CN214608869U - Unmanned aerial vehicle holds support - Google Patents
Unmanned aerial vehicle holds support Download PDFInfo
- Publication number
- CN214608869U CN214608869U CN202120463316.XU CN202120463316U CN214608869U CN 214608869 U CN214608869 U CN 214608869U CN 202120463316 U CN202120463316 U CN 202120463316U CN 214608869 U CN214608869 U CN 214608869U
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- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- bracing piece
- cushion
- buffer spring
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 238000009434 installation Methods 0.000 claims abstract description 22
- 230000000694 effects Effects 0.000 claims abstract description 12
- 230000007246 mechanism Effects 0.000 claims description 13
- 230000009467 reduction Effects 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle holds support, including the unmanned aerial vehicle main part, the bottom surface of unmanned aerial vehicle main part is equipped with the bracing piece, the equal fixed mounting in bottom of bracing piece has the cushion, the equal activity of surface of bracing piece has cup jointed the installation sleeve, one side fixed surface of installation sleeve installs the equipment rack, be equipped with buffer spring between installation sleeve and the cushion, buffer spring's one end and the top surface fixed connection of cushion, buffer spring's the other end and the telescopic bottom surface fixed connection of installation. Through the buffer spring of design, when the unmanned aerial vehicle main part descends and the cushion contacts to the bottom surface, because the outer wall at the bracing piece is cup jointed in the installation sleeve activity, and with buffer spring's one end fixed connection, so the impact force to the equipment rack can be through installation sleeve and the decurrent activity of buffer spring when the unmanned aerial vehicle main part falls to the ground to carry out effectual reduction, carry out effectual protection to the exploration equipment of equipment rack top surface.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to unmanned aerial vehicle holds support.
Background
The unmanned aircraft is an unmanned aircraft, abbreviated as "unmanned aerial vehicle" in english, and is an unmanned aircraft operated by using a radio remote control device and a self-contained program control device, or is operated by an on-board computer completely or intermittently and autonomously, and the application of the unmanned aircraft is more extensive at present, as is particularly obvious in the field of geographic exploration.
Current unmanned aerial vehicle can install some exploration equipment and hold the frame when geographical exploration usually, and current storage rack still has some problems when using, if when unmanned aerial vehicle descends to the ground, can produce great impact force to cause exploration equipment to damage, cause economic loss.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle holds support to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle holds support, includes the unmanned aerial vehicle main part, the bottom surface of unmanned aerial vehicle main part is equipped with the bracing piece, the quantity of bracing piece is four, four the bracing piece is fixed mounting in the bottom surface four corners of unmanned aerial vehicle main part respectively, the equal fixed mounting in bottom of bracing piece has the cushion, the diameter of cushion is greater than the diameter of bracing piece, the equal activity of surface of bracing piece has cup jointed the installation sleeve, a side fixed surface of installation sleeve installs the equipment rack, be equipped with buffer spring between installation sleeve and the cushion, buffer spring's one end and the top surface fixed connection of cushion, buffer spring's the other end and the telescopic bottom surface fixed connection of installation.
Preferably, the top surface both ends of equipment rack all are equipped with clamping mechanism, two clamping mechanism sets up for opposition, clamping mechanism includes fixed mounting board, threaded hole has been seted up on a side surface of fixed mounting board, the threaded rod has been cup jointed in the inside activity of threaded hole, the one end top surface fixed mounting of threaded rod has the knob, the other end top surface fixed mounting of threaded rod has to support tight board.
Preferably, the outer surface of the knob is uniformly provided with anti-skid grains.
Preferably, a plurality of anti-skidding grooves are formed in the surface of one side of the abutting plate, and the anti-skidding grooves are rectangular and are arranged at equal intervals.
Preferably, the bottom end of the cushion block is in a ball head shape, and the cushion block is a rubber block.
Compared with the prior art, the beneficial effects of the utility model are that:
1. through the buffer spring who designs, when the unmanned aerial vehicle main part descends and the cushion contacts to the bottom surface, because the outer wall at the bracing piece is cup jointed in the installation sleeve activity, and with buffer spring's one end fixed connection, so the impact force to the equipment rack when the unmanned aerial vehicle main part falls to the ground can be through installation sleeve and the decurrent activity of buffer spring, thereby carry out effectual reduction, carry out effectual protection to equipment rack top surface exploration equipment, solved current unmanned aerial vehicle main part when descending, the impact force of production can cause the problem of damage to the exploration of equipment rack top surface.
2. Through the clamping mechanism who designs, clamping mechanism includes fixed mounting board, threaded rod, knob, supports tight board and antiskid groove, when the top surface of equipment rack is placed to the exploration equipment, drives two and supports tight board and remove in opposite directions through twisting the knob to carry out effectual clamp to the exploration equipment of equipment rack top surface and fix, prevented the problem that the in-process that leads to the exploration equipment to drop at the transport.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the overall front view structure of the present invention;
fig. 3 is a schematic structural view of the clamping mechanism of the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. a support bar; 3. cushion blocks; 4. installing a sleeve; 5. placing a device rack; 6. a buffer spring; 7. a clamping mechanism; 701. fixing the mounting plate; 702. a threaded rod; 703. a knob; 704. a propping plate; 705. and (4) an anti-slip groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle holds support, including unmanned aerial vehicle main part 1, the bottom surface of unmanned aerial vehicle main part 1 is equipped with bracing piece 2, the quantity of bracing piece 2 is four, four bracing pieces 2 are fixed mounting respectively in the bottom surface four corners of unmanned aerial vehicle main part 1, the equal fixed mounting in bottom of bracing piece 2 has cushion 3, the diameter of cushion 3 is greater than the diameter of bracing piece 2, the equal activity of surface of bracing piece 2 has cup jointed installation sleeve 4, a side fixed surface of installation sleeve 4 installs equipment rack 5, be equipped with buffer spring 6 between installation sleeve 4 and the cushion 3, buffer spring 6's the one end and the top surface fixed connection of cushion 3, buffer spring 6's the other end and installation sleeve 4's bottom surface fixed connection.
In this embodiment, when unmanned aerial vehicle main part 1 descends and cushion 3 contacts to the bottom surface, because the outer wall at bracing piece 2 is cup jointed in the activity of installation sleeve 4, and with buffer spring 6's one end fixed connection, so the impact force to equipment rack 5 when unmanned aerial vehicle main part 1 falls to the ground can be through installation sleeve 4 and buffer spring 6 decurrent activity, thereby carry out effectual reduction, carry out effectual protection to equipment rack 5 top surface exploration equipment, solved current unmanned aerial vehicle main part 1 when descending, the impact force of production can cause the problem of damage to the exploration equipment of equipment rack 5 top surface.
Specifically, the two ends of the top surface of the equipment placing rack 5 are both provided with the clamping mechanisms 7, the two clamping mechanisms 7 are oppositely arranged, each clamping mechanism 7 comprises a fixed mounting plate 701, a threaded hole is formed in one side surface of each fixed mounting plate 701, a threaded rod 702 is sleeved in the threaded hole in a movable mode, a knob 703 is fixedly mounted on the top surface of one end of each threaded rod 702, and a clamping plate 704 is fixedly mounted on the top surface of the other end of each threaded rod 702.
In this embodiment, when the top surface of the device placement frame 5 is placed to the exploration device, the knob 703 is screwed to drive the two tightening plates 704 to move in opposite directions, so that the exploration device on the top surface of the device placement frame 5 is effectively clamped and fixed, and the problem that the exploration device drops in the conveying process is prevented.
Specifically, the outer surface of the knob 703 is uniformly provided with anti-slip threads.
In this embodiment, the slipping between the palm and the knob 703 when the knob 703 is screwed is effectively prevented.
Specifically, a plurality of anti-slip grooves 705 are formed in one side surface of the abutting plate 704, and the anti-slip grooves 705 are rectangular and arranged at equal intervals.
In this embodiment, through setting up anti-skidding groove 705 for anti-skidding groove 705 can be effectual press from both sides the tight equipment of exploration when with the surface contact of exploration equipment, has further guaranteed the stability of exploration equipment at 5 top surfaces of equipment rack.
Specifically, the bottom end of the cushion block 3 is in a ball head shape, and the cushion block 3 is a rubber block.
In this embodiment, when cushion 3 and ground contact, because cushion 3 is made by the rubber pad, so can further alleviate the impact force that produces because unmanned aerial vehicle main part 1 descends.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an unmanned aerial vehicle holds support, includes unmanned aerial vehicle main part (1), its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle main part (1), bracing piece (2), the bottom surface of bracing piece (2) is equipped with bracing piece (2), the quantity of bracing piece (2) is four, four bracing piece (2) fixed mounting is in the bottom surface four corners of unmanned aerial vehicle main part (1) respectively, the equal fixed mounting in bottom of bracing piece (2) has cushion (3), the diameter of cushion (3) is greater than the diameter of bracing piece (2), the equal activity of surface of bracing piece (2) has cup jointed installation sleeve (4), one side fixed surface of installation sleeve (4) installs equipment rack (5), be equipped with buffer spring (6) between installation sleeve (4) and cushion (3), the one end of buffer spring (6) and the top surface fixed connection of cushion (3), the other end of buffer spring (6) and the bottom surface fixed connection of installation sleeve (4).
2. The unmanned aerial vehicle holds support of claim 1, its characterized in that: the top surface both ends of equipment rack (5) all are equipped with clamping mechanism (7), two clamping mechanism (7) are opposite setting, clamping mechanism (7) are including fixed mounting panel (701), a side surface of fixed mounting panel (701) set up threaded hole, threaded rod (702) have been cup jointed in the inside activity of threaded hole, the one end top surface fixed mounting of threaded rod (702) has knob (703), the other end top surface fixed mounting of threaded rod (702) has and supports tight board (704).
3. The unmanned aerial vehicle holds support of claim 2, its characterized in that: the outer surface of the knob (703) is uniformly provided with anti-skid grains.
4. The unmanned aerial vehicle holds support of claim 2, its characterized in that: the anti-skidding device is characterized in that a plurality of anti-skidding grooves (705) are formed in the surface of one side of the abutting plate (704), and the anti-skidding grooves (705) are rectangular and are arranged at equal intervals.
5. The unmanned aerial vehicle holds support of claim 1, its characterized in that: the bottom end of the cushion block (3) is in a ball head shape, and the cushion block (3) is a rubber block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120463316.XU CN214608869U (en) | 2021-03-04 | 2021-03-04 | Unmanned aerial vehicle holds support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120463316.XU CN214608869U (en) | 2021-03-04 | 2021-03-04 | Unmanned aerial vehicle holds support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214608869U true CN214608869U (en) | 2021-11-05 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120463316.XU Expired - Fee Related CN214608869U (en) | 2021-03-04 | 2021-03-04 | Unmanned aerial vehicle holds support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214608869U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114655053A (en) * | 2022-04-18 | 2022-06-24 | 武汉海乐智能科技有限公司 | Unmanned aerial vehicle charging platform for electric power inspection |
-
2021
- 2021-03-04 CN CN202120463316.XU patent/CN214608869U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114655053A (en) * | 2022-04-18 | 2022-06-24 | 武汉海乐智能科技有限公司 | Unmanned aerial vehicle charging platform for electric power inspection |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211105 |
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| CF01 | Termination of patent right due to non-payment of annual fee |