CN207595287U - A kind of unmanned plane landing platform - Google Patents
A kind of unmanned plane landing platform Download PDFInfo
- Publication number
- CN207595287U CN207595287U CN201721519336.4U CN201721519336U CN207595287U CN 207595287 U CN207595287 U CN 207595287U CN 201721519336 U CN201721519336 U CN 201721519336U CN 207595287 U CN207595287 U CN 207595287U
- Authority
- CN
- China
- Prior art keywords
- panel
- unmanned plane
- support feet
- plane landing
- landing platform
- 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.)
- Active
Links
Landscapes
- Road Signs Or Road Markings (AREA)
Abstract
The utility model discloses a kind of unmanned plane landing platform, and multiple support feets including panel and positioned at below the panel, the multiple support feet is connect respectively with panel rotation；Limiting section and sticking department are further included between the support feet and panel, the limiting section is obtuse angle or right angle for keeping the angle of support feet and panel, and the sticking department is used for the relative position of lock support foot and panel；Multiple through-holes are provided on the panel, the through-hole is distributed on panel；Level meter is further included, the level meter is mounted on panel.The utility model is intended to provide a kind of unmanned plane landing platform, increases multi-rotor unmanned aerial vehicle effective operation time, improves plant protection operation efficiency；Meet unmanned plane landing demand under different terrain conditions, and play the role of reducing the ground effect generated during unmanned plane landing.
Description
Technical field
The utility model is related to unmanned air vehicle technique field more particularly to a kind of unmanned plane landing platforms.
Background technology
At present, as land transformation, farm land produce gradual scale, to improve agricultural production efficiency, reducing agricultural
Production cost makes the demand that unmanned plane carries out operations such as spraying insecticide with unmanned plane increase increasingly.Unmanned plane operating area is mostly
Complicated landforms, most operation fields such as abrupt slope, stone riprap, shrub be weedy do not have unmanned plane landing condition, take off at a distance
The effective operation time for greatly shortening unmanned plane or even its cruising ability can not be met into operation and carry out requirement；More rotors nobody
Machine before take-off, need to power on and be calibrated, self-test, and the process of self-test need to ensure that equipment level is placed, and otherwise may go out
Now calibrate, initialize phenomena such as mistake, and then cause unmanned plane and fall machine event, however in the wild under the conditions of be difficult to meet unmanned plane
Horizontal positioned requirement.
Utility model content
The utility model is intended to provide a kind of unmanned plane landing platform, increases multi-rotor unmanned aerial vehicle effective operation time, carries
High plant protection operation efficiency；Meet unmanned plane landing demand under different terrain conditions, and play and reduce what is generated during unmanned plane landing
The effect of ground effect.
In order to achieve the above objectives, the technical solution adopted in the utility model is as follows：
A kind of unmanned plane landing platform, multiple support feets including panel and positioned at below the panel, the multiple support feet
It is connect respectively with panel rotation；Limiting section and sticking department are further included between the support feet and panel, the limiting section is used to protect
The angle for holding support feet and panel is obtuse angle or right angle, and the sticking department is used for the relative position of lock support foot and panel；Institute
It states and multiple through-holes is provided on panel, the through-hole is distributed on panel；Level meter is further included, the level meter is mounted on panel
On.
Preferably, the support feet includes telescopic rod, and tie down screw is provided on telescopic rod.
Preferably, the support feet is three-stage folding rod, sets that there are two limit hinges in each support feet.
Preferably, the limiting section includes limit hinge, and the limit hinge and panel vertical connection, support feet are mounted on
On the outside of limit hinge.
Preferably, the sticking department includes lock hole and locking bolt, after support feet is determined with panel relative position, leads to
It crosses lock hole and locking bolt is locked.
Preferably, the level meter is Universal level-metre, and level meter is mounted on panel top end.
Preferably, further include it is multiple grab ground dragon's paw, each grab ground dragon's paw connect respectively with a support feet by rope.
Preferably, it is equipped with dragon's paw on the downside of the panel to link up with, grabs ground dragon's paw and be suspended on panel bottom.
Preferably, the panel and the marginal position of support feet are circular arc chamfering.
Preferably, the through-hole is the circular through hole of internal diameter 2cm.
Compared with prior art, the utility model has the advantages that：
The landing platform of the utility model reduces selectivity of the multi-rotor unmanned aerial vehicle to operating environment, shortens landing distance,
Increase multi-rotor unmanned aerial vehicle effective operation time, improve plant protection operation efficiency；Optimize multi-rotor unmanned aerial vehicle landing operating environment, subtract
Machine is fallen less, equipment damage event occurs；Multi-rotor unmanned aerial vehicle operation landing link difficulty is reduced, shortens multi-rotor unmanned aerial vehicle and flies hand
Training time；It can solve the problems, such as that multi-rotor unmanned aerial vehicle without special landing platform, meets unmanned plane landing under different terrain conditions
Demand, and play the ground effect for reducing and being generated during unmanned plane landing；Accordion structure is convenient for carrying, and is not take up transport space,
Platform using it is easy to operate, safe and reliable, meet the advantages that existing Multiple Type rotor wing unmanned aerial vehicle landing demand.
Description of the drawings
Fig. 1 is the utility model structure diagram；
Fig. 2 is panel construction schematic diagram；
Fig. 3 is limiting section and sticking department structure diagram；
Fig. 4 is preferred embodiment structure diagram；
In figure：1- panels, 2- support feets, 3- limiting sections, 4- sticking departments, 5- through-holes, 6- level meters, 7- grab ground dragon's paw, 8-
Rope, 9- tie down screws, 10- lock slots, 11- locking bolts.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing, to this reality
It is further elaborated with novel.
As shown in Figs. 1-2, a kind of unmanned plane landing platform, multiple support feets 2 including panel 1 and positioned at 1 lower section of panel,
The multiple support feet 2 is rotatablely connected respectively with panel 1；Limiting section 3 and locking are further included between the support feet 2 and panel 1
Portion 4, it is obtuse angle or right angle that the limiting section 3, which is used to keep the angle of support feet 2 and panel 1, and the sticking department 4 is for locking branch
The relative position of spike 2 and panel 1；Multiple through-holes 5 are provided on the panel 1, the through-hole 5 is distributed on panel 1；It further includes
Level meter 6, the level meter 6 are mounted on panel 1.
As shown in figure 3, in the present embodiment, it is preferred that the support feet 2 includes telescopic rod, and locking is provided on telescopic rod
Screw rod 9.Telescopic rod can independent telescope, so as to which landing platform by the telescopic adjustment of different telescopic rods, is made to adapt to ground,
Landing platform is made to keep horizontality；Telescopic rod is made of sleeve and push rod, and push rod is mating with sleeve, and sleeve side opens up
Screw hole, installation bolt in screw hole, the screw end of bolt can coordinate with push rod.
In the present embodiment, it is preferred that the support feet 2 is three-stage folding rod, sets that there are two limit in each support feet
Hinge.Folding rod is folded using three-stage, is set on each fold bar there are two limit hinge, folding rod is cut with scissors in itself also by limiting
Chain is connect with panel, and folding rod can only fold inwardly, is ensured that folding rod can collapse and is placed on the downside of panel, and pass through fastening
Part is fixed.
As shown in figure 3, in the present embodiment, it is preferred that the limiting section 3 includes limit hinge, the limit hinge and face
1 vertical connection of plate, support feet 2 are mounted on the outside of limit hinge.The sticking department 4 includes lock slots 10 and locking bolt 11, when
After support feet 2 is determined with 1 relative position of panel, locked by lock slots 10 and locking bolt 11.The level meter 6 is ten thousand
To level meter, level meter 6 is mounted on 1 top end of panel.
To ensure the stability of landing platform, by limiting section and sticking department, ensure that the angle of support feet and panel is blunt
Angle or right angle；The limit hinge at a substantially right angle for limiting section, limit hinge are fixed on the downside of panel, and support feet rotation connects
It is connected on limit hinge, support feet is located on the outside of limit hinge.Sticking department is located on limiting section, and arc is provided on limit hinge
Lock slots are provided with two groups of locking bolts and nut in lock slots, and lock slots, locking bolt and lock nut together constitute
Sticking department by way of two groups of locking bolts and lock nut clamping locking, jointly locks support placement of foot.
During due to operation in the wild, surface condition rather harsh, landing platform can not ensure level, need to adjust support feet
Position and length, by the Universal level-metre on panel, the direction for needing to adjust, tune promptly can be visually known
Whole support feet so that panel reaches horizontal, shortens the landing time, increases multi-rotor unmanned aerial vehicle effective operation time, improves plant protection
Operating efficiency
As shown in figure 4, in the present embodiment, it is preferred that further include it is multiple grab ground dragon's paw 7, each grab ground dragon's paw 7 respectively with one
A support feet 2 is connected by rope 8.1 downside of panel is equipped with dragon's paw and links up with, and grabs ground dragon's paw 7 and is suspended on 1 bottom of panel.Institute
It is circular arc chamfering to state panel 1 and the marginal position of support feet 2.The through-hole 5 is the circular through hole of internal diameter 2cm.
When the surface condition of field work is especially severe, it only can not be successfully by support feet and landing platform be fixed on ground
When, to enhance the stability of landing platform, it can be taken off being suspended on and grab ground dragon's paw on panel, will grab ground as fixed tent
Dragon's paw it is buried enter soil in, multiple ground dragon's paws of grabbing are distributed on the surroundings of panel, and stable pulling force is provided for landing platform, has been avoided
It drops platform and fixes shakiness.
Certainly, the utility model can also have other numerous embodiments, without departing substantially from the spirit of the present invention and its essence
In the case of, those skilled in the art can make various corresponding changes and deformation, but these according to the utility model
It is corresponding to change and deform the scope of the claims that all belong to appended by the utility model.
Claims (10)
1. a kind of unmanned plane landing platform, it is characterised in that：Multiple support feets including panel and positioned at below the panel are described more
A support feet is connect respectively with panel rotation；Limiting section and sticking department, the limiting are further included between the support feet and panel
Portion is obtuse angle or right angle for keeping the angle of support feet and panel, and the sticking department is opposite for lock support foot and panel
Position；Multiple through-holes are provided on the panel, the through-hole is distributed on panel；Further include level meter, the level meter installation
On panel.
2. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The support feet includes telescopic rod,
Tie down screw is provided on telescopic rod.
3. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The support feet is folded for three-stage
Bar, sets that there are two limit hinges in each support feet.
4. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The limiting section includes limiting and cuts with scissors
Chain, the limit hinge and panel vertical connection, support feet are mounted on the outside of limit hinge.
5. a kind of unmanned plane landing platform according to claim 4, it is characterised in that：The sticking department include lock hole with
Locking bolt after support feet is determined with panel relative position, is locked by lock hole and locking bolt.
6. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The level meter is universal horizontal
Instrument, level meter are mounted on panel top end.
7. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：Further include it is multiple grab ground dragon's paw, often
A ground dragon's paw of grabbing is connect respectively with a support feet by rope.
8. a kind of unmanned plane landing platform according to claim 7, it is characterised in that：Dragon's paw is equipped on the downside of the panel to hang
Hook grabs ground dragon's paw and is suspended on panel bottom.
9. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The edge of the panel and support feet
Position is circular arc chamfering.
10. a kind of unmanned plane landing platform according to claim 1, it is characterised in that：The through-hole is the circle of internal diameter 2cm
Shape through-hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721519336.4U CN207595287U (en) | 2017-11-15 | 2017-11-15 | A kind of unmanned plane landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721519336.4U CN207595287U (en) | 2017-11-15 | 2017-11-15 | A kind of unmanned plane landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207595287U true CN207595287U (en) | 2018-07-10 |
Family
ID=62758396
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721519336.4U Active CN207595287U (en) | 2017-11-15 | 2017-11-15 | A kind of unmanned plane landing platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207595287U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2710887C1 (en) * | 2019-04-29 | 2020-01-14 | Автономная некоммерческая организация высшего образования "Университет Иннополис" | Landing place for drone |
| CN112319834A (en) * | 2020-11-06 | 2021-02-05 | 贵州电网有限责任公司 | Unmanned aerial vehicle lifting platform for field power inspection |
| CN113859564A (en) * | 2021-10-09 | 2021-12-31 | 国网河北省电力有限公司检修分公司 | Supplementary lift operation platform under unmanned aerial vehicle all terrain environment |
-
2017
- 2017-11-15 CN CN201721519336.4U patent/CN207595287U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2710887C1 (en) * | 2019-04-29 | 2020-01-14 | Автономная некоммерческая организация высшего образования "Университет Иннополис" | Landing place for drone |
| CN112319834A (en) * | 2020-11-06 | 2021-02-05 | 贵州电网有限责任公司 | Unmanned aerial vehicle lifting platform for field power inspection |
| CN113859564A (en) * | 2021-10-09 | 2021-12-31 | 国网河北省电力有限公司检修分公司 | Supplementary lift operation platform under unmanned aerial vehicle all terrain environment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207595287U (en) | A kind of unmanned plane landing platform | |
| US9428877B2 (en) | Modular monopole tower foundation | |
| US20120228442A1 (en) | Portable modular monopole tower foundation | |
| US9732564B2 (en) | Drilling rig equipment platform | |
| CN101718615A (en) | Agricultural spraying operation wind field test equipment of movable unmanned helicopter and test method | |
| CN204819421U (en) | Foldable board operation panel of throwing | |
| CN105766543A (en) | Windproof anti-lodging fixing and supporting device for tree | |
| US20160237702A1 (en) | Adjustable Scaffolding | |
| CN206187300U (en) | Simple and easy fairway buoy light beacon | |
| JPWO2014132733A1 (en) | stepladder | |
| CN205429566U (en) | Crossing structure | |
| CN207580191U (en) | A kind of assembly unmanned plane landing platform | |
| CN203057878U (en) | Suspended lifting platform for mountainous and hilly orchard work | |
| CN209337945U (en) | Low wind speed wind-powered machine unit hub lifting overturning auxiliary device and its Lift-on/Lift-off System | |
| KR102022044B1 (en) | Overturn preventing device of high place works car | |
| CN205740192U (en) | A kind of guardrail for hydraulic lifter | |
| CN209635815U (en) | Shaft rot and photovoltaic bracket | |
| CN205092307U (en) | Adjustable triangle posture lifter | |
| CN209218791U (en) | A kind of Anti-Typhoon support construction of ornamental trees and shrubs | |
| CN204754150U (en) | Dish -type node formula scaffold | |
| CN207022748U (en) | A kind of high support frame of stability | |
| KR100493505B1 (en) | Method of constructing a transmission tower by helicopter | |
| US10557310B2 (en) | Convertible framework for post hole digger | |
| CN107117291A (en) | A kind of power-assisted transport foot stool and the unmanned plane with the foot stool | |
| CN206697838U (en) | Line maintenance aerial work platform |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211203 Address after: 315300 No. 598, enterprise East Road, Zhouxiang Town, Cixi City, Ningbo City, Zhejiang Province Patentee after: Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd. Address before: No. 3507, floor 35, building 1, No. 666, middle section of Tianfu Avenue, Chengdu hi tech Zone, China (Sichuan) pilot Free Trade Zone, Chengdu, Sichuan 610000 Patentee before: CHENGDU SKYLIN TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right |