CN205499319U - Big many rotor unmanned aerial vehicle of load horn plug device - Google Patents
Big many rotor unmanned aerial vehicle of load horn plug device Download PDFInfo
- Publication number
- CN205499319U CN205499319U CN201620240830.6U CN201620240830U CN205499319U CN 205499319 U CN205499319 U CN 205499319U CN 201620240830 U CN201620240830 U CN 201620240830U CN 205499319 U CN205499319 U CN 205499319U
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- China
- Prior art keywords
- pipe clamp
- connection clip
- grafting pipe
- unmanned aerial
- grafting
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Abstract
The utility model discloses a big many rotor unmanned aerial vehicle of load horn plug device, including fixed baseplate, inserting connection clip and rotor connecting pipe, fixed baseplate includes movable bed frame and lower fixed bed frame, the connection clip that inserts include and insert connection clip and underthrust connection clip, the rotor connecting pipe is inserted to establish and is being inserted in connection clip inserts connection clip and underthrust connection clip on, it passes through the pipe connector bolt and presss from both sides tight rotor connecting pipe to insert connection clip and underthrust connection clip on, it inserts in the activity of establishing on fixed baseplate bed frame and the fixed bed frame down to insert connection clip, the activity of going up bed frame press from both sides through the base bolt with fixed bed frame down and tightly insert connection clip. The quick dismantlement and the installation of horn of having realized the many rotors of big load, reliable structural design has avoided ordinary plug mechanism to the wearing and tearing of horn and part, has just designed purpose -made circuit connector, and direct plug does not need all to pull out to insert the connecting wire at every turn, has reduced field usage complexity greatly.
Description
Technical field
This utility model relates to unmanned plane field, in particular it relates to a kind of many rotors of heavy－duty without
Man-machine horn plug-in and pull-off device.
Background technology
The most rotor wing unmanned aerial vehicles are mostly integral type structure, and maximum take-off weight is basic
Both less than 20 kilograms, horn structure is divided into overall non-dismountable and folds two ways.For
Bigger oar and wheelbase, the transport of traditional non-dismountable horn is needed to use ratio for heavy－duty
Cumbersome, and the use of fold mechanism can be deteriorated by laser intensity, reliability step-down, particularly across
A period of time folding after there will be diastema, have potential risks to have influence on flying of unmanned plane
Row safety.
Utility model content
For the above-mentioned technical problem solved, this utility model provides a kind of many rotors of heavy－duty unmanned
Machine horn plug-in and pull-off device, the rotor solving existing many rotor wing unmanned aerial vehicles cannot realize dismounting and assemble
Problem.
The technical scheme in the invention for solving the above technical problem is: a kind of many rotations of heavy－duty
Wing unmanned plane horn plug-in and pull-off device, including fixed pedestal, grafting pipe clamp and rotor connecting tube, institute
The fixed pedestal stated includes movable pedestal and lower stationary base mount；Described insertion pipe folder includes
Grafting pipe clamp and lower grafting pipe clamp；Described rotor connecting tube is plugged in the upper insertion pipe of grafting pipe clamp
In folder and lower grafting pipe clamp, described upper grafting pipe clamp and lower grafting pipe clamp are pressed from both sides by pipe connecting bolt
Tight rotor connecting tube；Described grafting pipe clamp is plugged in the upper movable pedestal of fixed pedestal and lower fixing
In pedestal, described upper movable pedestal and lower stationary base mount clamp grafting pipe clamp by foundation bolt.
Further, described fixed pedestal rear end is provided with circuit socket location-plate, described
It is provided with circuit socket on circuit socket location-plate.
Further, described grafting pipe clamp rear end is provided with circuit plug location-plate, described
It is provided with circuit plug on circuit plug location-plate.
Further, described circuit plug coordinates grafting with circuit socket.
Further, described both sides, fixed pedestal front end are respectively arranged with limited impression.
Further, described both sides, grafting pipe clamp front end are respectively arranged with spacing preiection.
Further, described fixed pedestal and grafting pipe clamp match grafting time, described grafting
The spacing preiection of both sides, pipe clamp front end is connected in the limited impression of both sides, fixed pedestal front end.
To sum up, the beneficial effects of the utility model are: the horn achieving the many rotors of heavy－duty is fast
Quick-detach and installation, the design of reliable structure avoids common push-pull structure to horn and part
Abrasion, and devise special terminal, directly plug, it is not necessary to plug connects every time
Line, substantially reduces field usage complexity.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing being further appreciated by this utility model embodiment,
Constitute the part of the application, be not intended that the restriction to this utility model embodiment.At accompanying drawing
In:
Fig. 1 is the 45° angle rear perspective that this utility model fixed pedestal separates with grafting pipe clamp
Structural representation；
Fig. 2 is that the 45° angle forward sight that this utility model fixed pedestal separates with grafting pipe clamp is three-dimensional
Structural representation；
Fig. 3 is this utility model fixed pedestal and the 45° angle rear perspective of grafting pipe clamp grafting
Structural representation；
Fig. 4 is that the 45° angle forward sight of this utility model fixed pedestal and grafting pipe clamp grafting is three-dimensional
Structural representation；
Labelling and corresponding parts title in accompanying drawing:
1-fixed pedestal, 2-grafting pipe clamp, 3-rotor connecting tube, the upper movable pedestal of 4-, 5-
Lower stationary base mount, 6-upper grafting pipe clamp, grafting pipe clamp under 7-, 8-pipe connecting bolt, 9-pedestal spiral shell
Bolt, 10-circuit socket location-plate, 11-circuit socket, 12-circuit plug location-plate, 13-
Circuit plug, 14-limited impression, 15-spacing preiection, 16-Foundation anchor bolts.
Detailed description of the invention
Below in conjunction with embodiment, the utility model is described in further detail, but this practicality
Novel embodiment is not limited to this.
Embodiment 1
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug-in and pull-off device as Figure 1-4, including fixed base
Seat 1, grafting pipe clamp 2 and rotor connecting tube 3, fixed pedestal 1 includes movable pedestal 4 He
Lower stationary base mount 5；Grafting pipe clamp 2 includes grafting pipe clamp 6 and lower grafting pipe clamp 7；Rotor
Connecting tube 3 is plugged in upper grafting pipe clamp 6 and the lower grafting pipe clamp 7 of grafting pipe clamp 2, described
Upper grafting pipe clamp 6 and lower grafting pipe clamp 7 clamp rotor connecting tube 3 by pipe connecting bolt 8；
Grafting pipe clamp 2 is plugged in upper movable pedestal 4 and the lower stationary base mount 5 of fixed pedestal 1, institute
Upper movable pedestal 4 and the lower stationary base mount 5 stated clamp grafting pipe clamp 2 by foundation bolt 9.
Unmanned plane horn plug-in and pull-off device uses aircraft aluminum matter entirety to manufacture, light weight, it is adaptable to carry greatly
Weight unmanned plane horn system, quick and easy for installation, structural safety is reliable, and the life-span is long.
During use, fixed pedestal 1 is fixed on unmanned aerial vehicle body by Foundation anchor bolts 16, rotor
It is connected with rotor connecting tube 3, then, is plugged in the upper of fixed pedestal 1 by grafting pipe clamp 2
In movable pedestal 4 and lower stationary base mount 5, then clamp grafting pipe clamp 2 by foundation bolt 9；
Realize rotor to be connected with unmanned aerial vehicle body, when needing to dismantle rotor, only need to unclamp foundation bolt 9,
Grafting pipe clamp 2 just can directly be extracted in fixed pedestal 1.Whole plug-in system only need to dismantle base
Seat bolt 9 just can depart from grafting pipe clamp 2.
Embodiment 2
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug-in and pull-off device as Figure 1-4, is implementing
On the basis of example 1, fixed pedestal 1 rear end is provided with circuit socket location-plate 10, and circuit is inserted
Mouth location-plate 10 is bolted on fixed pedestal 1 rear end, on circuit socket location-plate 10
It is provided with circuit socket 11.Grafting pipe clamp 2 rear end is provided with circuit plug location-plate 12, electricity
Road plug location-plate 12 is bolted on grafting pipe clamp 2 rear end, circuit plug location-plate
Circuit plug 13 it is provided with on 12.Circuit plug 13 coordinates grafting with circuit socket 11.If
Count special terminal, directly plugged, it is not necessary to plug connecting line every time, significantly subtracted
Little field usage complexity.
Embodiment 3
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug-in and pull-off device as Figure 1-4, is implementing
On the basis of example 1, both sides, fixed pedestal 1 front end are respectively arranged with limited impression 14.Grafting
Both sides, pipe clamp 2 front end are respectively arranged with spacing preiection 15.Fixed pedestal 1 and grafting pipe clamp 2
Match grafting time, the spacing preiection 15 of both sides, grafting pipe clamp 2 front end is connected to fixed pedestal
In the limited impression 14 of 1 both sides, front end.
Grafting pipe clamp 2 is connected with fixed pedestal 1 concentric, plays the role of positioning at moving direction,
The spacing preiection 15 that both sides, grafting pipe clamp 2 front end are arranged limits direction and positioning action, makes
Obtaining the grafting pipe clamp 2 smooth and easy insertion fixed pedestal 1 of energy, fixed pedestal 1 and grafting pipe clamp use two
Individual foundation bolt 9 tightens up fixing, it is ensured that grafting pipe clamp 2 is accurately fixed on fixed pedestal 1,
Circuit plug 13 can be accurately positioned at inside circuit socket 11 simultaneously, because of foundation bolt 9
Effect so that whole grafting pipe clamp 2 not play inside fixed pedestal 1.
The above, be only preferred embodiment of the present utility model, not new to this practicality
Any pro forma restriction made by type, according to technical spirit of the present utility model, at this utility model
Spirit and principle within, any simple amendment that above example is made, equivalent
With improvement etc., within all still falling within the protection domain of technical solutions of the utility model.
Claims (7)
1. heavy－duty many rotor wing unmanned aerial vehicles horn plug-in and pull-off device, including fixed pedestal (1),
Grafting pipe clamp (2) and rotor connecting tube (3), it is characterised in that: described fixed pedestal (1)
Including upper movable pedestal (4) and lower stationary base mount (5)；Described grafting pipe clamp (2) includes
Upper grafting pipe clamp (6) and lower grafting pipe clamp (7)；Described rotor connecting tube (3) is plugged in slotting
In the upper grafting pipe clamp (6) of pipe connection clip (2) and lower grafting pipe clamp (7), described is upper slotting
Pipe connection clip (6) and lower grafting pipe clamp (7) clamp rotor connecting tube by pipe connecting bolt (8)
(3)；Described grafting pipe clamp (2) is plugged in the upper movable pedestal (4) of fixed pedestal (1)
Interior with lower stationary base mount (5), described upper movable pedestal (4) and lower stationary base mount (5)
By foundation bolt (9) clamping grafting pipe clamp (2).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug dress the most according to claim 1
Putting, described fixed pedestal (1) rear end is provided with circuit socket location-plate (10), described
Circuit socket (11) it is provided with on circuit socket location-plate (10).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug dress the most according to claim 2
Putting, described grafting pipe clamp (2) rear end is provided with circuit plug location-plate (12), described
Circuit plug (13) it is provided with on circuit plug location-plate (12).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug dress the most according to claim 3
Putting, described circuit plug (13) coordinates grafting with circuit socket (11).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug dress the most according to claim 1
Putting, described fixed pedestal (1) both sides, front end are respectively arranged with limited impression (14).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug dress the most according to claim 5
Putting, described grafting pipe clamp (2) both sides, front end are respectively arranged with spacing preiection (15).
A kind of heavy－duty many rotor wing unmanned aerial vehicles horn plug-in and pull-off device the most according to claim 6,
Described fixed pedestal (1) and grafting pipe clamp (2) match grafting time, described grafting pipe clamp
(2) spacing preiection (15) of both sides, front end is connected to the limit of fixed pedestal (1) both sides, front end
In position groove (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620240830.6U CN205499319U (en) | 2016-03-25 | 2016-03-25 | Big many rotor unmanned aerial vehicle of load horn plug device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620240830.6U CN205499319U (en) | 2016-03-25 | 2016-03-25 | Big many rotor unmanned aerial vehicle of load horn plug device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205499319U true CN205499319U (en) | 2016-08-24 |
Family
ID=56733786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620240830.6U Active CN205499319U (en) | 2016-03-25 | 2016-03-25 | Big many rotor unmanned aerial vehicle of load horn plug device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205499319U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018072324A1 (en) * | 2016-10-20 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN108382587A (en) * | 2018-01-31 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | The unmanned plane horn connection structure of connection easy to disassemble |
| EP3895982A4 (en) * | 2018-12-13 | 2022-01-26 | Guangzhou Xaircraft Technology Co., Ltd. | Frame for aircraft and aircraft |
-
2016
- 2016-03-25 CN CN201620240830.6U patent/CN205499319U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018072324A1 (en) * | 2016-10-20 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN109476369A (en) * | 2016-10-20 | 2019-03-15 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| CN108382587A (en) * | 2018-01-31 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | The unmanned plane horn connection structure of connection easy to disassemble |
| EP3895982A4 (en) * | 2018-12-13 | 2022-01-26 | Guangzhou Xaircraft Technology Co., Ltd. | Frame for aircraft and aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200805 Address after: Room 614, bonded building, west side of bonded Road, Hangzhou Airport Economic Zone, Jingjiang street, Xiaoshan District, Hangzhou City, Zhejiang Province Patentee after: Hangzhou Wanlin digital chain Technology Service Co., Ltd Address before: 225001 No. 43, Taizhou Road, Guangling District, Jiangsu, Yangzhou Patentee before: YANGZHOU JINJING AVIATION SCIENCE AND TECHNOLOGY Co.,Ltd. |
|
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: 310051 room 1802-1, building 1, Zhongying international business building, No. 998, Binhe Road, Changhe street, Binjiang District, Hangzhou City, Zhejiang Province Patentee after: Hangzhou Wanlin digital chain Technology Service Co.,Ltd. Address before: 311200 room 614, bonded building, West bonded Road, Hangzhou Airport Economic Zone, Jingjiang street, Xiaoshan District, Hangzhou City, Zhejiang Province Patentee before: Hangzhou Wanlin digital chain Technology Service Co.,Ltd. |