CN217893246U - A crashproof structure for unmanned aerial vehicle flight - Google Patents
A crashproof structure for unmanned aerial vehicle flight Download PDFInfo
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- CN217893246U CN217893246U CN202222207793.7U CN202222207793U CN217893246U CN 217893246 U CN217893246 U CN 217893246U CN 202222207793 U CN202222207793 U CN 202222207793U CN 217893246 U CN217893246 U CN 217893246U
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- anticollision
- strip
- unmanned aerial
- aerial vehicle
- anticollision strip
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Abstract
The utility model discloses an anticollision structure for unmanned aerial vehicle flight, including mounting panel and anticollision strip, the mounting panel is inside to have seted up all around and to run through the groove, and the inner wall department that runs through the groove is provided with the anticollision strip, the anticollision strip includes cambered surface portion and regulation and control groove, the outer wall one side of anticollision strip is provided with cambered surface portion, and the inside department of anticollision strip runs through and has seted up the regulation and control groove. This an anticollision structure for unmanned aerial vehicle flight, whole anticollision structure is with the anticollision strip in the outside, as protective structure, its junction adopts the detachable mode to install, with the mounting panel that has the screw inner wall, as the installed part, the mountable is fixed in the axostylus axostyle department of screw, and utilize upper end department evenly distributed's anticollision strip, protect the inboard screw, the anticollision strip in the outside can install the anticollision strip of suitable quantity according to the demand, place whole anticollision structure in the outside department of screw, in addition the anticollision strip can be according to running through the inslot degree of depth, better protect according to the demand.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an anticollision structure for unmanned aerial vehicle flight.
Background
Unmanned aerial vehicle is unmanned vehicles, is the unmanned aircraft who utilizes radio remote control equipment and the program control device of self-contained to control, can be more fit for in comparatively unsafe task, is the comparatively common equipment of some trades nowadays, and unmanned aerial vehicle striking building or trees and damage often can appear when the personnel operate unmanned aerial vehicle now, and unmanned aerial vehicle's screw can lead to unmanned aerial vehicle unbalance by the meeting of hitting, influences unmanned aerial vehicle's normal flight.
Current unmanned aerial vehicle does not possess the protective structure to the screw many times, leads to unmanned aerial vehicle flight safety to obtain not guaranteeing, and some unmanned aerial vehicles are not convenient for carry out nimble use of adjusting from the crashproof structure in area moreover.
Therefore, in view of the above, research and improvement are performed on the existing structure and defects, and an anti-collision structure for unmanned aerial vehicle flight is provided, so as to achieve the purpose of higher practical value.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an anticollision structure for unmanned aerial vehicle flight to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an anticollision structure for unmanned aerial vehicle flight, includes mounting panel and anticollision strip, the mounting panel is inside has been seted up all around and has been run through the groove, and the inner wall department that runs through the groove is provided with the anticollision strip, the anticollision strip includes cambered surface portion and regulation and control groove, outer wall one side of anticollision strip is provided with cambered surface portion, and the inside department of anticollision strip runs through and has seted up the regulation and control groove.
Furthermore, a threaded inner wall is arranged on the inner wall of the mounting plate.
Furthermore, the mounting panel constitutes the plug through running through between groove and the anticollision strip and is connected, and runs through between groove and the anticollision strip size and mutually supports.
Furthermore, a fixing bolt is arranged at the joint of the inside of the mounting plate and the inside of the anti-collision strip.
Furthermore, the mounting panel passes through to constitute detachable construction between fixing bolt and the anticollision strip.
Furthermore, the through grooves are uniformly distributed along the central axis of the mounting plate, and the mounting plate is provided with six groups.
Furthermore, the regulation and control groove is arranged along the inside department of anticollision strip and is distributed, and the regulation and control groove is provided with four groups.
The utility model provides an anticollision structure for unmanned aerial vehicle flight possesses following beneficial effect:
whole anticollision structure uses the anticollision strip in the outside, as protective structure, and its junction adopts the detachable mode to install, can install the anticollision strip of suitable quantity according to the demand, arranges whole anticollision structure in the outside department of screw, and the anticollision strip can be according to running through the inslot degree of depth in addition, and is better protected according to the demand.
1. The utility model discloses, with the mounting panel that has the screw thread inner wall, as the installed part, the mountable is fixed in the axostylus axostyle department of placing of screw to utilize upper end department evenly distributed's anticollision strip, protect the inside screw.
2. The utility model discloses, the crashproof strip in the outside can install the crashproof strip of suitable quantity according to the demand, arranges whole crashproof structure in the outside department of screw, and the crashproof strip can be according to running through the inslot degree of depth in addition, and better protects according to the demand.
Drawings
Fig. 1 is a schematic top view of an anti-collision structure for unmanned aerial vehicle flight according to the present invention;
fig. 2 is a schematic view of an elevation structure of an anti-collision structure for unmanned aerial vehicle flight according to the present invention;
fig. 3 is the utility model relates to an anticollision strip spatial structure schematic diagram for unmanned aerial vehicle flying anticollision structure.
In the figure: 1. mounting a plate; 2. the inner wall of the thread; 3. a through groove; 4. an anti-collision strip; 401. an arc surface portion; 402. a regulating groove; 5. and (5) fixing the bolt.
Detailed Description
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
As shown in fig. 1-3, an anti-collision structure for unmanned aerial vehicle flight comprises a mounting plate 1 and an anti-collision strip 4, a through groove 3 is arranged around the inside of the mounting plate 1, and the inner wall of the through groove 3 is provided with an anti-collision strip 4, the anti-collision strip 4 comprises an arc surface part 401 and a regulating groove 402, one side of the outer wall of the anti-collision strip 4 is provided with the arc surface part 401, and the inner part of the anti-collision strip 4 is provided with a regulating groove 402 in a penetrating way, the inner wall of the mounting plate 1 is provided with a threaded inner wall 2, the mounting plate 1 is connected with the anti-collision strip 4 in a plugging way through the penetrating groove 3, the through grooves 3 and the anti-collision strips 4 are matched with each other in size, the fixing bolts 5 are arranged at the connecting positions of the inner part of the mounting plate 1 and the inner parts of the anti-collision strips 4, the mounting plate 1 forms a detachable structure through the fixing bolts 5 and the anti-collision strips 4, the through grooves 3 are uniformly distributed along the central axis of the mounting plate 1, and the mounting plate 1 is provided with six groups, the regulating and controlling grooves 402 are distributed along the inner part of the bumper strip 4 in an arrangement shape, and the regulating grooves 402 are provided with four sets, with the mounting plate 1 with the threaded inner wall 2, as a mounting member, can be arranged at the shaft lever of the propeller for fixing, so that the propeller is positioned at the inner side of the anti-collision strip 4 for independent rotation, and the anti-collision strips 4 which are uniformly distributed at the upper end are utilized, the inner side screw propeller is protected, the anti-collision strips 4 on the outer side can be provided with a proper number of anti-collision strips 4 according to requirements, the whole anti-collision structure is arranged on the outer side of the screw propeller, in addition, the anti-collision strips 4 can be arranged according to the depth in the through groove 3, and is fixedly installed by matching with a regulating groove 402 at a corresponding position, and in addition, the cambered surface part 401 at the inner wall can ensure that when the propeller is placed, the position state of comparatively laminating to guarantee whole protective structure's occupation volume, better protect according to the demand.
In conclusion, as shown in fig. 1-3, this an anticollision structure for unmanned aerial vehicle flight, in use, at first with mounting panel 1 that has screw thread inner wall 2, as the installed part, the mountable is fixed in the axostylus axostyle department of screw, later the user is according to the demand, in the through groove 3 of mounting panel 1, insert anticollision strip 4, and the fixing bolt 5 of rotatory outside department simultaneously, it is fixed to lock inserted anticollision strip 4, make anticollision strip 4 carry out high regulation and control according to the position of screw pitch axostylus axostyle, and can be according to the environmental condition, rotatory suitable quantity of anticollision strip 4 carries out plug connection, thereby carry out omnidirectional protection to unmanned aerial vehicle's screw.
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to practitioners skilled in this art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (7)
1. The utility model provides an anticollision structure for unmanned aerial vehicle flight, includes mounting panel (1) and crashproof strip (4), its characterized in that: the utility model discloses a crash-proof structure, including mounting panel (1), mounting panel (3) inside has been seted up all around and has been run through groove (3), and the inner wall department that runs through groove (3) is provided with anticollision strip (4), anticollision strip (4) include cambered surface portion (401) and regulation and control groove (402), outer wall one side of anticollision strip (4) is provided with cambered surface portion (401), and the inside department of anticollision strip (4) runs through and has seted up regulation and control groove (402).
2. An anti-collision structure for unmanned aerial vehicle flight according to claim 1, characterized in that the mounting plate (1) is provided at its inner wall with a threaded inner wall (2).
3. The anti-collision structure for unmanned aerial vehicle flight according to claim 1, characterized in that the mounting plate (1) is connected with the anti-collision strip (4) in a plugging manner through the through groove (3), and the through groove (3) and the anti-collision strip (4) are matched with each other in size.
4. An anti-collision structure for unmanned aerial vehicle flight according to claim 1, characterized in that the junction of the inside of the mounting plate (1) and the inside of the bumper strip (4) is provided with a fixing bolt (5).
5. A crash structure for unmanned aerial vehicle flight according to claim 4, characterized in that the mounting plate (1) is detachable by means of fixing bolts (5) and crash strips (4).
6. The anti-collision structure for unmanned aerial vehicle flight according to claim 1, characterized in that the through slots (3) are uniformly distributed along the central axis of the mounting plate (1), and six groups of the mounting plate (1) are provided.
7. An anti-collision structure for unmanned aerial vehicle flight according to claim 1, characterized in that the regulation and control grooves (402) are distributed in an array along the inside of the anti-collision strip (4), and four groups of regulation and control grooves (402) are provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222207793.7U CN217893246U (en) | 2022-08-22 | 2022-08-22 | A crashproof structure for unmanned aerial vehicle flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222207793.7U CN217893246U (en) | 2022-08-22 | 2022-08-22 | A crashproof structure for unmanned aerial vehicle flight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217893246U true CN217893246U (en) | 2022-11-25 |
Family
ID=84142724
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222207793.7U Active CN217893246U (en) | 2022-08-22 | 2022-08-22 | A crashproof structure for unmanned aerial vehicle flight |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217893246U (en) |
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2022
- 2022-08-22 CN CN202222207793.7U patent/CN217893246U/en active Active
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