CN212099331U - Unmanned aerial vehicle buffer stop - Google Patents
Unmanned aerial vehicle buffer stop Download PDFInfo
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- CN212099331U CN212099331U CN202020810856.6U CN202020810856U CN212099331U CN 212099331 U CN212099331 U CN 212099331U CN 202020810856 U CN202020810856 U CN 202020810856U CN 212099331 U CN212099331 U CN 212099331U
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- aerial vehicle
- unmanned aerial
- clamping
- ring
- net ring
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Abstract
The utility model discloses an unmanned aerial vehicle buffer stop, including fixing the base subassembly on the unmanned aerial vehicle organism, the base subassembly is connected with corresponding anticollision net ring through four support arms, anticollision net ring cover is established on the unmanned aerial vehicle rotor, anticollision net ring adopts an organic whole to mould plastics and forms, anticollision net ring is including two rings of arranging from top to bottom, two connect through the annular net between the ring. The utility model discloses novel structure, easy dismounting, barrier propterty is good, and the anticollision net ring is established unmanned aerial vehicle rotor cover in inside, the effectual rotor that has protected unmanned aerial vehicle avoids the rotor to meet the barrier and suffer damage.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to an unmanned aerial vehicle buffer stop.
Background
At present, along with the improvement of unmanned aerial vehicle technique, unmanned aerial vehicle is very common in daily life to apply in many life fields, like photography, control, agricultural irrigation etc. unmanned aerial vehicle when using, in order to prevent that unmanned aerial vehicle from colliding the building when flight, can install crashproof protection ring on unmanned aerial vehicle, but current protection ring structure is simple, and barrier propterty is low, protection unmanned aerial vehicle's that can not be fine rotor.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle buffer stop solves current unmanned aerial vehicle protection ring simple structure, and barrier propterty is low, the problem of protection unmanned aerial vehicle's rotor that can not be fine.
In order to solve the technical problem, the utility model adopts the following technical scheme:
the utility model relates to an unmanned aerial vehicle buffer stop, including fixing the base subassembly on the unmanned aerial vehicle organism, the base subassembly is connected with corresponding anticollision net ring through four support arms, anticollision net ring cover is established on the unmanned aerial vehicle rotor, anticollision net ring adopts an organic whole to mould plastics and forms, anticollision net ring is including two rings of arranging from top to bottom, two connect through the ring network between the ring.
Further, the base subassembly includes bottom plate and connecting plate, the bottom plate is fixed on the unmanned aerial vehicle organism, the top surface of bottom plate is provided with the grafting square column, be provided with on the connecting plate with grafting square column complex grafting square hole, there is the jackscrew through threaded connection on the lateral wall about the connecting plate, the screwed end embedding of jackscrew is reserved in the hole of dodging on the grafting square column, four horns positions of connecting plate all through bolt assembly and corresponding the support arm is connected.
Furthermore, the support arm comprises a clamping arm, one end of the clamping arm is provided with a clamping bulge, and the other end of the clamping arm is provided with two clamping arms;
the clamping protrusion is in clamping fit with a clamping groove fixed on the circumferential outer wall of the anti-collision net ring;
the two clamping arms clamp the middle connecting plate together and are connected and fixed through a bolt assembly.
Furthermore, the clamping protrusion and the clamping groove are both in a dovetail shape.
Furthermore, a protective net cover is arranged at the top of the anti-collision net ring.
Compared with the prior art, the utility model discloses a beneficial technological effect:
the utility model discloses novel structure, easy dismounting, barrier propterty is good, and the anticollision net ring is established unmanned aerial vehicle rotor cover in inside, the effectual rotor that has protected unmanned aerial vehicle avoids the rotor to meet the barrier and suffer damage.
Drawings
The present invention will be further explained with reference to the following description of the drawings.
Fig. 1 is an installation schematic diagram of the unmanned aerial vehicle collision avoidance device of the present invention;
fig. 2 is a schematic structural view of the collision avoidance device of the unmanned aerial vehicle of the present invention;
FIG. 3 is a schematic structural view of the anti-collision net ring of the present invention;
fig. 4 is a schematic structural view of the base assembly of the present invention;
fig. 5 is a schematic structural view of the support arm of the present invention.
Description of reference numerals: 1. an unmanned aerial vehicle body; 2. a base assembly; 201. a base plate; 202. a connecting plate; 203. splicing a square column; 204. inserting a square hole; 205. carrying out top thread; 3. a support arm; 301. a clamping arm; 302. clamping the bulges; 303. a clamp arm; 304. clamping the groove; 4. an anti-collision net ring; 401. a circular ring; 402. an endless web; 5. a rotor wing of the unmanned aerial vehicle; 6. and (4) a protective net cover.
Detailed Description
In order to make the technical solutions of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings and the detailed description.
As shown in fig. 1 to 2, disclosed an unmanned aerial vehicle buffer stop in this embodiment, including fixing base subassembly 2 on unmanned aerial vehicle organism 1. Base subassembly 2 is connected with corresponding anticollision net ring 4 through four support arms 3, and the cover of anticollision net ring 4 is established on unmanned aerial vehicle rotor 5.
As shown in fig. 3, the anti-collision net ring 4 is formed by integral injection molding, the anti-collision net ring 4 includes two rings 401 arranged up and down, and the two rings 401 are connected by a ring net 402. It should be noted that the ring net 402 has certain strength and rigidity.
As shown in fig. 4, the base component 2 includes bottom plate 201 and connecting plate 202, bottom plate 201 passes through the bolt fastening on the unmanned aerial vehicle organism 1, the top surface integrated into one piece of bottom plate 201 has grafting square column 203, be provided with on the connecting plate 202 with grafting square column 203 complex grafting square hole 204, there is jackscrew 205 through threaded connection on the lateral wall about connecting plate 202, the screwed end embedding of jackscrew 205 is in keeping in the hole of dodging on grafting square column 203 in advance, four horns position of connecting plate 202 all is connected with corresponding support arm 3 through bolt assembly.
As shown in fig. 5, the support arm 3 is formed by integral injection molding, the support arm 3 includes a clamping arm 301, one end of the clamping arm 301 is provided with a clamping protrusion 302, and the other end of the clamping arm 301 is provided with two clamping arms 303. The clamping protrusion 302 is in clamping fit with a clamping groove 304 fixed on the outer circumferential wall of the anti-collision net ring 4, and it should be noted that the clamping groove 304 is bonded with two circular rings 401 and a ring net 402. The two clamping arms 303 clamp the middle connecting plate 202 together and are connected and fixed through a bolt assembly. In this embodiment, the snap projections 302 and snap recesses 304 are each dovetail shaped.
In order to improve the protective performance at the top of the anti-collision net ring 4, a protective net cover 6 is arranged at the top of the anti-collision net ring 4, and the protective net cover 6 is connected to the anti-collision net ring 4 through threads. Specifically, an external thread is provided on the upper ring 401, and the protective mesh cover 6 is screwed with the upper ring 401.
The above-mentioned embodiments are only intended to describe the preferred embodiments of the present invention, but not to limit the scope of the present invention, and those skilled in the art should also be able to make various modifications and improvements to the technical solution of the present invention without departing from the spirit of the present invention, and all such modifications and improvements are intended to fall within the scope of the present invention as defined in the appended claims.
Claims (5)
1. The utility model provides an unmanned aerial vehicle buffer stop, its characterized in that: including fixing base subassembly (2) on unmanned aerial vehicle organism (1), base subassembly (2) are connected with corresponding anticollision net ring (4) through four support arms (3), anticollision net ring (4) cover is established on unmanned aerial vehicle rotor (5), anticollision net ring (4) adopt an organic whole to mould plastics and form, anticollision net ring (4) are including two rings (401) of arranging from top to bottom, two connect through annular net (402) between ring (401).
2. The unmanned aerial vehicle buffer stop of claim 1, characterized in that: base subassembly (2) are including bottom plate (201) and connecting plate (202), bottom plate (201) are fixed on the unmanned aerial vehicle organism (1), the top surface of bottom plate (201) is provided with grafting square column (203), be provided with on connecting plate (202) with grafting square column (203) complex grafting square hole (204), there is jackscrew (205) through threaded connection on the lateral wall about connecting plate (202), the screwed end embedding of jackscrew (205) is reserved in the hole of dodging on grafting square column (203), four corner positions of connecting plate (202) all through bolt assembly and corresponding support arm (3) are connected.
3. The unmanned aerial vehicle buffer stop of claim 2, characterized in that: the support arm (3) comprises a clamping arm (301), a clamping bulge (302) is arranged at one end of the clamping arm (301), and two clamping arms (303) are arranged at the other end of the clamping arm (301);
the clamping protrusion (302) is in clamping fit with a clamping groove (304) fixed on the circumferential outer wall of the anti-collision net ring (4);
the two clamping arms (303) clamp the middle connecting plate (202) together and are connected and fixed through a bolt assembly.
4. The unmanned aerial vehicle buffer stop of claim 3, characterized in that: the clamping protrusion (302) and the clamping groove (304) are both in a dovetail shape.
5. The unmanned aerial vehicle buffer stop of claim 1, characterized in that: and a protective net cover (6) is arranged at the top of the anti-collision net ring (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020810856.6U CN212099331U (en) | 2020-05-15 | 2020-05-15 | Unmanned aerial vehicle buffer stop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020810856.6U CN212099331U (en) | 2020-05-15 | 2020-05-15 | Unmanned aerial vehicle buffer stop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212099331U true CN212099331U (en) | 2020-12-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020810856.6U Active CN212099331U (en) | 2020-05-15 | 2020-05-15 | Unmanned aerial vehicle buffer stop |
Country Status (1)
| Country | Link |
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| CN (1) | CN212099331U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
-
2020
- 2020-05-15 CN CN202020810856.6U patent/CN212099331U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
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