CN208453236U - Line defct inspection device - Google Patents
Line defct inspection device Download PDFInfo
- Publication number
- CN208453236U CN208453236U CN201820428988.5U CN201820428988U CN208453236U CN 208453236 U CN208453236 U CN 208453236U CN 201820428988 U CN201820428988 U CN 201820428988U CN 208453236 U CN208453236 U CN 208453236U
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- CN
- China
- Prior art keywords
- column
- chamber
- unmanned plane
- bottom end
- main body
- 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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Abstract
The utility model discloses line defct inspection devices, including unmanned plane main body and the video camera being mounted at unmanned plane bottom part body center, four corners below the unmanned plane main body are respectively and fixedly provided with third column, the second column is provided with below the third column, second chamber is provided in second column, the inner roof wall of the second chamber is provided with the second through hole corresponding with third column bottom end, the bottom end of the third column extends through the second through hole and into second chamber, the downside of the third column antetheca is arranged symmetrically, and there are two second gears.In the utility model, unmanned plane main body can drop to inclined ground, it is now in inner sidewall slide downward of the third column in the second through hole of shorter side, to guarantee the landing of unmanned plane main body so that stationarity, guarantee the case where shooting route of function short distance of camera shooting, the damping of setting can reduce vibration whole when landing, be worth promoting.
Description
Technical field
The utility model relates to line data-logging engineering device technique field more particularly to line defct inspection devices.
Background technique
As unmanned plane is in the application of power industry, unmanned plane is applied to electric power transmission line inspection, defect elimination, not by landform
Landforms limitation is particularly suitable for dangerously steep mountain area, the line walking under more river morphologies, defect elimination work.Relative to traditional manual inspection,
UAV Intelligent inspection reduces a large amount of human and material resources, effectively increases working efficiency, and improves patrol officer's work
Safety coefficient.
But unmanned plane, in the dangerously steep area inspection route such as remote, thickly forested mountains, unmanned plane needs to shoot clear close to route
Clear picture, when existing unmanned plane drops to dangerously steep area, since the support foot hight of ground inclination and unmanned plane is the same,
Unmanned plane is easy to happen rollover, and violent vibration can occur for the moment landed, and influence whole stationarity.
Utility model content
When dropping to dangerously steep area purpose of the utility model is to solve existing unmanned plane, due to ground inclination
And the support foot hight of unmanned plane is the same, and unmanned plane is easy to happen rollover, and violent vibration, shadow can occur for the moment landed
The problem of ringing entirety stationarity, and the line defct inspection device proposed.
To achieve the goals above, the utility model adopts the technical scheme that
Line defct inspection device, including unmanned plane main body and the video camera that is mounted at unmanned plane bottom part body center,
Four corners below the unmanned plane main body are respectively and fixedly provided with third column, and it is vertical that second is provided with below the third column
Column is provided with second chamber in second column, and the inner roof wall of the second chamber is provided with corresponding with third column bottom end
The second through hole, the bottom end of the third column is through the second through hole and extends into second chamber, the third column
The downside of antetheca is symmetrical arranged there are two second gear, central axis and third the column rotation connection of the second gear, described
The inner sidewall of second chamber is provided with the second tooth socket corresponding with second gear, and it is vertical that first is provided with below second column
Column is provided with first chamber in first column, and the inner roof wall of the first chamber is provided with corresponding with the second column bottom end
The first through hole, the bottom end of second column is through the first through hole and extends into first chamber, second column
The downside of antetheca is symmetrical arranged there are two first gear, the central axis of the first gear and the rotation connection of the second column, described
The inner sidewall of first chamber is provided with the first tooth socket corresponding with first gear, is provided in the first chamber and the second column
Corresponding damping.
Preferably, the damping includes partition, and the bottom end of second column is fixedly connected with partition, the partition
It is slidably connected with the inner sidewall of first chamber, multiple damping springs is connected between the partition and the inner bottom wall of first chamber.
Preferably, the two sides of the partition are provided with sliding block, and the inner sidewall of the first chamber is provided with and sliding block pair
The sliding slot answered.
Preferably, the bottom end of first column is pasted with non-slip mat.
Preferably, the inner sidewall sealing of the third column and the second through hole is slidably connected.
Preferably, the inner sidewall sealing of second column and the first through hole is slidably connected.
In the utility model, unmanned plane main body can drop to inclined ground, and the third for being now in shorter side is vertical
Column guarantees camera shooting function to guarantee that unmanned plane main body is landed so that stationarity in the inner sidewall slide downward of the second through hole
The case where shooting route of short distance, the damping of setting can reduce vibration whole when landing, be worth promoting.
Detailed description of the invention
Fig. 1 be the utility model proposes line defct inspection device structural schematic diagram；
Fig. 2 be the utility model proposes line defct inspection device in structural schematic diagram at A.
In figure: 1 unmanned plane main body, 2 second through holes, 3 third columns, 4 first through holes, 5 first columns, 6 sliding blocks, 7
Sliding slot, 8 second chambers, 9 second columns, 10 first chambers, 11 first gears, 12 first tooth sockets, 13 partitions, 14 damping springs,
15 non-slip mats, 16 video cameras, 17 second gears, 18 second tooth sockets.
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, line defct inspection device, including unmanned plane main body 1 and it is mounted on 1 bottom centre of unmanned plane main body
The video camera 16 at place, four corners of 1 lower section of unmanned plane main body are respectively and fixedly provided with third column 3, the lower section setting of third column 3
There is the second column 9, second chamber 8 is provided in the second column 9, the inner roof wall of second chamber 8 is provided with and 3 bottom end of third column
The bottom end of corresponding second through hole 2, third column 3 extends through the second through hole 2 and into second chamber 8, third column 3
The downside of antetheca is symmetrical arranged there are two second gear 17, and the central axis and third column 3 of second gear 17 are rotatablely connected, and second
The inner sidewall of chamber 8 is provided with second tooth socket 18 corresponding with second gear 17, and the lower section of the second column 9 is provided with the first column
5, first chamber 10 is provided in the first column 5, and the inner roof wall of first chamber 10 is provided with corresponding with 9 bottom end of the second column
The bottom end of pass through aperture 4, the second column 9 extends through the first through hole 4 and into first chamber 10,9 antetheca of the second column
Downside is symmetrical arranged there are two first gear 11, and the central axis of first gear 11 and the second column 9 are rotatablely connected, first chamber 10
Inner sidewall be provided with first tooth socket 12 corresponding with first gear 11, be provided in first chamber 10 corresponding with the second column 9
Damping.
In the utility model, damping includes partition 13, and the bottom end of the second column 9 is fixedly connected with partition 13, partition
13 are slidably connected with the inner sidewall of first chamber 10, and multiple damping bullets are connected between partition 13 and the inner bottom wall of first chamber 10
Spring 14, can reduce vibration whole when landing, and the two sides of partition 13 are provided with sliding block 6, the inner sidewall setting of first chamber 10
There is sliding slot 7 corresponding with sliding block 6, prevent partition 13 from shaking in first chamber 10, guarantees that partition 13 slides in the vertical direction,
The bottom end of first column 5 is pasted with non-slip mat 15, improves the skid resistance of 5 bottom end of the first column, third column 3 and the second through hole
2 inner sidewall sealing is slidably connected, and prevents sundries from entering the by the gap of 2 junction of third column 3 and the second through hole
In two chambers 8, the inner sidewall sealing of the second column 9 and the first through hole 4 is slidably connected, prevent sundries by the second column 9 with
The gap of first through hole, 4 junction enters in first chamber 10.
In the utility model, when dropping to dangerously steep area, due to ground inclination, third column 3 exists unmanned plane main body 1
The position located in second chamber 8 is also different, the slide downward in the second through hole 2 of the third column 3 in shorter side, if
The first gear 17 set can guarantee that third column 3 slides in the vertical direction, so that unmanned plane main body 1 is in dangerously steep area
It is more steady when landing, enable route at the shooting of 16 short distance of video camera the case where, the second column 9 can run through first
The inner sidewall in hole 4 slides, and the bottom end of the second column 9 is fixed with partition 13, connects between partition 13 and the inner bottom wall of first chamber 10
Multiple damping springs 14 are connected to, vibration whole when landing can be reduced, the first gear 11 of setting can guarantee the second column 9 perpendicular
Histogram upward sliding, the bottom of the first column 5 are pasted with non-slip mat 15, improve the skid resistance of 5 bottom of the first column.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not
It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. line defct inspection device, including unmanned plane main body (1) and it is mounted on the camera shooting of unmanned plane main body (1) bottom center
Machine (16), which is characterized in that four corners below the unmanned plane main body (1) are respectively and fixedly provided with third column (3), and described
It is provided with the second column (9), is provided with second chamber (8) in second column (9), described second below three columns (3)
The inner roof wall of chamber (8) is provided with the second through hole (2) corresponding with third column (3) bottom end, the bottom of the third column (3)
End extends through the second through hole (2) and into second chamber (8), is symmetrically arranged on the downside of third column (3) antetheca
Two second gears (17), the central axis of the second gear (17) and third column (3) are rotatablely connected, the second chamber
(8) inner sidewall is provided with the second tooth socket (18) corresponding with second gear (17), is provided with below second column (9)
First column (5), first column (5) is interior to be provided with first chamber (10), the inner roof wall setting of the first chamber (10)
There is the first through hole (4) corresponding with the second column (9) bottom end, the first through hole (4) are run through in the bottom end of second column (9)
And extend into first chamber (10), the downside of the second column (9) antetheca is arranged symmetrically, and there are two first gear (11), institutes
State first gear (11) central axis and the second column (9) be rotatablely connected, the inner sidewall of the first chamber (10) be provided with
Corresponding first tooth socket (12) of first gear (11), the first chamber (10) is interior to be provided with subtract corresponding with the second column (9)
Shake mechanism.
2. line defct inspection device according to claim 1, which is characterized in that the damping includes partition
(13), the bottom end of second column (9) is fixedly connected with partition (13), the inside of the partition (13) and first chamber (10)
Wall is slidably connected, and is connected with multiple damping springs (14) between the partition (13) and the inner bottom wall of first chamber (10).
3. line defct inspection device according to claim 2, which is characterized in that the two sides of the partition (13) are respectively provided with
Have sliding block (6), the inner sidewall of the first chamber (10) is provided with sliding slot (7) corresponding with sliding block (6).
4. line defct inspection device according to claim 1, which is characterized in that the bottom end of first column (5) is viscous
Post non-slip mat (15).
5. line defct inspection device according to claim 1, which is characterized in that the third column (3) is passed through with second
The inner sidewall sealing of perforation (2) is slidably connected.
6. line defct inspection device according to claim 1, which is characterized in that second column (9) is passed through with first
The inner sidewall sealing of perforation (4) is slidably connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820428988.5U CN208453236U (en) | 2018-03-28 | 2018-03-28 | Line defct inspection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820428988.5U CN208453236U (en) | 2018-03-28 | 2018-03-28 | Line defct inspection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208453236U true CN208453236U (en) | 2019-02-01 |
Family
ID=65156739
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820428988.5U Expired - Fee Related CN208453236U (en) | 2018-03-28 | 2018-03-28 | Line defct inspection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208453236U (en) |
-
2018
- 2018-03-28 CN CN201820428988.5U patent/CN208453236U/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: 20190201 |