CN207258010U - A kind of unmanned plane link - Google Patents
A kind of unmanned plane link Download PDFInfo
- Publication number
- CN207258010U CN207258010U CN201721346848.5U CN201721346848U CN207258010U CN 207258010 U CN207258010 U CN 207258010U CN 201721346848 U CN201721346848 U CN 201721346848U CN 207258010 U CN207258010 U CN 207258010U
- Authority
- CN
- China
- Prior art keywords
- main body
- hole
- earrings
- unmanned plane
- elastic
- 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
Links
Abstract
It the utility model is related to a kind of unmanned plane link, include top fixed seat, lower part fixed seat, and connecting rod, this link has further included a damping, damping is made of the docking boots in the middle part of being arranged at the stress carrier on the main body panel top of top fixed seat, being arranged at stress carrier downward and through main body panel middle part major diameter through hole, the elastic component being arranged at stress carrier and main body panel, and path through hole B is provided with stress carrier；Elastic component is by top elasticity earrings, lower elastic earrings, and the elastic ball composition being arranged between top elasticity earrings and lower elastic earrings；The lower elastic earrings of elastic component is snapped onto in the path through hole A on main body panel, the top elasticity Earrings buckles of elastic component are connected in the path through hole B on stress carrier, elastic ball is clamped between stress carrier and main body panel, and the connecting frame structure of taking photo by plane is simple, reasonable, easy to install and use, manufacture cost is low, stability is good.
Description
Technical field
The utility model belongs to unmanned plane shooting field, and in particular to a kind of unmanned plane link.
Background technology
With the continuous development and renewal of science and technology, applying for unmanned plane has occupied certain ratio in the modern life,
Including unmanned plane, in unmanned plane dispenser fertilising of agriculture field etc..But unmanned air vehicle technique and application are at present at home simultaneously
It is immature, there is no corresponding auxiliary facility in the field of taking photo by plane, so that the accessory acquisition of unmanned plane is very inconvenient.
It is existing to take photo by plane that there are problems with for unmanned plane pan-shot:
1st, without ready-made corollary equipment, majority is camera unmanned plane Hard link.
2nd, shooting picture shake is larger, and stability is poor, and many troubles are brought to post-production, influences final effect in blocks.
3rd, it is nearer from unmanned plane body due to Hard link, easily occur the part of aircraft in picture, influence shooting effect.
The content of the invention
The purpose of the utility model is to overcome the deficiencies in the prior art, there is provided one kind is simple and reasonable for structure, uses installation
Convenient, the manufacture unmanned plane link that cost is low, stability is good.
The technical solution of the utility model is as follows：A kind of unmanned plane link, includes and is used for and unmanned plane main body
The top fixed seat that is fixedly connected, the lower part fixed seat fixed for camera, and for pull open unmanned plane main body and camera it
Between spacing connecting rod, the top fixed seat is by main body panel and is arranged at the card base of main body panel left and right side and forms, institute
The card base stated sets position to coincide with unmanned plane bottom part body connection structure, and the main body panel is provided with one in heart position wherein
A major diameter through hole, and major diameter through hole annular array is provided with no less than three path through hole A；
This link has further included a damping, and the damping is by being arranged at the main body panel of top fixed seat
The stress carrier on top, be arranged in the middle part of stress carrier downward and pass through the docking boots of major diameter through hole in the middle part of main body panel, set
The elastic component being placed between stress carrier and main body panel forms, and is provided with much with annular array on the stress carrier
In three path through hole B, and the path through hole B is vertical corresponding up and down with path through hole A；
The elastic component is by top elasticity earrings, lower elastic earrings, and is arranged at top elasticity earrings and lower part
Elastic ball composition between elastic earrings, the top elasticity earrings, lower elastic earrings, elastic ball three are integrally formed
Structure；
The lower elastic earrings of the elastic component is snapped onto in the path through hole A on main body panel, the elastic component
Top elasticity Earrings buckles are connected in the path through hole B on stress carrier, and the elastic ball is clamped in stress carrier and master
Between body disc；Described connecting rod one end is fixed with the boots docking of docking on stress carrier, and the other end connects with lower part fixed seat
Connect fixation.
Described connecting rod one end is inserted into the docking boots being arranged on stress carrier, and is adopted and be screwed.
When the docking boots being arranged on stress carrier pass through major diameter through hole, it docks the edge of boots side wall and major diameter through hole
There is spacing, and spacing is much with 1mm.
The lower part fixed seat is in integrally inverted cone-shaped structure, and its upper part is provided with one and pair used is docked with connecting rod
Boots are connect, its inner hub location is provided with a screw for being used to be connected fixation with camera.
The connecting rod is scalable connecting rod.
The elastic component is rubber parts.
Beneficial effect is caused by the utility model：This link is easy for installation, it is possible to achieve camera and unmanned owner
The Fast Installation of body is fixed, it disassembles also more convenient.The setting of damping produces during can eliminating unmanned plane during flying
Dither, therefore reduce influence of the vibration to shooting picture, wherein, the main damping part of damping is elastic component,
This elastic component is with certain elastic flexible apparatus, is set between stress carrier and main body panel multiple, can make connection
Frame more balance and stability.The setting of connecting rod can widen the spacing between camera and unmanned plane main body, so as to not interfere with complete
The shooting picture of scape, and the flight attitude of unmanned plane is not influenced.
The card base that this link is set in the main body panel left and right side of top fixed seat on Local Members can be in order to even
The fixation of frame and unmanned plane main body is connect, the path through hole A set on main body panel can be incorporated in what is set on stress carrier
Path through hole B installs elastic component, and the top elasticity earrings of elastic component just snaps onto the path through hole B of stress carrier
Interior, the lower elastic earrings of elastic component is just snapped onto in the path through hole A of stress carrier, and elastic ball is just clamped in main body
It is rational in infrastructure, stable between disk and stress carrier.
The docking boots set on stress carrier and the docking boots set on lower part fixed seat top can be easily with connecting
Extension bar realizes docking, is that installation is more convenient.
Total the utility model has the advantages that simple and reasonable for structure, working stability.
Brief description of the drawings
Fig. 1 is the overall positive structure diagram of the utility model.
Fig. 2 is the overall overlooking the structure diagram of the utility model.
Fig. 3 is the top fixed seat overlooking the structure diagram of the utility model.
Fig. 4 is the damping structure diagram of the utility model.
Fig. 5 is the elastic component positive structure diagram of the utility model.
Fig. 6 is the elastic component overlooking the structure diagram of the utility model.
Fig. 7 is the elastic component schematic cross-sectional view of the utility model.
Fig. 8 is the stress carrier dimensional structure diagram of the utility model.
In figure：1st, top fixed seat 2, lower part fixed seat 3, connecting rod 4, main body panel 5, card base 6, major diameter are led to
Hole 7, path through hole A 8, damping 9, stress carrier 10, docking boots 11, elastic component 12, path through hole B
13rd, top elasticity earrings 14, lower elastic earrings 15, elastic ball 16, screw.
Embodiment
The technical solution of the utility model is described further with reference to specific embodiment.
Embodiment 1
As shown in Fig. 1-7：A kind of unmanned plane link, includes for being fixedly connected with unmanned plane main body
Portion's fixed seat 1, the lower part fixed seat 2 fixed for camera, and for pulling open the spacing between unmanned plane main body and camera
Connecting rod 3, the top fixed seat 1 are made of main body panel 4 with the card base 5 for being arranged at 4 left and right side of main body panel, the card
Foot 5 sets position to coincide with unmanned plane bottom part body connection structure, and heart position is provided with one greatly to the main body panel 4 wherein
Footpath through hole 6, and 6 annular array of major diameter through hole is provided with eight path through hole A7；
This link has further included a damping 8, and the damping 8 is by being arranged at the main body of top fixed seat
The stress carrier 9 on disk top, be arranged at the middle part of stress carrier 9 downward and pass through the docking of major diameter through hole 6 in the middle part of main body panel
Boots 10, the elastic component 11 being arranged between stress carrier 9 and main body panel 4 form, on the stress carrier 9 using center as
An annular array is provided with eight path through hole B12, and the path through hole B12 is vertical right up and down with path through hole A7
Should；
The elastic component 11 is by top elasticity earrings 13, lower elastic earrings 14, and is arranged at top elasticity earrings
Elastic ball 15 between lower elastic earrings forms, the top elasticity earrings 13, lower elastic earrings 14, elastic ball 15
Three is an integral molding structure；
The lower elastic earrings 14 of the elastic component 11 is snapped onto in the path through hole A7 on main body panel, the elasticity
The top elasticity earrings 13 of part 11 is snapped onto in the path through hole B12 on stress carrier, the elastic ball 15 be clamped in by
Between power carrier 9 and main body panel 4；Described 3 one end of connecting rod is fixed with the docking of boots 10 of docking on stress carrier 9, separately
One end is connected fixation with lower part fixed seat 2.
Described 3 one end of connecting rod is inserted into the docking boots 10 being arranged on stress carrier 9, and is consolidated using screw
It is fixed.
When the docking boots 10 being arranged on stress carrier 9 pass through major diameter through hole 6, it docks 10 side wall of boots and major diameter through hole
There are spacing, and spacing 3mm in 6 edge.
The overall lower part fixed seat 2 is in inverted cone-shaped structure, and its upper part is provided with one and docks what is used with connecting rod 3
Boots 10 are docked, its inner hub location is provided with a screw 16 for being used to be connected fixation with camera.
The elastic component 11 is rubber parts.
The utility model is when in use：Whole link realizes that installation is fixed by card base and unmanned plane main body, and camera leads to
Cross in the fixed seat of lower part the screw set to be fixed in the fixed seat of lower part, due to the setting of connecting rod, top fixed seat is with
Distance increases between portion's fixed seat, therefore increases the spacing between unmanned plane main body and camera, so that unmanned plane main body will not
Block the shooting of camera；Due to the setting of damping in whole flight shooting process, stress carrier and main body are arranged at
Elastic component between disk can play the role of preferable shock-absorbing, and when flight runs into high wind or turns to, the elastic force of elastic component can
To offset external force or inertia stress, stress carrier plays the role of stress equalization, can balanced eight elastic components by
Power, so that whole link is more stablized, the docking boots wherein set on stress carrier are when through major diameter through hole and big
The edge of footpath through hole has gap that connecting rod can be made to have certain free degree that dangles, on the one hand enable elastic component it is larger play it is slow
Punching acts on, and the hard friction between component on the other hand can be reduced, so as to increase the service life of whole device.
Claims (6)
1. a kind of unmanned plane link, include for be fixedly connected with unmanned plane main body top fixed seat, for phase
The lower part fixed seat that machine is fixed, and for pulling open the connecting rod of the spacing between unmanned plane main body and camera, it is characterised in that：
The top fixed seat is by main body panel and is arranged at the card base of main body panel left and right side and forms, the card base set position with
Unmanned plane bottom part body connection structure is coincide, and heart position is provided with a major diameter through hole to the main body panel wherein, and surrounds
Major diameter through hole annular array is provided with no less than three path through hole A；
This link has further included a damping, and the damping is by being arranged at the main body panel top of top fixed seat
Stress carrier, be arranged in the middle part of stress carrier downward and through docking boots of major diameter through hole in the middle part of main body panel, be arranged at
Elastic component between stress carrier and main body panel forms, and is set on the stress carrier using center as around a point annular array
It is equipped with and is no less than three path through hole B, and the path through hole B is vertical corresponding up and down with path through hole A；
The elastic component is by top elasticity earrings, lower elastic earrings, and is arranged at top elasticity earrings and lower elastic
Elastic ball composition between earrings, the top elasticity earrings, lower elastic earrings, elastic ball three are integrally formed knot
Structure；
The lower elastic earrings of the elastic component is snapped onto in the path through hole A on main body panel, the top of the elastic component
Elastic Earrings buckles are connected in the path through hole B on stress carrier, and the elastic ball is clamped in stress carrier and main body panel
Between；Described connecting rod one end is fixed with the boots docking of docking on stress carrier, and the other end is connected solid with lower part fixed seat
It is fixed.
A kind of 2. unmanned plane link according to claim 1, it is characterised in that：Connecting rod one end insertion
Into the docking boots being arranged on stress carrier, and adopt and be screwed.
A kind of 3. unmanned plane link according to claim 1, it is characterised in that：It is arranged on stress carrier
When docking boots pass through major diameter through hole, it, which docks boots side wall and the edge of major diameter through hole, spacing, and spacing is much with 1mm.
A kind of 4. unmanned plane link according to claim 1, it is characterised in that：The lower part fixed seat is overall
In inverted cone-shaped structure, its upper part is provided with one and the docking boots used is docked with connecting rod, its inner hub location is provided with one
A screw for being used to be connected fixation with camera.
A kind of 5. unmanned plane link according to claim 1, it is characterised in that：The connecting rod is scalable
Connecting rod.
A kind of 6. unmanned plane link according to claim 1, it is characterised in that：The elastic component is rubber
Part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721346848.5U CN207258010U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane link |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721346848.5U CN207258010U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane link |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207258010U true CN207258010U (en) | 2018-04-20 |
Family
ID=61916635
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721346848.5U Expired - Fee Related CN207258010U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane link |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207258010U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618673A (en) * | 2017-10-19 | 2018-01-23 | 河南焦傲文化传媒有限公司 | A kind of unmanned plane link |
-
2017
- 2017-10-19 CN CN201721346848.5U patent/CN207258010U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618673A (en) * | 2017-10-19 | 2018-01-23 | 河南焦傲文化传媒有限公司 | A kind of unmanned plane link |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204387182U (en) | Damping device and shock-absorbing ball thereof, adopt the UAV of this damping device | |
| CN207258010U (en) | A kind of unmanned plane link | |
| CN107618673A (en) | A kind of unmanned plane link | |
| CN202546188U (en) | Video camera fixing device and camera shooting device | |
| CN203398690U (en) | Tubular bus fitting with self-springing function | |
| CN206072225U (en) | Steel wire shock-absorbing ball and the damping for unmanned vehicle | |
| CN205029802U (en) | STB hard disk fixed structure | |
| CN206265330U (en) | Shock-absorbing ball, damping device and unmanned plane | |
| CN205073582U (en) | Hidden high jump take -off helps jump device | |
| CN203507455U (en) | Shuttlecock net rack capable of being detached and installed rapidly | |
| CN213677204U (en) | Digital image transmission unmanned aerial vehicle | |
| CN213677123U (en) | Remote high definition digital image transmission unmanned aerial vehicle | |
| CN204223047U (en) | Adjustable toy tricycle bench | |
| CN204258865U (en) | A kind of mobile phone external lens assembly | |
| CN203789291U (en) | Clamping buckle device | |
| CN206889548U (en) | Flying control equipment damping device | |
| CN206142051U (en) | Position adjustable screw set pin collector | |
| CN204502338U (en) | A kind of Novel volleyball frame | |
| CN207246168U (en) | A kind of quick despatch structure of hanging parts | |
| CN204387022U (en) | A kind of self-closing fastener | |
| CN213323657U (en) | Unmanned aerial vehicle's installation chassis | |
| CN204629000U (en) | A kind of two bulb universal regulated supporting structure assembly | |
| CN204492080U (en) | One can the dismountable decoration board mounting structure of load-bearing | |
| CN205385051U (en) | Novel battery installing support | |
| CN204944028U (en) | A kind of buckle-type back boards |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 450000 High-tech Industrial Development Zone, Zhengzhou City, Henan Province, No. 11 Changchun Road, No. 1 Building, Incubation Park, Henan National University, No. 7, No. 716 Patentee after: Henan Jiaoyao Information Technology Co., Ltd. Address before: 450000 High-tech Industrial Development Zone, Zhengzhou City, Henan Province, No. 11 Changchun Road, No. 1 Building, Incubation Park, Henan National University, No. 7, No. 716 Patentee before: Henan Jiao Ao culture media Co., Ltd. |
|
| 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: 20180420 Termination date: 20191019 |