CN208102318U - A kind of unmanned plane shock bracket - Google Patents
A kind of unmanned plane shock bracket Download PDFInfo
- Publication number
- CN208102318U CN208102318U CN201820490290.6U CN201820490290U CN208102318U CN 208102318 U CN208102318 U CN 208102318U CN 201820490290 U CN201820490290 U CN 201820490290U CN 208102318 U CN208102318 U CN 208102318U
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- China
- Prior art keywords
- annular slab
- unmanned plane
- sliding block
- screw rod
- connecting rod
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- 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.)
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Abstract
The utility model relates to damping device technology field, especially a kind of unmanned plane shock bracket, including annular slab and multiple connecting rods, multiple connecting rod upper ends pass through the different location that splicer is separately mounted to unmanned plane lower end, the connecting rod lower end is fixedly connected with sliding block, the sliding block side is provided with the through-hole through sliding block, the annular slab upper surface is provided with multiple U-shaped boards, the U-shaped board side is provided with the screw rod through U-shaped board, the through-hole of the sliding block is set on screw rod, and the diameter of through-hole is greater than the diameter of screw rod, reset spring is arranged on screw rod between the sliding block and U-shaped board, the annular slab lower end is fixedly connected with multiple shock structures.The utility model is provided with Multistage damping mechanism good damping effect, and structure is simple, handsome in appearance.
Description
Technical field
The utility model relates to damping device technology field more particularly to a kind of unmanned plane shock brackets.
Background technique
With the development of modernization science and technology, the purposes of unmanned plane is also more and more extensive, such as in war, agricultural is industrial, with
And daily entertainment can all touch unmanned plane, due to unmanned plane in landing because own wt and sinking speed adjust fault because
Element can collide or drop to ground with ground and bounce, the precise electronic that the judder of foot prop will lead to and its carry
Equipment breaks down, thus the buffering and damping device landed are particularly important.
Utility model content
Purpose of the utility model is to solve disadvantage existing in the prior art, and a kind of unmanned plane proposed is with subtracting
Shake bracket.
To achieve the goals above, the utility model uses following technical solution：
Design a kind of unmanned plane shock bracket, including annular slab and multiple connecting rods, multiple connecting rod upper ends are equal
The different location of unmanned plane lower end is separately mounted to by splicer, the connecting rod lower end is fixedly connected with sliding block, the cunning
Block side is provided with the through-hole through sliding block, and the annular slab upper surface is provided with multiple U-shaped boards, and multiple U-shaped boards are uniformly pacified
Mounted in the upper surface of annular slab, the U-shaped board side is provided with the screw rod through U-shaped board, and the other end of screw rod extend to it is U-shaped
The through-hole of the plate other side, the sliding block is set on screw rod, and the diameter of through-hole be greater than screw rod diameter, the sliding block with it is U-shaped
Reset spring is arranged on screw rod between plate, the annular slab lower end is fixedly connected with multiple shock structures.
Preferably, the annular slab is internally provided with cavity.
Preferably, the annular slab outer surface is coated with one layer of anti-corrosion layer, and anti-corrosion layer is specially zinc coat.
Preferably, the shock structure includes the connecting rod and casing being mounted on annular slab, and the shaft portion plugs
In casing, described sleeve pipe inner upper end two sides are fixedly installed limited block, outside the connecting rod between described sleeve pipe and annular slab also
It is arranged with damping spring, bottom is additionally provided with damping magnet in the connecting rod lower end and casing, and two damping magnet are
Peer's setting.
Preferably, described sleeve pipe exterior bottom is provided with pressure-reducing pad.
The utility model proposes a kind of unmanned plane shock bracket, beneficial effect is：The unmanned plane shock bracket
Provided with Multistage damping buffer unit, connecting rod, sliding block, reset spring, the setting of U-shaped board and sliding block makes unmanned plane land
When sliding block can be made to move on screw rod, to achieve the effect that damping, buffering, damping spring, casing, connecting rod and damping magnetic
Two damping magnet that unmanned plane is arranged in landing in the setting of iron are because opposite reason at the same level, mutually exclusive, to arrive
Up to the effect of damping, buffering, pressure-reducing pad can make unmanned plane reduce impact force in descent to the feedback of rack.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of unmanned plane shock bracket structural schematic diagram.
Fig. 2 be the utility model proposes a kind of unmanned plane shock bracket top view.
In figure：Damping magnet 1, annular slab 3, unmanned plane 4, through-hole 5, connecting rod 6, sliding block 7, reset spring 8, connects casing 2
Bar 9, U-shaped board 10, screw rod 11, pressure-reducing pad 12, damping spring 13, splicer 14, cavity 15, limited block 16, shock structure 17.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
Referring to Fig.1-2, including annular slab 3 and multiple connecting rods 6, multiple 6 upper ends of connecting rod pass through splicer 14 and distinguish
It is mounted on the different location of 4 lower end of unmanned plane, 6 lower end of connecting rod is fixedly connected with sliding block 7, and 7 side of sliding block is provided with through cunning
The through-hole 5 of block 7,3 upper surface of annular slab is provided with multiple U-shaped boards 10, and multiple U-shaped boards 10 are uniformly mounted on the upper of annular slab 3
Surface, 10 side of U-shaped board are provided with the screw rod 11 through U-shaped board 10, and to extend to U-shaped board 10 another for the other end of screw rod 11
The through-hole 5 of side, sliding block 7 is set on screw rod 11, and the diameter of through-hole 5 is greater than the diameter of screw rod 11, sliding block 7 and U-shaped board 10 it
Between screw rod 11 on be arranged with reset spring 8,3 lower end of annular slab is fixedly connected with multiple shock structures 17, when unmanned plane lands
The impact force of generation is transmitted to by the way that in connecting rod 6, connecting rod 6 pushes sliding block 7 to move on screw rod 11, passes through reset spring 8
Sliding block 7 is limited and buffered, to reach the cushioning effect to unmanned plane.
Annular slab 3 is internally provided with cavity 15, can make the weight saving of annular slab 3, to reduce the pressure of unmanned plane.
3 outer surface of annular slab is coated with one layer of anti-corrosion layer, and anti-corrosion layer is specially zinc coat, prevents corrosivity in air
Substance corrodes annular slab 3.
Shock structure includes the connecting rod 9 and casing 2 being mounted on annular slab 3, and 9 part of connecting rod is plugged in casing 2, set
2 inner upper end two sides of pipe are fixedly installed limited block 16, and damping spring is also arranged with outside the connecting rod 9 between casing 2 and annular slab 3
13, bottom is additionally provided with damping magnet 1 in 9 lower end of connecting rod and casing 2, and two damping magnet 1 are setting at the same level, connecting rod
9 move in casing 2, and stretching for cooperation damping spring 13 can make unmanned plane achieve the effect that damping, buffering, damping magnet 1
Setting make unmanned plane two damping magnet 1 be because opposite reason at the same level, mutually exclusive in landing, so that it is slow to reach damping
The effect of punching, 2 exterior bottom of casing are provided with pressure-reducing pad 12, can play the effect of pressure-reducing cushioning.
More than, the only preferable specific embodiment of the utility model, but the protection scope of the utility model is not limited to
In this, anyone skilled in the art within the technical scope disclosed by the utility model, according to the utility model
Technical solution and its utility model design be subject to equivalent substitution or change, should all cover the protection scope of the utility model it
It is interior.
Claims (5)
1. a kind of unmanned plane shock bracket, including annular slab (3) and multiple connecting rods (6), which is characterized in that multiple companies
Extension bar (6) upper end passes through the different location that splicer (14) is separately mounted to unmanned plane (4) lower end, under the connecting rod (6)
End is fixedly connected with sliding block (7), and sliding block (7) side is provided with the through-hole (5) through sliding block (7), on the annular slab (3)
Surface is provided with multiple U-shaped boards (10), and multiple U-shaped boards (10) are uniformly mounted on the upper surface of annular slab (3), the U-shaped board
(10) side is provided with the screw rod (11) through U-shaped board (10), and to extend to U-shaped board (10) another for the other end of screw rod (11)
The through-hole (5) of side, the sliding block (7) is set on screw rod (11), and the diameter of through-hole (5) is greater than the diameter of screw rod (11), institute
It states and is arranged with reset spring (8) on the screw rod (11) between sliding block (7) and U-shaped board (10), annular slab (3) lower end is fixed
It is connected with multiple shock structures (17).
2. a kind of unmanned plane shock bracket according to claim 1, which is characterized in that opened inside the annular slab (3)
Equipped with cavity (15).
3. a kind of unmanned plane shock bracket according to claim 1, which is characterized in that annular slab (3) outer surface
It is coated with one layer of anti-corrosion layer, and anti-corrosion layer is specially zinc coat.
4. a kind of unmanned plane shock bracket according to claim 1, which is characterized in that the shock structure (17) includes peace
Connecting rod (9) and casing (2) on annular slab (3), and the connecting rod (9) is partially plugged in casing (2), described sleeve pipe
(2) inner upper end two sides are fixedly installed limited block (16), and the connecting rod (9) between described sleeve pipe (2) and annular slab (3) also covers outside
Equipped with damping spring (13), connecting rod (9) lower end and casing (2) interior bottom are additionally provided with damping magnet (1), and two
Damping magnet (1) is setting at the same level.
5. a kind of unmanned plane shock bracket according to claim 4, which is characterized in that described sleeve pipe (2) exterior bottom
It is provided with pressure-reducing pad (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820490290.6U CN208102318U (en) | 2018-04-09 | 2018-04-09 | A kind of unmanned plane shock bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820490290.6U CN208102318U (en) | 2018-04-09 | 2018-04-09 | A kind of unmanned plane shock bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208102318U true CN208102318U (en) | 2018-11-16 |
Family
ID=64120953
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820490290.6U Active CN208102318U (en) | 2018-04-09 | 2018-04-09 | A kind of unmanned plane shock bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208102318U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109377828A (en) * | 2018-12-12 | 2019-02-22 | 济宁职业技术学院 | Hygiene educational aid case before a kind of multi-functional |
| CN110217382A (en) * | 2019-06-28 | 2019-09-10 | 南京工业职业技术学院 | A kind of unmanned plane damping undercarriage |
| CN111075639A (en) * | 2019-12-31 | 2020-04-28 | 华北电力大学（保定） | Wind power generation device with flexible telescopic fan blades |
| WO2021168744A1 (en) * | 2020-02-27 | 2021-09-02 | 南京唐壹信息科技有限公司 | Unmanned aerial vehicle for transporting materials |
-
2018
- 2018-04-09 CN CN201820490290.6U patent/CN208102318U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109377828A (en) * | 2018-12-12 | 2019-02-22 | 济宁职业技术学院 | Hygiene educational aid case before a kind of multi-functional |
| CN110217382A (en) * | 2019-06-28 | 2019-09-10 | 南京工业职业技术学院 | A kind of unmanned plane damping undercarriage |
| CN111075639A (en) * | 2019-12-31 | 2020-04-28 | 华北电力大学（保定） | Wind power generation device with flexible telescopic fan blades |
| CN111075639B (en) * | 2019-12-31 | 2020-12-29 | 华北电力大学（保定） | Wind power generation device with flexible telescopic fan blades |
| WO2021168744A1 (en) * | 2020-02-27 | 2021-09-02 | 南京唐壹信息科技有限公司 | Unmanned aerial vehicle for transporting materials |
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