CN205971880U - Cloud platform rapid disassembly structure - Google Patents
Cloud platform rapid disassembly structure Download PDFInfo
- Publication number
- CN205971880U CN205971880U CN201620903844.1U CN201620903844U CN205971880U CN 205971880 U CN205971880 U CN 205971880U CN 201620903844 U CN201620903844 U CN 201620903844U CN 205971880 U CN205971880 U CN 205971880U
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- CN
- China
- Prior art keywords
- guide rail
- head
- sliding chute
- slide block
- rail sliding
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Abstract
The utility model discloses a cloud platform rapid disassembly structure, including cloud platform, carbon fiber carry board and diplopore connection piece, carbon fiber carry board has guide rail chute, and guide rail chute one end is equipped with the baffle, is equipped with T type guide rail in the guide rail chute, is equipped with the slider in the T type guide rail, one side of guide rail chute and slider all is equipped with the screw, and guide rail chute, slider and diplopore connection piece pass through the screw and the screw is connected, and the slider has the shock attenuation upper cover plate, and the shock attenuation upper cover plate has a plurality of rubber shock absorber balls, and the rubber shock absorber ball has to be lapped under the shock attenuation, the cloud platform sets up apron below under the shock attenuation, should fixed mode dismantle with the installation all fairly simplely to can realize accurate location, ensure that shooting equipment can stabilize to connect to establish and avoid the landing, thereby provide work efficiency.
Description
Technical field
This utility model is related to vehicle technology field, particularly to a kind of head quick-disassembly structure.
Background technology
Existing a lot of head by the way of pipe clamp is fixing by head carry on carbon fibre carbon pipe, head will first pass through and subtract
Shake structure is fixed with pipe clamp, then passes through pipe clamp by head carry on the carbon fiber pipe being fixed on below aircraft, or head
Fix with carbon fiber pipe, then carbon fiber pipe carry is fixed on the pipe clamp below aircraft.The dismounting of this fixed form and installation
All more complicated, and precise positioning cannot be realized.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of head quick-disassembly structure, to solve to lead in prior art
The above-mentioned multinomial defect causing.
For achieving the above object, this utility model provides following technical scheme：A kind of head quick-disassembly structure, including cloud
Platform, carbon fiber carry plate and diplopore connection sheet, described carbon fiber carry plate has guide rail sliding chute, and guide rail sliding chute one end is provided with gear
Plate, is provided with T-shaped guide rail in guide rail sliding chute, be provided with slide block in T-shaped guide rail, and the side of described guide rail sliding chute and slide block is equipped with spiral shell
Hole, guide rail sliding chute, slide block and diplopore connection sheet pass through screw and screw connects, and slide block has damping upper cover plate, and damping is covered
Plate has some rubber shock-absorbing balls, and rubber shock-absorbing ball has damping lower cover, and described head is arranged under damping lower cover
Side.
Preferably, described guide rail sliding chute is arranged on the middle position of carbon fiber carry plate.
Preferably, described guide rail sliding chute both sides and carbon fiber carry plate relevant position are provided with connecting screw hole one, guide rail sliding chute
Both sides and carbon fiber carry plate pass through screw connection.
Preferably, on described lower vibration damper plate and head relevant position is provided with connecting screw hole two, and lower vibration damper plate leads to head
Cross screw connection.
Preferably, on described upper vibration damper plate and slide block relevant position is provided with connecting screw hole three, and upper vibration damper plate leads to slide block
Cross screw connection.
Preferably, described slide block is I shape.
Beneficial effect using above technical scheme is：A kind of head quick-disassembly structure of this utility model structure, in head
Upper installation quick-disassembly structure so that head can quick-detach and installation soon, minimizing the unmanned plane capture apparatus integral installation time, and by
The positioning of detent mechanism is it is ensured that capture apparatus can consolidate to connect sets and avoid landing, thus providing work efficiency.
Brief description
Fig. 1 is structural representation of the present utility model.
Wherein, 1- head, 2- carbon fiber carry plate, 3- diplopore connection sheet, 4- guide rail sliding chute, 5- baffle plate, 6-T type guide rail,
7- slide block, 8- screw, 9- damping upper cover plate, 10- rubber shock-absorbing ball, 11- damping lower cover, 12- connecting screw hole one, 13- connects
Screw two, 14- connecting screw hole three.
Specific embodiment
Describe preferred implementation of the present utility model below in conjunction with the accompanying drawings in detail.
Fig. 1 shows specific embodiment of the present utility model：A kind of head 1 quick-disassembly structure, hangs including head 1, carbon fiber
Support plate 2 and diplopore connection sheet 3, described carbon fiber carry plate 2 has guide rail sliding chute 4, and guide rail sliding chute 4 one end is provided with baffle plate 5, leads
It is provided with T-shaped guide rail 6 in rail chute 4, in T-shaped guide rail 6, is provided with slide block 7, the side of described guide rail sliding chute 4 and slide block 7 is equipped with spiral shell
Hole 8, guide rail sliding chute 4, slide block 7 and diplopore connection sheet 3 pass through screw and screw 8 connects, and slide block 7 has damping upper cover plate 9, subtracts
Shake upper cover plate 9 has some rubber shock-absorbing balls 10, and rubber shock-absorbing ball 10 has damping lower cover 11, and described head 1 is arranged
Below damping lower cover 11.
Guide rail sliding chute 4 is fixed on the middle position of carbon fiber carry plate 2, and carbon fiber carry plate 2 is fixed on unmanned plane body
Center, slide block 7 is arranged in guide rail sliding chute 4 along T-shaped guide rail 6, and when slide block 7 encounters baffle plate 5, slide block 7 is completely into guide rail
In chute 4, then with screw, diplopore connection sheet 3, slide block 7 and guide rail sliding chute 4 are fastenedly connected, make slide block 7 be fixed on guide rail sliding chute 4
Interior it is ensured that being not fall off when flight, damping upper cover plate 9, rubber shock-absorbing ball 10, damping lower cover are installed under slide block 7
11, guarantee the stability of head 1 when flight, more preferable protective effect is played to head 1.
In the present embodiment, described guide rail sliding chute 4 is arranged on the middle position of carbon fiber carry plate 2 it is ensured that head 1 entirety
Stability.
In the present embodiment, described guide rail sliding chute 4 both sides and carbon fiber carry plate 2 relevant position are provided with connecting screw hole 1,
Guide rail sliding chute 4 both sides and carbon fiber carry plate 2 pass through screw connection, and guide rail sliding chute 4 and carbon fiber carry plate 2 are fastenedly connected
Together it is ensured that safety and stability during flight.
In the present embodiment, on described lower vibration damper plate and head 1 relevant position be provided with connecting screw hole 2 13, on lower vibration damper plate and
Head 1 passes through screw connection, lower vibration damper plate and head 1 is fastened together it is ensured that safety and stability during flight.
In the present embodiment, on described upper vibration damper plate and slide block 7 relevant position be provided with connecting screw hole 3 14, on upper vibration damper plate and
Slide block 7 passes through screw connection.
In the present embodiment, described slide block 7 is I shape.
Based on above-mentioned：A kind of head 1 quick-disassembly structure of this utility model structure, on head 1 install quick-disassembly structure so that
Head 1 can quick-detach and installation soon, reduce the unmanned plane capture apparatus integral installation time, and the positioning by detent mechanism, really
Protect capture apparatus and can consolidate to connect and set and avoid landing, thus providing work efficiency.
Above-described is only preferred implementation of the present utility model it is noted that ordinary skill for this area
For personnel, on the premise of creating design without departing from this utility model, some deformation can also be made and improve, these all belong to
In protection domain of the present utility model.
Claims (6)
1. a kind of head quick-disassembly structure, including head, carbon fiber carry plate and diplopore connection sheet it is characterised in that：Described carbon is fine
Dimension carry plate has guide rail sliding chute, and guide rail sliding chute one end is provided with baffle plate, is provided with T-shaped guide rail, sets in T-shaped guide rail in guide rail sliding chute
Have slide block, the side of described guide rail sliding chute and slide block is equipped with screw, guide rail sliding chute, slide block and diplopore connection sheet pass through screw and
Screw connects, and slide block has damping upper cover plate, and damping upper cover plate has some rubber shock-absorbing balls, and rubber shock-absorbing ball has
Damping lower cover, described head is arranged on below damping lower cover.
2. a kind of head quick-disassembly structure according to claim 1 it is characterised in that：Described guide rail sliding chute is arranged on carbon fiber
The middle position of carry plate.
3. a kind of head quick-disassembly structure according to claim 1 it is characterised in that：Described guide rail sliding chute both sides and carbon fiber
Carry plate relevant position is provided with connecting screw hole one, and guide rail sliding chute both sides and carbon fiber carry plate pass through screw connection.
4. a kind of head quick-disassembly structure according to claim 1 it is characterised in that：With head phase on described damping lower cover
Answer position to be provided with connecting screw hole two, damping lower cover passes through screw connection with head.
5. a kind of head quick-disassembly structure according to claim 1 it is characterised in that：With slide block phase on described damping upper cover plate
Answer position to be provided with connecting screw hole three, damping upper cover plate passes through screw connection with slide block.
6. a kind of head quick-disassembly structure according to claim 1 it is characterised in that：Described slide block is I shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620903844.1U CN205971880U (en) | 2016-08-19 | 2016-08-19 | Cloud platform rapid disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620903844.1U CN205971880U (en) | 2016-08-19 | 2016-08-19 | Cloud platform rapid disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971880U true CN205971880U (en) | 2017-02-22 |
Family
ID=58032326
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620903844.1U Active CN205971880U (en) | 2016-08-19 | 2016-08-19 | Cloud platform rapid disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205971880U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892126A (en) * | 2017-03-13 | 2017-06-27 | 广州鼎飞航空科技有限公司 | A kind of unmanned aerial vehicle onboard disassembly and assembly structure and unmanned plane |
| CN110439240A (en) * | 2019-07-31 | 2019-11-12 | 广东博智林机器人有限公司 | The Quick Connect Kit of floating device |
-
2016
- 2016-08-19 CN CN201620903844.1U patent/CN205971880U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892126A (en) * | 2017-03-13 | 2017-06-27 | 广州鼎飞航空科技有限公司 | A kind of unmanned aerial vehicle onboard disassembly and assembly structure and unmanned plane |
| CN110439240A (en) * | 2019-07-31 | 2019-11-12 | 广东博智林机器人有限公司 | The Quick Connect Kit of floating device |
| CN110439240B (en) * | 2019-07-31 | 2021-06-04 | 广东博智林机器人有限公司 | Quick connecting device of floating device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |