CN214002038U - Unmanned aerial vehicle flight buffer stop - Google Patents
Unmanned aerial vehicle flight buffer stop Download PDFInfo
- Publication number
- CN214002038U CN214002038U CN202023048689.5U CN202023048689U CN214002038U CN 214002038 U CN214002038 U CN 214002038U CN 202023048689 U CN202023048689 U CN 202023048689U CN 214002038 U CN214002038 U CN 214002038U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- butt joint
- vehicle body
- buffer stop
- 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.)
- Expired - Fee Related
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- 210000001503 joint Anatomy 0.000 claims abstract description 39
- 241000883990 Flabellum Species 0.000 claims abstract description 12
- 230000001771 impaired effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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- Catching Or Destruction (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle flight buffer stop, including the unmanned aerial vehicle body, the top fixed mounting of unmanned aerial vehicle body has the assembly jig; a limiting block is fixedly connected inside the unmanned aerial vehicle body, a butt joint block clamped with the limiting block is sleeved on the assembly frame, fasteners are sleeved on two sides close to the bottom of the assembly frame in a threaded manner, and fixing rods are fixedly connected on two sides close to the top of the assembly frame; the equal fixedly connected with connecting rod in both sides of butt joint piece, the one end fixed mounting that butt joint piece was kept away from to the connecting rod has U type anticollision cover, the screw thread has cup jointed the bolt on the connecting rod. An unmanned aerial vehicle flight buffer stop, solved unmanned aerial vehicle flabellum in the middle of the flight by birds striking to prevent that unmanned aerial vehicle is impaired, bring better use prospect.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle anticollision technical field, in particular to unmanned aerial vehicle flight buffer stop.
Background
Unmanned aerial vehicle controls through the remote control among the prior art, can be used to make a video recording in the middle of the life, also can be used to the exploration in farmland, but unmanned aerial vehicle is easily strikeed by birds at the flight in-process, easily leads to the unmanned aerial vehicle flabellum to damage, directly leads to unmanned aerial vehicle crash to cause the loss, the use of giving people has brought certain adverse effect, for this, we propose an unmanned aerial vehicle flight buffer stop.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides an unmanned aerial vehicle flight buffer stop can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle flight anti-collision device comprises an unmanned aerial vehicle body, wherein an assembly jig is fixedly installed at the top of the unmanned aerial vehicle body;
a limiting block is fixedly connected inside the unmanned aerial vehicle body, a butt joint block clamped with the limiting block is sleeved on the assembly frame, fasteners are sleeved on two sides close to the bottom of the assembly frame in a threaded manner, and fixing rods are fixedly connected on two sides close to the top of the assembly frame;
the equal fixedly connected with connecting rod in both sides of butt joint piece, the one end fixed mounting that butt joint piece was kept away from to the connecting rod has U type anticollision cover, the screw thread has cup jointed the bolt on the connecting rod.
Preferably, a clamping groove is formed in the butt joint block, and the butt joint block is connected with the limiting block through the clamping groove in a clamping mode.
Preferably, threaded holes matched with the fasteners are formed in the two sides of the butt joint block and the limiting block, the butt joint block is in threaded connection with the fasteners, and the butt joint block is in threaded connection with the limiting block.
Preferably, the bolt passes through the bottom of the fixing rod and is locked by a nut.
Preferably, the periphery of unmanned aerial vehicle body flabellum is arranged in to U type anticollision cover, U type anticollision cover is the fretwork design.
Compared with the prior art, the utility model discloses following beneficial effect has: according to the unmanned aerial vehicle flight anti-collision device, the butt joint block can be sleeved on the assembly frame, so that the clamping groove in the butt joint block is in butt joint with the limiting block, then the position of the butt joint block on the limiting block is fixed through the fastening piece, in order to prevent the U-shaped anti-collision cover from deforming in the flight process of the unmanned aerial vehicle, the bolt can sequentially penetrate through the connecting rod and the fixing rod, and then the nut is locked, so that the anti-collision device can be installed, the installation stability of the anti-collision device can be improved through the structure, and the anti-collision device can be conveniently assembled; when the unmanned aerial vehicle body is at the flight in-process, can prevent through U type anticollision cover that birds from directly striking the flabellum of unmanned aerial vehicle body on to play certain guard action to unmanned aerial vehicle body flabellum, prevent that unmanned aerial vehicle body flabellum from receiving the damage, be favorable to people to use, whole unmanned aerial vehicle flight buffer stop simple structure, convenient operation, the effect of using is better for traditional mode.
Drawings
Fig. 1 is the utility model relates to an unmanned aerial vehicle flight buffer stop's overall structure schematic diagram.
Fig. 2 is the utility model relates to an unmanned aerial vehicle flight buffer stop's A's enlargements in fig. 1.
In the figure: 1. an unmanned aerial vehicle body; 2. an assembly frame; 3. a butt joint block; 4. a connecting rod; 5. fixing the rod; 6. A U-shaped anti-collision cover; 7. a fastener; 8. a limiting block; 9. and (4) bolts.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1-2, an unmanned aerial vehicle flight anti-collision device comprises an unmanned aerial vehicle body 1, wherein an assembly frame 2 is fixedly installed at the top of the unmanned aerial vehicle body 1;
a limiting block 8 is fixedly connected inside the unmanned aerial vehicle body 1, a butt joint block 3 clamped with the limiting block 8 is sleeved on the assembly frame 2, fasteners 7 are sleeved on two sides close to the bottom of the assembly frame 2 in a threaded manner, and fixing rods 5 are fixedly connected on two sides close to the top of the assembly frame 2;
the equal fixedly connected with connecting rod 4 in both sides of butt joint piece 3, the one end fixed mounting that butt joint piece 3 was kept away from to connecting rod 4 has U type anticollision cover 6, and the screw thread has cup jointed bolt 9 on connecting rod 4.
Further, a clamping groove is formed in the butt joint block 3, the butt joint block 3 is connected with the limiting block 8 through clamping between the clamping groove and the limiting block, and therefore the position of the butt joint block 3 on the assembling jig 2 is limited through the limiting block 8.
Further, the threaded holes matched with the fasteners 7 are formed in the two sides of the butt joint block 3 and the limiting block 8, the butt joint block 3 is in threaded connection with the fasteners 7, the butt joint block 3 is in threaded connection with the limiting block 8, and therefore the positions of the butt joint block 3 on the limiting block 8 are fixed through the fasteners 7.
Further, the bolt 9 penetrates the bottom of the fixing rod 5 and is locked by a nut, so that the structural strength of the anti-collision device is enhanced.
Further, the periphery of 1 flabellum of unmanned aerial vehicle body is arranged in to U type anticollision cover 6, and U type anticollision cover 6 is the fretwork design to in prevent birds through U type anticollision cover 6 and directly strike the flabellum on the unmanned aerial vehicle body 1, thereby play the effect of protection.
The utility model discloses theory of operation and use flow: when the anti-collision device is used, the butt joint block 3 can be sleeved on the assembly frame 2, so that a clamping groove in the butt joint block 3 is in butt joint with the limiting block 8, then the position of the butt joint block 3 on the limiting block 8 is fixed through the fastening piece 7, in order to prevent the U-shaped anti-collision cover 6 from deforming, the bolt 9 can sequentially penetrate through the connecting rod 4 and the fixing rod 5 and then is locked through the nut, the anti-collision device can be installed, the installation stability of the anti-collision device can be improved through the structure, and the anti-collision device can be conveniently assembled; when unmanned aerial vehicle body 1 is at the flight in-process, can prevent through U type anticollision cover 6 that birds from directly striking unmanned aerial vehicle body 1's flabellum on to play certain guard action to unmanned aerial vehicle body 1 flabellum, prevent that unmanned aerial vehicle body 1 flabellum from receiving the damage, be favorable to people to use.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides an unmanned aerial vehicle flight buffer stop, includes unmanned aerial vehicle body (1), its characterized in that: an assembly frame (2) is fixedly mounted at the top of the unmanned aerial vehicle body (1);
a limiting block (8) is fixedly connected to the inside of the unmanned aerial vehicle body (1), a butt joint block (3) clamped with the limiting block (8) is sleeved on the assembly frame (2), fasteners (7) are sleeved on two sides close to the bottom of the assembly frame (2) in a threaded manner, and fixing rods (5) are fixedly connected on two sides close to the top of the assembly frame (2);
the anti-collision device is characterized in that connecting rods (4) are fixedly connected to the two sides of the butt joint blocks (3), U-shaped anti-collision covers (6) are fixedly mounted at the ends, far away from the butt joint blocks (3), of the connecting rods (4), and bolts (9) are sleeved on the connecting rods (4) in a threaded mode.
2. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the butt joint block is characterized in that a clamping groove is formed in the butt joint block (3), and the butt joint block (3) is connected with the limiting block (8) in a clamping mode.
3. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: threaded holes matched with the fasteners (7) are formed in the two sides of the butt joint block (3) and the limiting block (8), the butt joint block (3) is in threaded connection with the fasteners (7), and the butt joint block (3) is in threaded connection with the limiting block (8).
4. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the bolt (9) penetrates through the bottom of the fixing rod (5) and is locked through a nut.
5. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the periphery of unmanned aerial vehicle body (1) flabellum is arranged in to U type anticollision cover (6), U type anticollision cover (6) are the fretwork design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023048689.5U CN214002038U (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle flight buffer stop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023048689.5U CN214002038U (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle flight buffer stop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214002038U true CN214002038U (en) | 2021-08-20 |
Family
ID=77312200
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023048689.5U Expired - Fee Related CN214002038U (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle flight buffer stop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214002038U (en) |
-
2020
- 2020-12-17 CN CN202023048689.5U patent/CN214002038U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210820 |