CN211844892U - Unmanned aerial vehicle with safeguard function - Google Patents
Unmanned aerial vehicle with safeguard function Download PDFInfo
- Publication number
- CN211844892U CN211844892U CN202020240817.7U CN202020240817U CN211844892U CN 211844892 U CN211844892 U CN 211844892U CN 202020240817 U CN202020240817 U CN 202020240817U CN 211844892 U CN211844892 U CN 211844892U
- Authority
- CN
- China
- Prior art keywords
- spring
- unmanned aerial
- aerial vehicle
- baffle
- telescopic link
- Prior art date
- 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.)
- Active
Links
- 238000003466 welding Methods 0.000 claims abstract description 12
- 238000005192 partition Methods 0.000 claims description 6
- 238000013016 damping Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 2
- 230000002349 favourable effect Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 2
- 239000002689 soil Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
Images
Landscapes
- Vibration Dampers (AREA)
Abstract
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle with safeguard function, which comprises a fixing plate and i, the middle part welding of terminal surface has the baffle under the fixed plate, the both sides horizontal welding of baffle has slide rail and forked tail slider, the forked tail slider has all welded the spring fixture block with one side that the baffle is relative, and install first spring between forked tail slider one side welded spring fixture block and the baffle one side welded spring fixture block, the lower terminal surface slope welding of forked tail slider has the telescopic link, and the lower terminal surface welding of telescopic link pars contractilis has the fixed block, the pars contractilis cover of telescopic link is equipped with the second spring, the through-hole has been seted up at the middle part of fixed block, and roll in the through-. The utility model discloses in, this landing support that has safeguard function is under the interact of first spring and second spring, the vibrations that bring when reduction that can be better descends to be favorable to safe landing.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle with safeguard function.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and the program control device who is owned to control, perhaps operate by the on-vehicle computer completely or intermittently independently, the support that rises and falls is installed to the undercarriage lower extreme terminal surface of unmanned aerial vehicle bottom of the body, current unmanned aerial vehicle support function singleness that rises and falls, the support of unmanned aerial vehicle undercarriage often all is planar structure, when unmanned aerial vehicle rises and falls in the more work area of grit soil block, planar structure's the support that rises and falls often makes unmanned aerial vehicle take place the slope easily, and then make the unmanned aerial vehicle organism impaired, thereby be unfavorable for landing of unmanned aerial vehicle safety.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle with safeguard function who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle with safeguard function, which comprises a fixing plate and i, the middle part welding of terminal surface has the baffle under the fixed plate, the horizontal welding in both sides of baffle has the slide rail, sliding fit has the forked tail slider in the spout of slide rail, the forked tail slider has all welded the spring fixture block with the relative one side of baffle, and install first spring between forked tail slider one side welded spring fixture block and the baffle one side welded spring fixture block, the lower terminal surface slope welding of forked tail slider has the telescopic link, the telescopic link includes fixed part and pars contractilis, and the lower terminal surface welding of telescopic link pars contractilis has the fixed block, the pars contractilis cover of telescopic link is equipped with the second spring, the through-hole has been seted up at the middle part.
Preferably, the second spring is located between the lower end face of the telescopic rod fixing portion and the upper end face of the fixing block.
Preferably, threaded through holes are formed in the two sides of the fixing plate, and bolts are installed in the threaded through holes in a spiral matching mode.
Preferably, the partition is located between the two first springs.
Preferably, a damping rubber block is glued and fixed on the outer side of the roller.
The utility model has the advantages that: the utility model discloses in, through set up buffering roller train on the unmanned aerial vehicle that has safeguard function here, and it is tensile fixed to the forked tail slider progress through first spring in the slide rail of terminal surface under the fixed plate, set up the telescopic link that has the second spring simultaneously at the lower terminal surface of forked tail slider, when unmanned aerial vehicle rises and falls at the more work area of grit soil block, this support that rises and falls that has safeguard function is under the interact of first spring and second spring, the vibrations that bring during reduction that can be better descends, thereby be favorable to safe landing.
Drawings
Fig. 1 is a schematic view of a main view structure of an unmanned aerial vehicle with a protection function provided by the present invention;
fig. 2 is a schematic side view of an unmanned aerial vehicle with a protection function according to the present invention;
fig. 3 is the utility model provides an unmanned aerial vehicle's upward view structure schematic with safeguard function.
In the figure: 1 fixed plate, 2 slide rails, 3 baffles, 4 forked tail sliders, 5 spring fixture blocks, 6 first springs, 7 bolts, 8 telescopic links, 9 second springs, 10 fixed blocks, 11 roller shafts, 12 gyro wheels.
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.
Referring to fig. 1-3, an unmanned aerial vehicle with a protection function comprises a fixing plate 1, wherein threaded through holes are formed in both sides of the fixing plate 1, bolts 7 are arranged in the threaded through holes in a spiral matching manner, so that a landing support of the unmanned aerial vehicle with the protection function can be better installed and fixed on an unmanned aerial vehicle body, a partition plate 3 is welded in the middle of the lower end face of the fixing plate 1, slide rails 2 are horizontally welded on both sides of the partition plate 3, the partition plate 3 is positioned between two first springs 6, so that a dovetail slide block 4 in the yellow section 2 can be conveniently stretched and fixed, a dovetail slide block 4 is arranged in a slide groove of the slide rail 2 in a sliding fit manner, spring clamping blocks 5 are welded on one sides of the dovetail slide blocks 4 opposite to the partition plate 3, first springs 6 are arranged between the spring clamping blocks 5 welded on one side of the dovetail slide block 4 and the spring clamping blocks 5 welded on, when in use, the first spring 6 is prevented from shifting, the lower end surface of the dovetail slide block 4 is welded with the telescopic rod 8 in an inclined way, the telescopic rod 8 comprises a fixed part and a telescopic part, and the lower end surface of the telescopic part of the telescopic rod 8 is welded with a fixed block 10, the telescopic part of the telescopic rod 8 is sleeved with a second spring 9, the second spring 9 is positioned between the lower end surface of the fixed part of the telescopic rod 8 and the upper end surface of the fixed block 10, when the unmanned aerial vehicle rises and falls in a working area with more sand and soil blocks, the rising and falling support with the protection function can better reduce the vibration caused by falling under the interaction of the first spring 6 and the second spring 9, thereby be favorable to safe landing, the through-hole has been seted up at the middle part of fixed block 10, and the roll 11 is installed in the through-hole rolling, and the one end installation of roll 11 is fixed with gyro wheel 12, and the outside veneer of gyro wheel 12 is fixed with the yielding rubber piece, can play certain buffering cushioning effect.
In this embodiment, unmanned aerial vehicle with safeguard function is when using, the operator fixes this roller train installation on fixed plate 1 through rotating bolt 7, then it is fixed with this fixed plate 1 and the installation of unmanned aerial vehicle body, when unmanned aerial vehicle rises and falls at the more work area of grit soil block, forked tail slider 4 removes in slide rail 2 under the extension of first spring 6, buffer damping effect when can playing certain left and right sides atress, forked tail slider 4 has the telescopic link 8 of second spring 9 down also can play the cushioning effect when certain upper and lower atress simultaneously, this unmanned aerial vehicle landing support with safeguard function is under the interact of first spring 6 and second spring 9, the vibrations that bring when the grit soil block are descended to reduction unmanned aerial vehicle that can be better, thereby be favorable to landing of unmanned aerial vehicle safety.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle with safeguard function, which comprises a fixing plate (1) and is characterized in that, the middle part welding of terminal surface has baffle (3) under fixed plate (1), the both sides horizontal welding of baffle (3) has slide rail (2), sliding fit has forked tail slider (4) in the spout of slide rail (2), spring fixture block (5) have all been welded to one side that forked tail slider (4) and baffle (3) are relative, and install first spring (6) between forked tail slider (4) one side welded spring fixture block (5) and baffle (3) one side welded spring fixture block (5), the lower terminal surface slope welding of forked tail slider (4) has telescopic link (8), telescopic link (8) include fixed part and pars contractilis, and the lower terminal surface welding of telescopic link (8) pars contractilis had fixed block (10), the pars contractilis cover of telescopic link (8) is equipped with second spring (9, a through hole is formed in the middle of the fixing block (10), a roller shaft (11) is installed in the through hole in a rolling mode, and a roller (12) is installed and fixed at one end of the roller shaft (11).
2. The unmanned aerial vehicle with safeguard function according to claim 1, characterized in that, the second spring (9) is located between the lower terminal surface of telescopic link (8) fixed part and the up end of fixed block (10).
3. The unmanned aerial vehicle with the protection function according to claim 1, wherein threaded through holes are formed in both sides of the fixing plate (1), and bolts (7) are installed in the threaded through holes in a screw fit mode.
4. Unmanned aerial vehicle with safeguard function according to claim 1, characterized in that the partition (3) is located between two first springs (6).
5. The unmanned aerial vehicle with protection function of claim 1, wherein the outside of the roller (12) is glued and fixed with a damping rubber block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020240817.7U CN211844892U (en) | 2020-03-02 | 2020-03-02 | Unmanned aerial vehicle with safeguard function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020240817.7U CN211844892U (en) | 2020-03-02 | 2020-03-02 | Unmanned aerial vehicle with safeguard function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211844892U true CN211844892U (en) | 2020-11-03 |
Family
ID=73238325
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020240817.7U Active CN211844892U (en) | 2020-03-02 | 2020-03-02 | Unmanned aerial vehicle with safeguard function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211844892U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162313A (en) * | 2021-12-29 | 2022-03-11 | 浙江东田科技有限公司 | A remove unmanned aerial vehicle for agricultural monitoring |
-
2020
- 2020-03-02 CN CN202020240817.7U patent/CN211844892U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162313A (en) * | 2021-12-29 | 2022-03-11 | 浙江东田科技有限公司 | A remove unmanned aerial vehicle for agricultural monitoring |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104442880A (en) | Suspension type monorail train bogie | |
| CN102390447B (en) | Low-mounted crawler track walking system with suspended shock-absorbing device | |
| CN107554547B (en) | Straddle type monorail train and portal frame type bogie thereof | |
| CN204079186U (en) | Lay the lift car of shock absorption device | |
| CN211844892U (en) | Unmanned aerial vehicle with safeguard function | |
| CN103963860B (en) | A robot differential link type crawler chassis | |
| CN206155604U (en) | Asymmetric upper block is from tensioning formula crawler attachment | |
| CN203600978U (en) | Spacing bell-type engine mounting assembly | |
| CN106043324B (en) | Trolley structure of aerial bus and running track thereof | |
| CN209702068U (en) | A kind of damping device for lift car | |
| CN204956726U (en) | Electric tricycle seat shock -absorbing structure | |
| CN202243748U (en) | Overhead continuous track travelling system with suspending damping device | |
| CN204745485U (en) | Treadmill rear wheel shock mitigation system | |
| CN203702951U (en) | V-shaped rubber supporting part | |
| CN210371781U (en) | Shock absorber and shock attenuation equipment and haulage vehicle that remove on-vehicle mass spectrograph | |
| CN207579873U (en) | A kind of straddle-type monorail train and its dual-axis bogie | |
| CN215204853U (en) | Single track hangs people's car of suspension shock mitigation system | |
| CN207405512U (en) | A kind of urban road deceleration device | |
| CN210942004U (en) | Tractor cab vibration/noise reduction equipment | |
| CN216414064U (en) | Generator base with vibration/noise reduction function | |
| CN203637548U (en) | Box-type limiting engine suspension assembly | |
| CN202225933U (en) | Low-mounted caterpillar walking system with suspension vibration reduction device | |
| CN104085401A (en) | Traction transformer suspension device for railway vehicle and railway vehicle | |
| CN203902547U (en) | Rail vehicle traction transformer suspension device and rail vehicle | |
| CN219821786U (en) | Unmanned aerial vehicle with shock-absorbing function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |