) are arranged on the top outer wall of the bottom plate (1), a bidirectional threaded rod (26) is installed between the inner walls of opposite ends of the two fixed blocks (25) in a rotating mode, two baffles (27) are sleeved on the circumferential outer wall of the bidirectional threaded rod (26) in a sliding mode through threads, four trapezoid grooves (28) are formed in the top outer wall of the bottom plate (1), trapezoid blocks (29) are arranged on the bottom outer wall of each baffle (27), the trapezoid blocks (29) are matched with the trapezoid grooves (28), two supporting legs (20) are arranged on the bottom outer wall of the unmanned aerial vehicle body (2), and the baffles (27) are matched with the supporting legs (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320223503.XU CN219532639U (en) | 2023-02-15 | 2023-02-15 | Many atmospheric inspection unmanned aerial vehicle based on cluster formation |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320223503.XU CN219532639U (en) | 2023-02-15 | 2023-02-15 | Many atmospheric inspection unmanned aerial vehicle based on cluster formation |
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| CN219532639U true CN219532639U (en) | 2023-08-15 |
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| CN202320223503.XU Active CN219532639U (en) | 2023-02-15 | 2023-02-15 | Many atmospheric inspection unmanned aerial vehicle based on cluster formation |
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| CN (1) | CN219532639U (en) |
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Effective date of registration: 20240308 Address after: Room 1838, 18 / F, block a, overseas talents building, 999 Gaoxin Avenue, Donghu New Technology Development Zone, Wuhan City, Hubei Province, 430000 Patentee after: WUHAN YIHESMART TECHNOLOGY CO.,LTD. Country or region after: China Address before: 244000 15 / F, building 1-a1, Tongguan Shugu, Tongguan District, Tongling City, Anhui Province Patentee before: Anhui Yunwu Intelligent Technology Co.,Ltd. Country or region before: China |