CN218112982U - Anti type unmanned aerial vehicle that hits - Google Patents
Anti type unmanned aerial vehicle that hits Download PDFInfo
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- CN218112982U CN218112982U CN202222635654.4U CN202222635654U CN218112982U CN 218112982 U CN218112982 U CN 218112982U CN 202222635654 U CN202222635654 U CN 202222635654U CN 218112982 U CN218112982 U CN 218112982U
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Abstract
The utility model relates to an unmanned air vehicle technique field specifically indicates an anti type unmanned aerial vehicle that hits. Including the unmanned aerial vehicle body, there is anti subassembly that hits through a plurality of coupling assembling around the unmanned aerial vehicle body, coupling assembling includes the fixed block, there is rotatory piece fixed block one side, there is a plurality of clamping around the rotatory piece, there is the connecting block rotatory piece one end, there is a plurality of fixture block around the connecting block, there is the connecting plate clamping one side, pass through bolt one between connecting plate and the connecting block, there is the connecting rod connecting block one side, anti subassembly that hits includes the lantern ring, there are a plurality of anticollision boards around the lantern ring, cushion the subassembly through a plurality of between the lantern ring and the anticollision board, the buffering subassembly includes inserted bar and sleeve, the inserted bar is pegged graft in the sleeve, pass through spring coupling between sleeve and the inserted bar, be connected through bolt two between sleeve and the anticollision board. The utility model discloses a can alleviate by external impact's strength, conveniently dismantle anti subassembly that hits, the anti type unmanned aerial vehicle that hits of the unmanned aerial vehicle body of being convenient for overhaul.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically indicates an anti type unmanned aerial vehicle that hits.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicle traveles in the air, hits other objects easily, perhaps is hit by unidentified thing, installs the inconvenient later stage of anti-collision assembly back to unmanned aerial vehicle and overhauls unmanned aerial vehicle simultaneously, consequently need provide an anti type unmanned aerial vehicle that hits.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to provide a can alleviate by the strength of external force striking, conveniently dismantle anti subassembly that hits, the anti type unmanned aerial vehicle that hits of the unmanned aerial vehicle body of being convenient for overhaul.
The utility model discloses the technical scheme who adopts does: the utility model provides an anti type unmanned aerial vehicle that hits which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, be connected with the anti-collision subassembly through a plurality of coupling assembling around the unmanned aerial vehicle body, coupling assembling can connect the anti-collision subassembly to make things convenient for the anti-collision subassembly of dismouting, later stage easy access unmanned aerial vehicle body, the anti-collision subassembly can be alleviated the strength by external force striking, thereby protect the unmanned aerial vehicle body, coupling assembling is including setting up the fixed block at the unmanned aerial vehicle body, fixed being connected with rotatory piece in fixed block one side, fixed being equipped with a plurality of clamping around the rotatory piece, rotatory piece one end swing joint has the connecting block, the fixed fixture block that is equipped with a plurality of and clamping joint around the connecting block, the fixed connecting plate that is equipped with in clamping one side, pass through bolt one between connecting plate and the connecting block, connecting block one side is fixed be equipped with the connecting rod that hits subassembly fixed connection with the anti-collision, the anti-collision subassembly includes the lantern ring of being connected with a plurality of connecting rods, be equipped with a plurality of anti-collision plates around the lantern ring, through a plurality of buffering subassembly between the lantern ring and the anti-collision plate, the buffering subassembly is including fixed inserted bar and the sleeve that sets up at the anti-collision plate, the inserted bar in the sleeve, pass through spring coupling between sleeve and anti-collision plate.
When unmanned aerial vehicle need fly, can dock the connecting block that the connecting rod is connected with rotatory piece, then rotatory piece to can be with clamping and fixture block joint, when receiving the striking, make the sleeve move about on the inserted bar, make the spring receive the extrusion, thereby alleviate external force.
Furthermore, a first threaded hole for a first bolt to rotate in a threaded manner is formed in the connecting plate and the connecting block.
Furthermore, one end of the spring is fixedly connected with the inserted rod, and the other end of the spring is fixedly connected with the sleeve.
Furthermore, the sleeve and the anti-collision plate are provided with a second threaded hole for the second bolt to rotate in a threaded manner.
Furthermore, one side of the clamping block is an arc-shaped curved surface.
Further, the connecting rod is fixedly connected with the lantern ring.
Further, unmanned aerial vehicle body and fixed block fixed connection.
The utility model discloses beneficial effect:
the utility model has simple integral structure. This anti type unmanned aerial vehicle that hits through coupling assembling's setting, can connect anti subassembly that hits to make things convenient for the dismouting to hit the subassembly, later stage easy access unmanned aerial vehicle body, through the setting of anti subassembly that hits, can alleviate the strength by external force striking, thereby protection unmanned aerial vehicle body.
Drawings
Fig. 1 is the utility model relates to an anti type unmanned aerial vehicle's that hits overall structure schematic diagram.
Fig. 2 is the utility model discloses an anti-collision type unmanned aerial vehicle's anti-collision subassembly part schematic structure.
Fig. 3 is the utility model discloses an anti type unmanned aerial vehicle's that hits A portion schematic structure.
In the drawings:
1. an unmanned aerial vehicle body; 2. a connection assembly; 3. an anti-collision assembly; 2.1, fixing blocks; 2.2, rotating the block; 2.3, clamping; 2.4, connecting blocks; 2.5, clamping blocks; 2.6, connecting plates; 2.7, a first bolt; 2.8, connecting rods; 3.1, a lantern ring; 3.2, an anti-collision plate; 3.3, inserting a rod; 3.4, sleeve; 3.5, a spring; 3.6 and a second bolt.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings.
In order to solve and to alleviate the strength by external impact, conveniently dismantle anti subassembly that hits, the unmanned aerial vehicle body of being convenient for overhaul, the utility model provides an anti type unmanned aerial vehicle that hits as shown in the figure, its characterized in that: including unmanned aerial vehicle body 1, be connected with anti subassembly 3 that hits through a plurality of coupling assembling 2 around unmanned aerial vehicle body 1, coupling assembling 2 can connect anti subassembly 3 that hits to make things convenient for the dismouting to hit subassembly 3, later stage easy access unmanned aerial vehicle body 1, anti subassembly 3 can alleviate the strength by external force striking, thereby protection unmanned aerial vehicle body 1, coupling assembling 2 is including setting up fixed block 2.1 at unmanned aerial vehicle body 1, fixed block 2.1 one side is rotated and is connected with rotatory piece 2.2, fixed a plurality of clamping 2.3 that is equipped with around rotatory piece 2.2, rotatory piece 2.2 one end swing joint has connecting block 2.4, fixed fixture block 2.5 that is equipped with a plurality of and clamping 2.3 joint around connecting block 2.4, clamping 2.3 one side is fixed and is equipped with connecting plate 2.6, pass through bolt one 2.7 between connecting plate 2.6 and connecting block 2.4, connecting block 2.4 one side is fixed and is equipped with connecting rod 2.8 with anti subassembly 3 fixed connection of hitting, when needing to connect anti subassembly 3, can install connecting block 2.4 and 2.2.2.2.3 with the rotatory piece 2.3, thereby the connecting block 2.5 and the connecting block 2.2.3 is connected with the rotatory piece, thereby the connecting block 2.2.2.3 of connecting block is hit to the unmanned aerial vehicle body is connected.
The anti-collision assembly 3 comprises a lantern ring 3.1 connected with a plurality of connecting rods 2.8, a plurality of anti-collision plates 3.2 are arranged around the lantern ring 3.1, the lantern ring 3.1 and the anti-collision plates 3.2 are connected through a plurality of buffer assemblies, each buffer assembly comprises an inserted bar 3.3 fixedly arranged on the lantern ring 3.1 and a sleeve 3.4 movably arranged on the anti-collision plate 3.2, the inserted bar 3.3 is inserted into the sleeve 3.4, the sleeves 3.4 and the inserted bars 3.3 are connected through springs 3.5, the sleeves 3.4 and the anti-collision plates 3.2 are connected through bolts two 3.6, when the anti-collision plates are collided, the sleeves 3.4 are pushed by the anti-collision plates 3.2, the sleeves 3.4 move on the inserted bars 3.3, the springs 3.5 are squeezed, external force is relieved, and if the anti-collision plates 3.2 are damaged, the sleeves 3.4 and the anti-collision plates 3.2 can be separated by rotating the bolts two 3.6, so that the anti-collision plates 3.2 can be replaced.
The utility model discloses in be equipped with on connecting plate 2.6 and connecting block 2.4 and supply the rotatory screw hole one of a 2.7 screw thread of bolt.
The utility model discloses in spring 3.5's one end fixed connection inserted bar 3.3, spring 3.5's other end fixed connection sleeve 3.4.
The utility model discloses in be equipped with on sleeve 3.4 and the anticollision board 3.2 and supply two 3.6 screw thread rotatory screw hole two of bolt.
The utility model discloses in fixture block 2.5 one side is the arc curved surface.
The utility model discloses in connecting rod 2.8 and lantern ring 3.1 fixed connection.
The utility model discloses in unmanned aerial vehicle body 1 and fixed block 2.1 fixed connection.
The anti type unmanned aerial vehicle that hits of this embodiment, when unmanned aerial vehicle need fly, can dock connecting block 2.4 and rotatory piece 2.2 that connecting rod 2.8 is connected, then rotatory piece 2.2 to can be with clamping 2.3 and fixture block 2.5 joint, accessible bolt 2.7 connection connecting plate 2.6 and connecting block 2.4 after that, thereby will hit subassembly 3 and install on unmanned aerial vehicle body 1. When the collision occurs, firstly, the anti-collision plate 3.2 pushes the sleeve 3.4, so that the sleeve 3.4 moves on the inserted rod 3.3, the spring 3.5 is extruded, and the external force is relieved, if the anti-collision plate 3.2 is damaged by collision, the sleeve 3.4 and the anti-collision plate 3.2 can be separated by rotating the bolt II 3.6, and therefore the anti-collision plate 3.2 can be replaced.
The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, it should be understood that those skilled in the art should also understand the scope of the present invention without inventively designing the similar structure and embodiments of the present invention without departing from the spirit of the present invention.
Claims (7)
1. The utility model provides an anti type unmanned aerial vehicle that hits which characterized in that: including unmanned aerial vehicle body (1), be connected with anticollision subassembly (3) through a plurality of coupling assembling (2) around unmanned aerial vehicle body (1), coupling assembling (2) are including setting up fixed block (2.1) at unmanned aerial vehicle body (1), fixed block (2.1) one side rotation is connected with rotatory piece (2.2), fixed a plurality of clamping (2.3) around rotatory piece (2.2), rotatory piece (2.2) one end swing joint has connecting block (2.4), fixed fixture block (2.5) that is equipped with a plurality of and clamping (2.3) joint around connecting block (2.4), clamping (2.3) one side is fixed and is equipped with connecting plate (2.6), pass through bolt one (2.7) between connecting plate (2.6) and connecting block (2.4), connecting rod (2.8) that fixed connection with anticollision subassembly (3) are equipped with anticollision subassembly (3) on one side of connecting block (2.4), anticollision subassembly (3) include the connecting rod (3.1) that are connected with a plurality of connecting rod (2.8), the buffer lantern ring (3.1.3) and the buffer lantern ring (3.3) set up through the buffer lantern ring (3.3) between the anticollision subassembly (3.3), the fender ring (3.3) and buffer lantern ring (3) including the fender ring (3.3) set up on the fender sleeve) around the fender ring (2.3), the inserted bar (3.3) is inserted in the sleeve (3.4), the sleeve (3.4) is connected with the inserted bar (3.3) through a spring (3.5), and the sleeve (3.4) is connected with the anti-collision plate (3.2) through a bolt II (3.6).
2. An anti-collision unmanned aerial vehicle according to claim 1, wherein: and a first threaded hole for the first bolt (2.7) to rotate in a threaded manner is formed in the connecting plate (2.6) and the connecting block (2.4).
3. An anti-collision unmanned aerial vehicle according to claim 1, wherein: one end of the spring (3.5) is fixedly connected with the inserted bar (3.3), and the other end of the spring (3.5) is fixedly connected with the sleeve (3.4).
4. An anti-collision unmanned aerial vehicle as claimed in claim 1, wherein: and a second threaded hole for the second bolt (3.6) to rotate in a threaded manner is formed in the sleeve (3.4) and the anti-collision plate (3.2).
5. An anti-collision unmanned aerial vehicle as claimed in claim 1, wherein: one side of the clamping block (2.5) is an arc-shaped curved surface.
6. An anti-collision unmanned aerial vehicle as claimed in claim 1, wherein: the connecting rod (2.8) is fixedly connected with the lantern ring (3.1).
7. An anti-collision unmanned aerial vehicle according to claim 1, wherein: unmanned aerial vehicle body (1) and fixed block (2.1) fixed connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222635654.4U CN218112982U (en) | 2022-10-08 | 2022-10-08 | Anti type unmanned aerial vehicle that hits |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222635654.4U CN218112982U (en) | 2022-10-08 | 2022-10-08 | Anti type unmanned aerial vehicle that hits |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218112982U true CN218112982U (en) | 2022-12-23 |
Family
ID=84496732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222635654.4U Active CN218112982U (en) | 2022-10-08 | 2022-10-08 | Anti type unmanned aerial vehicle that hits |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218112982U (en) |
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2022
- 2022-10-08 CN CN202222635654.4U patent/CN218112982U/en active Active
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