CN212125510U - Unmanned aerial vehicle protection architecture - Google Patents
Unmanned aerial vehicle protection architecture Download PDFInfo
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- CN212125510U CN212125510U CN201922274753.2U CN201922274753U CN212125510U CN 212125510 U CN212125510 U CN 212125510U CN 201922274753 U CN201922274753 U CN 201922274753U CN 212125510 U CN212125510 U CN 212125510U
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- sliding block
- aerial vehicle
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- machine body
- protection
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Abstract
The utility model discloses an unmanned aerial vehicle protection architecture, include: the unmanned aerial vehicle comprises a machine body, protective supports connected with two sides below the machine body, and machine arms arranged on two sides of the machine body; the anti-collision cover is arranged above the machine body, and an opening of the anti-collision cover is concave to the direction of the machine body; a lateral anti-collision plate disposed on a side wall of the machine body; the first connecting lug is arranged between the two protective brackets; a first connecting rod is arranged between the two sliding blocks and the first connecting lug; a second connecting lug is arranged on the inner side wall of the protective support, a second sliding block is arranged on one side of the first sliding block, and a second connecting rod is arranged between the second connecting lug and the second sliding block; the both sides wall of first sliding block and second sliding block all is provided with blotter, crashproof. It has realized carrying out the omnidirectional protection to unmanned aerial vehicle to can effectual buffering unmanned aerial vehicle descend or the collision that takes place when falling.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle protection architecture.
Background
The unmanned aerial vehicle is an information-based high-tech product, has extremely important functions in civil and military aspects, and has very wide application in civil industries such as city management, agriculture, geology, meteorology, emergency rescue and relief work and the like. At present, also having taken necessary safeguard measure to unmanned aerial vehicle, all will be the biggest efforts protection unmanned aerial vehicle's fuselage when unmanned aerial vehicle descends or breaks down at the in-process of flight, however, present unmanned aerial vehicle protection architecture can not carry out the omnidirectional protection to unmanned aerial vehicle, and collision that can not effectual buffering unmanned aerial vehicle takes place when descending or fall can't satisfy user's requirement.
The small unmanned aerial vehicle is a hot problem of domestic and foreign research in recent years, and is widely applied to the fields of agriculture, exploration, commerce and aerial photography. No matter be unmanned aerial vehicle when running into the barrier and explode the machine, when catching black unmanned aerial vehicle, still when unmanned aerial vehicle takes place the operation trouble, all can lead to unmanned aerial vehicle to fall. Unmanned aerial vehicle's home range generally is in the urban area, its unusual falls, still can give personnel when leading to the fact serious damage to unmanned aerial vehicle itself, the property brings great danger, link unmanned aerial vehicle and protective structure together, therefore, if can propose an unmanned aerial vehicle protective structure, carry out the omnidirectional protection to unmanned aerial vehicle, and can effectual buffering unmanned aerial vehicle descend or the collision that takes place when falling, protection unmanned aerial vehicle avoids damaging, has profound meaning.
SUMMERY OF THE UTILITY MODEL
It is an object of the present invention to solve at least the above problems and to provide at least the advantages which will be described later.
The utility model discloses it is still another purpose to provide an unmanned aerial vehicle protection architecture, realized carrying out the omnidirectional protection to unmanned aerial vehicle to can effectual buffering unmanned aerial vehicle descend or the collision that takes place when falling.
In order to achieve the above and other objects, the present invention adopts the following technical solutions:
an unmanned aerial vehicle protection architecture, comprising:
the unmanned aerial vehicle comprises a machine body, protective supports connected with two sides below the machine body, and machine arms arranged on two sides of the machine body;
the anti-collision cover is arranged above the machine body, and an opening of the anti-collision cover is concave to the direction of the machine body;
a lateral anti-collision plate disposed on a side wall of the machine body;
the first connecting lug is arranged between the two protective brackets, a sliding rod is also arranged between the two protective brackets, and a telescopic spring is arranged on the sliding rod; the outer side part of the telescopic spring is sleeved with two first sliding blocks; a first connecting rod is arranged between the two sliding blocks and the first connecting lug; a second connecting lug is arranged on the inner side wall of the protective support, a second sliding block is arranged on one side of the first sliding block, and a second connecting rod is arranged between the second connecting lug and the second sliding block; two side walls of the first sliding block and the second sliding block are provided with buffer pads for preventing collision; and
a rechargeable battery enclosed within the body.
Preferably, the first sliding block and the second sliding block are separated by a partition plate, the sliding rod is connected with the first sliding block and the second sliding block in a sliding manner, the first connecting rod is connected with the sliding block and the first connecting lug in a rotating manner, and the second connecting rod is connected with the second connecting lug and the second sliding block in a rotating manner.
Preferably, the unmanned aerial vehicle protection architecture, still include:
a bottom guard mechanism including a guard base and a first compression spring; the first compression spring is located at the connecting end of the machine body and the protection support and located inside the protection support, the protection base is located below the protection support, the cross section of the protection base is concave, and the protection support is connected with the protection base in a welded mode.
Preferably, the outside of the horn is provided with a rubber crash pad.
Preferably, the unmanned aerial vehicle protection architecture, still include:
the two piston rods are symmetrically arranged below the anti-collision cover; the piston rod is positioned in the movable sleeve, a second compression spring is arranged in the movable sleeve, and the piston rod is fixedly connected with the second compression spring; the piston rod is connected with the movable sleeve in a sliding mode, and one end of the piston rod penetrates through the movable sleeve and extends into the movable sleeve.
Preferably, the anti-collision cover is fixedly connected with the piston rod, and when the piston rod is subjected to radial pressure of the anti-collision cover, the piston rod downwards compresses the second compression spring along the vertical direction in the movable sleeve.
The utility model discloses at least, include following beneficial effect:
in the unmanned aerial vehicle protection structure of the utility model, the upper part of the machine body is protected by the arranged anti-collision cover, and simultaneously, a second compression spring is arranged between the piston rod and the movable sleeve, thereby improving the anti-seismic efficiency above the machine body, the left and right sides of the unmanned aerial vehicle are provided with the lateral anti-collision plates, and simultaneously, the outer part of the machine arm is also provided with the anti-collision rubber pads in a sealing way, thereby realizing the buffer protection of the left and right sides of the machine body and the machine arm, when the unmanned aerial vehicle descends, the first compression spring arranged at the connecting end of the protective bracket and the machine body firstly performs the buffer action, the concave protective base connected below the protective bracket can continuously perform the buffer action, the second sliding block rotationally connected with the second connecting rod arranged at the inner side wall of the protective bracket extrudes the expansion springs at the two sides on the sliding rod, performs the buffer protection to part of the, the extension spring of first sliding block compression both sides on the slide bar is rotated to the head rod, and the both sides outside of first sliding block and second sliding block has all set up the blotter, and the collision that can effectual buffering unmanned aerial vehicle take place when descending or fall prevents that the striking between the structure is effectual to realized carrying out the omnidirectional protection to unmanned aerial vehicle.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle protection structure provided by the present invention;
fig. 2 is a connection relation diagram of the piston rod and the movable sleeve of the unmanned aerial vehicle protection structure provided by the present invention;
fig. 3 is the utility model provides a structural schematic of unmanned aerial vehicle protection architecture horn.
Detailed Description
The present invention is described in detail below with reference to the attached drawings so that those skilled in the art can implement the invention by referring to the description.
As shown in fig. 1-3, an unmanned aerial vehicle protection architecture includes: unmanned aerial vehicle, its include organism 1, with protective cradle 7 that 1 below both sides of organism are connected, and set up the horn 5 of 1 both sides of organism.
And the anti-collision cover 2 is arranged above the machine body 1, and an opening of the anti-collision cover 2 is concave to the direction of the machine body 1.
And a lateral anti-collision plate 6 disposed on a side wall of the machine body 1.
The first connecting lug 10 is arranged between the two protective brackets 7, a sliding rod 16 is further arranged between the two protective brackets 7, and a telescopic spring is arranged on the sliding rod 16; the outer side part of the telescopic spring is sleeved with two first sliding blocks 15, and the number of the first sliding blocks 15 is two; a first connecting rod 17 is arranged between the two sliding blocks 15 and the first connecting lug 10; a second connecting lug 11 is arranged on the inner side wall of the protective bracket 7, a second sliding block 13 is arranged on one side of the first sliding block 15, and a second connecting rod 12 is arranged between the second connecting lug 11 and the second sliding block 13; two side walls of the first sliding block 15 and the second sliding block 13 are provided with buffer pads 14 for preventing collision; and a rechargeable battery enclosed in the body 1.
In the above scheme, through the setting of anticollision cover, first engaging lug and cushion, it is effectual to prevent the striking between the structure to realized carrying out the omnidirectional protection to unmanned aerial vehicle.
In a preferred embodiment, the first sliding block 15 and the second sliding block 13 are separated by a partition, the sliding rod 16 is slidably connected to both the first sliding block 15 and the second sliding block 13, the first connecting rod 17 is rotatably connected to both the sliding block 15 and the first connecting lug 10, and the second connecting rod 12 is rotatably connected to both the second connecting lug 11 and the second sliding block 13.
In the above scheme, the first connecting lug connected below the machine body is stressed, the first connecting rod rotates, and the first sliding block is driven to compress the telescopic springs on the two sides on the sliding rod.
In a preferred embodiment, the method further comprises: a bottom protection mechanism comprising a protection base 9 and a first compression spring 8; first compression spring 8 is located organism 1 and protective bracket 7's link, and is located protective bracket 7's inside, protection base 9 is located protective bracket 7's below, and protective base 9's cross section is concave type, protective bracket 7 and protective base 9 welded connection.
In the above scheme, when unmanned aerial vehicle descended, the first compression spring that protective bracket and organism link set up at first carries out the cushioning effect, the concave type protection base that protective bracket below was connected can continue to cushion, the second connecting rod that protective bracket inside wall set up rotates the expanding spring that the second sliding block of connecting extrudees both sides on the slide bar, cushion the protection to partly impact force that the descending received, meanwhile, the first connecting ear that organism below is connected receives pressure, the head rod rotates, drive the expanding spring of first sliding block compression both sides on the slide bar simultaneously, first sliding block has all set up the blotter with the both sides outside of second sliding block, can effectual buffering unmanned aerial vehicle at the descending or the collision that takes place when falling.
In a preferred scheme, the outer part of the machine arm 5 is provided with a crash rubber pad 19.
In the scheme, the buffer protection of the left side, the right side and the arm of the machine body is realized.
In a preferred embodiment, the method further comprises: the two piston rods 3 are symmetrically arranged below the anti-collision cover 2; the piston rod 3 is positioned inside the movable sleeve 4, a second compression spring 18 is arranged inside the movable sleeve 4, and the piston rod 3 is fixedly connected with the second compression spring 18; the piston rod 3 is connected with the movable sleeve 4 in a sliding mode, and one end of the piston rod 3 penetrates through the movable sleeve 4 and extends into the movable sleeve 4.
In the above scheme, the anticollision cover protects the top of organism, has set up second compression spring simultaneously between piston rod and movable sleeve, improves the antidetonation efficiency of organism top.
In a preferred scheme, the crash cover 2 is fixedly connected with the piston rod 3, and when the piston rod 3 is subjected to the radial pressure of the crash cover 2, the piston rod 3 compresses the second compression spring 18 downwards along the vertical direction in the movable sleeve 4.
In the above scheme, the piston rod slides more reasonably and quickly along the radial direction of the movable sleeve through the arrangement of the second compression spring.
While the embodiments of the invention have been described above, it is not intended to be limited to the details shown, or described, but rather to cover all modifications, which would come within the scope of the invention, as defined by the claims and the equivalents thereof, and which fall within the limits of the claims and the equivalents thereof.
Claims (6)
1. An unmanned aerial vehicle protection architecture, a serial communication port, include:
the unmanned aerial vehicle comprises a machine body, protective supports connected with two sides below the machine body, and machine arms arranged on two sides of the machine body;
the anti-collision cover is arranged above the machine body, and an opening of the anti-collision cover is concave to the direction of the machine body;
a lateral anti-collision plate disposed on a side wall of the machine body;
the first connecting lug is arranged between the two protective brackets, a sliding rod is also arranged between the two protective brackets, and a telescopic spring is arranged on the sliding rod; the outer side part of the telescopic spring is sleeved with two first sliding blocks; a first connecting rod is arranged between the two sliding blocks and the first connecting lug; a second connecting lug is arranged on the inner side wall of the protective support, a second sliding block is arranged on one side of the first sliding block, and a second connecting rod is arranged between the second connecting lug and the second sliding block; two side walls of the first sliding block and the second sliding block are provided with buffer pads for preventing collision; and
a rechargeable battery enclosed within the body.
2. The unmanned aerial vehicle protection architecture of claim 1, wherein the first sliding block and the second sliding block are separated by a partition, the sliding rod is slidably connected with the first sliding block and the second sliding block, the first connecting rod is rotatably connected with the sliding block and the first connecting lug, and the second connecting rod is rotatably connected with the second connecting lug and the second sliding block.
3. The unmanned aerial vehicle protection architecture of claim 1, further comprising:
a bottom guard mechanism including a guard base and a first compression spring; the first compression spring is located at the connecting end of the machine body and the protection support and located inside the protection support, the protection base is located below the protection support, the cross section of the protection base is concave, and the protection support is connected with the protection base in a welded mode.
4. An unmanned aerial vehicle protection architecture as claimed in claim 1, wherein the outside of the horn is provided with a crash rubber pad.
5. The unmanned aerial vehicle protection architecture of claim 1, further comprising:
the two piston rods are symmetrically arranged below the anti-collision cover; the piston rod is positioned in the movable sleeve, a second compression spring is arranged in the movable sleeve, and the piston rod is fixedly connected with the second compression spring; the piston rod is connected with the movable sleeve in a sliding mode, and one end of the piston rod penetrates through the movable sleeve and extends into the movable sleeve.
6. The unmanned aerial vehicle protection architecture of claim 5, wherein the crash shield is fixedly connected with the piston rod, and when the piston rod is subjected to a radial pressure of the crash shield, the piston rod compresses the second compression spring downwards along a vertical direction in the movable sleeve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922274753.2U CN212125510U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle protection architecture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922274753.2U CN212125510U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle protection architecture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212125510U true CN212125510U (en) | 2020-12-11 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922274753.2U Active CN212125510U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle protection architecture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212125510U (en) |
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2019
- 2019-12-04 CN CN201922274753.2U patent/CN212125510U/en active Active
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