CN220701382U - Assembled unmanned aerial vehicle of concatenation - Google Patents
Assembled unmanned aerial vehicle of concatenation Download PDFInfo
- Publication number
- CN220701382U CN220701382U CN202322441369.3U CN202322441369U CN220701382U CN 220701382 U CN220701382 U CN 220701382U CN 202322441369 U CN202322441369 U CN 202322441369U CN 220701382 U CN220701382 U CN 220701382U
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- aerial vehicle
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- 238000009434 installation Methods 0.000 claims description 13
- 230000000694 effects Effects 0.000 abstract description 2
- 230000002035 prolonged effect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles and discloses a spliced assembled unmanned aerial vehicle, which comprises a fixed shell, wherein two fixed blocks are fixedly connected to the inner top of the fixed shell, a sliding rod is fixedly connected to the inner part of the fixed block, auxiliary blocks are slidingly connected to the outer parts Zhou Jun of the two parts of the sliding rod, third springs are arranged on opposite sides of the auxiliary blocks, second springs are arranged on the similar sides of the auxiliary blocks, auxiliary plates are rotatably connected to the lower parts of the two auxiliary blocks, mounting blocks are rotatably connected to the similar parts of the auxiliary plates, and sliding plates are arranged in the fixed shell. According to the utility model, when the unmanned aerial vehicle descends to the ground, the unmanned aerial vehicle can be slowed down, so that the use effect of the spliced assembled unmanned aerial vehicle is improved, the service life of internal parts of the spliced assembled unmanned aerial vehicle is prolonged, meanwhile, the spliced assembled unmanned aerial vehicle is convenient for a user to assemble or disassemble, and meanwhile, the spliced assembled unmanned aerial vehicle is convenient to carry out, so that the damage phenomenon is reduced.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a spliced and assembled unmanned aerial vehicle.
Background
Unmanned aerial vehicle is the aircraft that can independently fly under unmanned circumstances, and it can use remote controller, computer program or preset route to control, and unmanned aerial vehicle wide application is in a plurality of fields including business, scientific research and amusement etc., and common unmanned aerial vehicle is the pin-connected panel basically, because its inside module can be selected according to the demand to realize flexibility and customizable nature.
However, when the existing part spliced assembled unmanned aerial vehicle falls, due to manual operation, improper operation cannot be avoided, and the unmanned aerial vehicle is crashed to the ground when falling to damage to parts in the unmanned aerial vehicle.
Disclosure of Invention
In order to make up for the defects, the utility model provides a spliced assembled unmanned aerial vehicle, which aims to solve the problems that the unmanned aerial vehicle in the prior art is unavoidably operated by manual operation during landing, parts inside the unmanned aerial vehicle cannot be timely slowed down to cause damage, and when the unmanned aerial vehicle needs to be carried out, the unmanned aerial vehicle cannot be disassembled and carried due to the large size of the unmanned aerial vehicle, so that the unmanned aerial vehicle is easily damaged, and the use of the unmanned aerial vehicle is affected.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides a concatenation assembled unmanned aerial vehicle, includes the fixed shell, the inside fixedly connected with two fixed blocks of top in the fixed shell, the inside fixedly connected with slide bar of fixed block, zhou Jun sliding connection has the auxiliary block outside the slide bar both parts, the opposite one side of auxiliary block all is provided with the third spring, the similar one side of auxiliary block all is provided with the second spring, two auxiliary block lower part all rotates and is connected with the accessory plate, the similar one portion of accessory plate all rotates and is connected with the installation piece, the inside slide that is provided with of fixed shell, the equal fixedly connected with slider of slide left and right sides, the inside sliding connection of slider has the installation pole, slider upper portion is provided with first spring.
As a further description of the above technical solution:
the fixed shell comprises a fixed shell body and is characterized in that a bottom plate is fixedly connected to the upper portion of the fixed shell body, a plurality of shells are arranged on the upper portion of the bottom plate body, a top plate is arranged on the upper portion of the shells, a plurality of fixing bolts are arranged inside the top plate body, a mounting plate is arranged on the upper portion of the top plate body, a plurality of auxiliary bolts are arranged inside the mounting plate body, wings are arranged at four corners of the upper portion of the bottom plate body, and mounting bolts are arranged inside the wings.
As a further description of the above technical solution:
the wing is connected with the bottom plate through the mounting bolts.
As a further description of the above technical solution:
the one end that the third spring is close is all fixed connection in the one portion that supplementary piece is opposite, the one end that the third spring is opposite is all fixed connection inside the fixed shell, the one end that the second spring is opposite is all fixed connection in the one portion that supplementary piece is close, the one end that the second spring is close is all fixed connection inside the fixed block.
As a further description of the above technical solution:
the upper end of the first spring is fixedly connected inside the fixed shell, and the lower end of the first spring is fixedly connected to the upper part of the sliding block.
As a further description of the above technical solution:
the installation pole both ends are all fixed connection inside the fixed shell, the equal fixed connection in fixed shell in slide bar both ends.
As a further description of the above technical solution:
two the slider sliding connection is in the inside both sides of fixed shell, and a plurality of the installation piece is all fixed connection at the slide top.
As a further description of the above technical solution: the lower part of the sliding plate is fixedly connected with two supporting rods, and the periphery of the lower part of the supporting rods is fixedly connected with a fixing rod.
The utility model has the following beneficial effects:
1. according to the utility model, through the cooperation among the fixed block, the sliding rod, the auxiliary block, the first spring, the second spring, the auxiliary plate and the sliding block, the unmanned aerial vehicle can be slowed down when the unmanned aerial vehicle descends to the ground, so that the use effect of the unmanned aerial vehicle is improved, and the service life of internal parts of the unmanned aerial vehicle is prolonged.
2. According to the utility model, the spliced assembled unmanned aerial vehicle is convenient for a user to assemble or disassemble by matching the bottom plate, the shell, the top plate, the mounting plate, the fixing bolts, the auxiliary bolts and the wings, and meanwhile, the unmanned aerial vehicle is convenient to carry out, so that the damage phenomenon is reduced.
Drawings
Fig. 1 is a perspective view of a splice assembly type unmanned aerial vehicle according to the present utility model;
fig. 2 is a schematic diagram of a support rod structure of a spliced and assembled unmanned aerial vehicle according to the present utility model;
fig. 3 is a schematic diagram of an auxiliary block structure of the spliced and assembled unmanned aerial vehicle according to the present utility model;
fig. 4 is a schematic diagram of a shell structure of the spliced and assembled unmanned aerial vehicle.
Legend description:
1. a mounting plate; 2. a fixed case; 3. a support rod; 4. a fixed rod; 5. a slide block; 6. a first spring; 7. a mounting rod; 8. an auxiliary block; 9. a fixed block; 10. a mounting block; 11. a second spring; 12. a slide plate; 13. an auxiliary plate; 14. a third spring; 15. a slide bar; 16. a fixing bolt; 17. an auxiliary bolt; 18. a top plate; 19. installing a bolt; 20. a bottom plate; 21. a housing; 22. and (3) a wing.
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.
Referring to fig. 1-4, one embodiment provided by the present utility model is: concatenation assembled unmanned aerial vehicle, including fixed shell 2, top fixedly connected with two fixed blocks 9 in the fixed shell 2, the inside fixedly connected with slide bar 15 of fixed block 9, the external Zhou Jun sliding connection of slide bar 15 two parts has auxiliary block 8, the opposite one side of auxiliary block 8 all is provided with third spring 14, the similar one side of auxiliary block 8 all is provided with second spring 11, two auxiliary block 8 lower parts all rotate and are connected with auxiliary plate 13, the similar one part of auxiliary plate 13 all rotates and is connected with installation piece 10, the inside slide 12 that is provided with of fixed shell 2, slide 12 left and right sides all fixedly connected with slider 5, slider 5 inside sliding connection has installation pole 7, slider 5 upper portion is provided with first spring 6, at first decline unmanned aerial vehicle to ground, because of gravity reasons, can drive slide 12 upward movement through dead lever 4 and bracing piece 3, because rotate between installation piece 10 and the auxiliary plate 13 and auxiliary block 8 and be connected, thereby drive auxiliary block 8 and remove at 15 two parts, because the opposite one side of auxiliary block 8 all is provided with third spring 14, simultaneously fixed block 9 can also let the slider 5 through setting up in the second spring 11 and through the second spring 11, thereby can also let the slider 5 side-side spring 12 in the second spring 12 is further stable in the process of sliding connection, and the slider 5 is further stable and the slider 5, and the side is more stable and the slider is in the second spring 12 is carried out in the process is more stable and the second spring 5.
The fixing shell 2 is fixedly connected with the bottom plate 20 at the upper part, the fixing shell 2 is fixed between the bolts and the bottom plate 20, a plurality of shells 21 are arranged at the upper part of the bottom plate 20, a top plate 18 is arranged at the upper part of the shells 21, a plurality of fixing bolts 16 are arranged in the top plate 18, a mounting plate 1 is arranged at the upper part of the top plate 18, a plurality of auxiliary bolts 17 are arranged in the mounting plate 1, wings 22 are arranged at four corners at the upper part of the bottom plate 20, mounting bolts 19 are arranged in the wings 22, the fixing bolts 16 are screwed, so that the top plate 18 and the shells 21 are disassembled, then the mounting bolts 19 are screwed by using auxiliary tools, so that the wings 22 are disassembled, and the auxiliary bolts 17 are screwed, so that the mounting plate 1 is convenient to disassemble, after disassembly, the user places the disassembled parts in a storage box one by one, so that the user can go out, the mounting plate 1 is connected between the auxiliary bolts 17 and the top plate 18, thereby facilitating the subsequent disassembly of parts in the unmanned aerial vehicle, the top plate 18, the shell 21 and the bottom plate 20 are connected through the fixing bolts 16, thereby facilitating the assembly of the whole unmanned aerial vehicle shell, the wing 22 is connected with the bottom plate 20 through the mounting bolts 19, thereby facilitating the assembly of the wing 22 in the machine body, the similar ends of the third springs 14 are fixedly connected with the opposite parts of the auxiliary block 8, the opposite ends of the third springs 14 are fixedly connected with the inside of the fixing shell 2, the opposite ends of the second springs 11 are fixedly connected with the similar parts of the auxiliary block 8, the similar ends of the second springs 11 are fixedly connected with the inside of the fixing block 9, thereby slowing down the auxiliary block 8 through the elasticity of the second springs 11 and the third springs 14, further slowing down the sliding plate 12 at the lower part of the mounting block 10, further slowing down the unmanned aerial vehicle, the upper end fixed connection of first spring 6 is inside fixed shell 2, first spring 6 lower extreme fixed connection is on slider 5 upper portion, elasticity through first spring 6, thereby slow down slider 5, and then slow down slide 12, installation pole 7 both ends all fixed connection is inside fixed shell 2, thereby make things convenient for slider 5 to carry out the left and right movement at its periphery, slide bar 15 both ends all fixed connection is inside fixed shell 2, thereby make things convenient for auxiliary block 8 to carry out the left and right movement at its periphery, two slider 5 sliding connection is in the inside both sides of fixed shell 2, thereby make slide 12 more firm at the in-process of sliding, a plurality of installation pieces 10 all fixed connection are at slide 12 top, thereby drive slide 12 upward movement through auxiliary plate 13, slide 12 lower part fixedly connected with two bracing pieces 3, bracing piece 3 lower part periphery fixedly connected with dead lever 4, thereby conveniently support and play unmanned aerial vehicle.
Working principle: when the device is used by a user, firstly, the unmanned aerial vehicle is lowered to the ground, the sliding plate 12 is driven to move upwards through the fixed rod 4 and the supporting rod 3 due to gravity, the installation block 10 is connected with the auxiliary plate 13 in a rotating way, meanwhile, the auxiliary plate 13 is connected with the auxiliary block 8 in a rotating way, so that the auxiliary block 8 is driven to move at two parts of the sliding rod 15, the opposite sides of the auxiliary block 8 are respectively provided with the third springs 14, meanwhile, the two sides of the fixed block 9 are respectively provided with the second springs 11 and the third springs 14, so that the sliding plate 12 is slowed down by the elasticity of the second springs 11 and the third springs 14 in the process of sliding the auxiliary block 8 left and right, the sliding block 5 is respectively provided with the sliding block 5 at the periphery of the installation rod 7, the sliding block 5 slides in the fixed shell 2, so that the sliding block 5 is slowed down by the elasticity of the first springs 6, the sliding plate 12 is further slowed down, and can also make slide 12 more firm at the in-process that removes, and then slow down unmanned aerial vehicle pressure, when the user need dismantle unmanned aerial vehicle, at first twist fixing bolt 16, thereby dismantle roof 18 and shell 21, afterwards through using appurtenance to twist mounting bolt 19, thereby dismantle wing 22, simultaneously with supplementary bolt 17 is twisted, thereby conveniently dismantle mounting panel 1, after the dismantlement, the user places the part after dismantling one by one in depositing the case, thereby convenience of customers go out and carry, when the unmanned aerial vehicle of needs assembling, at first link together wing 22 through mounting bolt 19 and bottom plate 20, then place four shells 21 on bottom plate 20 upper portion, simultaneously place roof 18 on four shells 21 upper portion, then fix it together through fixing bolt 16, simultaneously fix mounting panel 1 on roof 18 upper portion through supplementary bolt 17, thereby completing the assembly.
Finally, it should be noted that: the foregoing description is only illustrative of the preferred embodiments of the present utility model, and although the present utility model has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present utility model.
Claims (8)
1. Splice assembled unmanned aerial vehicle, including fixed shell (2), its characterized in that: the utility model discloses a fixed shell, including fixed shell (2), fixed shell, auxiliary block (8), slide plate (12), slide plate (5), auxiliary block (8) are provided with first spring (6) and second spring (11), two fixed block (9) are fixedly connected with at top in fixed shell (2), fixed block (9) inside fixedly connected with slide bar (15), slide bar (15) two outside Zhou Jun sliding connection have auxiliary block (8), one side opposite auxiliary block (8) all is provided with third spring (14), one side that auxiliary block (8) is close all is provided with second spring (11), two auxiliary block (8) lower part all rotates and is connected with auxiliary plate (13), one that auxiliary plate (13) is close all rotates and is connected with installation piece (10), fixed shell (2) inside is provided with slide plate (12), slide plate (12) both sides all fixedly connected with slider (5), slider (5) inside sliding connection has installation pole (7), slider (5) upper portion is provided with first spring (6).
2. The splice assembly drone of claim 1, wherein: the utility model discloses a fixing device for a motor vehicle, including fixed shell (2) upper portion fixedly connected with bottom plate (20), bottom plate (20) upper portion is provided with a plurality of shell (21), shell (21) upper portion is provided with roof (18), roof (18) inside is provided with a plurality of fixing bolt (16), roof (18) upper portion is provided with mounting panel (1), mounting panel (1) inside is provided with a plurality of auxiliary bolt (17), bottom plate (20) upper portion four corners all is provided with wing (22), wing (22) inside is provided with mounting bolt (19).
3. The splice assembly drone of claim 2, wherein: the wing mounting structure is characterized in that the mounting plate (1) is connected with the top plate (18) through auxiliary bolts (17), the top plate (18), the shell (21) and the bottom plate (20) are connected through fixing bolts (16), and the wing (22) is connected with the bottom plate (20) through mounting bolts (19).
4. The splice assembly drone of claim 1, wherein: the one end that third spring (14) is close all fixed connection is in the one portion that auxiliary block (8) is opposite, the one end that third spring (14) is opposite all fixed connection is inside fixed shell (2), the one end that second spring (11) is opposite all fixed connection is in one portion that auxiliary block (8) is close, the one end that second spring (11) is close all fixed connection is inside fixed block (9).
5. The splice assembly drone of claim 1, wherein: the upper end of the first spring (6) is fixedly connected inside the fixed shell (2), and the lower end of the first spring (6) is fixedly connected to the upper portion of the sliding block (5).
6. The splice assembly drone of claim 1, wherein: the two ends of the mounting rod (7) are fixedly connected inside the fixed shell (2), and the two ends of the sliding rod (15) are fixedly connected inside the fixed shell (2).
7. The splice assembly drone of claim 1, wherein: two sliding blocks (5) are slidably connected to two sides inside the fixed shell (2), and a plurality of mounting blocks (10) are fixedly connected to the top of the sliding plate (12).
8. The splice assembly drone of claim 1, wherein: two support rods (3) are fixedly connected to the lower portion of the sliding plate (12), and fixing rods (4) are fixedly connected to the periphery of the lower portion of the support rods (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322441369.3U CN220701382U (en) | 2023-09-08 | 2023-09-08 | Assembled unmanned aerial vehicle of concatenation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322441369.3U CN220701382U (en) | 2023-09-08 | 2023-09-08 | Assembled unmanned aerial vehicle of concatenation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220701382U true CN220701382U (en) | 2024-04-02 |
Family
ID=90452027
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322441369.3U Active CN220701382U (en) | 2023-09-08 | 2023-09-08 | Assembled unmanned aerial vehicle of concatenation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220701382U (en) |
-
2023
- 2023-09-08 CN CN202322441369.3U patent/CN220701382U/en active Active
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