CN214986032U - Take six unmanned aerial vehicle who keeps away barrier - Google Patents
Take six unmanned aerial vehicle who keeps away barrier Download PDFInfo
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- CN214986032U CN214986032U CN202121322981.3U CN202121322981U CN214986032U CN 214986032 U CN214986032 U CN 214986032U CN 202121322981 U CN202121322981 U CN 202121322981U CN 214986032 U CN214986032 U CN 214986032U
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- aerial vehicle
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- 230000004888 barrier function Effects 0.000 title claims description 14
- 238000009434 installation Methods 0.000 claims abstract description 13
- 230000003139 buffering effect Effects 0.000 claims abstract description 12
- 239000007853 buffer solution Substances 0.000 claims description 13
- 238000004891 communication Methods 0.000 claims description 7
- 238000005259 measurement Methods 0.000 claims description 4
- 230000008447 perception Effects 0.000 claims description 3
- 238000010030 laminating Methods 0.000 description 11
- 238000000034 method Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000035899 viability Effects 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle with six-side obstacle avoidance, which comprises an unmanned aerial vehicle body and a buffering base arranged at the lower end of the unmanned aerial vehicle body, wherein the outer side surface of the buffering base is provided with supporting legs, the unmanned aerial vehicle body is in signal connection with an obstacle avoidance system, the buffering base comprises a linking disc, an air bag arranged at the lower end of the linking disc and an installation column cap arranged at the center of the upper surface of the linking disc, a sliding rod is connected with the inside of a sleeve, a semicircular cushion block is arranged at one end of the sliding rod, a sliding block is arranged at the other end of the sliding rod, the sliding block is connected with a sliding groove, when the unmanned aerial vehicle body falls to the ground, the air bag is directly contacted with the ground to absorb the impact force of the ground to the unmanned aerial vehicle body, the semicircular cushion block is contacted with the ground, the sliding rod slides up and down along the inside of the sleeve by utilizing a reset spring connected between the sliding rod and the sleeve, and then four supporting legs at the outer side of the buffering base maintain the smoothness of the falling to the buffering base by self-adjusting the height, in order to reduce the damage that causes when the unmanned aerial vehicle body accident falls to the ground.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle of six obstacles of keeping away in area.
Background
The unmanned plane is called unmanned plane for short, is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, and can be defined as follows from the technical perspective: compared with manned aircraft, the unmanned fixed wing aircraft has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
Unmanned aerial vehicle leads to malfunctioning if meet with unexpected striking at the flight in-process, perhaps the electric quantity exhausts, makes unmanned aerial vehicle directly fall from the eminence, easily causes its damage, directly leads to scrapping when serious.
To above problem, improve current device, provided an unmanned aerial vehicle who takes six faces to keep away the barrier.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle of six obstacles of keeping away in area adopts this device to work to unmanned aerial vehicle directly falls from the eminence and easily causes damaged problem in having solved above-mentioned background.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with six sides of obstacle avoidance comprises an unmanned aerial vehicle body and a buffer base arranged at the lower end of the unmanned aerial vehicle body, wherein supporting legs are arranged on the outer side surface of the buffer base, and the unmanned aerial vehicle body is in signal connection with an obstacle avoidance system;
the buffer base comprises a connecting disc, an air bag arranged at the lower end of the connecting disc and a mounting column head mounted in the center of the upper surface of the connecting disc.
Furthermore, the supporting leg comprises a sleeve connected with the outer edge of the connecting disc and a supporting rod arranged inside the sleeve, and a sliding groove is formed in the surface of the sleeve.
Further, the bracing piece includes the slide bar that is connected with telescopic inside and sets up the semicircle cushion in slide bar one end to and install the slider at the slide bar other end, the slider is connected with the spout.
Further, the installation column cap is including seting up the activity groove on installation column cap surface and setting up the draw runner at activity groove both sides to and install the spacing subassembly in activity inslot portion, the laminating appearance groove has been seted up to the inside of installation column cap.
Further, spacing subassembly is including intercepting the piece and installing the linkage plate in interception piece one side to and set up the linking strip in linkage plate one end, the both ends of linking strip all are provided with the extension piece, and the surface of linking strip is provided with the handle, and connecting spring is installed to one side of extending the piece, and connecting spring's one end is connected with the internal surface of draw runner board, and laminating arc groove has been seted up on the surface of intercepting the piece.
Further, the lower surface of unmanned aerial vehicle body is provided with the installation piece, and the surface of installation piece is provided with the connecting rod, and the semicircle paster is installed to the one end of connecting rod, and the semicircle paster holds the groove with the laminating and is connected, and the laminating arc groove is connected with the connecting rod.
Furthermore, the obstacle avoidance system comprises an obstacle sensing module for sensing external obstacles, a height measurement module for measuring the height above the ground and an assembly navigation module for route guidance, the obstacle avoidance system is in signal connection with a wireless communication module and a route control module, and the obstacle avoidance system is connected with the route control module through the wireless communication module.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model provides a take six unmanned aerial vehicle who keeps away barrier, the slide bar is connected with telescopic inside, the semicircle cushion sets up the one end at the slide bar, the other end at the slide bar is installed to the slider, the slider is connected with the spout, when the unmanned aerial vehicle body falls to the ground, the gasbag is direct and ground contact, in order to absorb the impact force of ground to the unmanned aerial vehicle body, semicircle cushion and ground contact therewith, utilize the reset spring who is connected between slide bar and the sleeve, elasticity makes the slide bar slide from top to bottom along telescopic inside, and then four supporting legs in the buffering base outside lead to the fact the damage through spontaneous height-adjusting in order to maintain the gentleness that the buffering base falls to the ground, in order to reduce the unexpected damage that causes when falling to the ground of unmanned aerial vehicle body.
2. The utility model provides a take six unmanned aerial vehicle who keeps away barrier, the both ends that link up the strip all are provided with the extension piece, the surface that links up the strip is provided with the handle, extend one side of piece and install coupling spring, coupling spring's one end is connected with the internal surface of draw runner board, laminating arc groove has been seted up on the surface that blocks the piece, through the pulling handle, make the extension piece slide along the inside of draw runner board, make the interception piece break away from the activity groove, it holds the groove with the laminating to make semicircle paster again be connected, relieve the handle, the interception piece resumes the normal position, the laminating arc groove that both sides blocked the piece carries out the clamp of laminating to the connecting rod, die semicircle paster lock in laminating holds the groove, and then accomplish the installation of buffer base to the unmanned aerial vehicle body, be convenient for follow-up loading and unloading.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the assembly structure of the buffer base and the support legs of the present invention;
FIG. 3 is a schematic structural view of the mounting column cap of the present invention;
FIG. 4 is a schematic view of the structure of the attaching container of the present invention;
fig. 5 is a schematic structural view of the limiting assembly of the present invention;
fig. 6 is a side view of the structure of the unmanned aerial vehicle body of the present invention;
fig. 7 is a system block diagram of the present invention.
In the figure: 1. an unmanned body; 11. mounting blocks; 12. a connecting rod; 13. a semicircular sticking block; 2. a buffer base; 21. a splice tray; 22. an air bag; 23. mounting a column head; 231. a movable groove; 232. a slide bar plate; 233. a limiting component; 2331. an intercepting block; 2332. a connector tile; 2333. a connecting strip; 2334. an extension block; 2335. pulling a handle; 2336. a connecting spring; 2337. fitting an arc groove; 234. fitting the accommodating groove; 3. supporting legs; 31. a sleeve; 32. a support bar; 321. a slide bar; 322. a semicircular cushion block; 323. a slider; 33. a chute; 4. an obstacle avoidance system; 41. an obstacle sensing module; 42. a height measurement module; 43. assembling a navigation module; 44. a wireless communication module; 45. and the navigation control module.
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.
Please refer to fig. 1, 2 and 7, an unmanned aerial vehicle with six surfaces for avoiding obstacles comprises an unmanned aerial vehicle body 1 and a buffering base 2 arranged at the lower end of the unmanned aerial vehicle body 1, wherein supporting legs 3 are arranged on the outer side surface of the buffering base 2, the unmanned aerial vehicle body 1 is in signal connection with an obstacle avoiding system 4, the buffering base 2 comprises a connecting disc 21, an air bag 22 arranged at the lower end of the connecting disc 21, and an installation column head 23 arranged at the center of the upper surface of the connecting disc 21.
Referring to fig. 2 to 4, the support legs 3 include a sleeve 31 connected to an outer edge of the adapter 21 and a support bar 32 disposed inside the sleeve 31, a sliding groove 33 is formed on a surface of the sleeve 31, the support bar 32 includes a sliding rod 321 connected to an inside of the sleeve 31, a semi-circular pad 322 disposed at one end of the sliding rod 321, and a slider 323 disposed at the other end of the sliding rod 321, the slider 323 is connected to the sliding groove 33, when the drone body 1 lands, the air bag 22 directly contacts with the ground to absorb an impact force of the ground on the drone body 1, the semi-circular pad 322 contacts with the ground, the sliding rod 321 elastically slides up and down along the inside of the sleeve 31 by a return spring connected between the sliding rod 321 and the sleeve 31, and further four support legs 3 outside the buffer base 2 automatically adjust a height to maintain smoothness of the landing of the buffer base 2 to reduce damage of the drone body 1 caused by accidental landing, the sliding rod 321 is connected with the inner bottom surface of the sleeve 31 through a return spring, the mounting column head 23 comprises a movable groove 231 arranged on the surface of the mounting column head 23, sliding strip plates 232 arranged on two sides of the movable groove 231, and a limiting assembly 233 arranged inside the movable groove 231, and a joint accommodating groove 234 is arranged inside the mounting column head 23.
Referring to fig. 5-7, the position limiting assembly 233 includes an intercepting block 2331, a connecting plate 2332 installed at one side of the intercepting block 2331, and a connecting bar 2333 installed at one end of the connecting plate 2332, both ends of the connecting bar 2333 are provided with extension blocks 2334, the outer surface of the connecting bar 2333 is provided with a pull handle 2335, one side of the extension block 2334 is provided with a connecting spring 2336, one end of the connecting spring 2336 is connected with the inner surface of the slide bar plate 232, the surface of the intercepting block 2331 is provided with a fitting arc groove 2337, the extension block 2334 slides along the inner part of the slide bar plate 232 by pulling the pull handle 2335, the intercepting block 2331 is separated from the movable groove 231, the semicircular fitting block 13 is connected with the fitting accommodating groove 234, the pull handle 2335 is released, the intercepting block 2331 is restored to its original position, the fitting arc grooves 2337 of the intercepting blocks 2331 at both sides apply a clamp to the connecting rod 12, the semicircular fitting block 13 is locked in the fitting accommodating groove 234, thereby completing the installation of the buffering base 2 to the unmanned aerial vehicle body 1, be convenient for follow-up loading and unloading, unmanned aerial vehicle body 1's lower surface is provided with installation piece 11, installation piece 11's surface is provided with connecting rod 12, semicircle sticking block 13 is installed to the one end of connecting rod 12, semicircle sticking block 13 is connected with laminating appearance groove 234, laminating arc groove 2337 is connected with connecting rod 12, keep away barrier system 4 including the barrier perception module 41 that is used for the external barrier of perception and the height measurement module 42 that is used for measuring terrain clearance, and be used for route guide's equipment navigation module 43, keep away barrier system 4 signal connection and have wireless communication module 44 and airline control module 45, keep away barrier system 4 and be connected with airline control module 45 through wireless communication module 44.
The working principle is as follows: when the unmanned aerial vehicle body 1 falls to the ground, the air bag 22 directly contacts with the ground to absorb the impact force of the ground to the unmanned aerial vehicle body 1, the semi-circular cushion block 322 contacts with the ground, the slide rod 321 elastically slides up and down along the inside of the sleeve 31 by utilizing the return spring connected between the slide rod 321 and the sleeve 31, then the four support legs 3 outside the buffer base 2 maintain the smoothness of the falling of the buffer base 2 by automatically adjusting the height to reduce the damage caused when the unmanned aerial vehicle body 1 falls to the ground accidentally, the extension block 2334 slides along the inside of the slide plate 232 by pulling the pull handle 2335 to separate the interception block 2331 from the movable groove 231, then the semi-circular sticking block 13 is connected with the sticking accommodating groove 234, the pull handle 2335 is released, the interception block 2331 returns to the original position, the sticking arc grooves 2337 of the interception blocks 2331 at two sides stick the connecting rod 12 to be stuck and clamped, and the sticking block 13 is locked in the sticking accommodating groove 234, and then accomplish the installation of buffer base 2 to the unmanned aerial vehicle body 1, the follow-up loading and unloading of being convenient for.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
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 (7)
1. The utility model provides an unmanned aerial vehicle of six obstacles of avoiding in area, includes unmanned aerial vehicle body (1) and sets up at buffering base (2) of unmanned aerial vehicle body (1) lower extreme, its characterized in that: the outer side surface of the buffer base (2) is provided with supporting legs (3), and the unmanned aerial vehicle body (1) is in signal connection with an obstacle avoidance system (4);
the buffer base (2) comprises a connecting disc (21), an air bag (22) arranged at the lower end of the connecting disc (21), and an installation column head (23) installed in the center of the upper surface of the connecting disc (21).
2. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 1, wherein: the supporting legs (3) comprise sleeves (31) connected with the outer edges of the connecting discs (21) and supporting rods (32) arranged inside the sleeves (31), and sliding grooves (33) are formed in the surfaces of the sleeves (31).
3. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 2, wherein: the supporting rod (32) comprises a sliding rod (321) connected with the inside of the sleeve (31), a semicircular cushion block (322) arranged at one end of the sliding rod (321), and a sliding block (323) arranged at the other end of the sliding rod (321), wherein the sliding block (323) is connected with the sliding groove (33).
4. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 1, wherein: the mounting column cap (23) comprises a movable groove (231) formed in the surface of the mounting column cap (23), sliding plates (232) arranged on two sides of the movable groove (231) and a limiting assembly (233) mounted inside the movable groove (231), and a fitting accommodating groove (234) is formed inside the mounting column cap (23).
5. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 4, wherein: the limiting assembly (233) comprises an intercepting block (2331), a connecting plate (2332) arranged on one side of the intercepting block (2331) and a connecting bar (2333) arranged at one end of the connecting plate (2332), extending blocks (2334) are arranged at two ends of the connecting bar (2333), a pull handle (2335) is arranged on the outer surface of the connecting bar (2333), a connecting spring (2336) is arranged on one side of the extending block (2334), one end of the connecting spring (2336) is connected with the inner surface of the sliding plate (232), and a fitting arc groove (2337) is formed in the surface of the intercepting block (2331).
6. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 1, wherein: the lower surface of the unmanned aerial vehicle body (1) is provided with a mounting block (11), the surface of the mounting block (11) is provided with a connecting rod (12), one end of the connecting rod (12) is provided with a semicircular sticking block (13), the semicircular sticking block (13) is connected with a sticking accommodating groove (234), and a sticking arc groove (2337) is connected with the connecting rod (12).
7. An unmanned aerial vehicle with six faces of avoiding obstacles as claimed in claim 1, wherein: keep away barrier system (4) including being used for perceiving the obstacle perception module (41) of external barrier and being used for measuring height measurement module (42) off the ground to and be used for route guide's equipment navigation module (43), keep away barrier system (4) signal connection has wireless communication module (44) and route control module (45), keep away barrier system (4) and be connected with route control module (45) through wireless communication module (44).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121322981.3U CN214986032U (en) | 2021-06-15 | 2021-06-15 | Take six unmanned aerial vehicle who keeps away barrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121322981.3U CN214986032U (en) | 2021-06-15 | 2021-06-15 | Take six unmanned aerial vehicle who keeps away barrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986032U true CN214986032U (en) | 2021-12-03 |
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ID=79127869
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121322981.3U Expired - Fee Related CN214986032U (en) | 2021-06-15 | 2021-06-15 | Take six unmanned aerial vehicle who keeps away barrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214986032U (en) |
-
2021
- 2021-06-15 CN CN202121322981.3U patent/CN214986032U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211203 |